SAE Technical Paper Series 2015
DOI: 10.4271/2015-01-0676
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Finite Element Analysis of Transient Thermoelastic Behavior in Multi-Disc Clutches

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Cited by 9 publications
(7 citation statements)
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“…However, once the clutch plates have cooled to ambient temperature, the wear that occurred at the previous contact point results in a surface recess; contact is thus established elsewhere during the next engagement which forces the change in EFR. Zhao et al [22] and Abdullah et al [23,24] predicted a single contact pressure/temperature peak despite no wear being included in their models whereas the TCFEA only predicted a single peak when wear was included. This difference may be the result of the TCFEA simulating only a single clutch-plate pair, and hence a single friction interface, whereas Zhao et al [22] and Abdullah et al [23,24] simulated the full multi-plate aircraft clutch.…”
Section: Discussionmentioning
confidence: 99%
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“…However, once the clutch plates have cooled to ambient temperature, the wear that occurred at the previous contact point results in a surface recess; contact is thus established elsewhere during the next engagement which forces the change in EFR. Zhao et al [22] and Abdullah et al [23,24] predicted a single contact pressure/temperature peak despite no wear being included in their models whereas the TCFEA only predicted a single peak when wear was included. This difference may be the result of the TCFEA simulating only a single clutch-plate pair, and hence a single friction interface, whereas Zhao et al [22] and Abdullah et al [23,24] simulated the full multi-plate aircraft clutch.…”
Section: Discussionmentioning
confidence: 99%
“…Zhao et al [22] and Abdullah et al [23,24] predicted a single contact pressure/temperature peak despite no wear being included in their models whereas the TCFEA only predicted a single peak when wear was included. This difference may be the result of the TCFEA simulating only a single clutch-plate pair, and hence a single friction interface, whereas Zhao et al [22] and Abdullah et al [23,24] simulated the full multi-plate aircraft clutch. The aggregate effect of TEI on all the friction surfaces may have resulted in a single contact area and hot band being predicted in their simulations even in the absence of any wear.…”
Section: Discussionmentioning
confidence: 99%
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