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- Permanent Link:
- https://ufdc.ufl.edu/UFE0024432/00001
## Material Information- Title:
- A Finite Element Approach to Spur Gear Response and Wear Under Non-Ideal Loading
- Creator:
- Stoker, Kyle
- Place of Publication:
- [Gainesville, Fla.]
Florida - Publisher:
- University of Florida
- Publication Date:
- 2009
- Language:
- english
- Physical Description:
- 1 online resource (83 p.)
## Thesis/Dissertation Information- Degree:
- Master's ( M.S.)
- Degree Grantor:
- University of Florida
- Degree Disciplines:
- Mechanical Engineering
Mechanical and Aerospace Engineering - Committee Chair:
- Kim, Nam Ho
- Committee Members:
- Schmitz, Tony L.
Sawyer, Wallace G. - Graduation Date:
- 5/2/2009
## Subjects- Subjects / Keywords:
- Axes of rotation ( jstor )
Axial stress ( jstor ) Bending ( jstor ) Contact loads ( jstor ) Design analysis ( jstor ) Design engineering ( jstor ) Gears ( jstor ) Geometry ( jstor ) Sliding ( jstor ) Stress cycles ( jstor ) Mechanical and Aerospace Engineering -- Dissertations, Academic -- UF element, finite, gear, ideal, loading, non, spur, wear - Genre:
- bibliography ( marcgt )
theses ( marcgt ) government publication (state, provincial, terriorial, dependent) ( marcgt ) born-digital ( sobekcm ) Electronic Thesis or Dissertation Mechanical Engineering thesis, M.S.
## Notes- Abstract:
- Abstract of Thesis Presented to the Graduate School of the University of Florida in Partial Fulfillment of the Requirements for the Degree of Master of Science A FINITE ELEMENT APPROACH TO SPUR GEAR RESPONSE AND WEAR UNDER NON-IDEAL LOADING By Kyle C. Stoker May 2009 Chair: Nam Ho Kim Major: Mechanical Engineering Spur gear response and wear is an engineering problem which has been around for hundreds of years. The method to determine stresses analytically has been developed extensively by the American Gear Manufacturers Association, and experimental techniques investigating wear of spur gears is well documented. Currently engineers design gears based on a fixed safety factor which determines the lifetime of a gear based on predictable loads and stresses. Additionally, all mechanical assemblies are subject to tolerances that limit the amount of error between physical components. When assemblies are operated at the limits of these errors, stresses and wear will increase. This research has provided the engineer with a tool to predict where and by how much the stresses of spur gears will increase when non-ideal conditions are present for both 2 dimensional and 3 dimensional analysis. A wide range of spur gears can be input to the parametric code and the Finite Element Analysis program will solve the contact problem and produce valid results. A method to predict progressive wear evolution for a 2 dimensional spur gear according to Archard?s wear law has been implemented within the FEA code. The research has shown that with an increase in the axial separation wear depths will increase and the wear profile will be modified. ( en )
- General Note:
- In the series University of Florida Digital Collections.
- General Note:
- Includes vita.
- Bibliography:
- Includes bibliographical references.
- Source of Description:
- Description based on online resource; title from PDF title page.
- Source of Description:
- This bibliographic record is available under the Creative Commons CC0 public domain dedication. The University of Florida Libraries, as creator of this bibliographic record, has waived all rights to it worldwide under copyright law, including all related and neighboring rights, to the extent allowed by law.
- Thesis:
- Thesis (M.S.)--University of Florida, 2009.
- Local:
- Adviser: Kim, Nam Ho.
- Statement of Responsibility:
- by Kyle Stoker.
## Record Information- Source Institution:
- UFRGP
- Rights Management:
- Copyright Stoker, Kyle. Permission granted to the University of Florida to digitize, archive and distribute this item for non-profit research and educational purposes. Any reuse of this item in excess of fair use or other copyright exemptions requires permission of the copyright holder.
- Resource Identifier:
- 665097246 ( OCLC )
- Classification:
- LD1780 2009 ( lcc )
## UFDC Membership |

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PAGE 1 1 A FINITE ELEMENT APPROACH TO SPUR GEAR RESPONSE AND WEAR UNDER NONIDEAL LOADING By KYLE C. STOKER A THESIS PRESENTED TO THE GRADUATE SCHOOL OF THE UNIVERSITY OF FLORIDA IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE D EGREE OF MASTER OF SCIENCE UNIVERSITY OF FLORIDA 2009 PAGE 2 2 2009 Kyle C. Stoker PAGE 3 3 ACKNOWLEDGMENTS I would first like to thank my parents for their unwavering support of all my endeavors. Throughout my life they have always encourage d me to express my individuality and intelligence to the best of my abilities. Without their help my successful completion of a graduate degree would be impossible. I would next like to thank my advisor, Dr. Nam Ho Kim. Dr. Kim provided me with the fund ing and research ideas to make this thesis possible. His constant guidance and respect for all of his students is crucial for successful research. His professional attitude helped me to grow and mature professionally while at the University of Florida. I would also like to thank my lab mates, graduate professors and friends who have contributed so much to my research. PAGE 4 4 TABLE OF CONTENTS page ACKNOWLEDGMENTS .................................................................................................................... 3 LIST OF TABLES ................................................................................................................................ 5 LIST OF FIGURES .............................................................................................................................. 6 ABSTRACT .......................................................................................................................................... 8 CHAPTER 1 INTRODUCTION ......................................................................................................................... 9 2 LITERATURE REVIEW ........................................................................................................... 14 Current Trends in Bending Stress Analysis ............................................................................... 14 Current Trends in Contact Analysis ........................................................................................... 16 Current Trends in Wear Analysis ............................................................................................... 18 Gear Misalignment and its Effects ............................................................................................. 20 3 SCOPE AND OBJECTIVE ........................................................................................................ 21 Problem Statement ...................................................................................................................... 21 Justification of Rese arch Uniqueness ........................................................................................ 21 Usefulness of Current Research ................................................................................................. 25 4 RESEARCH METHOD AND RESULTS ................................................................................ 28 Lewis Bending and A merican G ear M anufacturers A ssociation Gear Standard .................... 28 Hertzian Contact Stress ............................................................................................................... 32 Spur Gear Numerical Analysis Utilizing ANSYS .................................................................... 34 Comparison of Numerical to Analytical Results ....................................................................... 41 Two Dimensional Non -i deal Loading C onditions .................................................................... 44 Three Dimensional Non i deal Loading Condtions ................................................................... 46 Archards Wear Model for Gear Wear ...................................................................................... 50 5 CONCLUSIONS ......................................................................................................................... 77 Conclusions of Research ............................................................................................................. 77 Summary of Contributions ......................................................................................................... 77 Future Research ........................................................................................................................... 78 LIST OF REFERENCES ................................................................................................................... 79 BIOGRAPHICAL SKETCH ............................................................................................................. 83 PAGE 5 5 LIST OF TABLES Table page 4 1 Parameters for spur gear and pinion ..................................................................................... 56 4 2 Comparison of analytical to numer ical bending stress ........................................................ 56 4 3 Comparison of analytical to numerical contact stress .......................................................... 56 4 4 Comparison of analytical to numerical ben ding stress 0.01 increase ............................... 56 4 5 Comparison of analytical to numerical bending stress 0.02 increase ............................... 56 4 6 Comparison of analytical to numerical contact stress 0.02 increase ................................. 57 4 7 Bending stress values for ideal 3 dimensional spur gear ..................................................... 5 7 4 8 Compariso n of ideal 3 dimensional bending stress to out of plane translation .................. 57 4 9 Comparison of ideal 3 dimensional bending stress to baxis rotation ................................ 57 4 10 Comparison of maximum wear depths ................................................................................. 57 PAGE 6 6 LIST OF FIGURES Figure page 4 1 Beam in bending ..................................................................................................................... 58 4 2 Cantilever beam with tip load ................................................................................................ 58 4 3 Spur gear geometry ................................................................................................................ 59 4 4 A merican gear manufacturers association gear parameters ................................................ 59 4 5 American gear manufacturers association gear parameters cont. ....................................... 60 4 6 Hertzian contact (cylinder an d gear) ..................................................................................... 60 4 7 Additional spur gear parameters ............................................................................................ 61 4 8 Finite element mesh of spur gear .......................................................................................... 61 4 9 Contact and target elements ................................................................................................... 62 4 10 F inite element analysis code hierarchy ................................................................................. 62 4 11 American gear manufacturers association gear constants and results ................................ 63 4 13 Reduced Von Mises stress plot ............................................................................................. 64 4 14 Comparison of numerical and an alytical results .................................................................. 64 4 15 Spur gear contact stress .......................................................................................................... 65 4 16 Comparison of numerical to analytical results (contact stress) ........................................... 65 4 17 Non -ideal axial separation ..................................................................................................... 66 4 18 Bending stress with 0.01 axial increase .............................................................................. 66 4 19 Bending stress with 0.01 and 0.02 axial increase ............................................................. 67 4 20 Contact stress with 0.02 axial increase ............................................................................... 68 4 21 Three dimensional spur gear mesh ........................................................................................ 68 4 22 Out of plane translation .......................................................................................................... 69 4 23 b axis rotation ......................................................................................................................... 69 4 24 Three dimensional ideal contact stress ................................................................................. 70 PAGE 7 7 4 25 Ideal contact stress vs out of plane translation (3 dimensional) .......................................... 71 4 26 Ideal contact stress vs b axis rotation (3 dimensional) ........................................................ 71 4 27 Normal direction for wear update ......................................................................................... 72 4 28 F inite element analysis code hierarchy for wear simulation ............................................... 72 4 29 Progressive wear; first vs. last cycle ..................................................................................... 73 4 30 Total accu mulated wear depth (ideal separation) ................................................................. 73 4 31 Gear sliding distance .............................................................................................................. 74 4 32 Incremental wear profiles ...................................................................................................... 74 4 33 Wear depth superimposed on gear surface ........................................................................... 75 4 34 Progressive wear, first vs. last cycle (non ideal separation) ................................................ 75 4 35 Total accumulated wear depth (non ideal separation) ......................................................... 76 PAGE 8 8 Abstract of Thesis Presented to the Graduate School of the University of Florida in Partial Fulfillment of the Requi rements for the Degree of Master of Science A FINITE ELEMENT APPROACH TO SPUR GEAR RESPONSE AND WEAR UNDER NONIDEAL LOADING By Kyle C. Stoker May 2009 Chair: Nam Ho Kim Major: Mechanical Engineering Spur gear response and wear is an engineering probl em which has been around for hundreds of years. The method to determine stresses analytically has been developed extensively by the American Gear Manufacturers Association, and experimental techniques investigating wear of spur gears is well documented. Currently engineers design gears based on a fixed safety factor which determines the lifetime of a gear based on predictable loads and stresses. Additionally, all mechanical assemblies are subject to tolerances that limit the amount of error between physi cal components. When assemblies are operated at the limits of these errors, stresses and wear will increase. This research has provided the engineer with a tool to predict where and by how much the stresses of spur gears will increase when nonideal condi tions are present for both 2 dimensional and 3 dimensional analysis. A wide range of spur gears can be input to the parametric code and the Finite Element Analysis program will solve the contact problem and produce valid results. A method to predict progressive wear evolution for a 2 dimensional spur gear according to Archards wear law has been implemented within the FEA code. The research has shown that with an increase in the axial separation wear depths will increase and the wear profile will be modi fied. PAGE 9 9 CHAPTER 1 INTRODUCTION Gears are an integral and necessary component in our everyday lives. They are present in the automobiles and bicycles we travel with, satellites we communicate with, and computers we work with. Gears have been around for hundreds of years and their shapes, sizes, and uses are limitless. For the vast majority of our history gears have been understood only functionally. That is to say, the way they transmit power and the size they need to be to transmit that power have been w ell known for many years. It was not until recently that humans began to use mathematics and engineering to more accurately and safely design these gears. Wilfred Lewis introduced a method to calculate the amount of stress at the base of a gear tooth in 1892. His method was based upon a cantilever beam which was subjected to a load at the tip of the beam. Although this method was crude, it remains one of the bases for gear design to this day. Heinrich Hertz began his own work on contact pressures aroun d the same time in 1895. His research on the elastic contact of two cylindrical bodies allowed engineers to calculate the contact pressure between a gear and a pinion. With these tools engineers were able to better predict the bending stress and contact pressures of gear pairs to allow for more robust design. Continuing with this trend gear design engineers sought to reduce the overall weight and size of gear pairs while still maintaining a high level of safety. In this discussion, safety is defined as the ratio of actual stress to allowable stress. If this ratio exceeds one, the component will fail. Many organizations, including the American Gear Manufacturers Association (AGMA) have sought to standardize the gear design process by developing their own formulas for gear design. The major changes over Lewis original equations are the ability to take into account the geometrical complexity of the gear tooth, as well as the actual location of the contact. PAGE 10 10 With the advent of Finite Element Analysis and Computer Aided Design (FEA and CAD) the ability to quickly and accurately design gears has been greatly improved upon. With modern CAD programs a typical gear and pinion can be modeled relatively easy. With better computing power, FEA software can quick ly and efficiently analyze the stresses and contact pressures in gear pairs. These tools make the design and analysis stage much cheaper and faster for the design engineer. Because actual experiments are costly and take large amounts of time, a repeatabl e and accurate design tool is crucial for real world application. With the advent of tighter tolerances and more demand to produce lightweight structures small deviations in tolerances can cause gears to fail before their specified lifetime. These devi ations are present in any mechanical system and are prescribed by the engineer. Typical tolerances can change in any of the three principal directions by as much as 0.02", or 0.508 mm. Within this small window of allowable tolerances drastic changes in b ending stress and contact pressure can occur. As the distance between the gear and pinions axis of rotation increases the bending stress and contact pressure rise. A relatively small rise in bending stress can cause a gear tooth to fail at lower cycle n umbers than the design calls for. With an increase in the contact pressure between a gear and pinion wear will be increased as well. With increased wear, gear failure may occur sooner by pitting, corrosion, and adhesive wear. Much work has been done exp erimentally over a wide range of circumstances. The effect of higher torques on the load carrying capabilities of gears has been extensively studied to determine the allowable operating conditions. In addition to higher torques, higher operating speeds have been experimented with to see how the wear regime may change from oxidation wear to bulk wear. Because of these extensive studies and experiments many gear manufacturers today use case PAGE 11 11 hardened gears to alleviate the harmful effects of high contact pr essure. These hardened regions of the gear tooth allow for higher contact pressures without the detrimental effects. Although much study has been done on the mechanisms of gear wear and the major contributors to that wear, there is still a lack of unders tanding when it comes to the tolerances and how they affect the wear characteristics. Inherent in any mechanical system will be a small window of allowable space that the gears can be assembled in. In worst -case scenarios these small windows of tolerance s may stack up to produce an overall large deviation from ideal assembly. With modern CAD and FEA software the input of these tolerance deviations are relatively simple, cheap, and repeatable. The purpose of this research is to provide a parametric gea r design code capable of introducing these tolerance anomalies, or non-ideal conditions. The program can quickly and accurately model a real world gear and pinion and introduce a variety of non ideal conditions. With these nonideal conditions in place the gear and pinion will be rotated and the contact pressures and bending stresses compared to the ideal case. We will see that both the contact pressure and bending stress will increase as these conditions are imposed. One important discovery was that with minimal changes to the axial separation between the gear and pinion contact pressures can drastically increase over a portion of the rotation due to a decrease in the load sharing capabilities of the gear pair. This phenomenon will be discussed more in depth in Chapter 4. In addition to developing a parametric tool capable of predicting where and by how much bending stress and contact pressures increase due to tolerance errors, this program will also be able to predict the wear profile over thousands of cycles. This was accomplished by designing an FEA code that selectively modifies nodal locations according to Archards wear model. As the nonideal conditions are introduced the contact pressure between the gear and pinion was PAGE 12 12 found to increase. Because Archards wear model is directly proportional to the contact pressure, the predicted wear will increase. Also, as the non -ideal conditions are imposed the sliding characteristics of the gear and pinion are modified. This program is able to capture these geometric effects and include them within the wear regime. This research will provide an efficient and repeatable process which will determine where and by how much the wear will change and the effect this has on the predicted life cycle of the gear The final stage of this research proposes a relatively simple experimental set up that could be designed and built to validate these results. Typical gear test rigs available for purchase can range in excess of $10,000. For most applications this exor bitant price eliminates the possibility of on -site testing. A much simpler and pragmatic solution is proposed that has a total cost of under $1,000. The capabilities of this rig would be two-fold. One, the test rig will be able to provide an input torqu e to a drive gear, which turns the driven gear. After a pre determined set of cycles the amount of wear in two nylon gears can be determined by a mass measurement. The second part of the experiment would be to introduce the nonideal conditions to investigate how the amount of wear is affected. The purpose of this would be to validate the theoretical results. This discussion will continue with a review of the current and past practices for gear design in Chapte r 2. L iterature review s of the current t rends and practices for gear design and analysis will also be included. Chapter 3 will concisely state the contribution of this work to the engineering community, and justify the originality of this research. Chapter 4 is the main body of this thesis and will include the procedure and methods for obtaining the results. Chapter 5 focuses on the specific conclusions and the contribution of new knowledge. Some future PAGE 13 13 research recommendations will also be made pertaining to additional wear analysis and an e xperimental test rig. PAGE 14 14 CHAPTER 2 LITERATURE REVIEW Current Trends in Bending Stress Analysis Until the mid 20th century all gear design was based upon Lewis original bending equation [1,2]. Lewis based his analysis on a cantilever beam and assumed that f ailure will occur at the weakest point of this beam. Lewis considered the weakest point as the cross -section at the base of the spur gear. However, failure due to flexural stresses on bodies with changing or asymmetrical cross -sections was proved inaccur ate by Dolan and Broghamer [2]. Their approach used photoelastic experiments to visualize the stress concentrations due to the fillets at the base of spur gears. By these visualization techniques they were able to more accurately predict at what stress l evels gears will fail due to high bending stresses. Much early work was done using photoelastic experiments to design spur gears based on the stresses observed at the most critical points [3]. The correct placement of keyways in relation to gear teeth as well as the maximum acceptable diameters was recommended. While these methods were useful in determining static stresses in spur gears, the photoelastic trend moved toward dynamic analysis [4]. Dynamic photoelastic analysis allowed scientists to documen t the scattered stress values due to gear vibration and power transmission. With this continuing trend of experimental bending stress analysis the American Gear Manufacturers Association (AGMA) published their own standard based on Lewis original equatio n [5]. Established in 1982, this standard is still widely used in gear design today [6]. The current trend is to more accurately compute and predict the geometry factors which are critical in determining bending stresses for a wide variety of gears [7]. These geometry factors account for the changing shape of the gear tooth, the point where the load is applied, as well as the fillet radius at the tip and base of the tooth. PAGE 15 15 Until the mid 1980s the majority of spur gear design and bending analysis was still being done by hand. Although Finite Element Analysis has been around for over half a century, it was not until computing power increased that the real advantages of this method became apparent. With the advent of more powerful computers the ability to analyze and describe the stress state of spur gears increased dramatically. One of the first mentions of Finite Element Analysis with respect to spur gears [8] identifies the importance of this type of analysis. Early FEA of spur gears was very labor intensive for the engineer. The first challenge to overcome was properly modeling the spur gear to capture the correct geometry. Once the geometry has been modeled the types of elements and mesh is crucial. Areas where higher stresses and deformations occur needed to be meshed more densely so that the results were accurate. Many of the first attempts of FEA on spur gears were modeled in 2 dimensions to simplify the solution. Beginning in the early 1990s many attempts were made to analyze the stresses of spur gears using 3D FEA [9]. Again, the accepted method was to accurately model the spur gear, appropriately mesh the gear, and analyze the bending stress. The advantage of this method over experimental techniques is a more cost effective and repeata ble result can be obtained. By verifying that the FEA results correspond closely to experimental results the validity of this type of method has also been confirmed. Modeling spur gears and analyzing the results using the Finite Element Method has led to many insights which may not have been immediately apparent. With dynamic analysis, authors have noted that impact loads can be as much as 1.5 times that of static loads, which is of great importance when selecting appropriate gears [9]. Others have obse rved how the transmission error of spur gears is affected by the size and shape of the gear tooth profile [10]. The current trend of gear design is becoming more focused on designing different shaped gears to transmit higher loads without failure. The purpose of this method is to more precisely PAGE 16 16 engineer these gears so that the maximum efficiency can be achieved. By changing the shape of the gear tooth to an asymmetrical design the authors have proven a decrease in both bending stress and contact pressure [11]. With the ability to accurately and cost effectively model spur gears and obtain accurate bending stress results engineers are attempting to reduce the size of the gears so that cost and weight can be minimized. Current gear design utilizes a safe ty factor when determining the allowable stress versus the actual stress, and safety factor values can be quite high depending on the application. H igh safety factor s would mean that the stress that the gear tooth can transmit is much higher than the actu al stress the tooth will ever be exposed to. While this type of design is desirable for longevity and reliability the cost of manufacture and assembly is inherently increased due to extra material and machining costs. Recent attempts to design the gears based on safety factor matching was introduced [12]. By defining allowable limits for safety factor and other tolerances the authors were able to again modify the shape of the gear to reduce stress in critical regions. The current trend of gear design focuses on minimizing the bending stresses encountered at the base of the spur gear. To aid in this design FEM has taken a strong role as a tool to help identify critical areas. One of the focuses of this research will be to develop an FEA tool which is capa ble of modeling spur gears. I mprovement s on some existing work will be introduced a s the ability to parametrically modify the gear dimensions. By inputting the correct dimensions for any spur gear an accurate model can be created. In addition to mod eling spur gears the program will also be able to quickly and accurately measure the bending stress of the spur gear Current Trends in Contact Analysis In addition to the previously mentioned research the contact pressure at the point of mesh between ge ar and pinion is of great importance. Archard was one of the premier scientists to PAGE 17 17 experiment with contact pressure between two deformable bodies in the 20th century [13]. His work led to many of the modern techniques and formulations that are present today for contact analysis [13,14]. His theory expanded upon the works of Heinrich Hertz, who calculated the contact pressure between two deformable cylinders [15]. In much the same way as the bending stress between the gear and pinion was investigated, th e contact pressure was investigated as well. The difference between the two is that the contact pressure analysis is much more straightforward than the bending stress analysis. While the bending stress is dependant on the geometry and shape of the gear t ooth, the contact pressure is mainly a function of the type of material in contact and the radius of curvature [16]. There has been some research into the contact pressure between a spur gear and pinion, and asymmetrical gearing has again been proven usef ul. The authors of this study were able to design asymmetrical gears to increase the load carrying capacity as well as reduce the overall weight of the system [17]. FEM approach es were used in their research and the results are well documented. Also rel ated to the contact pressure is a vast amount of work on the stiffness of spur gear teeth and the appropriate method of modeling using FEA [18]. Their work has proved the nonlinearity present at the beginning of contact between teeth, as well as the impo rtance of the point of contact. Although the contact pressure problem has been solved and the accuracy validated, there remains much work to be done on the analysis of spur gears when improperly al igned. P roperly aligned spur gear s are designed to mesh w ith the pinion at a precise point. This point is known as the pitch point and provides the maximum amount of power transmission between gear and pinion. Although contact pressures can be high at this point, the metal on metal sliding is theoretically z ero. Because of this condition the wear at this point will be low. If the point of contact is modified due to errors in assembly the contact pressure can increase because of geometric differences PAGE 18 18 between the gear and pinion. This phenomenon will be disc ussed in Chapter 4. In addition to higher contact pressures, the amount of sliding between gear and pinion will increase and cause the wear to increase as well. Current Trends in Wear Analysis There are many mechanisms which are influenced by contact pres sure. One of the most important in gears is the amount of wear that is observed on the surfaces of the gear and pinion. This relationship is directly proportional and was first proposed by Archard [19]. Archards approach utilizes the relationship betwe en contact pressure and sliding distance along with a unique wear constant to predict the amount of material that would be removed when two metallic objects are in contact. Early experimentation was concerned with the amount and location of wear between l ubricated gears [20]. The main focal point of these experiments was to determine the cause of gear failure as it is related to gear wear. Failure from wear can be defined as pitting, corrosion, bulk wear, scoring, and creep. By understanding the process with which wear occurs engineers design spur gears with those considerations in mind. One of the most well documented wear regimes is the tendency for wear to occur mainly at the tip and root of the gear [21]. This is related to Archards wear model because of the geometry of the spur gear. Wear is proportional to the contact pressure as well as relative sliding between the two materials. At the optimal point of contact, known as the pitch point, there is relatively little sliding. The maximum amoun t of power is transmitted between the gear and pinion at this point, and engineers plan on this when designing the shape of spur gears. The shape is known as an involute curve and is crucial for minimal wear between gear and pinion. As the ability to u nderstand the complex wear processes increased the emphasis on experimentation and theoretical analysis grew increasingly popular. One of the most prevalent and accurate methods to measure gear wear was developed using the FZG gear test rig [22]. PAGE 19 19 This ex perimental test rig can accurately apply a torque to a shaft which rotates a gear and pinion. The gears can be either lubricated or un lubricated and the amount of wear is measured by precise mass measurements. Typically, the profile of the gear tooth is measured by a probe to determine the wear depth along the tooth. One important experimentation was conducted by A Flodin and S Andersson [23]. The authors used an FZG rig to study mild wear in spur gears. A known phenomenon in the gear industry is the initially improved contact conditions which are generated as wear just begins to occur. This is generally attributed to small imperfections and roughness on the surface of gear teeth being worn away. Their study proved the observed phenomenon of locally high contact pressures being reduced by the improved contact conditions. Another important landmark for this study was the use of the single point observation method. By following the contact pressures and wear depths at a single point a repeatable tre nd can be observed. They proved their experimental results with a numerical simulation as well. Archards wear equation has been further validated by studies employing Signorinis contact law and Coulombs law of friction to spur gear wear analysis [24]. Further studies have included the dynamic effects of wear to the analysis [25]. By generating an accurate geometrical model depicting spur gear wear the authors showed that the gear ratio can change, which will cause a modification of the durability of the gears in real world application. Other studies have been done on wear of helical gears [26], nylon gears [27], and coated gears lubricated with biodegradable lubricants [28]. The common thread between all of these studies is clear. The need to accur ately model spur gears and correctly predict progressive wear is crucial in the design of gears. Without including progressive effects the safety factor and allowable lifetime of the gear can be affected. Increases in contact pressure and bending stress will invariably lead to more wear and fatigue damage. PAGE 20 20 Gear Misalignment and its Effects One topic that has not been discussed thoroughly is the effect of non -ideal loading conditions on the wear of spur gears. N onideal conditions are characterized by a change in the tolerances or specifications which define the acceptable assembly of a gear train. Some studies have been conducted on how the noise or vibration of spur gears are affected by manufacturing error (tooth surface roughness) or misalignment [2 9,30], although there was no mention of how this could affect wear. Another study modeled face gear drives and the increase in contact pressure and bending stress when misaligned [31]. Their study observed significant increases in the contact pressure, a s well as reduction in the load sharing effects of the teeth. Their recommendations include a more simplified modeling procedure and mesh algorithm to reduce the amount of modeling time. They also suggested including additional misalignments to properly provide gui delines for gear design. One recent study of spur gear misalignment and machining errors confirmed these results [32]. To date, the author has not seen any research on the effects of these misalignments on the bending stress and contact pressure as it pertains to the amount and location of wear. By accurately modeling a spur gear in mesh, introducing misalignments and non-ideal conditions, and predicting the resultant progressive wear using FEM an innovative and valuable design tool will be pr oduced. PAGE 21 21 CHAPTER 3 SCOPE AND OBJECTIVE Problem Statement The main purpose of this research is to provide a parametric spur gear design code which has the ability to predict progressive wear evolution, bending stress increase, and contact pressure increase when subjected to non ideal loading conditions. These nonideal loading conditions are defined by accepted engineering tolerances imposed on real mechanical structures. As the normal life cycle of the mechanical system progresses the outer limits of thes e tolerances will be experienced in some cases. Due to higher stresses and contact pressures the wear will increase along the profile of the gear tooth. This research will provide an engineer with the ability to better design and specify spur gears which are expected to experience these conditions. The ability to more precisely engineer gears closer to a safety factor of one will save manufacturing and materials cost. By better understanding the process which leads to ultimate failure a more reliable an d better engineered product can be produced. Justification of Research Uniqueness In the past there has been some research into the transmission error as gear trains operate [33]. In Chapter 2 the studies done on how the noise and vibrations of gears are affected by misalignment and tooth roughness were also documented [29,30]. The authors in this paper [34] noticed the inherent lack of research in the contact fatigue analysis of gears. Although their research proposed an experimental method to determine how shot -peening may reduce the amount of cracks and surface fatigue experienced on gear teeth, their focus calls for an understanding of the process as it occurs. Another experimental study notes that extremely high pressures and stresses can result fro m a small misalignment of the gear shafts [35]. Fatigue failure due to misalignment of shafts is generally a sudden phenomenon with no warning. PAGE 22 22 Depending on the amount of misalignment, the gear may fail after a relatively short amount of time, or the gea r may last longer. Another study involved a pinion which had failed in service [36]. The conclusion of this study was that the misalignment and improper heat treatment of the gear was fully responsible for the failure. Their recommendations include ensuring that the gears are properly aligned as well as an ability to measure the torque as the gears are in service. One NASA study suggested that an ability to optimize the gear tooth shape to lower contact pressures, as well as a numerical method to diagno se the remaining lifetime of a gear tr ain would be valuable [37]. T ool s capable of predicting the remaining lifetime of a gear train assembled within specific tolerances would be useful for this type of application. To this date there have been many expe riments and research stu dies on spur gear analysis. S earch ing spur gear on a journal article search engine yields over 42,000 hits. Spur gears themselves have been around for thousands of years as well. As the understanding of the dynamics and mathema tics of these gears progressed the ability to better engineer their design improved. Lewis and Hertz were some of the founding fathers of modern gear design technology and their influence is no doubt still felt to this day. Beginning in the early 20th century the understanding of these gears had increased enough to allow for a more thoughtful design. By studying the mechanics behind stress concentrations, metallic wear, and fatigue failure a standardized approach to gear design began to emerge. As exper imental techniques improved the ability to justify these equations were first realized by photoelastic experiments. The actual location and severity of the stress increases could be determined even as the gears themselves rotated. With this new understan ding of where the maximum stress and contact pressure was occurring engineers were able to better design their gear trains. They decided on allowable tolerances for the shafts on which these gears were rotating, as well as minimum thicknesses and diameter s for the gears PAGE 23 23 themselves. As even more research was being conducted in the 1950s a new approach was emerging. Finite Element Analysis began as a somewhat limited field of research. Engineers realized the powerful capability of this new field, but were unable to realize its full potential. Experimental techniques were still being improved upon and the wear mechanisms which influenced the eventual failure of the gear teeth were better understood. Archard introduced his unique contribution to the wear community by capturing the basic components of wear behavior. By developing a wear constant he was able to relate the wear depth to contact pressure and sliding distance. Experimental rigs such as the FZG spur gear test rig were developed to validate his results. As computing power increased the FEA approach was again revisited. Engineers realized that by accurately modeling real world gears in a computational environment, the finite element equations could be included to analyze static loads. Once the validity of this approach was confirmed the trend moved toward dynamic analysis. The effects of impact loading, gear tooth geometry, and types of lubrication were all considered. With the results of the finite element analysis engineers were able to av oid detrimental engineering decisions which would ultimately cause the failure of the gear tooth. Finite element methods began to see use as an optimization tool where the tooth geometry could be modified to reduce the bending stress and contact pressures. Current research of spur gears is focused on avoiding premature failure and understanding the cause of this failure. By designing spur gears closer to a singular value for the safety factor, costs can be reduced dramatically. The reduction of these costs will be realized through less material being used in gear manufacture, as well as a better understanding of when and where maintenance should be preformed. PAGE 24 24 The originality of this research stems first from its parametric design. Some parameters inhe rent to every spur gear have been identified and separated from the gear code which generates the geometry. Any feasible spur gear design can be simply input into this separate file and a new spur gear can quickly and efficiently be modeled. The design e ngineer will not have to spend countless hours modifying or correcting existing models. With this parametric capability numerous spur gear designs can be thoroughly investigated which can be applicable to a wide variety of industries. Some preliminary r esearch has been conducted on how misalignments of gear shafts can affect the bending stress and contact pressure. The vast majority of this work has been done experimentally and there exists no standardized method of analytical study. With a parametric program the input of these nonideal conditions is trivial. By identifying the typical tolerances present in todays mechanical systems the limits of these conditions have been studied in this research. There are three major non ideal conditions which wi ll be considered in this research. The first is the axial separation between the centers of rotation of a spur gear and pinion. The second is an out of plane translation of the spur gear and pinion. The final non-ideal condition is a rotation about the b axis. The b axis is analogous to a rotation around the y axis. Hence, a and c rotations occur about the x and z axes. Although there has been a large number of studies conducted on how the bending stress and contact pressure are altered by conditions such as these, the majority involves experimental results. The authors mainly comment on specific instances and gears without providing a useful analysis tool. This research is unique in the fact that a repeatable and efficient computer code is g enerated to fully analyze these non ideal conditions. By a better understanding of the mechanics involved when gears are operated under these conditions a better design can result. PAGE 25 25 The final original contribution of this research to the engineering commu nity is its ability to predict the amount of wear in 2 dimensions. Archards wear model is used in this wear prediction and progressive wear is considered. Progressive wear is defined as the ability of previous wear to impact the contact pressures of the current cycle and modify the wear profile accordingly. Much experimental analysis has been conducted on the wear characteristics of spur gears. The types of wear have been studied extensively and the manner in which this wear causes gear failure has bee n documented. This research is unique in that the effect that non ideal loading conditions have on the amount of wear is emphasized. Although it is known that a spur gear will wear out, little research has been conducted on how the increasing contact pre ssure due to non -ideal conditions will affect future life cycle predictions. This research will shed light on the severity and location of wear increase due to non -ideal loading so that engineers can plan for this phenomenon according to the specific appl ication of each gear set. Usefulness of Current Research The usefulness of this research will be most applicable to the gear design community. As mentioned in Chapter 2, the current trend of gear design and analysis is most assuredly focused on the reduct ion of cost while maintaining the same level of accuracy and reliability. In the past, the method to ensure reliability was often to over design the gear and pinion. Over design refers to the use of more material or tighter tolerances to ensure that the gear train will not fail before the expected lifetime of the part. While this method ensures reliability it does not advantageously affect the cost of manufacture and assembly. As each engineering application is unique, so too should be the types of gear s and the tolerance requirements for each case. With the advent of higher performing CPUs, the extension of FEA to gear design was inevitable. As mentioned previously, this research will provide the engineer with a tool to quickly change gear parameters and study how nonideal conditions will change the way the gear PAGE 26 26 behaves. This behavior is captured in three separate but interrelated phenomena. This research will first be able to quickly measure the severity and location that bending stress increases d ue to non ideal loading. This will be useful to the engineer when specifying the thickness and size of gear teeth. If for example, a tolerance of 0 .001 is mandatory for a specific application the design engineer can quickly calculate how much fluctuation in bending stress is expected. Depending on this value different materials and sizes of gears can be more precisely determined. The more understanding the engineer has on how tolerances and assembly affect the gear response, the better. Along with be ing able to quickly determine how bending stresses increase, the corresponding increase in contact pressure can be studied as well. Because spur gears are designed using an involute curve the location of contact is crucial. To understand what an involute curve is, imagine a strip of thin sheet metal wrapped around a cylinder of any diameter. If you were able to unwrap this piece of stiff metal from the cylinder, the curve that the end of the strip of metal generates in space would be known as an involute curve. This will be discussed more fully in Chapter 4. The main advantage of using involute curves in spur gear design is that at the pitch point the relative sliding between gear and pinion will be minimal. Because relative sliding between metals is n ecessary for wear to occur, this minimizes the wear depth. In addition to this, the maximum amount of power is transmitted from the drive gear to the driven. When the axial separation or b axis modifications are introduced this advantageous effect will n o longer be present. Because of this the contact pressure can increase substantially, causing localized stress intensities. Theses high values of contact pressure will cause the gear train to fail sooner than expected. At t he outcome of this research th e ability to better understand PAGE 27 27 this situation will be provided. Depending on the application, the design engineer can decide how crucial tolerances for his or her specific gears are. The aspect of this research that is most useful is the ability to predic t the progressive wear evolution, especially when nonideal conditions are present. The amount of research conducted on spur gear wear has been documented in Chapter 2. For over 60 years there have been numerous experimental studies on the effects of lub rication, tooth shape, and operating conditions on the amount of wear. Attempts have been made to modify gear tooth shape based on these observations. Along with experimentation there have also been many analytical studies on spur gear wear. These analy tical studies all employ some type of finite element method to determine the contact pressures of spur gears accurately. The attempts to then model the wear have been minimal, and most of the contributions have come from Anders Flodin. His methods have v alidated the relationship between finite element predictions and the real wear regimes that are evident in spur gear drives. The new contribution to this already established research will be the addition of the nonideal loading conditions. All types of spur gear assemblies are subject to tolerance specifications. The level of accuracy in manufacture and assembly is directly influenced by these specifications. This research will provide engineers with the ability to quickly determine how these tolerance s affect the amount and location of wear. With better engineering techniques and analysis the failure of spur gears due to bending stress has been decreased. The majority of failure occurs due to wear, and this research will provide a direct correlation between tolerances and gear wear. For each specific application the effects on wear can be predicted. This will be useful as the trend of gear design continues towards a more cost efficient product. By fully understanding the process of wear and how wea r regimes may change due to nonideal conditions a robust and efficient tool has been developed. PAGE 28 28 CHAPTER 4 RESEARCH METHOD AND RESULTS Lewis Bending and AGMA Gear Standard As mentioned in Chapter 2 the basis for bending stress analysis of spur gears is ba sed upon Wilfred Lewis original formulation. His theory began with the basis that a spur gear can be simplified as a short beam which is subjected to both tension and compression. Figure 1 illustrates a beam which is subjected to a bending moment at each end. With a bending moment M applied as shown, and the distance from the free edge of the beam to the neutral axis c, the stress is related by Equation 4 1. Mc I 4 1 With this basic formulation for the bendi ng stress of a beam, Lewis was able to extend his assumption to a cantilever beam with a load applied at the tip, shown in Figure 4 2. With a load applied at the tip of the beam, Lewis was able to provide a somewhat accurate representation of a spur gear t ooth. The obvious limitations are numerous. One limitation is that this representation does not take into account the point at which the load would be applied during the real meshing of a gear and pinion. In Chapter 2, it was stated that engineers desig n spur gears to transmit their loads at the pitch point of the gear and pinion where sliding is a minimum. Also, a cantilever beam is generally a long, slender beam whose aspect ratio is different from that of the spur gear tooth. Spur gear teeth are sho rt and stubby, and may respond differently to an applied load. Finally, the geometries of a cantilever beam and spur gear tooth are drastically different. Spur gear teeth have a constantly changing cross -section and fillet radii at the base of each tooth which cause fluctuations in the predicted bending stress. Regardless, this derivation is given to show the evolution of the spur gear bending problem. Equation 42 gives the bending PAGE 29 29 stress relation when the values for the second moment of inertia I are substituted into Equation 41, where L is the length of the beam, t is the thickness, F is the face width, and W is the point where the load is applied. 26 McWL IFt where 312 Ft I 4 2 Equation 4 2 was used for the i nitial analysis of spur gears and it was soon realized that this equation was not valid for most types of spur gears. In order to have an accurate representation of the spur gear response it is necessary to include the relevant geometrical parameters whic h influence the bending stress. Because of the complexity of these parameters, the basic geometry of the spur gear will first be introduced. Then, a more detailed view of a single spur gear tooth will be given and the derivation of the bending stress exp lained. Figure 4 3 represents the typical geometry which is present on a spur gear. The circular thickness is analogous to t in Equation 4 2, the face width is analogous to F, and the length of the tooth is the distance from the fillet radius to the tip. The region of interest for bending stress is at the very bottom area of the spur gear. Because of the transition from a relatively wide and thick tooth to a narrow base, this area experiences the greatest compression and tension on the tooth. Although t he area in compression will have a higher magnitude of stress, gear failure typically occurs in tension due to the formation of cracks. While compression acts to push cracks together, the tension continues to grow the cracks by pulling them apart. Also, the line labeled circular pitch is the diameter on which the majority of contact should occur. This ensures that the maximum amount of power is being transferred, with the minimum amount of slipping. Now that the geometry of the spur gear has been in troduced, it is necessary to define additional parameters which will be used to fully capture the geometry of the spur gear tooth. By PAGE 30 3 0 solving for these geometrical parameters the most accurate analytical solution of the bending stress and contact pressure can be achieved. Figure 4 4 will be referenced throughout the derivation of the AGMA bending stress equation. This derivation is derived in part from [38]. First, a bending stress equation similar to Lewis original is given. For this equation both t he bending and radial stresses are shown: 3cos 1 12 12wD bendingwxxy y 4 3 sin 12w radialw y 4 4 In Equation 4 3, coswDwxx is t w sinww multiplied by the distance from the base of the tooth to give the bending moment. Y is the distance from the center line to the edge of the gear tooth. The remaining portion of Equation 43 is the second moment of the are a. Equation 4 4 uses the radial force along with the thickness 2y to produce the radial stress. Stress concentration factors were introduced in the 1950s to calculate a factor based on geometrical features which would modify the expect ed stress values [39]. For spur gears, the most important stress concentrator occurs at the base of the spur gear tooth. Equation 4 5 gives the stress concentration factor Kf 2 3122k k f fDyy Kk rxx 4 5 In Equati on 4 5, k1, k2, and k3 2 1 2 2 2 30.30540.004890.000069 0.36200.012680.000104 0.29340.006090.000087ss ss ssk k k are all constants given by Dolan and Broghamer in their initial photoelastic experiments [40]. 4 6 PAGE 31 31 In Equation 4 s is the pressure angle, a constant specified for a ll gears. For this case the pressure angle is 20. Rf 2()rrT frT sgrrTaer rr Raer is the fillet radius of curvature, and is given by Equation 47. 4 7 Figure 4 5 is a schematic of how the radius of a gear tooth is for med. In Figure 4 5, A is the gear tooth being generated, and B is the rack cutter. Rsg is the radius of circles centered at the gear axis, for the standard gear. RrT is the radius of the section on the gear tooth cutter which forms the gear fillet radiu s. Ar 2 max1.5 .5tan cosD w twfmxx m w K myy is a point on the radius of the rack cutter which is doing the actual cutting. Finally, e is a profile shift that is necessary for the rack cutter to be in the proper position to cut the gear tooth fillet. Combining Equations 4 3 through 4 7 yield s the final form of the fillet stress formulation. 4 8 The only term not defined in Equation 4 8 is the module m. rp m 4 9 In Equa tion 4 9, pr is a constant known as the rack pitch. Equation 4 8 will be the basis for the analytical bending stress of the spur gear. This equation takes into account the individual geometry of each spur gear, and gives an accurate result for the maximum bending stress. This maximum bending stress is based on x and y locations along the fillet radius of the gear tooth. Equation 4 8 will be used to prove that the results gained from the numerical analysis are consistent with stresses encountered in reali ty. PAGE 32 32 Hertzian Contact Stress The contact stress or contact pressure will be used interchangeably throughout this paper. Either term refers to the amount of stress at the point where a gear and pinion are in mesh. As will be discussed in subsequent subchapters, the value of the contact pressure is extremely important when attempting to predict the amount of wear depth that will occur as the gears rotate. The derivation of this equation was first performed by Henrich Hertz in the late 1800s. Hertzs appro ach is a derivation based upon the elastic contact of two cylinders. When two cylinders are in contact their contact profile is defined by a line. This analogy can be applied to the point of contact between a gear and pinion. Because the profile of a sp ur gear tooth is defined by an involute curve, the radii of the cylinder which generated the curve and the radius of curvature of each tooth is the same. Figure 4 6 w ill clarify this proposition. The Euler -Savary equation proves the relationship between a circle, whose center is denoted as E, and the point of contact A which momentarily corresponds to that circle. Then, Equation 4 10. tanbREAR 4 10 This idea was derived by a combination of the following two sources [38,41]. With the proof that the instantaneous radius of curvature of the involute curve will be equal to the radius of curvature of a cylinder in contact with another cylinder, the contact stress derivation can continue. In reference to the two cylinders in contact, the maximum surface pressure is given by [42], shown as Equation 4 11. max2 W p bl 4 11 PAGE 33 33 With similar convention as shown previously, a force W presses the two cylinders of length l together. The b term in the denominator is the half -width, given in Equation 412. 1/2 22 1122 121/1/ 2 1/1/ EE W b ldd 4 12 M ore convenient convention gives the elastic coefficient Cp 22 12 1211 1pCEE as Equation 4 13. 4 13 In Equat ion 4 1,2 are Poissons ratios, and E1,2 1/2 1211 coscp ww C Frr are Youngs modulus for the gear and pinion. Equation 4 13, 412 and 4 11 can be combined to yield the surface compressive maximum stress as Equation 414. 4 14 The load intensity factor w is given in Equation 4 15. W w F 4 15 In Equation 4 15, uppercase W is the force on the tooth, and F is the face width of the tooth. Referring back to equation 4 14, r1 and r2 w are the instantaneous radii of curvature of the gear and pinion. The cos term relates to the same angle of load as in Equation 4 8. So far the methods for obtaining both the AGMA bending stress equa tion and the Hertzian compressive stress have been derived. These equations are essential in validating the results from a numerical analysis. Although a numerical analysis can greatly enhance the ability to analyze a structure, the results obtained must be accurate. The focus of this paper will now shift to an explanation of how the geometry of the gears are produced in two dimensions using PAGE 34 34 ANSYS, how the boundary conditions and elements are chosen, and the method for obtaining an accurate analysis and post -processing. Once this has been explained, the results will be compared to the analytical results so that the justification and confidence of the results can be verified. Spur Gear Numerical Analysis Utilizing ANSYS The first step to conduct a success ful Finite Element Analysis is to create an accurate geometry for the type of analysis you wish to consider. For this research, the structure of interest is a spur gear and pinion meshing with each other. ANSYS Parametric Design Language (APDL) is used t o create the gear and pinion model, to apply contact and boundary conditions, to control nonlinear solution s e quence, and interpret analysis results. The code that was developed for this problem is separated into four different files, each of which serves its own purpose in creating the model performing analysis, and interpreting the results The first files purpose is to provide the parameteric abilities of the gear design code. Some parameters which are specific to gears are provided as input to the pr ogram. These parameters are all of the necessary components which must be specified to completely generate a gear and pinion. Table 4 1 comprises the entirety of the first file. Its purpose is to provide these necessary inputs to the second file which generates the actual geometries. A more detailed view of a spur gear tooth is shown in Figure 4 7 The modification of these parameters can yield a limitless combination of spur gear teeth. This provides the de sign engineer with a powerful parametric tool capable of quickly adapting to new designs. The second file in the spur gear code serves to generate the 2 dimensional geometry of the gear. One of the main components of this code is the ability to generate a parametrically PAGE 35 35 controlled involute curve to define the tooth shape. I nvolute curve s can be thought of as follows. First, pick a cylinder of any diameter, and place a piece of string tangent to a point on the surface. While keeping the string taut, rot ate the string around the radius of the cylinder. The points traced by the end of the string will constitute an involute curve. Another definition of an involute curve is given as, any curve orthogonal to all the tangents to a given curve [43]. To gen erate the involute curve an arbitrary number of points are chosen to fit the involute curve. For spur gear analysis, 50 points are sufficient. The curves are generated based on the root radius of the gear and pinion. Root radius refers to the radius fro m the center of the gear to the bottom of the tooth. To find an x and y point which would lie on the involute curve the following equations are needed. 2 cos() sin() sin() sin() rT s xcr ycr xxcs yycs 4 16 In Equation 4 16, r is the aforementioned radius, and T is a factor which ranges from zero to one in steps of fifty, depending on the current point of interest. Because there are 50 points chosen to fit the involute curve, there will be 50 different angular values which correspond to the current x and y location. The symbol is used to indicate the angular value which may range from zero to ninety. Once the involute curve has been generated the rest of the geometry is created using similar techniques. The next step in the modeling portion of the code is to generate the finite element mesh which will discretize the gear and pinion into many small pieces. For the 2 -dimensional analysis there are three different types of elements which should be discuss ed. The first type of element PAGE 36 36 is a 4 -node 2-dimensional element, referred to as PLANE182 in ANSYS APDL. This element comprises the bulk of the gear and pinion area. This type of element incorporates finite strain deformation with large rotation, based u pon the principle of virtual work. Assumptions for the use of this type of element are: strain is not infinitesimal, geometry changes during deformation, to simulate nonlinear behavior incremental analysis is used and Cauchy stress is used with a particul ar algorithm to take finite deformation into account. Although the equation for virtual work, Cauchy stress, and displacement formulation are given, the discussion of their theory is not relevant to this research. Refer to [44] for a more complete descri ption of these equations. BS ijij ii ii VSSedVfudVfuds 4 17 1 2j i ij jiu u e xx 4 18 ijij VWedV 4 19 kk ijijklkl ij ikkj ij VVuDu DWeCDedV eDedV xx 4 20 ij is the Cauchy stress component, eij is the deformation tensor where ui is the displacement and xi is the current coordinate. The body and surface for ces are fB and fS The best method for meshing a gear and pinion was developed through an iterative process. With any numerical analysis the computation al time that is necessary to solve the global matrix of equations is a concern. With a high density of elements results will be accurate to a certain degree. However, this causes the CPU time to increase. While a lower density will respectively. The virtual work equation is presented in Equation 4 19, where W is the internal virtual work. The terms in the lower portion of the integral, S and V, are the surface of the deformed body, and volume of deformed body. Fi nally, Equation 4 20 is the pure deformation formula, and is a set of linear equations which can be solved iteratively. PAGE 37 37 yield quicker results the accuracy is not guaranteed. There are a number of methods to modify the mesh in order to achieve accurate results, with minimal computational effort. For this system the area with the highest level of interest is the contact between the gear and pi nion, as well as the base of the teeth. To obtain accurate results it was necessary to increase the mesh density at these points of interest. This capability has been programmed into the code to automatically increase the mesh density near the regions of interest. This ensures accurate results with minimal computation. Figure 4 8 illustrates the mesh necessary to obtain accurate results. There are a few important aspects of this figure which should be mentioned. The first is that away from the gear and pinion teeth the density of the mesh is much less than at the points of contact and root of the teeth. The mesh density is much higher where contact occurs, but only to a certain extent. D ensely mesh ing the entire tooth is not necessary only the line o f contact is meshed more densely. Also, the pinion (on the left) rotates counter -clockwise, meaning that only the contact side of the teeth needs higher density meshing. Corresponding to this direction of rotation is an intuitive understanding of where f ailure would be expected to occur based on loading. Although the compressive stress at the base of the gear tooth may be higher than the tensile stress, cracks will occur on the tensile side of the gear tooth, eventually leading to catastrophic failure [4 5]. The authors of this study modeled a crack on the tensile side of the gear tooth to predict remaining useful life. Therefore, it was only necessary to increase the mesh density on this region of the gear tooth to provide accurate tensile stress result s. The combination of all of these factors led to the shortest possible computation time while still providing accurate results. PAGE 38 38 The next type of element necessary to complete this analysis is known as a contact element. The complement to this element is necessary as well, and is known as the target element. The geometry of the contact and target elements are shown in Figure 4 9. In Figure 4 9 the top surface is denoted as the Target Surface. This target surface is defined by the geometry of the gear or pinion. As mentioned before the geometry of this section was generated through a combination of an involute curve and then subsequently meshed with the 2 dimensional plane stress elements. The Target Element is overlaid on the mesh already created o n the gear surface. The node numbering that was used for the 2 dimensional elements is employed with the target element as well. T arget element s will conform to the type of mesh which is present on the surface of the geometry. This means that a target e lement could be either one, two, or three nodes if midside nodes are used for the underlying surface. For this analysis, a 2 node target element is used to represent the contact between gear and pinion. For the entire surface of the gear and pinion, target elements are generated to create a target surface. The next region of interest is the Contact Surface. The contact surface corresponds to the opposite surface from the target surface where contact is expected to occur. Similar to the target elemen t, the contact element conforms to the geometry and mesh type of the underlying surface. Because the gear and pinion are similar, the contact element will also be a 2 node element. The contact element is necessary to solve for the contact pressure and sl iding distance between the gear and pinion. ANSYS searches for contact between the target and contact surfaces, and contact must always occur in the normal direction. It is necessary to input the type of stress state for this element, which is plane stress. In addition to inputting plane stress, the thickness of the gear is input so that results are consistent. In Figure 4 9 notice that the contact element and target element are not necessarily contacting at the nodal locations. Contact is PAGE 39 39 calculated at integration points located within each element, and then averaged across the element surface. The contact element is a non -linear element, and requires full iterative Newton solutions. Because of this, computational time can be significant depending on the number of contact elements which are present. The previous explanation shows how a contact set would be applied between a gear and pinion. However, because there is only one target surface and one contact surface, results would only be given on the contact surface. To remedy this situation, the opposite formulation is necessary to obtain results on both surfaces. This is achieved by creating a target surface where the contact surface was present in Figure 4 9, and a contact surface where the targe t surface was. By this procedure results for the contact pressure can be obtained for both gear and pinion. Now that the gear and pinion have been meshed with both solid elements and contact elements, results for both bending stress and contact stress wi ll be available. The next step in the modeling process is to begin applying boundary conditions and necessary restrictions to ensure that the results obtained are accurate. The first step in applying these boundary conditions is to generate an additional set of elements known as rigid elements. The purpose of these rigid elements is to apply kinematic constraints between nodes. These elements are necessary to properly constrain the rotations of the gear and pinion. The specific type of element is kno wn as a rigid beam, and the direct elimination method is used to apply the constraints. The direct elimination method is imposed by internally generated multipoint constraint equations [46]. N ode s are created at the center of rotation for both the gear a nd pinion. This node is constrained in all six degrees of freedom, and the rigid beam elements are connected between this node and the inside diameter of the gear and pinion. The final step in the modeling process is to copy the area of the pinion in minute increments until contact occurs with PAGE 40 40 the gear. This is done iteratively until contact just occurs, and then the process is stopped. At this point, the finite element solution is ready to begin. The simulation phase of the finite element gear program is divided into two parts. The first section of the code is responsible for first ensuring that the non linear geometry option is selected. Then, a torque is applied to the pinion around the z axis. Recall that contact has already been established betwe en the gear and the pinion. R amp load ing is used to gradually apply this torque while the gear is held in place. Once this solution has converged for the prescribed number of sub-steps, the next section of the solution code is run. For this portion, the rotation of the gear about the z axis is prescribed. The applied torque from the previous load step is held constant at the prescribed value. Because only a portion of the gear is being modeled, the rotation is confined to 2 N wh ere N is the number of teeth of the gear. This rotation is broken up into 40 sub -steps which solve the non linear contact equations at each step. Based on the geometry and mesh shown this solution phase generally takes around 90 minutes of CPU time to co mplete. Once the solution is complete, the post processing of the data may commence. The post processing of the data is straight forward for bending stress and contact pressure calculations. For the bending stress it was mentioned previously that the reg ion where tensile stress is present is the region of interest. The node at which the maximum value is achieved throughout the solution process is noted, and the data for each sub -step recorded. Next, for the contact pressure the same type of analysis is performed. The critical node is chosen and its contact pressure values throughout the analysis are recorded. The only difference with the contact pressure calculation involves the scarcity of data. Contact may only occur for one or two sub -steps in the entire 40 sub-step process. Therefore, the Von Mises contact stress is also PAGE 41 41 recorded at the node of interest. When the contact is actually occurring, the values for contact pressure and Von Mises stress will closely correspond. Figure 4 10 presents a sc hematic of the FEA code, and the following subchapter will compare the numerical to the analytical results. Comparison of Numerical to Analytical Results The first step in comparing the numerical to analytical results was choosing a valid gear for the ana lysis. One reference in the gearing community was chosen, and was able to provide relevant data for a typical gear [47]. Based upon recommendations, an input torque of 800 N -m was applied to the pinion. The corresponding calculations from the parameters given in Table 4 1 are shown in Figure 4 11. This spreadsheet contains the relevant equations discussed previously. Figure 4 11 provides all of the necessary information to predict both the contact pressure and maximum bending stress in accordance with t he AGMA guidelines. The first parameter column mainly lists the values given in Table 4 1. Judicious decisions are necessary to properly determine whether parameters from the gear or pinion should be used. In all cases, the value which would provide a h igher stress or contact pressure are utilized. The remaining columns are based on AGMA calculations that were given in previous sections. These are mostly geometric properties specific to this particular gear. Whenever a new or different gear is introdu ced, one must manually input the parameters of column one to generate results. Also, in the final column of Figure 4 11 x and y values of 34.45 and 3.71 mms are given. These values were chosen to maximize the final result for t. The x and y values must correspond to real values which are present at the base of the pinion. Values which lie outside of the gear volume are invalid. The process of maximizing the x and y values can vary depending on the software used. Microsoft Excel has an embedded feature which allows the user to maximize an equation based on given constraints. This was the method chosen for this research. From Figure 4 11 the highlighted PAGE 42 42 c t Figure 4 14 are the relevant outputs desired by the user. The se are the analytical maximums and will be compared to the numerical analysis to verify their accuracy. Using the method described previously, the pertinent information was input to the first file of the FEA program. The area was then meshed, and the simu lation was run. The post processing of the data will give the results needed to compare with the analytical solution. Figure 412 is a contour plot of the Von Mises Stress. There are a number of important aspects of Figure 4 12 which should be noted. The first is the Step and Sub indicators in the top left of Figure 4 12. This indicates that the data being read is from the first load step (applied torque with fixed boundary conditions on gear and pinion) and sub -step 17 out of 40. The second is the thin lines which radiate away from the inner diameter of the gear and pinion. These are the rigid link elements, and their presence creates artificial stresses due to the constraints. In order to view the results accurately, the elements which are affected b y the constraints are unselected. Figure 4 13 is the same data, with the elements affected by the constraints unselected. From Figure 4 13 a graphic representation of the Von -Mises stress is given for all elements. As expected, the maximum regions are at the base of the pinion where tension and compression occur. For a more accurate representation of these results, the node at which this maximum value occurs will be selected. Then, the stress curve for the entire analysis will be plotted so that certain trends and comparisons may be made. is a plot which was generated using the data over all sub -steps for the node which experiences the highest value of tensile stress. This will be the region of the pinion which wo uld be expected to experience the maximum tensile stresses which would ultimately cause failure due to the formation of cracks. The solid line in Figure 4 14 plots the data over the range PAGE 43 43 of motion discussed previously, 2 N or 14.4 degrees. The solid black data point is the point where the analytical equations predicted the maximum value. Table 4 2 gives the percent difference between the two. With a relatively close correlation between the analytical an d numerical results the accuracy of the F EA program can be verified. One important aspect of Figure 4 14 that should be discussed is the region around 4 degrees of rotation. The Von Mises stress directly before this region is in creasing relatively quickly, and then suddenly decreases. This is due to a phenomenon in gearing known as load sharing and will be a crucial element in the nonideal loading cases. For now, it is viewed as an advantageous effect because the stress valu e is decreased due to three teeth being in contact at the same time, thus causing the bending stress to decrease. Next, the contact pressure at the critical node in contact will be discussed. The same analysis is used to generate the contact pressure plo ts, the only difference being the point of rotation in which this maximum value is achieved. For the Hertzian contact model, the maximum is calculated when the tip of the pinion is contacting the gear surface. Because of the reduced area of contact, loca l values of pressure can be very high. Figure 4 15 illustrates the contact pressure graphically. Because the surface of the gear tooth is discretized into many small pieces, contact only occurs in a relatively low number of contact events. To better plot the data, the assumption that at the point of contact, Von Mises Stress is equal to contact pressure is used. Figure 4 16 illustrates these values. Figure 4 16 plots the Von Mises stress for the node which experiences the highest contact pressure in the ideal separation case. The maximum value given by ANSYS for the contact pressure was 1431 MPa. The solid data point represents the analytical value obtained from the PAGE 44 44 AGMA equations. Table 4 3 presents the percent difference between the numerical and ana lytical results. With the data presented in the figures and tables, the accuracy of the numerical analysis is confirmed. With an accurate numerical analysis, the confidence of the FEA program can be ensured. This same analysis will be extended to the 2 d imensional case for non ideal loading conditions. Two Dimensional Non -Ideal Loading Conditions Inherent in any mechanical system are tolerances which describe the clearances between parts. For this research the clearances in question are due to the shafts on which the gear and pinion are mounted. When an engineer begins design of this system the decision of what an allowable tolerance may be is made. This decision is ultimately based on the end use of the gear. For non critical gear trains clearances wi ll be larger than critical gear trains. For our discussion, a maximum tolerance of 0.02 inches, or 0.508 mms will be employed. For the 2 dimensional case, this means that the axial separation between gear and pinion can be either ideal, or any number of combinations up to .02 inches from ideal. In much the same way as before, the Von Mises and contact stress will be recorded for three different cases. First, an increase of 0.01 inches will be explored, followed by the maximum increase of 0.02 inches. Figure 4 17 will clarify the non -ideal axial separation problem. From Figure 4 17 the type of non-ideal condition which can be applied to 2 dimensional gear analysis is evident. This separation will be modified and the effects on the bending and contact stress will be presented. The first case is an increase of 0.01 inches, and the same node from before is used to plot the bending stress. The dashed line in Figure 4 18 represents the 0.01 inch increase of axial separation. Immediately apparent is the a cross the board increase in the bending stress at the base of the gear PAGE 45 45 tooth. This is due to the increased bending moment induced by a larger moment arm. Table 4 4 relates the percent increase between maximum values. With a 0.01 inch increase in axial se paration, a 1.39% increase in the maximum bendin g stress value is realized Although this value falls within the error range of the numerical analysis, the obvious trend is an increase in the bending stress, which will lead to fatigue failure at a diminis hed number of cycles. The relevance of this will be discussed further at the maximum non -ideal axial separation. For brevity, the comparison of contact pressures will be reserved for the 0.02 inch increase. The same procedure was followed as before, wi th a 0.02 inch increase in the axial separation between gear and pinion. Figure 4 19 compares all three cases. The final percent difference between the ideal case and 0.02 inch non -ideal case is given in Table 4 5. From Table 4 5, a 2.35% increase in the maximum bending stress is predicted with an increase in axial separation of 0.02 inches. More important than this increase in the maximum bending stress is the region where load sharing is evident in the ideal case. As mentioned previously, this advantag eous effect is due to three of the gear teeth being in contact for a portion of rotation. This reduction in the bending stress is advantageous, and design engineers rely on this phenomenon. With an increase in the axial separation, this effect is elimina ted and the stress will increase for a period of rotation, due to one tooth being in contact. This effect would have the largest impact on the life cycle analysis of the gear. With a 10% increase in stress, life cycle fatigue analysis shows a reductio n of 50 % expected lifetime [42]. The difference between the ideal case and non -ideal case where load sha ring is reduced is 49.15% This effect would be major and cannot be ignored for gear design in which tolerances meet or exceed 0 .02 inches. PAGE 46 46 Next, the Von Mises stress at the point of contact is given for the same node as was previously recorded. Figure 4 20 is a plot of the Von Mises Stress for a node near the tip of the pinion. When an ideal separation between gear and pinion exists, the maximum value o btained from ANSYS was 1431 MPa. With a 0.02 inch increase in the separation between gear and pinion, the contact pressure can be as large as 1648 MPa. In Figure 4 20, keep in mind that the axial separation between gear and pinion has increased. Due to this change in separation, the point of contact is no longer the same as the ideal case. This is the reason why the dashed plot shows contact occurring at an earlier angular rotation than the ideal case. Due to the axial separation increase of 0.02 inch es, the contact pressure can i ncrease by as much as 15 % This would undoubtedly lead to higher rates of wear and fatigue. Thus far the method to simulate a 2 dimensional gear subject to increases in axial separation has been presented. The next section will present the 3 dimensional case, and the non ideal conditions that may arise. Three Dimensional Non -Ideal Loading Condtions The method of producing a 3 dimensional volume in ANSYS is similar to the 2 dimensional method. The same file is used to first generate the 2 dimensional area which is identical to the gear and pinion used in the previous sub -chapter. Then, the area can be extruded to produce a 3 dimensional volume. Instead of using 2 dimensional plane stress elements, the element type is modif ied to represent the new 3 dimensional geometry. For the area mesh of the gear and pinion, the plane stre ss 4 node element was used. C ommands in ANSYS are issued to extrude the area to generate a volume. This will create 8 node brick elements for the bu lk material, known as SOLID45 in ANSYS. In addition to solid elements, the contact elements for 3 dimensional analysis must be modified as well. For the target elements, TARGE170 is the PAGE 47 47 preferred element for 3 dimensional analysis. This element can be u sed to represent any number of geometries, corresponding to the underlying structure. Because the 8 node brick element is the underlying structure, 4 node quadrilateral target elements are generated. Similar to the 2 dimensional analysis, generation of c ontact elements on the converse surface is necessary as well. CONTA173 elements are used in ANSYS, which are 3 dimensional 4 node contact elements. This element conforms to the underlying geometry of the associated surface, and is overlaid on the SOLID45 elements. Also, it is necessary to create contact and target elements on both the gear and pinion so that results are available for each. Figure 4 21 presents the 3 dimensional gear and pinion which will be used for this analysis. Next, two additional non -ideal loading conditions will be presented. Figure 4 21 represents the 3 dimensional model assembled under optimal conditions. The results from this analysis will be compared to combinations of the following non-ideal cases: out of plane translation and b axis rotation. The increased axial separation case has been discussed previously and the results are similar. The corresponding representations will be followed by a brief description to completely describe the type of nonideal condition. Figure 4 22 presents the first two nonideal loading conditions. The figure labeled front view relates the increased axial separation discussed previously. The top view relates the out of plane translation. The offset shown above is 0.02 inches, similar to the maximum axial separation. Figure 4 23 gives the baxis rotation, which is the notation in the industry for rotation about the y axis. The following will help to clarify this situation. Figure 4 23 is a highly exaggerated case for the final non ideal loading condition. The b axis rotation corresponds to a rotation about the yaxis, and a value of 5 degrees is shown in Figure 4 23 so that the baxis rotation can be seen clearly. For this research, the maximum b axis rotation PAGE 48 48 is taken to be 0.5 degree s. Next, the results for both the ideal and nonideal loading cases will be presented. First, the results for the ideal 3 dimensional spur gear are given. For the 3 dimensional case, a number of important modifications have been made. The first is the s ize of the gear. In the 2 dimensional case, the face width of the gear is 31.75 mm. For lower computational time, this was modified to 1.25 mm. For a gear whose face width has been reduced to such a small degree, the load must be reduced as well. The t orque was changed to 5 Nm to compensate for the reduction in face width. Finally, the method used to compare the results will be modified as well. Along the base of the gear tooth, 6 nodes are chosen and the Von Mises stress recorded at each sub -step. T he maximum of these values will be compared for each case to determine the response. The contact stress will be plotted as before. Table 4 7 gives the node number and stress values for the nodes at the base of the gear tooth. Table 4 7 is the bending str ess data recorded at the base of the gear. These values were chosen during the load step where the maximum bending stress occurs. This data will be compared to the cases for the out of plane translation, and the rotation in the baxis. Figure 4 24 gives the contact stress for the node which experiences the maximum value. Figure 4 24 is a plot of the contact stress for the node which experiences the maximum value for the ideal case. The maximum contact stress value is 85.28 MPa and occurs at about 11.5 degrees of rotation. The next case will be the out of plane translation. Because the width of the gear has been reduced by a large amount, the amount of expected out of plane translation must decrease as well. For this research the maximum out of plane translation was reduced to 0.25 mm. Table 4 8 gives the comparison to the ideal case for the bending stress values. PAGE 49 49 Table 4 8 compares the bending stress for the same nodes for both the ideal and non -ideal case. For each node an increase in the bending stress is noted, with a m aximum increase of 45.75% The ideal vs. non-ideal contact stress is presented in Figure 4 25. Figure 4 25 presents the ideal contact stress vs. the out of plane contact stress. This data is plotted for the same node as before, and contact occurs during the same rotational angles. With an out of plane translation the contact stress increases from 85.28 MPa to 130.35 M Pa, a difference of 52.8% The reason the contact pressure increases can be explained because of the smaller area of contact. In effect, providing an out of plane translation is reducing the area of contact while keeping the same torque constant. This reduction in contact area will cause the contact stress to increase. The final non ideal case will compare the id eal bending and contact to a rotation about the b axis. Table 4 9 presents the data for the ideal vs. the non ideal case. For all nodes a reduction in the bending stress is noted, with the ma ximum reduction of 50.08% Finally, the comparison of the ideal contact stress vs. b axis rotation is given. Figure 4 26 presents both the ideal contact stress and baxis rotational contact stress. As before, the ideal stress is 85.28 MPa, and the non-ideal case is 144.24 MPa. This is a percent dif ference o f 69.13% When the baxis rotation is introduced, the line of contact between gear and pinion is disrupted. Because ideal contact conditions no longer exist, the contact stress will increase. The trend of non ideal conditions on the response of the spur gear i s consistent. With out of plane translations and b axis rotations, the bending stress increases in the first case, and decreases in the latter. Due to these modifications of the stress values, the predicted lifetime of the spur gear will be modified. In addition to the bending stress, the contact stress increases for PAGE 50 50 each non -ideal case as well. With an increase in the contact stress, Archards wear model will predict higher levels of wear depth. This phenomenon will be presented in the case where non ideal wear is presented. Archards Wear Model for Gear Wear The analysis up to this point has focused on the response of both the bending and contact stress of a gear and pinion due to the introduction of certain non-ideal loading conditions. The remainin g focus will now center on predicting progressive wear evolution using ANSYS. Progressive wear evolution is the combination of predicting a certain wear depth based on a set extrapolation scheme, modifying the nodal locations based on contact pressure, sli ding distance, and a wear constant, and finally rerunning the simulation based on these new nodal locations. In this manner, the influence of past wear on current wear is included. Archards wear model is based on the assumption that the wear volume due to abrasive wear is given as: NF V K sH 4 21 In Equation 4 21, V is the worn volume, s is the sliding distance, K is the wear constant, non -dimensional in Equation 4 21, FN Vh KP sAs dh KP ds is the normal load, and H is the hardness of the material [19,48]. For a more convenient notation, the wear depth is given as Equation 4 22. or hKPs 4 22 By dividing through by th e area A, the volume divided by area leaves height h. Then, the wear progress can be described by a differential equation with its prediction as an initial value PAGE 51 51 problem [49]. In Equation 4 22, K has the units of 3mm Nm From ANSYS, the contact pressure and sliding distance are both degrees of freedom for the selected node, and thus their data is readily obtained. The next topic of concern is picking a valid wear constant value. To do this, a number of experimental papers will be re ferenced. An experimental study conducted by Walton and Goodwin [50] noted wear constants from 2.4105 to 9.3108 where the wear constant is non -dimensional. These values were experimentally studied for spur gears subject to nonlubricated sliding. Ot her studies have found experimental values as low as 11011 for the wear rate of lubricated spur gears [51]. Thus, careful consideration must be taken into account when choosing a valid wear constant. Once the wear depth is calculated in ANSYS, the dir ection in which to update the wear depth is crucial. Because the nodal locations are being modified, each node will have a unique direction for update. Because the contact pressure is assumed to be normal to the surface, the nodal locations will also be updated normal to the surface. Figure 4 27 shows the typical arrangement of nodes on the surface of a gear tooth. From Figure 4 27, an arbitrary node is located at position x,y. Its neighboring nodes are located at positions xn+1,yn+1 and xn 1,yn 1 11 11 xnn ynndxx dyy The desired normal direction is N. Then, the difference between these coordinates is given by Equation 4 23. 4 23 In Equation 4 23 dx and dy are the difference in location between node n +1 and node n 1. Then, the normal direction can be computed via Equation 4 24. PAGE 52 52 22 0 001 ()()0 ijk Ndkdxdy idyjdxk dyidxj N dxdy 4 24 In Equation 4 24, the normal direction N is the cross product of the d vector and unit vector k, in the positive z -direction. The cross product divided by the magnitude then yields the normal direction. The nodal locations will then be updated by the product of the normal direction N, and the wear depth h. The next step in the calculation of wear dep th and geometry update for the spur gear problem is to decide on a value of the wear constant. For this research where un-lubricated sliding of spur gears is considered, a value of 3108 3mm Nm is used. The final step before results of the wear analysis are presented involves the hierarchal scheme used in ANSYS to solve the wear problem, while still extrapolating to reduce computational time. Figure 4 28 will be presented to give the reader the understanding of how the wear program is included in the previously presented FEA program. In Figure 4 28 the same files are present as in the previous explanation. The addition of an extra file which does the wear depth calculations and geometry update is the only new addition. This file is embedded within the analysis section of the FEA code. The prescribed number of cycles can be input to the simulation code, and the wear code will run until that number of cycles has been completed. Thus far, the FEA code and the results shown are from one complete cycle of the gear and pinion. For the wear code it is necessary to run multiple cycles in order to predict wear and the PAGE 53 53 evolution of this wear. Therefore, 20 wear cycles were chosen with an extrapolation of 3,000 cycles per analysis. This r esults in a total number of gear cycles of 60,000 over the course of 20 FEA simulations. From writing and experimenting with the FEA code 60,000 revolutions of the gear was the maximum number attainable without re -meshing. When more revolutions and wear cycles were attempted, the FEA solver diverges because of excessive element distortion. To best illustrate the wear results a number of plots will be generated. All nodes along the exterior of the pinion were selected, and their corresponding wear depth recorded. The plots will be presented with the node number on the x axis, and the wear depth in mm on the yaxis. This first plot shows incremental wear from the first cycle and the last cycle. This is not the total accumulated wear, but illustrates how the progressive wear evolves from cycle 1 to cycle 60,000. Figure 4 29 presents the data for the first and last wear cycle for the middle tooth of the pinion. The first cycle, shown as the solid line, has a maximum nodal wear depth of about 2104 From Figure 4 30 the oscillations seen in the incremental wear depths have diminished. The maximum wear depth for 60,000 cycles is predicted to be about 310 mm. As this would represent a valley in the surface of the pinion, less contact would occur at this point until the surrounding areas surface is worn away. This is the reason that the final cycle has less wear depth in this region. Also, for the first cycle there is an oscillation in the wear depths seen from node 1677 to node 1687. As the wear progresses, the final wear cycle indicated by the dashed line is deeper at points in which the solid line are shallower. This further indicates the evolution of pro gressive wear. One final comment on Figure 4 29 is the area of relatively little wear for both the first and last cycle. This will be explained with a corresponding plot of the sliding distance between gear and pinion, but for now the total accumulated w ear depth for 60,000 cycles is given in Figure 430. 3 mm, with the same PAGE 54 54 area of minimal wear as seen in the previous plot. This is due to the advantageous effects of the involute curve as discussed before. At this point of contact between gear and pinion, little sliding is occurring between the two. Because of this and the relationship that wear i s directly proportional to sliding distance, lesser values of wear depth are predicted. Figure 4 31 is a plot of the accumulated sliding distance for each node along the point of contact. It can be seen that around nodes 1695 and 1696 there is very littl e sliding distance. Figure 4 31 confirms the prediction that the sliding distance around the aforementioned nodes will be minimal. Because of this, the wear around the pitch point will be minimal as well. The final plot for the wear depths shows the acc umulating wear through each of the 20 cycles. The final figure for the ideal wear case takes the total wear depth values for the tooth on both the gear and pinion, and overlays these results on the undeformed surface of the gear teeth. It is necessary to magnify the wear depth by 75x in order to see the wear profile clearly. To explore the effects of non ideal loading on the wear profile, the same procedure was utilized as in the bending and contact stress cases. The number of cycles and wear constant re main the same (60,000 cycles and K=3108), and the axial separation is increased to the maximum of 0.508 mm. A comparison of the first and last cycles of incremental wear is given in Figure 4 34. From the first wear cycle, the maximum predicted wear dept h is 9104One of the major differences between this plot and mm. Compared to the ideal case, this is a difference of 77.8% The last wear cycle is plotted as well, and the progressive wear is evident by points which are further below the surface exhibiting less wear. Figure 4 35 gives the total accumulated wear for the entire 60,000 cycles. Figure 4 30 is the location where minimal sliding occurs. Because the separation between gear and pinion has increased, t he point PAGE 55 55 at which the gears transmit their power is modified. When this point of contact is modified, ideal power transmission will not be realized. In turn, this causes the wear between gear and pinion to increase. In addition to the point of minimal s liding being modified, the bending stress increases as well. Thus there will be more wear near the base of the tooth with an increased value for the bending stress. Table 4 10 gives the percent differences between the ideal and non ideal case. From Tabl e 4 10 the maximum we ar depth increased 22.59% with an increase of 0.508 mm axial separation. PAGE 56 56 Table 4 1 Parameters for spur gear and pinion Pinion (unit: mm) Gear (unit: mm) No. of Teeth 25 31 Pitch Diameter 79.38 98.43 Involute Diameter 74.59 92.49 Addendum 4.43 4.18 Dedendum 5.05 5.3 Tooth Thickness 4.9 4.9 Face Width 31.75 31.75 Root Fillet Radius 1.04 0.99 Tooth Fillet Radius 0.78 0.99 Elastic Modulus 206.80 GPa Poissons Ratio 0.33 Distance b/w axes 88.9 mm Element Size for Teeth 0.1 Element Size for Body 1.0 Friction Coefficient 0.0 Applied Torque 800 N m Table 4 2 Comparison of analytical to numerical bending stress Analytical Stress (MPa) Numerical Stress (MPa) Percent Difference 578.73 MPa 565.22 MPa 2.33% Table 4 3 Comparison of analytical to numerical contact stress Analytical Stres s (MPa) Numerical Stress (MPa) Percent Difference 1466 MPa 1431 MPa 2.39% Table 4 4 Comparison of analytical to numerical bending stress 0.01 increase Analytical Stress (MPa) Numerical Stress (MPa) Percent Difference 565.22 MPa 573.1 MPa 1.39% Table 4 5 Comparison of analytical to numerical bending stress 0.02 increase Analytical Stress (MPa) Numerical Stress (MPa) Percent Difference 565.22 MPa 578.5 MPa 2.35% PAGE 57 57 Table 4 6 Co mparison of analytical to numerical contact stress 0.02 increase Analytical Stress (MPa) Numerical Stress (MPa) Percent Difference 1431 MPa 1648 MPa 15.16% Table 4 7 Bending stress values for ideal 3 dimensional spur gear Node 2996 Node 3539 Node 3538 Node 3537 Node 3536 Node 369 7.61 MPa 6.37 MPa 7.34MPa 7.73 MPa 7.86 MPa 4.74 MPa Table 4 8 Comparison of ideal 3 dimensional bending stress to out of plane translation Node 2996 Node 3539 Node 3538 Node 3537 Node 3536 Node 369 Ideal 7.61 MP a 6.37 MPa 7.34 MPa 7.73 MPa 7.86 MPa 4.74 MPa Non -Ideal 11.03 MPa 8.96 MPa 10.54 MPa 11.21 MPa 11.45 MPa 27.68MPa Difference 44.95% 40.61% 43.59% 44.97% 45.75% 27.68% Table 4 9 Comparison of ideal 3 dimensional bending stress to baxis rotation Node 2996 Node 3539 Node 3538 Node 3537 Node 3536 Node 369 Ideal 7.61 MPa 6.37 MPa 7.34 MPa 7.73 MPa 7.86 MPa 4.74 MPa Non -Ideal 3.80 MPa 3.63 MPa 3.89 MPa 3.96 MPa 3.96 MPa 3.31MPa Difference 50.08% 43.10% 47.03% 48.75% 49.55% 30.27% Table 4 10. Comparison of maximum wear depths Ideal Wear Depth (mm) Non Ideal Wear Depth (mm) Percent Difference 0.003079183 0.0 03774735 22.59% PAGE 58 58 Figure 4 1 Beam in bending Figure 4 2 Cantilever beam with tip load PAGE 59 59 Figure 4 3 Spur gear geometry Figure 4 4 AGMA gear parameters PAGE 60 60 Figure 4 5 AGMA gear parameters cont. Figure 4 6 Hertzian contact (cylinder and gear) PAGE 61 61 Figure 4 7 Additional spur gear parameters Figure 4 8 Finite element mesh of spur gear PAGE 62 62 Figure 4 9 Contact and target elements Figure 4 10. FEA code hierarchy PAGE 63 63 Parameter Value Unit Parameter Value Unit Parameter Value Unit Parameter Value Unit Module 2.59 mm RT144.12 mm Rw140.64 -3.62 Pressure Angle 0.35 radians RT253.39 mm W41.51 deg s' -3.69 Pinion Teeth # 25.00 teeth Rs132.39 mm W-4.01 deg s -7.72 Gear Teeth # 31.00 teeth Rs240.17 mm xW40.55 1.55 Center Distance 88.90 mm Rb130.44 mm yW-2.84 -7.57 Face Width 31.75 mm Rb237.74 mm W45.51 deg g-0.31 radians Pinion Thickness 4.90 mm 39.92 xD43.44 mm R 34.78 Gear Thickness 4.90 mm ps8.14 mm e11.14 R5.28 Pinion Diameter 88.24 mm pb7.65 mm ar-e1-rrT-0.74 x 34.45 Gear Diameter 106.78 mm mc1.65 rf4.05 y 3.71 Addendum 4.43 mm W 26282.99 N h 1.78 k10.18 Tooth Tip Radius 4.03 mm W/Fm 319.46 MPa xr'-0.40 k20.15 Torque 800.00 N-m 124.29 yr'2.40 k30.45 Cp 190.30 Mpa^.5 232.76 Rsg32.39 Kf1.18 Pinion tip radius 0.76 mm kc0.43 Ur-6.02 mm kt1.81 Gear tip radius 0.67 mm c1466.06 MPa 0.74 t578.73 Mpa Figure 4 11. AGMA gear constants and results Figure 4 12. Full Von Mises stress plo t PAGE 64 64 Figure 4 13.Reduced Von Mises stress plot 0 5 10 15 100 150 200 250 300 350 400 450 500 550 600 Rotational Angle (Degrees)Von Mises Stress (MPa)Comparison of Numerical and Analytical Results Numerical Data Analytical Result Figure 4 14. Comparison of numerical and analytical results PAGE 65 65 Figure 4 15. Spur gear contact stress 0 5 10 15 0 500 1000 1500 Rotational Angle (Degrees)Contact Stress (MPa)Comparison of Numerical to Analytical Results Analytical Result Figure 4 16. Comparison of numerical to analytical results (contact stress) PAGE 66 66 Figure 4 17. Non -ideal axial separation 0 5 10 15 100 150 200 250 300 350 400 450 500 550 600 Rotational Angle (Degrees)Von Mises Stress (MPa)Ideal Separation vs. 0.01" Increase Ideal Separation 0.01" Increase Figure 4 18. Bending stress with 0.01 axial increase PAGE 67 67 0 5 10 15 100 200 300 400 500 600 700 Rotational Angle (Degrees)Von Mises Stress (MPa)Ideal Separation vs. Non-Ideal Separation Ideal Separation 0.01" Increase 0.02" Increase Figure 4 19. Bending stress with 0.01 and 0.02 axial increase PAGE 68 68 0 5 10 15 0 200 400 600 800 1000 1200 1400 1600 1800 Rotational Angle (Degrees)Von Mises Stress (MPa)Ideal Separation vs. 0.02" Increase (Contact Stress) Ideal Separation 0.02" Increase Figure 4 20. Contact stress with 0.02 axial increase Figure 4 21. 3 dimensional spur gear mesh PAGE 69 69 Figure 4 22. Out of plane translation Figure 4 23. b axis rotation PAGE 70 70 Figure 4 24. 3 dimensional ideal contact stress PAGE 71 71 Figure 4 25. Ideal contact stress vs out of plane translation (3 dimensional) Figure 4 26. Ideal contact stress vs b axis rotation (3 dimensional) PAGE 72 72 Figure 4 27. Normal direction for wear update Figure 4 28. FEA code hierarchy for wear simulation PAGE 73 73 First vs. Last Wear Cycle 0 0.00005 0.0001 0.00015 0.0002 0.00025 1675 1680 1685 1690 1695 1700 1705 1710 1715 Node Number Wear Depth (mm) First Cycle Last Cycle Figure 4 29. Progressive wear; first vs. last cycl e Total Wear Depth 0 0.0005 0.001 0.0015 0.002 0.0025 0.003 0.0035 1677 1682 1687 1692 1697 1702 1707 Node Number Wear Depth (mm) Total Wear Depth Figure 4 30. Total accumulated wear depth (ideal separation) PAGE 74 74 Gear sliding distance 0.00E+00 1.00E-02 2.00E-02 3.00E-02 4.00E-02 5.00E-02 6.00E-02 1677 1682 1687 1692 1697 1702 1707 Node Number Sliding Distance (mm) Sliding distance Figure 4 31. Gear sliding distance Accumulating Wear Depth 0 0.0005 0.001 0.0015 0.002 0.0025 0.003 0.0035 1675 1680 1685 1690 1695 1700 1705 1710 1715 Node Number Wear Depth (mm) Figure 4 32. Incremental wear profiles PAGE 75 75 10.5 11 11.5 12 12.5 13 13.5 14 14.5 15 15.5 -5.5 -5 -4.5 -4 -3.5 -3 -2.5 x-locationy-location75x Gear/Pinion Wear Profile Figure 4 33. Wear depth superimposed on gear surface First vs. Last Wear Cycle 0 0.0001 0.0002 0.0003 0.0004 0.0005 0.0006 0.0007 0.0008 0.0009 0.001 1677 1682 1687 1692 1697 1702 1707 Node Number Wear Depth (mm) First Wear Cycle Last Wear Cycle Figure 4 34. Progressive wear, first vs. last cycle (nonideal separation) PAGE 76 76 Total Accumulated Wear (Non-Ideal Case) 0 0.0005 0.001 0.0015 0.002 0.0025 0.003 0.0035 0.004 1677 1682 1687 1692 1697 1702 1707 Node Number Wear Depth (mm) Total Wear Figure 4 35. Total accumulated wear depth (non ideal separat ion) PAGE 77 77 CHAPTER 5 CONCLUSIONS Conclusions of Research 1 The most useful contribution of this research was an ability to predict the reduction of the beneficial load sharing phenomenon present in all spur gears. As mentioned in Chapter 3, engineers use this d esirable trait to reduce the bending stress in spur gears. With an increase in axial separation of 0.02 inches, or 0.508 mms, the load sharing effect is eliminated, and the difference in bending stress between ideal and nonideal cases can be as much as 4 9.15% This increase in bending stress would lead to gear failure sooner than expected. 2 Another important topic mentioned in Chapter 3 was the ability of the FEA program to predict progressive wear in 2 dimensions. The program uses nodal updating techniques to progressively update the wear profile for a maximum of 60,000 gear cycles. From Figure 4 29 and Figure 4 34 the progressive wear for the 2 dimensional spur gear is shown. Areas with greater wear depths are not in contact and thus do not experience as much wear in subsequent wear iterations. In addition to modeling progressive wear, the wear depth increased when nonideal conditions were presented. With a 0.508 mm increase in the axial separation, the wear depth increased by 22.58% 3 In Chapter 3 the necessity of a program which is able to predict the location and severity of bending stress increase was stated. This ability was demonstrated for both a 2 dimensional and 3 dimensional analysis subjected to non ideal conditions. For the 2 dimensional analysis and the type of gear chosen, the accuracy of the FEA program was verified, and the maximum bending stress was found to be 565.22 M Pa with an error o f 2.33% When subjected to non -ideal axial separations, the bending stress can increase to 578.5 MPa, an increase of 2.33% In addition, the contact stress is accurate and with an increase in axial separation the maximum value can increase to 1648 MPa, a 15.16% increa se. For the 3 dimensional case, an out of plane translation can increase the maximum bending stress by 45 percent, and a b axis rotation of .5 degrees can decrease the bending stress by 50.08% For the out of plane translation, the contact stress increas es by 52.8% and for the b axis rotation the contact s tress increases by 69.13% Summary of Contributions 1 From Chapter 3, the first unique contribution of this research was the ability to parametrically introduce non ideal loading conditions and study how these conditions affect both 2 dimensional and 3 dimensional gear response. By providing a parametric tool, design engineers can accurately predict the increases in both bending and contact stress, and design gears closer to safety factors for a more opti mized gear train. In addition, the ability to predict when load sharing effects will be eliminated was introduced. 2 Although wear has been modeled using FEA in the past, there have been no studies of how non ideal loading conditions affect the amount of pr ogressive wear. The code introduced through this research has the ability to predict the precise amount and location that the wear PAGE 78 78 profile will change. This will prove useful when specifying the material type or hardness requirements when non ideal loadi ng may be expected to occur. Future Research 1 The most important future research that should be considered would be to continue the 3 dimensional wear code. The main obstacle for this code is properly determining the normal directions of each node along th e contact surface. With this normal direction computation an ability for node numbering independence is desired. Much painstaking effort could be implemented to manually compute normal directions by recording nodal connectivity and computing normal vectors via cross product operations. Another method which could compute these vectors without knowledge of the node numbers or neighboring nodes would be useful. 2 Once the 3 dimensional wear code has been developed, the next logical step would be to study the effects of non ideal loading on the wear profile. The 3 dimensional spur gear FEA code can accommodate many different nonideal loading conditions, and the insight of how this affects wear depth would be useful. 3 Another research topic would be to introduc e different types of gears. Spur gears are the most simple type of gear, and many other designs are in use today. The ability to model and analyze these different gears would be greatly beneficial 4 An optimization problem of the gear shape to reduce bendi ng stress, contact stress and wear depth would benefit the gear design community. Some research has been completed on this topic, and the next step would be to include nonideal loading and wear depth calculations. 5 Finally, an experimental test rig to val idate the theoretical assumptions of Archards wear law and the Finite Element Analysis would be a good research topic. Because a typical metallic gear may experience millions of cycles before appreciable wear is noticed, nylon gears would be the ideal ch oice for a wear analysis. N ylon gear s shoul d be mounted on shafts which are supported by bearings, with the drive shaft connected to an electrical motor. Because of the high wear rate of nylon along with a much easier material to deform, the input torque should be no more than 3.5 N -m. The application of this torque should be brought about by a clutch mechanism or similar device applied to the shaft not connected to the motor. Other experimental test rigs to date have used a combination of pre loading a torsion bar with a defined strain which is measured by a strain gauge. The baseline wear should be calculated by a measured mass loss of the nylon gear, along with a tooth profile measurement. Nonideal conditions can be imposed by precisely machining a mounting plate for the shaft not connected to the motor. Very precise mounting holes can be drilled corresponding to increases in axial separation, out of plane translation and baxis rotation. The response of the nylon gear can then be determined after the appropriate number of cycles have been run. PAGE 79 79 LIST OF REFERENCES [1] W Lewis, Investigation of the Strength of Gear Teeth. Proceedings of Engineering Club, Philadelphia, PA, 1893. p. 16 23 [2] Thomas J. Dolan, Edward L. Broghamer, A Photoelastic Study of Stresses in Gear Tooth Fillets. Engineering Experiment Station Bulletin Series No. 335, University of Illinois, Urbana Champaign, 1942 [3] Paul H. 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Goodwin, The wear of unlubricated metallic spur gears, Wear 222 (1998) 103113 [51] Anders Flodin, Wear of Spur and Helical Gears, Doctoral Thesis, Department of Machine Design, Royal Institute of Technology, S 100 44 Stockholm, Sweden PAGE 83 83 BIOGRAPHICAL SKETCH Kyle Stoker began his undergraduate course work at the University of Florida in August 2002. He graduated cum laude in May 2007 with a B achelor of Science in mechanical e ngineering. Kyle then continued his education at the University of Florida under the advisory of Dr. Nam Ho Kim. Kyle will be re cei ving a Master of Science in mechanical engineering in May of 2009. |