FIELD: aeronautical engineering; means of escape. SUBSTANCE: system includes ejection seat with powder engine and control device. Engine is provided with explosive charge electrically connected with control device and actuating cylinder mounted along longitudinal axis of engine nozzle. Profiled rod secured in actuating cylinder is directed to cavity of throat section of engine nozzle. Explosive charge operates at g-loads and speed of aircraft exceeding critical magnitudes. EFFECT: enhanced reliability. 4 dwg
Title | Year | Author | Number |
---|---|---|---|
EJECTION SEAT | 1990 |
|
RU2101217C1 |
FLYING VEHICLE EJECTION SEAT | 1993 |
|
RU2088484C1 |
TRAINING APPARATUS | 1992 |
|
RU2037209C1 |
EJECTION SEAT CARTRIDGE FOR MANNED FLYING VEHICLE | 2002 |
|
RU2230211C1 |
EJECTION SEAT | 1997 |
|
RU2119878C1 |
METHOD OF STARTING AFTERBURNER CHAMBER OF GAS-TURBINE ENGINE | 1991 |
|
RU2027887C1 |
EJECTION SEAT | 2003 |
|
RU2238222C1 |
MANEUVERABLE HIGH-ALTITUDE AIRPLANE WITH ONBOARD OXYGEN GENERATION SYSTEM AND OXYGEN UNITS OF EJECTION CREW SEATS | 2006 |
|
RU2328415C2 |
AIRCRAFT CANOPY EMERGENCY OPENING CONTROL SYSTEM | 2022 |
|
RU2783689C1 |
EJECTION UNIT FOR EMERGENCY RESCUE OF PILOT | 2002 |
|
RU2232698C1 |
Authors
Dates
1997-11-10—Published
1993-03-17—Filed