FIELD: aviation.
SUBSTANCE: flight control device for aerial vehicle includes lever (8) connected to the casing (1), supporting frame (4) connected to the casing by first rotating connections around the first axis (X). The lever is connected to the frame by means of a pivot connection around the second axis (Y). The device also includes the first transmission shaft (12) and the first connection with the control lever mechanism first gear shaft, the second transmission shaft (23) and the second control lever connection mechanism with the second shaft. The first shaft and the first mechanism of connection are connected to each other by means of the pivot link around the fifth of axis (C), tilted relative to the first axis and the third axis, and the second shaft and the second mechanism of connection are connected to each other by a pivot link around the sixth axis (F), tilted relative to the second axis and the fourth axis.
EFFECT: simplification of the installation of a flight control device in the crew compartment.
11 cl, 21 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT FLIGHT CONTROL DEVICE | 2019 |
|
RU2769431C1 |
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| TIRE TESTER | 2020 |
|
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|
RU2779841C2 |
| AIRCRAFT WITH FLAPPING WINGS | 2008 |
|
RU2438929C2 |
| VARIABLE-SPEED DRIVE | 0 |
|
SU1199674A1 |
