Pneumatic gear motor application

Details Pneumatic gear motor application Pneumatic gear motor application

1976-05-12

1977-10-04

Tudor, Harold

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

222 3, 244 78, 418206, F15C 312, F41G 700

Patent

active

040520242

ABSTRACT:
A pneumatic gear motor application in which a tank filled to a predetermined pressure with an inert gas such as nitrogen is heated by a heat squib device to raise the temperature of the gas and also to increase the pressure of the gas in the storage tank and be supplied through a first frangible valve to a pressure regulator for regulating an outlet pressure to a servo valve for controlling flow to and from a pneumatic motor. The pneumatic motor drives through a reduction gear mechanism that drives a worm and worm gear to actuate a control fin of a missile. The missile has four drive motors and four control fins to provide guidance for the missile.

REFERENCES:
patent: 3154015 (1964-10-01), Muller
patent: 3163014 (1964-12-01), Wismar
patent: 3174435 (1965-03-01), Sisson et al.
patent: 3260271 (1966-07-01), Katz
patent: 3610267 (1971-10-01), Warren
Fundamentals of Rockets, Missiles and Spacecraft, by Hobbs 1963, pp. 88, 9.

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