Position control of jet pipe in missile attitude control system

Details Position control of jet pipe in missile attitude control system Position control of jet pipe in missile attitude control system

1975-04-17

1976-12-28

Croyle, Carlton R.

Power plants

Reaction motor

With thrust direction modifying means

23926519, 137 83, F02K 100

Patent

active

039993817

ABSTRACT:
A pure fluid interface device for proportional linear control of high temature, high pressure, hot gas flow from the exhaust of a rocket motor. The interface device receives the hot gas by direct bleeding from the rocket exhaust system and directs the gas to the control system of a missile airframe.
The proportional linear control of the interface is achieved through a pair of positive displacement pistons which engage a jet pipe, charged with the hot gas, for pivotal movement of the jet pipe for alignment of the orifice of the jet pipe with one or both exit ports in the body of the interface device to direct the hot gas through the desired exit port.

REFERENCES:
patent: 2341644 (1944-02-01), Moller et al.
patent: 2392300 (1946-01-01), Ziebolz et al.
patent: 3239150 (1966-04-01), Chisel
patent: 3285262 (1966-11-01), Ernst et al.
patent: 3606902 (1971-09-01), Shinn et al.

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