[go: up one dir, main page]

RU2000109471A - REACTIVE AIRCRAFT CONTROL SYSTEM - Google Patents

REACTIVE AIRCRAFT CONTROL SYSTEM

Info

Publication number
RU2000109471A
RU2000109471A RU2000109471/02A RU2000109471A RU2000109471A RU 2000109471 A RU2000109471 A RU 2000109471A RU 2000109471/02 A RU2000109471/02 A RU 2000109471/02A RU 2000109471 A RU2000109471 A RU 2000109471A RU 2000109471 A RU2000109471 A RU 2000109471A
Authority
RU
Russia
Prior art keywords
control system
aircraft control
reactive
reactive aircraft
fuel supply
Prior art date
Application number
RU2000109471/02A
Other languages
Russian (ru)
Inventor
Александр Викторович Ермишин
Владимир Александрович Поршнев
Олег Николаевич Федорец
Original Assignee
Александр Викторович Ермишин
Filing date
Publication date
Application filed by Александр Викторович Ермишин filed Critical Александр Викторович Ермишин
Publication of RU2000109471A publication Critical patent/RU2000109471A/en

Links

Claims (1)

Реактивная система управления летательными аппаратами, состоящая из системы топливоподачи, системы управления и системы исполнительных устройств, отличающаяся тем, что система исполнительных устройств представляет собой совокупность детонационных камер, сообщенных единой системой управления с системой топливоподачи и с инициаторами через блок клапанов и регуляторов.A reactive aircraft control system, consisting of a fuel supply system, a control system and an actuation system, characterized in that the actuation system is a set of detonation chambers communicated by a single control system with a fuel supply system and initiators through a block of valves and regulators.
RU2000109471/02A 2000-04-17 REACTIVE AIRCRAFT CONTROL SYSTEM RU2000109471A (en)

Publications (1)

Publication Number Publication Date
RU2000109471A true RU2000109471A (en) 2001-12-27

Family

ID=

Similar Documents

Publication Publication Date Title
WO2004015357A3 (en) Gas operating system for firearm simulators
EP1090817A4 (en) Gas generator
JPS6412906A (en) Shock absorber
DE58901046D1 (en) AIR COMPRESSING, VALVE CONTROLLED INTERNAL COMBUSTION ENGINE.
AUPR919301A0 (en) Improvements to a valve controlled divided chamber I.C. engine
WO2002033343A3 (en) New generation non-lethal and lethal projectiles for arms
EP1336757A3 (en) Control device for variable displacement type compressor
WO2003074858A3 (en) Ramjet engine combustion chamber and ramjet engine equipped with same
AU2329701A (en) Engine idle speed control
EP1433961A3 (en) Solenoid valve for reduced energy consumption
DE69021760D1 (en) Fuel pressure control valve.
RU2000109471A (en) REACTIVE AIRCRAFT CONTROL SYSTEM
JPS548266A (en) Brake fluidic pressure control system
KR950701592A (en) DEVICE FOR RENDERING A STORAGE CONTAINER INERT]
JPS5364121A (en) Control valves for exhaust reflux devices
JPS6440770A (en) Valve base with integral flow controller
DE69408158D1 (en) CHARGED INTERNAL COMBUSTION ENGINE WITH INLET PRESSURE CONTROL
DE69605579D1 (en) Projectile control with a multi-chamber, single jet engine
RU2003109907A (en) FUEL SUPPLY CONTROL SYSTEM FOR GAS-TURBINE ENGINE
DE69200532D1 (en) Two-stroke engine with selective control for the charge introduced into the combustion chamber.
DE69201194D1 (en) Gas flow control valve.
ES8603215A1 (en) Internal combustion engine.
RU2002107688A (en) Gas flow control device
WO2001050007A3 (en) Control valve comprising an actuator guided by a tappet, for an injector in a fuel injection system
JPS5614603A (en) Control circuit for actuator