FIELD: aviation; life-saving appliances and rescue equipment in manufacture of promising helicopters. SUBSTANCE: helicopter is provided with parachute system located in compartment of upper part of fuselage under rotor, devices for separation of main rotor from fuselage which are located in fuselage near base of external part of main rotor shaft. For rescue of helicopter, main rotor is separated from fuselage and parachute is deployed, after which landing is performed. EFFECT: extended field of application; enhanced safety of passengers. 3 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF RESCUE OF HELICOPTER | 2000 |
|
RU2203836C2 |
HELICOPTER RESCUE DEVICE | 2000 |
|
RU2201380C2 |
HELICOPTER | 2000 |
|
RU2213026C2 |
HELICOPTER | 2000 |
|
RU2213027C2 |
METHOD OF EMERGENCY EVACUATION FROM HELICOPTER | 2000 |
|
RU2207301C2 |
METHOD OF HELICOPTER RESCUE | 2000 |
|
RU2201383C2 |
METHOD OF EMERGENCY EVACUATION OF PASSENGERS FROM AIRCRAFT | 2000 |
|
RU2177441C2 |
METHOD OF EMERGENCY EVACUATION OF PASSENGERS FROM AIRCRAFT | 2000 |
|
RU2171206C1 |
AIRCRAFT | 2000 |
|
RU2176209C1 |
HELICOPTER RESCUE FACILITY | 2000 |
|
RU2207302C2 |
Authors
Dates
2003-03-27—Published
2000-08-08—Filed