Thrust vector control actuator

Details Thrust vector control actuator Thrust vector control actuator

1983-07-29

1985-10-29

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

With means controlling amount, shape or direction of...

60232, F02K 984

Patent

active

045496951

ABSTRACT:
A system is disclosed for moving a load from an equilibrium position to which it is urged by extraneous forces, with reduced power required of the motive system. In the system, a load is engaged by means storing potential energy when the load is in its equilibrium position and returning the potential energy to the load as it is moved from the equilibrium position. Such a nozzle-actuating system includes generally a frame, an electric motor drive, and a member, driven by the electric motor drive, that is movably carried by the frame and connected with the rocket nozzle. The frame and driven member can include a cam and spring arrangement to provide a force counteracting the force imposed on the driven member by the rocket nozzle when it is displaced from its normal position by the electric motor drive.

REFERENCES:
patent: 3401887 (1968-09-01), Sheppard
patent: 3436021 (1969-04-01), Walton et al.
patent: 3659788 (1972-05-01), Oldfield et al.

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