Ablative brake bushing for axle thermal protection

Details Ablative brake bushing for axle thermal protection Ablative brake bushing for axle thermal protection

F - Mech Eng,Light,Heat,Weapons

16

D

F16D 65/12 (2006.01) F16D 55/36 (2006.01) F16D 65/84 (2006.01) F16D 55/00 (2006.01)

Patent

CA 2090334

2090334 9205369 PCTABS00011 The ablative bushing (40, 140, 240) is disposed between a torque tube pedestal (18) and an axle (30) of an aircraft. The ablative bushing (40, 140) encircles an axle bushing (26) located around the axle (30), so as to be disposed between the torque tube pedestal (18) and axle bushing (26). The ablative bushing (240) may also be located between a torque tube pedestal flange (114) and an axle flange (35). The ablative bushing (40, 140, 240) ablates at a predetermined temperature in order to introduce an air gap between the torque tube pedestal (18) and axle (30) to prevent excessive heat flow to the axle (30) during a rejected take-off stop.

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