Device special for airplane launch
A technology of aircraft and control devices, which is applied in the direction of launching/dragging transmission devices, etc., can solve the problems of large fuel consumption, long aircraft, and only one aircraft can take off, and achieve the effects of improved survivability, stable thrust, and simple structure
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Embodiment 1
[0041] Embodiment 1: The aircraft launching device is provided by a flow control valve 1, a power generator 2, a gearbox 3, a hydraulic pump station 4, a hydraulic rubber hose 5, a hydraulic pusher 6, a bearing frame, a thruster, a guide rail 9, a frame 10 and mercury Device 29 is composed. The mercury provider 29 is connected to the bottom of the power generator 2 through the flow control valve 1 through the pipe, the output shaft of the power generator 2 is connected to the gearbox 3 shaft through the coupling, and the output shaft of the gearbox 3 is connected to the hydraulic pump through the coupling The input shaft of station 4 is connected, the hydraulic output port of hydraulic pump station 4 is connected with hydraulic hose 5, the other end of hydraulic hose 5 is connected with the inlet of hydraulic pusher 6, hydraulic pusher 6 is fixed on guide rail 9 or bracket 10, hydraulic pusher 6 The output end links to each other with the carrier, and the carrier is placed on ...
Embodiment 2
[0063] Embodiment 2: The hydraulic pusher includes a rack 15, a transmission hydraulic cylinder 16, and a flange 17. There is a flange 17 fixed on the support 10 below the cylinder body of the hydraulic cylinder, and the gear on the cylinder body meshes with the rack. The rack is fixed on the carrier frame 7.
[0064] Working principle: The hydraulic oil output from the hydraulic rubber hose enters the transmission hydraulic cylinder 16 to push the piston to move, the piston drives the gear to rotate, and the gear drives the rack to make the carrier 7 move in a straight line.
[0065] The outlet pipe valve 18 of the mercury provider is connected to a pressure regulating box 23 for adjusting and maintaining a stable mercury pressure, and the others are the same as in Embodiment 1.
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