A shock absorber assembly is configured to be operatively connected to a drive shaft of a power drive unit (PDU) of an aircraft. The shock absorber assembly may include a first hub, a second hub, and a bull gear having at least a portion sandwiched between the first and second hubs. The bull gear is configured to rotate independently of the first and second hubs a controlled distance in response to a mechanical malfunction of the PDU.
SHOCK ABSORBER ASSEMBLY FOR POWER DRIVE UNIT OF A VEHICLE
2016-08-25
Patent
Electronic Resource
English
SHOCK ABSORBER ASSEMBLY FOR POWER DRIVE UNIT OF A VEHICLE
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