GAS-DISTRIBUTING DEVICE Russian patent published in 2007 - IPC F16K11/02 F02K9/80 F16K31/42 

Abstract RU 2311579 C1

FIELD: flight vehicle control system, in particular, gas-jet systems, designed for control of rockets and jet projectiles.

SUBSTANCE: the gas-distributing system has an electromagnet, gas power amplifier, type "nozzle-shutter", with inlet and outlet throttle valves, and a power cylinder with a piston a cylindrical hole is made in the piston. This hole passes through the center of the piston perpendicularly to the longitudinal axis. A spherical stem of the rotary valve is positioned in the mentioned hole. The working surfaces of the rotary valve are made cylindrical, and their axes are inclined at an angle to the longitudinal axis of the valve. The inlet and outlet throttle valves of the power amplifier have different diameters. The ratio of the inlet throttle valve diameter to the outlet throttle valve diameter is at least 0.727.

EFFECT: provided maximum power of the gas-distributing device due to selection of rational designed parameters.

1 dwg

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Authors

Osin Viktor Konstantinovich

Kalganov Vladimir Ivanovich

Bataev Aleksandr Andreevich

Kirillov Leonid Konstantinovich

Makarovets Nikolaj Aleksandrovich

Denezhkin Gennadij Alekseevich

Semilet Viktor Vasil'Evich

Tregubov Viktor Ivanovich

Koroleva Natal'Ja Borisovna

Sudorgin Valerij Fedorovich

Borisov Oleg Grigor'Evich

Dates

2007-11-27Published

2006-09-14Filed