Thrust reverser actuation
AssigneeGoodrich Actuation Systems Limited
InventorsMichael Paul Somerfield, Benjamin Thomas Tucker
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Abstract
A thrust reverser drive arrangement is described for use in driving a thrust reverser cowl for movement relative to first and second guide tracks, the drive arrangement comprising a first actuator located, in use, close to the first guide track, and a second actuator located, in use, close to the second guide track, the actuators being arranged to be driven in synchronism and at the same speed by a drive motor to drive the cowl for movement, wherein at least one of the first and second actuators is provided with a load limiter to limit the transmission of loads through that actuator in the event that that actuator is subject to a compressive loading greater than a predetermined level.
Claims4
A thrust reverser drive arrangement for use in driving a thrust reverser cowl for movement relative to first and second guide tracks, the drive arrangement comprising:
- a first actuator located, in use, close to the first guide track;
- and
- a second actuator located, in use, close to the second guide track,
- the first actuator and the second actuator being arranged to be driven axially in synchronism and at the same speed by a drive motor to drive the thrust reverser cowl for movement,
- wherein at least one of the first and second actuators is provided with a load limiter in a housing of the first actuator or the second actuator, the load limiter interposed between the housing and a rotary actuator member of that actuator at a location radially outward of an axially actuatable output member of that actuator in at least one position of that actuator, and operable to apply a braking load to limit the transmission of loads through that actuator in the event that that actuator is subject to a compressive loading greater than a predetermined level,
- the load limiter being operable to apply a braking load to that actuator to resist rotation thereof, thereby reacting applied torque to the housing of that actuator rather than increasing the axial compression of the output member.
Dependencies are inferred from the claim text.