Electromechanical actuator assembly with mechanical override feature
AssigneeB/E Aerospace, Inc.
InventorsPradeep Acharya, Stephen H. Davies, Sreekanth Rao
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AssigneeB/E Aerospace, Inc.
InventorsPradeep Acharya, Stephen H. Davies, Sreekanth Rao
Estimating the term…
An electromechanical actuator assembly (EMA) for driving one or more adjustable seat components includes a rotationally constrained ring gear and an override mechanism for use during a power failure condition to allow the ring gear to rotate to manually return the one or more adjustable components to a taxi, takeoff and landing (TTOL) compliant position. In embodiments, the override mechanism includes an internally splined pinion gear, an internally splined anti-rotation bushing, and an externally splined release pin. During a powered condition of the EMA, the externally splined release pin is engaged with the internally splined pinion gear to rotationally constrain the pinion gear and ring gear meshed with the pinion gear. During a power failure condition, the externally splined release pin can be disengaged from the pinion gear to allow the pinion gear and ring gear to be rotated.
An electromechanical actuator assembly (EMA), comprising:
A passenger seat assembly, comprising:
A mechanism for controlling ring gear rotation, comprising:
Dependencies are inferred from the claim text.