FIELD: aircraft engineering.
SUBSTANCE: claimed transmission comprises shafts and rotor drive gearings. The rotor hub with the gearing driven gear and a wobble plate are fitted at the cylinder of the ID making at least the cross-section of the installed injection seat.
EFFECT: safe upward ejection of the crew.
4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HELICOPTER | 2016 |
|
RU2629731C1 |
| HELICOPTER ROTOR | 2015 |
|
RU2616771C2 |
| FLYING VEHICLE | 0 |
|
SU1827363A1 |
| MAIN REDUCTION GEAR OF COAXIAL DRIVE CIRCUIT OF ROTORS OF LIGHT OR ULTRA-LIGHT HELICOPTER | 2023 |
|
RU2824002C1 |
| HELICOPTER DRIVETRAIN | 2013 |
|
RU2559676C2 |
| HELICOPTER TRANSMISSION TAIL GEARBOX | 2005 |
|
RU2280594C1 |
| HIGH-SPEED HELICOPTER | 1992 |
|
RU2005656C1 |
| SYSTEM FOR CONTROLLING GENERAL AND CYCLICAL ANGLES OF MOUNTING OF BLADES OF PROPELLER | 0 |
|
SU1837034A1 |
| MAIN ROTOR OF AERIAL VEHICLE WITH RETRACTABLE BLADES | 2017 |
|
RU2668482C1 |
| ATTACHMENT, DRIVE AND COAXIAL HELICOPTER BLADE CONTROL ASSEMBLY | 2015 |
|
RU2630269C2 |
