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Airplane auxiliary take-off device with pneumatic control system

A technology of pneumatic control system and air supply system, which is applied in the direction of parking devices, aircraft parts, ground devices, etc., and can solve problems such as large fuel consumption and impact on endurance

Pending Publication Date: 2020-06-16
邯郸市复兴区宏昌科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of the above defects, the present invention provides an aircraft auxiliary take-off device with a pneumatic control system to solve the problem that the aircraft consumes a large amount of fuel during take-off and affects the endurance

Method used

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  • Airplane auxiliary take-off device with pneumatic control system
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  • Airplane auxiliary take-off device with pneumatic control system

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Embodiment Construction

[0028] The present invention is described in detail below in conjunction with accompanying drawing, according to Figure 1-15 As shown, a kind of aircraft auxiliary take-off device with pneumatic control system, comprises lower guide rail 1, is provided with air guide rail 2 above lower guide rail 1, is fixed with take-off platform 3 above air guide rail 2, is provided with pneumatic The control system 5 and the storage battery 22, the pneumatic control system 5 communicate with the air guide rail 2; the lower end of the take-off platform 3 is fixed with a linear motor iron 7, and the two sides of the lower end of the linear motor iron 7 are provided with a linear motor coil 8, and a linear motor coil 8 Be fixed on the ground; The rear end both sides of take-off platform 3 are respectively fixed with installation fixed plate 9, and fixed shaft 12 is fixed on the installation fixed plate 9, and fixed shaft 12 is connected hinged shaft 13 by lever-10, and hinged shaft 13 passes l...

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Abstract

The invention discloses an airplane auxiliary take-off device with a pneumatic control system, which is characterized in that an air guide rail is arranged above a lower guide rail, a take-off platform is fixed above the air guide rail, the pneumatic control system and a storage battery are arranged in the take-off platform, and the pneumatic control system is communicated with the air guide rail;linear motor core iron is fixed to the lower end of the take-off platform, and linear motor coils are arranged on the two sides of the lower end of the linear motor core iron and fixed to the ground.A ventilating plate is arranged at the bottom end of the air guide rail; castruty holes are formed in the ventilation plate, an air guide rail cavity is formed between the ventilation plate and the air guide rail in a sealed mode and communicated with a pneumatic control system through a pipeline, a front check block and a rear check block are fixed to the top end of the take-off platform, and the rear check block is detachably fixed to the top end of the take-off platform through bolts. The aircraft has the beneficial effect that the problem that a large amount of oil is consumed when the aircraft takes off is solved.

Description

technical field [0001] The invention relates to the technical field of aircraft take-off equipment, and more specifically relates to an aircraft auxiliary take-off device with a pneumatic control system. Background technique [0002] Airplane is an indispensable means of transportation in today's society. Generally, when an airplane takes off, it needs to taxi on a straight runway for a long distance. The take-off can be completed when the aircraft takes off, and the runways of the airports are hundreds of meters or even thousands of meters long; therefore, the aircraft will consume a lot of fuel during take-off to affect the endurance, and the strength of the endurance is very important for combat aircraft. [0003] Therefore, it is a problem to be solved by those skilled in the art to invent an aircraft auxiliary take-off device that can increase the endurance of the aircraft. Contents of the invention [0004] In view of the above defects, the present invention provide...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/00B64F1/02
CPCB64F1/00B64F1/002B64F1/02B64F1/025
Inventor 张红昌付建超周天宇
Owner 邯郸市复兴区宏昌科技有限公司