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Full Terms & Conditions of access and use can be found at https://www.tandfonline.com/action/journalInformation?journalCode=utrb20 Tribology Transactions ISSN: 1040-2004 (Print) 1547-397X (Online) Journal homepage: https://www.tandfonline.com/loi/utrb20 Influence of the DIN 3962 Quality Class on the Efficiency in Honed Powder Metal and Wrought Steel Gears Edwin Bergstedt, Anders Holmberg, Per Lindholm & Ulf Olofsson To cite this article: Edwin Bergstedt, Anders Holmberg, Per Lindholm & Ulf Olofsson (2020) Influence of the DIN 3962 Quality Class on the Efficiency in Honed Powder Metal and Wrought Steel Gears, Tribology Transactions, 63:6, 1076-1084, DOI: 10.1080/10402004.2020.1790707 To link to this article: https://doi.org/10.1080/10402004.2020.1790707 © 2020 The Author(s). Published with license by Taylor & Francis Group, LLC. Published online: 12 Aug 2020. Submit your article to this journal Article views: 330 View related articles View Crossmark data
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Page 1: Influence of the DIN 3962 Quality Class on the Efficiency ...

Full Terms & Conditions of access and use can be found athttps://www.tandfonline.com/action/journalInformation?journalCode=utrb20

Tribology Transactions

ISSN: 1040-2004 (Print) 1547-397X (Online) Journal homepage: https://www.tandfonline.com/loi/utrb20

Influence of the DIN 3962 Quality Class on theEfficiency in Honed Powder Metal and WroughtSteel Gears

Edwin Bergstedt, Anders Holmberg, Per Lindholm & Ulf Olofsson

To cite this article: Edwin Bergstedt, Anders Holmberg, Per Lindholm & Ulf Olofsson (2020)Influence of the DIN 3962 Quality Class on the Efficiency in Honed Powder Metal and WroughtSteel Gears, Tribology Transactions, 63:6, 1076-1084, DOI: 10.1080/10402004.2020.1790707

To link to this article: https://doi.org/10.1080/10402004.2020.1790707

© 2020 The Author(s). Published withlicense by Taylor & Francis Group, LLC.

Published online: 12 Aug 2020.

Submit your article to this journal

Article views: 330

View related articles

View Crossmark data

Page 2: Influence of the DIN 3962 Quality Class on the Efficiency ...

Influence of the DIN 3962 Quality Class on the Efficiency in Honed PowderMetal and Wrought Steel Gears

Edwin Bergstedta , Anders Holmbergb, Per Lindholma, and Ulf Olofssona

aDepartment of Machine Design, KTH Royal Institute of Technology, Stockholm, Sweden; bDepartment of Engineering Sciences, AppliedMaterials Science, Uppsala University, Uppsala, Sweden

ABSTRACTTo increase the efficiency of a gearbox, research on gear mesh loss is of importance. Britton et al.concluded that the surface finishing method affects the gear mesh efficiency. The efficiency bene-fits of superfinishing a surface and reducing the surface roughness have been reported byKahraman. A novel method for calculating the bearing loss torque was proposed by Tu et al.Andersson et al. found that the efficiency can vary between 2 and 5% during repeated efficiencytests due to variations in the assembly process. This work investigates how the honing surface fin-ishing process and DIN 3962 quality class affect the gear mesh efficiency by performing tests inan FZG back-to-back test rig. Two materials, a powder metal and a wrought steel, were tested. Allgears were finished using a honing process and sorted according the measured quality class.Powder metal gears of class 6, 7, 8, and �9 and wrought steel gears of class 6, 7, and �9 weretested. The efficiency were calculated from measuring the torque required to maintain a constantvelocity of the FZG test rig. The results from the efficiency tests showed no significant differencein efficiency between the wrought steel and powder metal steel gears. In addition, no obviouscorrelation between the DIN 3962 quality class and the gear mesh efficiency could be found.When examining the wrought steel material it was found that the reproducibility of the efficiencywas comparable to the assembly error of the test rig, despite the variation in quality class.

ARTICLE HISTORYReceived 28 February 2020Accepted 26 June 2020

KEYWORDSFZG; gear; efficiency;powder metal; honing

Introduction

In a time when global warming poses imminent threat tohumanity, every action to decrease the emission of green-house gasses is of importance. One way to decrease emis-sions is to use power transmissions more effectively. Gearsare an effective way of transferring mechanical power butthere are losses in the gear mesh contact. Multiple factorsinfluence the gear mesh efficiency, such as material (1) andsurface roughness (2).

A new and emerging field in gear manufacturing is gearsmade from powder metallurgy (PM) materials. This methodof producing gears shows potential of reducing the cost andthe number of processing steps (3) compared to traditionalgear manufacturing (4). Powder metal gears can be made tonear-net-shape by filling a gear-shaped cavity with metalpowder, compacting the powder using a pressing stamp, andfusing the particles in a diffusion-based sintering process (5).

In recent decades, advances in technology such as warmpressing (5) and new alloying systems have reduced the per-formance gap between sintered and conventional wroughtsteel gears. Nevertheless, powder metal steel has limitationsin highly loaded applications. This is mainly due to the

inherent porosity of the material, as the pores reduce themechanical properties of the material (5). The pores degradethe mechanical properties in multiple ways. Pores are irregu-lar in size and shape and can have sharp edges and couldtherefore be considered as material defects. Defects, espe-cially those with sharp edges, can cause stress concentra-tions, which serves as crack initiation points inside thematerial (6).

The relative density of the powder metal material willalso influence several mechanical properties. The dynamicYoung’s modulus, hardness, and tensile strength of powdermetal steel are shown to have a roughly linear relation tothe relative density (7, 8).

A common way of assessing the dimensional tolerance ofgears is by assigning a quality class. The DIN 3962 (9)standard defines a range of parameters for the gear, geartooth, and gear flank surface. A lower quality class indicatesa higher geometric accuracy, thus increasing the tolerancerequirements on secondary operations; for example, machin-ing and surface finishing. There are a number of parametersin the DIN 3962 gear standard that determine a gears finalquality class. According to the standard, the form deviationsof the gear are measured on at least three teeth, evenly

CONTACT Edwin Bergstedt [email protected] led by N. Weinzapfel.� 2020 The Author(s). Published with license by Taylor & Francis Group, LLC.This is an Open Access article distributed under the terms of the Creative Commons Attribution-NonCommercial-NoDerivatives License (http://creativecommons.org/licenses/by-nc-nd/4.0/), which permits non-commercial re-use, distribution, and reproduction in any medium, provided the original work is properly cited, and is not altered, transformed, or built upon inany way.

TRIBOLOGY TRANSACTIONS2020, VOL. 63, NO. 6, 1076–1084https://doi.org/10.1080/10402004.2020.1790707

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spaced around the gear. For each parameter measured thereis a corresponding quality class range in the standard. Inevaluation of the gear, the final quality class is simply deter-mined by the parameter with the worst quality.

To be able to optimize the cost in relation to the gearmesh efficiency, the effect of the quality class needs to be eval-uated. A good surface finish with tight tolerances is costly toachieve (10). Previous studies on ground and superfinishedgears have concluded that the surface finishing method affectsthe gear mesh efficiency (11, 12). This article seeks to investi-gate whether the DIN 3962 quality class can be related to thegear mesh efficiency and whether there are any differences inthe efficiency of honed powder metal and wrought steel gears.

Material and methods

Test equipment

The efficiency measurements were performed on an FZGback-to-back gear test rig (13) configured for measuring effi-ciency; see Fig. 1. The test rig consist of a test gearbox [1] anda slave gearbox [3], which are connected by two shafts. Thegearboxes are identical in all regards except that the test gear-box has one less axle shaft seal than the slave gearbox. Thegears are mounted on the first shaft and the pinions aremounted on the second. The pinion shaft is divided by a loadcoupling [2], enabling loading of the power loop. A motor [5]drives the power loop to the desired speed. As the power inthe FZG rig is circulating, the motor only needs to supply thetorque equal to the total losses in order to maintain thedesired rotational speed. A torque sensor [4] is used to meas-ure the torque applied by the motor. The load torque in theinner power loop is measured using a strain gauge on the pin-ion shaft. The reading from the strain gauge was used to verifythat each test was loaded to the same specified torque.

For each test performed a new set of gears was used. Thisrequires partial dismounting of the test rig. The motor andtorque sensor were removed in order to change gears in theslave gearbox. The gears in the test and slave gearboxes werechanged by removing the top and side panels of the gearboxes.After the gears were changed the test rig was reassembled.The test rig was disassembled and reassembled in the sameorder every time, because previous work by Andersson et al.(14) showed that the rebuild of the FZG test rig can affect theefficiency measurements. Andersson et al. (14) concluded that

the reproducibility was between 2.42 and 5.04% in the speedrange 0.5 to 20 m/s, where reproducibility is the standarddeviation divided by the mean value. Therefore, any measureddifference in efficiency among the samples in a group needs tobe larger than the natural scatter of the assembly process inorder to be deemed significant.

The gearboxes were filled with a polyalphaolefin lubricant upto the center of the shaft, corresponding to a volume of 1.5L.The polyalphaolefin lubricant had a specified nominal viscosityof 64.1mm2/s (cSt) at 40 �C and 11.8mm2/s (cSt) at 100 �C.

Calculating the gear mesh efficiency

Because the FZG test rig is a circulating power loop, thelosses in the FZG rig are assumed to be equal to the torquesupplied by the motor to maintain a constant velocity. Thelosses in the closed power loop can be classified as eitherload dependent or load independent.

Load-dependent losses are losses that change with theload; that is, bearing losses and losses in the gear mesh.Load-independent losses are losses that occur independentof the applied load, such as oil churning losses and lossesrelated to the bearing seals. The total loss is equal to thesum of the load-dependent and the load-independent losstorque, shown in Eq. [1]:

Ttotal ¼ Tload�dependent � Tload�independent: [1]

To obtain the load-dependent gear mesh losses, the bear-ing losses and the load-independent losses have to be sub-tracted from the total loss. The load-independent losseswere obtained for each tested speed by running the FZG rigwith no applied torque inside the power loop.

Equation [2] was used to calculate the efficiency of onegearbox. The measured torque loss was divided by the prod-uct of the gear ratio (u) and the nominal torque transferredby the pinion (T1); to obtain the efficiency for one gearboxthe ratio is multiplied by 0.5. The value for T1 was given bythe applied load in the inner power loop, and the load wasassumed to remain constant during the experiment.

gtotal ¼ 1� 0:5Ttotal

uT1: [2]

There are many available models for estimating the bear-ing losses. SKF Industries (15) has developed one commonly

Figure 1. Schematic of the FZG back-to-back test rig: 1, test gearbox; 2, load coupling; 3, slave gearbox; 4, torque sensor; 5, motor. Source: The figure is created byEdwin86bergstedt and is not altered. The figure is licensed under the Creative Commons Attribution-Share Alike 4.0 International license, https://creativecommons.org/licenses/by-sa/4.0/deed.en

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used model for the NJ 406 cylindrical roller bearings used inthe FZG rig. In this work, the STA bearing model (16)developed at KTH was used, shown in Eq. [3], where n isthe rotational speed and the parameters A, B, and C aredetermined experimentally and depend on load, tempera-ture, lubricant, and bearing type. The parameters for A, B,and C used in this study are provided in Table 1.

TSTA, 1, 2 ¼ Anþ Bnþ C: [3]

The bearing torque loss are calculated using Eq. [4],where x1,2 is the ingoing angular speed of the pinion andgear shafts:

Tbearing ¼ 4TSTA, 1x1 þ TSTA, 2x2

x2

� �: [4]

By subtracting the bearing torque loss from the load-dependent losses, the gear mesh loss torque is obtained asshown in Eq. [5].

Tmesh ¼ Tload�dependent � Tbearing: [5]

The gear mesh efficiency is calculated using Eq. [6].

gmesh ¼ 1� 0:5Tmesh

uT1: [6]

Test specimens

In this test the gears were produced from two types of mate-rials, a wrought steel material commonly used for gears anda commercial powder metal material. The wrought steelused is 16MnCr5, and the composition of the wrought steeland powder metal steel are provided in Table 2.

The gears from the wrought steel material were generatedin a traditional manner through various machining opera-tions. The powder metal material, on the other hand, wasproduced to near-net-shape by compacting and sinteringmetal powder. All gears were case hardened to a surfacehardness of 800 Hv0.1. The heat during the hardening pro-cess distorts the surface; therefore, to obtain the desiredform and surface roughness a finishing operationwas performed.

For this study, all gears were first ground and later final-ized using a honing process. The geometry of the gears is astandard FZG PT-C gear with the inclusion of a tip relief of20 lm, starting at a diameter of 80.3 and 115.9mm for thepinion and gear, respectively. Complete specification of thegear parameters was published by Sj€oberg et al. (12).

Test plan and procedure

The test plan was designed in accordance with the availablegears. Ideally three sets of gears are tested for each material

and quality class. The quality class of the available gearsposed a limitation; the number of tests per material andquality class is provided in Table 3. There were no wroughtsteel gears available with quality class 8. One test per mater-ial was performed using gears of the worst quality classavailable, denoted in Table 3 as quality class �9. These twotests were made to obtain data for gears with extremelypoor geometrical tolerances.

The efficiency test procedure is the same as used previ-ously by Li et al. (1). The running-in procedure was per-formed by running the gears for four hours at a pitch linevelocity of 0.5 m/s. The pitch line torque in relation to thepinion shaft was set to 94Nm during running-in. This wasdone to be compliant with previous work using running-inloads of either 94 or 302Nm (17).

The oil temperature in the gearboxes was held at 90 �C(þ4 to �1 �C). During running-in, the speed, outside losstorque, and temperature data for the gearboxes wererecorded at a sample rate of 1Hz.

The efficiency test procedure was repeated four timeswith applied pitch line torques of 0, 61, 94, and 183Nm.For each load, the efficiency tests were performed in 5-minsequences, one for each of the eight pitch line velocitiestested: 0.5, 1, 2, 3.2, 8.3, 10, 15, and 20 m/s. Each efficiencytest was repeated three times using new gears in both gear-boxes when possible.

Surface characterization

The tooth profile was measured in situ using a stylus profil-ometer, using a stylus with a tip radius of 2 lm see Fig. 2. Thein situ methodology was developed by Sosa et al. (18). Amounting bracket was bolted to the test gearbox, were two 3-mm guiding pins ensured an accurate positioning. The instru-ment was placed and secured to the bracket using straps. Thebracket featured a positioning system that allowed adjustmentin the width direction of the gear tooth with an accuracy of ±5mm. Hence, the position of the measurements on the geartooth can be determined with good accuracy.

All of the measurements were performed on the sametooth. By using a spirit level, the angular position of thegear could be maintained with an accuracy of ±15min ofarc throughout all measurements. The involute profile wasmeasured initially and after the efficiency measurement. The

Table 1. Constants for A, B, and C in dip lubrication.

61 Nm 94 Nm 183Nm

A 2.19e-05 2.67e-05 2.78e-05B 1.26eþ 00 3.41eþ 00 6.51eþ 00C �5.80e-03 �1.00e-02 �5.40e-03

Table 2. Chemical composition of the wrought steel and powdermetal materials.

Chemical composition (wt%)

Fe Mn Cr Ni C S P Si

16MnCr5 96.95–98.78 1–1.3 1.1 — 0.14–0.19 �0.035 �0.025 0.4Powder metal

steel98.8 0.5 — 0.5 0.2 — — —

Table 3. Number of gears tested and the quality class for the wrought steeland powder metal materials.

Index rowDIN 3962 quality class 6 7 8 �916MnCr5 3 3 0 1Powder metal steel 2 3 2 1

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six involute profiles were measured in the middle of thetooth width using a measurement length of 6mm, and theprofiles were spaced 0.1mm apart.

To obtain the surface roughness from the measured pro-file, the form of the involute was removed by fitting a sixth-degree polynomial to the profile. The remainder is the sur-face topography, which is a combination of waviness, rough-ness, surface lay, and other flaws (19). To separate thesurface roughness from the waviness, a Gaussian filter wasused with a cutoff length of 0.8mm. From the obtained fil-tered surface profile, the Ra and Rz surface parameterswere calculated.

Surface samples from the tooth flanks of all quality classesof the powder metal and wrought steel were studied beforeand after the efficiency test. The analyses were performed witha scanning electron microscope (SEM) equipped with anenergy-dispersive spectrometer. The surface was also analyzedusing a vertical scanning interferometry instrument.

Results

The results from the efficiency measurements are shown inFig. 3. The largest difference in efficiency between the

Figure 2. Overview of the in situ setup for measuring the gear flank.

Figure 3. Gear mesh efficiency for the wrought steel (W) and PM for all speeds at three tested torque levels (61, 94, and 183 Nm).

Figure 4. Gear mesh efficiency and reproducibility for wrought steel (W) andPM for all speeds at the highest torque tested (183 Nm).

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torque levels was 0.18%. Because there was no apparent dif-ference between the tested torque except the magnitude ofthe losses, only the highest torque tested is included in thediscussion. This was done to improve readability and reducethe clutter in the plots.

Figure 4 shows the efficiency at 183Nm and the reprodu-cibility for the measured torque loss, where the

reproducibility is the standard deviation divided by themean efficiency value at each tested speed.

The efficiency measurements for each test for the wroughtand powder metal materials are given in Figs. 5 and 6, respect-ively. These figures show the numerical values for the efficiency.Each cell is colored according to the corresponding value,where higher efficiency values are depicted in lighter color.

Figure 5. Gear mesh efficiency values for each speed and quality class (QC) for the wrought steel (W) with an applied torque of 183 Nm. Each cell is colored accord-ing to the corresponding value, where higher efficiency values are depicted in lighter color.

Figure 6. Gear mesh efficiency values for each speed and quality class (QC) for the PM steel with an applied torque of 183 Nm. Each cell is colored according to thecorresponding value, where higher efficiency values are depicted in lighter color.

Table 4. Average Ra and Rz surface roughness parameters with correspondingstandard deviation and DIN 3962 quality class of the wrought (W) steel surfacebefore and after efficiency testing.

Surface roughness of the wrought steel gears

Initial After efficiency testing

Quality class Ra Ra SD Rz Rz SD Ra Ra SD Rz Rz SD

6 0.17 0.01 1.54 0.09 0.15 0.01 1.28 0.066 0.18 0.01 1.59 0.08 0.15 0.01 1.30 0.046 0.41 0.02 3.43 0.34 0.34 0.02 2.74 0.227 0.52 0.02 4.19 0.21 0.40 0.01 3.02 0.147 0.18 0.01 1.61 0.04 0.17 0.04 1.38 0.207 0.18 0.01 1.57 0.15 0.16 0.01 1.43 0.098 — — — — — — — —8 — — — — — — — —�9 0.18 0.01 1.57 0.10 0.16 0.01 1.35 0.10

Table 5. Average Ra and Rz surface roughness parameters and correspondingstandard deviation and DIN 3962 quality class of the PM steel surface beforeand after efficiency testing.

Surface roughness of the powder metal steel gears

Initial After efficiency testing

Quality class Ra Ra SD Rz Rz SD Ra Ra SD Rz Rz SD

6 0.18 0.01 1.5 0.07 0.15 0.01 1.32 0.126 0.18 0.01 1.71 0.14 0.17 0.01 1.51 0.146 — — — — — — — —7 0.46 0.02 3.87 0.26 0.38 0.02 2.88 0.187 0.19 0.01 1.71 0.15 0.17 0.01 1.50 0.147 0.48 0.02 3.58 0.29 0.39 0.01 3.05 0.188 0.49 0.01 3.89 0.13 0.38 0.01 2.89 0.188 0.44 0.01 3.37 0.18 0.31 0.01 2.66 0.21�9 0.49 0.01 4.20 0.45 0.35 0.01 2.97 0.28

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The initial surface profile was measured six times oneach gear, and the surface roughness was obtained from anaverage of the six measurements. The results are shown inTables 4 and 5. The table contain the average Ra and Rz sur-face parameters, as well as their corresponding standarddeviation and DIN 3962 quality class.

Figure 7 shows SEM images of the surface after the effi-ciency test; the figure shows that there are no apparent dif-ferences in surface structure between quality classes 6 and 7or between the PM and wrought steel. Quality class �9exhibits a rougher surface, with higher asperities and deepervalleys from the honing process. Figure 8 presents theAbbott-Firestone bearing curves for PM with quality classes6 and �9 derived from the vertical scanning interferometrymeasurements. In the figure it can be seen that quality class�9 has a steeper slope than quality class 6, meaning that theload bearing surface area is smaller for quality class �9.

After the efficiency test, no apparent difference in termsof damage was seen on the surfaces of the PM and wroughtsteel or between the different quality classes.

Sliding wear defects in the form of asperities deformed inthe direction of sliding are seen on all surfaces, especiallywhere the slide-to-roll ratio is high; see Fig. 9. Deformedasperities can also be seen at the pitch line where pure

rolling occurs. Another type of sliding wear can be observedin the form of closely packed dents, forming what appearsto be shallow pits (see Fig. 9).

This type of sliding wear is localized and sparsely foundon parts of the surface. Asperities with missing fragmentsare also found on the entire surface for all quality classes;however, they appear more frequent on quality class �9 (seeFig. 7b). Despite the finding of asperities with missing frag-ments, no actual wear particles were observed anywhere onthe surface.

Discussion

The gear mesh efficiency data presented in Fig. 4 show thatthere is no significant difference in mean efficiency betweenthe wrought and powder metal steel gears when includingall quality classes. By examining the efficiency data per qual-ity class in Figs. 5 and 6 one can observe that the differenceis small among the individual tests and no clear trend canbe seen between the quality class and the measured gearmesh efficiency.

From the reproducibility given in Fig. 4, it is clear thatthe wrought steel gears tend to exhibit a more robust

Figure 7. SEM images of representative surfaces after efficiency testing for the best and worst quality classes for both the PM and wrought steel material.

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behavior throughout the experiments than the powder metalgears. It is worth noting that the reproducibility of thewrought steel material is in the same range as the FZG rigassembly error (2.42–5.04%) shown by Andersson et al. (14).

By inspecting the efficiency measurements shown in Figs.5 and 6, there are no apparent indications that the efficiencyis affected by the DIN 3962 quality class. Therefore, theDIN 3962 quality class cannot solely be used to ensure ahigh efficiency in the gears mesh contact. According to the

DIN 3962 classification, the parameter with the largest devi-ation determines the final quality class of the gear. Thus,some of the form parameters might have a large impact onthe gear mesh efficiency and others will have limited influ-ence. Further studies are needed to clarify the importance ofthe different form parameters used in the DIN 3962 stand-ard in regards to the gear mesh efficiency.

Previous studies have investigated the efficiency ofground and superfinished surfaces of quality class 5 for thesame materials used in this study (1, 12, 17). Although thereare large variations in quality class for honed wrought steelgears, the reproducibility is still within the range of theassembly error. Hence, in this test the difference in qualityclass seems to be of less importance to the gear mesh effi-ciency than the surface finishing method.

With the previous studies in mind, one can conclude thathoned wrought steel gears tend to be less efficient thanground and superfinished gears. The honed powder metalgears were less efficient than gears with ground surfaces butroughly equivalent to the superfinished gears, although thecomparison is slightly unfair because the geometrical toler-ances of the ground and superfinished gears were better forquality class 5.

Figure 10 shows the initial surface roughness parameterRa (Tables 4 and 5) plotted against the gear mesh efficiencyfrom Figs. 5 and 6. By inspecting the figure, it is clear thatthe wrought steel gears were smoother than the powdermetal material. Figure 10 also shows that the test samples’

Figure 8. Abbott-Firestone bearing curves for PM with quality classes 6 and �9 measured after the efficiency test.

Figure 9. SEM image of PM with quality class 7; deformed asperities can beseen, as well as a region with closely packed dents forming a shallow pit.

1082 E. BERGSTEDT ET AL.

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surface roughness is divided into two discrete levels, onefine and one slightly courser level. The differences in surfaceroughness cannot be linked directly to the quality class ofthe gears. However, one can observe that gears with a lowRa value are more likely to have higher gear mesh efficiency.

Several studies on both ball-on-disc machines and geartest rigs have shown that a decrease in surface roughnesscan reduce friction losses in a sliding and rolling contact (2,20, 21). A polished surface reduces the asperity peak height,thus limiting the effects of sliding interaction between asper-ities. The surface roughness is included in the specific filmthickness equation according to ISO 6336-22. A decrease insurface roughness increases the specific film thickness. Thisprovides a larger separation between the surfaces, furtherreducing the friction.

The lubrication regime can be estimated using theStribeck curve and film thickness parameter. Anderssonet al. (17) calculated the Hersey number and specific filmthickness using the same experimental setup as used in thisarticle. Because the oil and velocity are the same in bothstudies, the difference lies in the surface roughness and fric-tion losses. The surface roughness of the ground gears testedby Andersson et al. (17) is in between the two discrete levelsof surface roughness for the honed gears. Therefore, alongwith the measured losses, it is assumed that the lubricationregime is in the same vicinity as for the ground gears testedby Andersson et al. (17); that is, mainly the mixed lubrica-tion regime and borderline to elastohydrodynamic lubrica-tion at the highest speeds.

Surfaces of samples with quality class �9 are rougherthan those of the other quality classes. This could possiblybe due to the higher geometrical tolerances that come witha higher quality class. The bearing curves shown in Fig. 8implies that the surface of quality class �9 will distributethe applied load over a smaller area, giving higher surfacepressures at the point of contact. This should in theoryresult in larger initial deformations of the surface of thesamples with quality class �9.

No obvious difference in the amount and type of wearbetween quality classes and material is found on the surfacesafter testing. The type of wear found arises mainly from therelative sliding between the surfaces and appears in thesame way on both the PM and wrought steel materials.

Conclusions

Honed gears made from powder metal and wrought steelmaterials were manufactured. The gears were measured inaccordance with DIN 3962 and awarded a quality class.After efficiency tests in an FZG gear test rig, the followingconclusions were drawn:

� There are no significant differences in efficiency forhoned powder metal and wrought steel gears.

� There was no obvious correlation when comparing thegear mesh efficiency with the DIN 3962 quality class.

Figure 10. Gear mesh efficiency and initial Ra surface roughness for wrought steel (W) and PM at the highest torque and speed tested (183 Nm and 20 m/s).

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� Even with large variation in quality class, the reproduci-bility for the wrought steel gears was shown to be in thesame range as the FZG rig assembly error.

� The honed wrought steel gears tested in this study wereless efficient compared to gears with ground and super-finished surfaces previously tested. The honed powdermetal gears were less efficient than the ground gears butroughly equivalent to the superfinished powdermetal gears.

� No obvious difference in the amount and type of wearbetween quality classes and material is found on the sur-faces after testing. The type of wear found arises mainlyfrom the relative sliding between the surfaces andappears in the same way on both the PM and wroughtsteel materials.

Acknowledgement

Special thanks to Dr. Michael Andersson, H€ogan€as AB, for his guid-ance and knowledge of powder metal materials.

Funding

Financial support from the Swedish Foundation for Strategic Researchthrough the Nanotechnology Enhanced Sintered Steel ProcessingProject (Grant No. GMT14-0045) is acknowledged.

ORCID

Edwin Bergstedt http://orcid.org/0000-0001-9346-7467

References

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(17) Andersson, M., Sosa, M., and Olofsson, U. (2016), “The Effectof Running-In on the Efficiency of Superfinished Gears,”Tribology International, 93, pp 71–77. Available at: http://www.sciencedirect.com/science/article/pii/S0301679X15003527. doi:10.1016/j.triboint.2015.08.010

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(21) Kahraman, A. (2013), “Impact of NiB Coating on theEfficiency, Scuffing, and Wear of Gear Contacts,” ADA583849,Defence Technical Information Center, Virginia.

1084 E. BERGSTEDT ET AL.


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