Dynamic test optimization device of rotor wing unmanned aerial vehicle and duct unmanned aerial vehicle as well as optimization method thereof
A technology of unmanned rotor and optimized device, applied in the field of unmanned aerial vehicle, can solve the problems of single transmission movement, large friction force, inability to transmit tensile force and torsion force at the same time, and achieve the effect of eliminating the simple structure
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[0021] Example: A power test optimization device for rotary-wing drones and ducted drones of the present invention includes a computer, a connector 1, an optical axis 2, two linear rotary bearings 3, two bolt rolling bearings 7, and a tension pressure sensor 13 The torsion sensor 16, the connecting sleeve 8, and the connecting plate 4. The tension and pressure sensor 13 and the torsion sensor 16 are both connected to the computer via a wireless network, and a first flat pad 18 is installed inside the connector 1, and the optical axis 2 One end is installed in the socket of the first flat washer 18 and fixed by the first screw 19 and the first nut 20. The connecting sleeve 8 and the two linear rotation bearings 3 are both installed on the optical shaft 2. The connecting sleeve 8 is located between the two linear rotary bearings 3, the outer wall of one end of the connecting sleeve 8 is provided with a connecting sleeve side plate 25, and the bottom of the two side plates of the c...
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