FIELD: aviation; rescue of helicopters. SUBSTANCE: proposed facility includes braking mechanism of main rotor shaft, parachute connected with flying vehicle by means of ropes through distributing mechanism and rockets connected with parachute lines. Parachute is located in compartment of upper portion of fuselage under rotor. EFFECT: extended field of application; possibility of rescue of helicopter at low altitudes. 2 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF HELICOPTER RESCUE | 2000 |
|
RU2201383C2 |
| HELICOPTER RESCUE DEVICE | 2000 |
|
RU2201380C2 |
| METHOD OF RESCUE OF HELICOPTER | 2000 |
|
RU2203836C2 |
| DEVICE FOR RESCUE OF AIRCRAFT | 2000 |
|
RU2211174C2 |
| METHOD OF RESCUE OF AIRCRAFT | 2000 |
|
RU2211175C2 |
| AVIATION PASSENGER SELF-CONTAINED RESCUE CAPSULE | 2000 |
|
RU2171210C1 |
| METHOD OF SELF-BRAKING OF AVIATION SELF- CONTAINED PASSENGER RESCUE CAPSULE | 2000 |
|
RU2177440C2 |
| AVIATION PASSENGER SELF-CONTAINED RESCUE CAPSULE | 2000 |
|
RU2171209C1 |
| METHOD OF SELF-BRAKING OF AVIATION SELF-CONTAINED PASSENGER RESCUE CAPSULE | 2000 |
|
RU2177439C2 |
| METHOD OF HELICOPTER RESCUE | 2000 |
|
RU2201381C2 |
