FIELD: aviation; rescue of passengers and flying vehicles; manufacture of promising helicopters at high safety of passengers. SUBSTANCE: proposed device has unit for separation of main rotor shaft from fuselage of helicopter, parachute located in compartment in upper part of fuselage under rotor and secured to helicopter by means of ropes through distributing mechanism; proposed device includes also rockets connected with parachute lines. Proposed device ensures rescue of helicopter at low altitudes at momentary increase of breaking force. EFFECT: possibility of rescue of helicopter at low altitudes. 4 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF RESCUE OF HELICOPTER | 2000 |
|
RU2203836C2 |
METHOD OF HELICOPTER RESCUE | 2000 |
|
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HELICOPTER RESCUE FACILITY | 2000 |
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METHOD OF RESCUE OF AIRCRAFT | 2000 |
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RU2201381C2 |
AVIATION PASSENGER SELF-CONTAINED RESCUE CAPSULE | 2000 |
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AVIATION PASSENGER SELF-CONTAINED RESCUE CAPSULE | 2000 |
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RU2171209C1 |
METHOD OF SELF-BRAKING OF AVIATION SELF- CONTAINED PASSENGER RESCUE CAPSULE | 2000 |
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RU2177440C2 |
METHOD OF SELF-BRAKING OF AVIATION SELF-CONTAINED PASSENGER RESCUE CAPSULE | 2000 |
|
RU2177439C2 |
Authors
Dates
2003-03-27—Published
2000-08-08—Filed