FIELD: flying vehicles, type helicopter. SUBSTANCE: boss has upper plate and lower plate 4 which are interconnected by means of external fittings 14 and spherical laminated stops 8 in such manner that plates are located at definite distance relative to each other forming free space between them where spherical stops 8 are positioned. Located in peripheral portion of these plates are external fittings 14 through which fastenings 5 interconnecting these plates and spherical stops pass. EFFECT: simplified construction and reduced mass. 14 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
PROPELLER BLADE; BLADE FOR HELICOPTER TAIL ROTOR IN PARTICULAR | 1999 |
|
RU2190559C2 |
MAIN ROTOR HUB OF ROTARY-WING FLYING VEHICLE | 1991 |
|
RU2087379C1 |
MAIN ROTOR | 2005 |
|
RU2296697C1 |
MAIN ROTOR | 2005 |
|
RU2281885C1 |
CONTROLLABLE MAIN ROTOR | 1990 |
|
SU1826421A1 |
BUSH OF HELICOPTER LIFTING ROTOR | 2008 |
|
RU2360834C1 |
HELICOPTER MAIN ROTOR | 2004 |
|
RU2267447C1 |
HELICOPTER MAIN ROTOR | 2005 |
|
RU2289530C1 |
FLYING VEHICLE PROPELLER ENCASED IN COWL AND ROTORCRAFT | 2014 |
|
RU2570971C2 |
HELICOPTER MAIN ROTOR HUB | 1997 |
|
RU2119876C1 |
Authors
Dates
2001-01-20—Published
1998-03-04—Filed