Patent ID: 6227247
Filing Date: 2001-05-08
Classification: F02K,F15C,F42B,Y10T

Abstract:
A thruster valve comprising:a housing having a sleeve disposed therein, said sleeve open at a first end;a thrust nozzle for producing thrust, the inlet of said nozzle in opposed relation to and spaced from said first end;a piston, extending from a head to a back, mounted in said sleeve and continuously moveable from a closed position where the head of said piston abuts said nozzle inlet to an open position where said head is spaced from said nozzle inlet;a front annulus surrounding the head of said piston for receiving a hot gas, said front annulus in fluid communication with said nozzle;a back chamber bounded by the back face of said piston and said housing;at least one intermediate annulus surrounding said piston and disposed between said front annulus and said back chamber,a plurality of passages for flowing the hot gas from said front annulus to said intermediate annulus and to said back chamber;a flapper chamber disposed in said housing, said flapper chamber having first and second nozzles in opposed relation, said first nozzle in fluid communication with said back chamber and said second nozzle is in fluid communication with said intermediate annulus;a flapper disposed in said flapper chamber and positionable from a first position closing said first nozzle to a second position closing said second nozzle;a first metering slot in fluid communication with said back chamber and a second metering slot in fluid communication with said intermediate annulus, said first metering slot and said first nozzle configured so that in the steady state condition the sum of their flow areas is a constant and said second metering slot and said second nozzle configured so that in the steady state condition the sum of their flow areas is a constant; andmeans for positioning said flapper.