Tandem electric double-rotor helicopter and control system thereof
A control system and dual-rotor technology, applied in the direction of rotorcraft, aircraft control, motor vehicles, etc., can solve the problems of high use and maintenance costs, large fuselage space, and high center of gravity requirements, and achieve large load capacity, high aerodynamic efficiency, and high mechanical efficiency. Small size effect
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[0038] In order to further understand the content, features and effects of the present invention, the following examples are given, and detailed descriptions are given below with reference to the accompanying drawings.
[0039] Aiming at the problems existing in the prior art, the present invention provides a tandem electric dual-rotor helicopter. Figure 1 to Figure 3 The present invention is described in detail.
[0040] Such as Figure 1-Figure 3 As shown, the tandem electric dual-rotor helicopter provided by the embodiment of the present invention includes a fuselage 1, a landing gear, a rotor device 4, a control device, a power device 9, a control device 13 and a cargo box 14.
[0041]Landing gear is provided with two groups, is respectively front landing gear 2 and rear landing gear 3, and front landing gear 2 and rear landing gear 3 are respectively fixed on the front and rear positions of fuselage 1 bottom. Rotor device 4 is provided with two groups, is respectively ...
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