FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular, to designs of helicopter control systems. The control system of a coaxial helicopter consists of a combined control unit and transverse control, longitudinal control, general pitch control and directional control channels connected therewith. Each control channel comprises a control body, a trimming mechanism and a kinematic mechanism. Moreover, the control channels are placed under the cabin floor and connected with the combined control unit by means of flexible rods secured on the central glazing beam rigidly connected to the frame of the helicopter cabin.
EFFECT: compactness of the elements of the control system, vacation of a useful volume under the cabin floor are ensured.
7 cl, 8 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HELICOPTER LANDING GEAR WHEEL BRAKING SYSTEM | 2023 |
|
RU2796557C1 |
| MECHANICAL SYSTEM OF HELICOPTER ROTORS BRAKING SYSTEM | 2019 |
|
RU2729870C1 |
| HELICOPTER CABIN WITH TRAUMA-RESISTANT CONTROLS | 2004 |
|
RU2265556C1 |
| HELICOPTER | 2004 |
|
RU2263607C1 |
| HELICOPTER CONTROL SYSTEM | 2023 |
|
RU2819837C1 |
| COAXIAL BEARING SYSTEM | 2019 |
|
RU2726560C1 |
| HELICOPTER WITH COAXIAL MAIN ROTORS | 2004 |
|
RU2265554C1 |
| SUMMING MECHANISM FOR CONTROL SYSTEMS OF COMMON AND CYCLIC PITCH OF HELICOPTERS OF THREE-POINT CONTROL SYSTEM WITH INCLINED ARRANGEMENT OF HYDRAULIC ACTUATORS | 2014 |
|
RU2578706C1 |
| MULTI-PURPOSE HELICOPTER AND HELICOPTER FUEL SYSTEM | 2020 |
|
RU2752810C1 |
| HELICOPTER SWASHPLATE | 2019 |
|
RU2728945C1 |
