1998
DOI: 10.1080/10402009808983758
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A Method of Influence Functions for Thermal Analyses of Tribological Elements

Abstract: Miami, Florida 33199Calculations for temperature and thermal defwmation in jinite tribological systems usually require finite-element (FEM) procedures. Because these calculations may be intermediate steps in iterations Jor film thicknesses and pressure distributions, combining FEM procedures into the iteration process may be considerably costly w even impractical. This paper reports the development of two influence functions for calculating the steady-state temperature and the consequent thennal dejmation for … Show more

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Cited by 11 publications
(4 citation statements)
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References 13 publications
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“…To assess the asperity contact pressure occurring at the bearing-bush interface, the elastic-plastic contact model developed by Kogut and Etsion (2003) is used in this study. In addition, the elastic deformation driven by the hydrodynamic and contact pressure is calculated with influence function method established by Shi and Wang (1998). Actually, in the authors' previous study (Xiang et al, 2019a(Xiang et al, , 2019b(Xiang et al, , 2019c(Xiang et al, , 2019d, the influence function method has successfully been used to calculate the elastic deformation of oil-lubricated coupled bearing.…”
Section: Thrust Bearingmentioning
confidence: 99%
“…To assess the asperity contact pressure occurring at the bearing-bush interface, the elastic-plastic contact model developed by Kogut and Etsion (2003) is used in this study. In addition, the elastic deformation driven by the hydrodynamic and contact pressure is calculated with influence function method established by Shi and Wang (1998). Actually, in the authors' previous study (Xiang et al, 2019a(Xiang et al, , 2019b(Xiang et al, , 2019c(Xiang et al, , 2019d, the influence function method has successfully been used to calculate the elastic deformation of oil-lubricated coupled bearing.…”
Section: Thrust Bearingmentioning
confidence: 99%
“…The film thickness of the thrust bearing was described by: where h g is the geometry clearance of the thrust bearing [shown in Figure 1(c)], with h g = h p + h g = h p + α t r sin(β − θ) , where h p is the geometry film thickness, α t and β are the inclined angle and pad angle of the thrust pad, respectively [as shown in Figure 1(c)]; h groove and δ ET are the groove depth and elastic deformation of the thrust bearing, respectively; The influence coefficient method presented by Shi and Wang (1998) was applied to calculate the elastic deformation of the coupled bearing. It is noteworthy that the same mesh was applied to calculate the Reynolds equation and the elastic deformation in the presented study.…”
Section: Mathematical Modelmentioning
confidence: 99%
“…The product a J DT J r J is the clearance change while 1 þ e cosðy J À jÞ is the adjustment at a different circumferential location when e is given. The bearing thermal deformation, journal and bearing elastic deformations are calculated using the influence-function methods described by Shi and Wang [17,18]. It should be pointed out that, in the case of a deformable cantilever shaft, the shaft deflection might also modify the film thickness because the shaft deflection may be of the same order of magnitude as the bearing surface deformation.…”
Section: Thermoelastic Deformation Submodelmentioning
confidence: 99%