Review Article

Computer Simulation/Prediction of Wear in Mechanical Components

Table 3

References for the various wear simulation and prediction procedures (wear models, contact analyses, and geometry update).

ApplicationsReferenceWear modelContact analysisGeometry updateComment
ArchardPartial-EHL contacts wear modelOtherFEMEFMBEMOther

Cam-follower[8]xxxContact forces are determined analytically and the contact location is determined numerically using an iterative search.
[9]xxxContact pressure is determined numerically by discretizing the surface and determining the pressure in the individual surface.
[10]xxxPressure contact analysis base on infinite half plane assumption. Wear conducted in for three cases: 1) wear on cam alone, 2) wear on follower alone and 3) wear on both cam and follower
[103]xxxFinite element analysis (FEA) conducted to determine contact pressure, whereas the sliding distances are determined analytically based on Hertz theory.
Gear wear[12]xxSpur gear
[13]xxx
[14]xxx
[17]xxx
[104]xxxx
[105]xxx
[106]xxxImplicit treatment of wear by substituting Archard’s wear law into the contact law (Signoroni’s contact law) wherein wear is built into any particular load step being considered
[15]xxxHelical gear
[16]xxx
[18]xxx
[19]xxx
[25]xxx
[20]xxx
[107]xxSpur and helical gears.
[108]xxxHypoid gears.
Bearings wear[33]xxx
Cylinder/piston/piston ring wear[60]xxxxTwo wear models are used to cover the different load-bearing conditions (presence of lubrication).
[109]xxAnalytical method employed to estimate bore wear pattern for a piston engine. Hydrodynamic lubrication theory between the piston ring and the cylinder is considered.
[110]xxSimulation results from the first part of this study [109] are compared with the actual worn cylinder bores.
[111]x
Other components and general geometries[97]xxxCylinder on flat and sphere on flat configuration are considered for wear prediction.
[98]xxxxThe geometry considered is of conical spinning contact.
[99]xxxSeveral geometries are considered including (1) sphere on plane contact, (2) cone on cone conforming contact, (3) cone on cone nonconforming contact, and (4) cone on torus contact. The pin-on-disk tribology experiment was also simulated.
[100]xxxWear simulation implemented using parallel computation to speed up the analysis.
[101]xxxWear analysis of a revolute joint (of a slider crank mechanism) conducted within a multibody dynamics frame work coupling wear and system dynamics.
[93]xxxA wear simulation procedure–based BEM is used to predict wear on pin-on-disk configuration. Wear is considered for the case when (1) only pin is wearing and (2) when both the pin and the disk are modeled to wear.
[102]xxxxComparison between the FEM and EFM procedure in wear analysis of a revolute joint of a planar mechanism.
[112]xxA time-varying wear coefficient to represent three lubrication conditions including dry contact, boundary lubrication, and full-film lubrication.
[113]xxxWear analysis on metallic bodies in oscillatory contacts.
[114]xxxA closed form expression for wear on a simple scotch yoke mechanism is derived.
[115]xxxWear simulation is conducted on a cylindrical steel roller that is configured to oscillate against a steel plate.
[116]xxxxWear or planar multibody systems.
[117]xxx3D wear analysis in rolling contact problems.
[118]xxx3D fretting wear analysis.
[119]xxxA wear test procedure (ring-on-disc wear configuration) is simulated using a BEM formulation.
[112]xxxTime-varying wear coefficient to cater for effects on lubrication. Remeshing at contact element and the proximity of elements.
[120]xxxBall on disk tribometer experiment is simulated and compared to actual experiments.
[121]xxxGeometry update based on moving the nodal wear. Wear analysis on 2D cylinder on flat and 3D spherical contact.
[122]xxxWear analysis on radial sliding laminated polymeric composite bearings contacting with rotary shaft.
[123]xxxWear analysis of (thermal and mechanical) spherical plain bearing. Remesh model after every cycle to reflect wear.
[124]xxxWear estimates on a slider crank mechanism.
[125]xxxRemesh model after every cycle to reflect wear.
[126]xxxRemesh model after wear cycle to reflect wear.
[127]xxxGeometry update involves repositioning of node and remeshing.
[128]xxxFEM-based procedure for fretting wear analysis of aero-engine spline coupling.
[129]xxxWear model is a modification of Rhee’s wear formula.
[130]xxxContact analysis involved geometry discretization and contact properties estimated for the discretized sections.