FIELD: aviation; devices for emergency landing of helicopter. SUBSTANCE: helicopter has casing, rotor and parachute. Rotor is enclosed in latticed box which is secured on helicopter casing below rotor. Parachute is located on upper surface of box and is connected with rocket below center of mass by means of rope. Axis of rocket lies in plane parallel to rotor shaft. EFFECT: enhanced efficiency. 2 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HELICOPTER RESCUE DEVICE | 1997 |
|
RU2121942C1 |
| METHOD OF RESCUE OF HELICOPTER | 1997 |
|
RU2130872C1 |
| DEVICE FOR RESCUE OF HELICOPTER | 1997 |
|
RU2130861C1 |
| DEVICE FOR RECOVERY OF HELICOPTER | 1997 |
|
RU2128602C1 |
| METHOD OF RESCUE OF HELICOPTER | 1997 |
|
RU2130871C1 |
| RESCUE DEVICE FOR HELICOPTER | 1997 |
|
RU2111148C1 |
| METHOD OF RESCUE OF HELICOPTER | 1997 |
|
RU2130873C1 |
| HELICOPTER | 1998 |
|
RU2150410C1 |
| METHOD OF FORMING RUNWAY FOR FLYING VEHICLE | 1997 |
|
RU2130876C1 |
| FLYING VEHICLE RESCUE COMPLEX | 1994 |
|
RU2088481C1 |
