FIELD: aeronautical engineering. SUBSTANCE: change of chord length L and shift 
of aerodynamic center are of such amount that leading edge 5 and trailing edge 6 of blade 1 have no break in longitudinal direction; common aerodynamic center is located in pitch change axis. EFFECT: enhanced efficiency. 12 cl, 10 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| BLADE WITH SWEPT TIP FOR ROTATING LIFTING SURFACE OF FLYING VEHICLE | 1997 |
|
RU2139811C1 |
| DEVICE FOR DAMPENING TORQUE OF HELICOPTER | 1995 |
|
RU2138422C1 |
| HELICOPTER WITH ONE MAIN ROTOR AND METHOD OF COMPENSATION OF CONTRA-ROTATING TORQUE OF MAIN ROTOR OF SINGLE-ROTOR HELICOPTER | 1993 |
|
RU2086476C1 |
| HELICOPTER TAIL ROTOR BLADE IN FAIRING MADE FROM THERMOPLASTIC COMPOSITE MATERIAL (VERSIONS) AND METHOD OF ITS MANUFACTURE | 1993 |
|
RU2111894C1 |
| DEVICE FOR COMPENSATION OF REACTION TORQUE OF MAIN ROTOR OF ROTARY-WING FLYING VEHICLE | 1995 |
|
RU2099247C1 |
| DEVICE FOR SECURING BLADE TO ROTOR HUB WITH MULTI-LAYER FASTENING PART, ROTOR BLADE PROVIDED WITH SUCH PART AND ROTOR WITH SUCH BLADES | 1993 |
|
RU2114762C1 |
| ROTARY-WINGED AIRCRAFT PROPELLER BLADE | 2015 |
|
RU2603710C1 |
| BLADE MADE FROM THERMOPLASTIC COMPOSITE MATERIAL FOR HELICOPTER TAIL ROTOR AND METHOD OF MANUFACTURE OF SUCH BLADE | 1993 |
|
RU2113379C1 |
| METHOD OF HANDLING FLYING VEHICLE AT LOW-ALTITUDE FLIGHT AND SYSTEM FOR REALIZATION OF THIS METHOD | 1994 |
|
RU2095280C1 |
| PROPELLER BLADE AND AEROFOIL PROFILE OF BLADE (VERSIONS) | 1996 |
|
RU2145293C1 |
