Tilted four-rotor aircraft
A technology of tilting quadrotors and aircraft, which is applied in the field of unmanned aviation, can solve the problems such as the lack of progress of aircraft, and achieve the effects of overcoming excessive tilt angle errors, ensuring accuracy, and simplifying complexity
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[0019] The present invention will be described in further detail below in conjunction with the accompanying drawings.
[0020] see figure 1 , the present invention comprises fuselage 7, and described fuselage 7 is provided with two secondary wings, is specifically front wing 1 and rear wing 13, and the two ends of front wing 1, the two ends of rear wing respectively are provided with a There are four sets of rotor systems in total. The front wing 1 and the rear wing 13 are all provided with a worm gear shaft 2 for driving the rotor system to perform tilting motion. The worm gear shaft 2 passes through the fuselage 1, and the worm gear shaft 2 is installed on the The inside of the front wing 1 and the rear wing 13 play a certain supporting role; wherein each group of rotor systems includes a DC brushless motor 16, a propeller 14 and a motor mounting seat 6, and the motor mounting seat 6 is arranged on the end of the worm gear shaft 2 A DC brushless motor 16 is installed on the...
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