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 | 
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 | RU2296697C1 | 
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 | 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