FIELD: aircraft rescue equipment. SUBSTANCE: upper portion of aircraft fuselage has compartment where parachute is located. Rockets 5 are located in guide barrels under said compartment. Lines 6 are secured to rockets 5. For rescue of aircraft, parachute is deployed; parachute is connected with rope 7 by means of lines 8; lines 6 are connected with rope 7. Lines 6 are brought through distributing mechanism into guide barrels and are secured to rockets 5. EFFECT: extended field of application; enhanced efficiency. 2 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF RESCUE OF AIRCRAFT | 2000 |
|
RU2211175C2 |
| AVIATION PASSENGER SELF-CONTAINED RESCUE CAPSULE | 2000 |
|
RU2171210C1 |
| HELICOPTER RESCUE FACILITY | 2000 |
|
RU2207302C2 |
| METHOD OF HELICOPTER RESCUE | 2000 |
|
RU2201383C2 |
| HELICOPTER RESCUE DEVICE | 2000 |
|
RU2201380C2 |
| METHOD OF SELF-BRAKING OF AVIATION SELF- CONTAINED PASSENGER RESCUE CAPSULE | 2000 |
|
RU2177440C2 |
| METHOD OF RESCUE OF HELICOPTER | 2000 |
|
RU2203836C2 |
| 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 |
