A vertical take-off and landing UAV with foldable wings
A technology of vertical take-off and landing and unmanned aerial vehicles, which is applied in the direction of rotorcraft, motor vehicles, aircraft parts, etc., can solve the problems of long running distance, inability to effectively monitor the enemy, and difficulty in finding the runway, etc., to achieve the effect of eliminating the wake vortex
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[0018] The following embodiments will further illustrate the present invention with reference to the accompanying drawings.
[0019] see Figure 1~4 , the embodiment of the present invention is provided with left wing 1, right wing 2, main wing 3, left wing propeller engine 41, right wing propeller engine 42, main propeller engine 43, left camera 61, right camera 62, main camera 63, left rudder surface 71, right rudder surface 72, main rudder surface 73.
[0020] Described left wing 1 and right wing 2 are connected with main wing 3 respectively, and left wing propeller engine 41 is arranged on the inner side of left wing 1 just above, and right wing propeller engine 42 is located at the inner side of right wing 2 just above. Above, the main propeller engine 43 is located on the inside of the main wing 3 just above; the left camera 61 is located on the outer side of the left wing 1, the right camera 62 is located on the outer side of the right wing 2, and the main camera 63 is...
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