Two-brake torque limiting device
AssigneeSmiths Aerospace, Inc.
InventorMark R. Serven
Life of this patent
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AssigneeSmiths Aerospace, Inc.
InventorMark R. Serven
Estimating the term…
The apparatus of the invention enables a two-brake torque limiting device to fix the position of one or more flaps and/or slats on an airplane wing when unplanned or abnormal conditions exist. The two-brake torque limiting device may include a trigger brake, a lock down brake, and a speed-increasing device. The trigger brake may use an electromagnetic brake to apply a braking force to the lock down section. The braking force transferred to the lock down section from the trigger section may be transferred through a speed-increasing device. The speed-increasing device allows for the use of a small and a lightweight electromagnetic brake. The invention also provides a method for reducing asymmetry in the wings of an aircraft using an asymmetry detection device, using a trigger brake, using a speed-increasing gear, and using a lock down brake.
A two-brake torque limiting device comprising:
A two-brake torque limiting device comprising:
A method for reducing asymmetry in the wings of an aircraft, the aircraft's wings having a plurality of flaps and slats, a plurality of flap/slat actuators that extend and retract the flaps and slats, a plurality of drive shaft lines that drive the flap/slat actuators, and a two-brake torque limiting device that applies a braking force to the drive shaft lines when one of the following occurs 1) one of the torques on the plurality of flap/slat actuators exceeds a preset value 2) a control signal is received from an asymmetry detection device or 3) a combination of 1 and 2, said method comprising the steps of:
Dependencies are inferred from the claim text.