Relatively static airplane lifting device and control method thereof
A relatively static, landing gear technology, applied in the direction of parking gear, launch/drag transmission, etc., can solve the problems of single function, small range of use of electromagnetic ejection system, and long development
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[0065] The present invention will be described in detail below in conjunction with the accompanying drawings.
[0066] Such as figure 1 As shown, a relatively stationary aircraft landing gear includes a transmission mechanism 1 embedded in the deck 11, the transmission mechanism 1 includes a middle frame 2, and several driven rollers 3 are embedded in the horizontal and vertical directions of the middle frame 2. The surface of the drum 3 is covered with a conveyor belt 4 , and the inner side of the conveyor belt 4 is equipped with a carrying roller 5 , and a plurality of displacement speed sensors 6 are arranged on both sides of the conveyor belt 4 .
[0067] Such as figure 2 As shown, the transmission mechanism 1 also includes a motor 7, the power output shaft of the motor 7 is connected to the first power input of the speed reducer 9 through a coupling 10, and the second power input of the speed reducer 9 is connected to the power output of the brake 8 Connection, the pow...
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