发明名称 |
METHOD FOR FIXING AN ACTUATOR FOR ROTATABLY DRIVING A WHEEL OF AN AIRCRAFT |
摘要 |
The invention relates to a method for fixing to an aircraft landing gear (1) at least one actuator (30) for rotatably driving a wheel (3) which is rotatably mounted on an axle (2) of the landing gear, the wheel being associated with a brake (5) which comprises an actuator carrier (8) which carries brake actuators, the actuator carrier being fitted onto the axle and stopped in terms of rotation by an obstacle (12) which is fixedly joined to the landing gear and which is introduced into one of the stop holes (11) of the actuator carrier, wherein the drive actuator is fixedly joined to the actuator carrier in the region of a stop hole of the actuator carrier which does not receive the obstacle. |
申请公布号 |
US2016152326(A1) |
申请公布日期 |
2016.06.02 |
申请号 |
US201514945552 |
申请日期 |
2015.11.19 |
申请人 |
MESSIER-BUGATTI-DOWTY |
发明人 |
MARTIN Frederic |
分类号 |
B64C25/40;F16H1/10;B64C25/34 |
主分类号 |
B64C25/40 |
代理机构 |
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代理人 |
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主权项 |
1. Method for fixing to an aircraft landing gear (1) at least one actuator (30) for rotatably driving at least one wheel (3) which is rotatably mounted on an axle (2) of the landing gear, the wheel being associated with a brake (5) which comprises an actuator carrier (8) having a plate (9) which carries brake actuators, and which has two rotation stop holes (11) so that, when the actuator carrier is fitted onto the axle, it is stopped in terms of rotation by an obstacle (12) which is fixedly joined to the landing gear and which is introduced into one of the stop holes (11) of the plate, characterised in that the drive actuator is attached and fixed to the actuator carrier in the region of the stop hole of the plate which does not receive the obstacle. |
地址 |
VELIZY VILLACOUBLAY FR |