FIELD: aviation.
SUBSTANCE: invention relates to the aircraft flight control devices. For example, the device is the helicopter overall pitch control knob device. Device contains the crankcase, the output shaft, which is intended for connection with the flight control knob and mounted rotatably with respect to the crankcase, primary and secondary channels and the clutch. Channels contain the first and second torque generating elements, respectively, adapted to act on the output shaft by means of torque. Clutch is made with the possibility of selectively connecting the primary and secondary channels with the output shaft.
EFFECT: increased reliability when used.
16 cl, 9 dwg
Title | Year | Author | Number |
---|---|---|---|
AUTOMOTIVE MULTIPLE-SPEED GEARBOX | 2012 |
|
RU2508486C1 |
GEAR BOX AND MECHANISED AGRICULTURAL DEVICE | 2011 |
|
RU2561157C2 |
HIGH-PERFORMANCE INDUSTRIAL TRANSMISSION | 2017 |
|
RU2748925C2 |
ROTOR INTERNAL COMBUSTION ENGINE | 1995 |
|
RU2083850C1 |
VEHICLE TRANSMISSION | 0 |
|
SU1342758A1 |
CRANE CAR CHASSIS | 2018 |
|
RU2684838C1 |
GEARBOX | 2010 |
|
RU2556403C2 |
TRANSPORT FACILITY GEARBOX (VERSIONS) | 2011 |
|
RU2472995C1 |
FLOATING VEHICLE TRANSMISSION | 2003 |
|
RU2243109C2 |
AUTOMOTIVE GEARBOX WITH SEVERAL CLUTCHES | 2009 |
|
RU2529113C2 |
Authors
Dates
2019-01-31—Published
2015-09-09—Filed