Tail rotor driving system of helicopter, control method thereof and helicopter
A drive system and control method technology, applied in the aviation field, can solve problems such as tail rotor failure, failure to provide sufficient pulling force, tail rotor stall, etc., to achieve the effects of ensuring stable operation, reducing aircraft heading disturbance, and reducing power consumption
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[0028] The following describes in detail the embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein the same or similar reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary, and are intended to explain the present invention and should not be construed as limiting the present invention.
[0029] The following describes a helicopter tail rotor drive system and a control method thereof, and a helicopter according to embodiments of the present invention with reference to the accompanying drawings.
[0030] figure 1 It is a schematic structural diagram of a tail rotor drive system of a helicopter according to an embodiment of the present invention.
[0031] like figure 1 As shown, the tail rotor drive system includes: a tail rotor 11 , a tail rotor variable pitch structure ...
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