FIELD: aviation; lifesaving appliances; rescue facilities; manufacture of promising helicopters. SUBSTANCE: helicopter is provided with units for separation of main rotor from fuselage , parachute system located in upper portion of helicopter fuselage under propeller, parachute connected with flying vehicle by means of ropes through distributing mechanism and rockets connected with parachute lines. For rescue of helicopter, main rotor is separated from fuselage, parachute is deployed and landing of helicopter is performed. EFFECT: extended field of application. 3 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF HELICOPTER RESCUE | 2000 |
|
RU2201383C2 |
| HELICOPTER RESCUE DEVICE | 2000 |
|
RU2201380C2 |
| HELICOPTER RESCUE FACILITY | 2000 |
|
RU2207302C2 |
| METHOD OF HELICOPTER RESCUE | 2000 |
|
RU2201381C2 |
| AVIATION PASSENGER SELF-CONTAINED RESCUE CAPSULE | 2000 |
|
RU2171210C1 |
| AVIATION PASSENGER SELF-CONTAINED RESCUE CAPSULE | 2000 |
|
RU2171209C1 |
| DEVICE FOR RESCUE OF AIRCRAFT | 2000 |
|
RU2211174C2 |
| METHOD OF RESCUE OF AIRCRAFT | 2000 |
|
RU2211175C2 |
| METHOD OF SELF-BRAKING OF AVIATION SELF- CONTAINED PASSENGER RESCUE CAPSULE | 2000 |
|
RU2177440C2 |
| METHOD OF RESCUE OF HELICOPTER | 2000 |
|
RU2203837C2 |
