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

Active Publication Date: 2020-01-24
XIJING UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Whether it is a fighter aircraft of an aircraft carrier or a civilian flight, it is required to take off and land in a limited space plane as much as possible. In the early 19th century, someone proposed electromagnetic launch technology, but it was not mature. After decades of exploration With research, people have successively developed various linear launch devices or models based on the principle of electromagnetic induction, and successfully applied them to the electromagnetic ejection take-off of aircraft carriers. Although this epoch-making research result has proved that the research on electromagnetic launch technology can indeed It is moving towards a new stage, but due to the influence of technology in related research fields, its next step of development will be very long. Due to the reasons of the device itself, the development of this technology is limited to use on aircraft carriers, and it can only assist take-off. There is no deceleration effect in the process, so the range of use of the electromagnetic ejection system is small and the function is single

Method used

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  • Relatively static airplane lifting device and control method thereof
  • Relatively static airplane lifting device and control method thereof
  • Relatively static airplane lifting device and control method thereof

Examples

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Embodiment Construction

[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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Abstract

The invention relates to a relatively static airplane lifting device and a control method thereof. The device comprises a transmission mechanism embedded in a deck, wherein the transmission mechanismcomprises a middle frame and a motor; a plurality of driven rollers are embedded in the middle frame in the horizontal and vertical directions; a conveyor belt is laid on the surface of the driven rollers; bearing idlers are arranged on the inner side of the conveyor belt; a plurality of displacement speed sensors are arranged on two sides of the conveyor belt; signal output of the displacement speed sensor is connected with input of the motor and input of a brake. By controlling the speed of the conveyor belt and power of the motor, an airplane can take off smoothly and land relatively still.The device has the characteristic of small occupied space.

Description

technical field [0001] The invention belongs to the technical field of aircraft landing and landing, and in particular relates to a relatively static aircraft landing and landing device and a control method thereof. Background technique [0002] Whether it is a fighter aircraft of an aircraft carrier or a civilian flight, it is required to take off and land in a limited space plane as much as possible. In the early 19th century, someone proposed electromagnetic launch technology, but it was not mature. After decades of exploration With research, people have successively developed various linear launch devices or models based on the principle of electromagnetic induction, and successfully applied them to the electromagnetic ejection take-off of aircraft carriers. Although this epoch-making research result has proved that the research on electromagnetic launch technology can indeed It is moving towards a new stage, but due to the influence of technology in related research fie...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/04B64F1/02
CPCB64F1/04B64F1/02
Inventor 高育宾
Owner XIJING UNIV
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