Fixed-wing unmanned airplane takeoff method
A technology of unmanned aerial vehicles and fixed wings, applied in the field of aircraft, can solve the problems affecting the endurance time and flight attitude, and achieve the effect of light weight, not easy to shake, and prolong the endurance time
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Example Embodiment
[0037] Example 1
[0038] Such as figure 1 As shown, this embodiment provides an unmanned aerial vehicle release mechanism, including: steering gear 101: steering gear 101 includes an output shaft; steering wheel 102: one end of the steering wheel 102 is fixedly connected to the output shaft; transmission rod 20: one end of connecting rod 60 The pin lever 30 is hinged to the other end of the steering wheel 102: one end of the pin lever 30 is hinged to the other end of the connecting rod; the mounting block 40: the mounting block 40 is fixedly installed on the steering gear 101, the middle of the mounting block 40 is provided with a card slot 401, the mounting block 40 A through hole 402 is provided in the transverse direction. The other end of the latch rod 30 penetrates through the through hole 402 and extends into the slot 401. The inner wall of the slot 401 on the side away from the steering wheel 102 abuts against the other end of the latch rod 30, and the steering gear 101 ca...
Example Embodiment
[0042] Example 2
[0043] Such as figure 2 As shown, this embodiment provides a fixed-wing unmanned aerial vehicle, including the unmanned aerial vehicle release mechanism of Embodiment 1. It also includes a multi-axis aircraft, a fixed-wing aircraft 50 and a connecting rod 60. One end of the connecting rod 60 is connected to the fixed wing. The aircraft 50 is connected, and the other end of the connecting rod 60 is provided with a hanging ring 70; the rudder plate 102 is fixedly connected to the multi-axis aircraft, and the hanging ring 70 is located in the slot 401 and sleeved on the bolt rod 30.
[0044] The structures of the multi-rotor aircraft and the fixed-wing aircraft 50 are all existing technologies.
[0045] The multi-axis aircraft and the fixed wing aircraft 50 are connected by a drone release mechanism. The fixed wing aircraft 50 is hung on the latch rod 30 in the slot 401 through the hanging ring 70 set on the connecting rod 60, and the steering gear 101 is controlled ...
Example Embodiment
[0046] Example 3
[0047] Such as image 3 As shown, this embodiment provides a fixed-wing unmanned aerial vehicle, including the unmanned aerial vehicle release mechanism of Embodiment 1. It also includes a multi-axis aircraft, a fixed-wing aircraft 50 and a connecting rod 60. One end of the connecting rod 60 is connected to the fixed wing. The aircraft 50 is connected, and the other end of the connecting rod 60 is provided with a hanging ring 70; the rudder plate 102 is fixedly connected to the multi-axis aircraft, and the hanging ring 70 is located in the slot 401 and sleeved on the pin rod 30; also includes a fixed ring 80 and a carbon fiber sleeve 90, the fixed ring 80 is fixedly installed at one end of the connecting rod 60, the carbon fiber sleeve 90 is symmetrically arranged on the fixed airfoil 50, the axis of the carbon fiber sleeve 90 is perpendicular to the symmetry axis of the fixed airfoil 50, and the inner wall of the fixed ring 80 and the carbon fiber sleeve The ...
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