Balance load actuator

Aeronautics and astronautics – Aircraft structure – Details

Reexamination Certificate

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Details

C292S127000, C292S169110, C049S356000

Reexamination Certificate

active

06837461

ABSTRACT:
The present invention provides a balance load actuator for effecting motion between a first part and a second part. An embodiment of the present invention comprises a main housing; a shaft; a motion transfer assembly; and a load balancing assembly. The balance load actuator receives substantial external loads through a load balance assembly and distributes the loads to the main housing, thus relieving undue stress otherwise exerted on the shaft and enabling lighter and smaller design components and construct.

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