Airplane auxiliary take-off device with arresting mechanism
An aircraft and linear motor technology, applied in the direction of launch/tug transmission, etc., can solve the problems of affecting the endurance and consuming a large amount of fuel.
Pending Publication Date: 2020-06-16
邯郸市复兴区宏昌科技有限公司
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Problems solved by technology
[0004] In view of the above defects, the present invention provides an aircraft auxiliary take-off device with an arresting mechanism to solve the problem that the aircraft consumes a large amount of fuel during take-off and affects the endurance
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[0026] The present invention is described in detail below in conjunction with accompanying drawing, according to Figure 1-13 As shown, an aircraft auxiliary take-off device with an arresting mechanism includes a lower guide rail 1, an air guide rail 2 is arranged above the lower guide rail 1, a take-off platform 3 is fixed above the air guide rail 2, and a pressurized The air pump 5 and the storage battery 22, the pressurized air pump 5 communicates with the air guide rail 2 through the air delivery pipeline 6; a linear motor core 7 is fixed at the lower end of the take-off platform 3, and a linear motor coil 8 is arranged on both sides of the lower end of the linear motor core 7 , the linear motor coil 8 is fixed on the ground; the two sides of the rear end of the take-off platform 3 are respectively fixed with a fixed plate 9, and a fixed shaft 12 is fixed on the fixed plate 9, and the fixed shaft 12 is connected to the hinged shaft 13 by a lever one 10, Articulated shaft 1...
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The aircraft auxiliary take-off device 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, a pressurizing air pump and a storage battery are arranged in the take-off platform, and the pressurizing air pump is communicated with the air guide rail through an air conveying pipeline; linear motor core iron is fixed tothe 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, wherein a permeable plate is arranged at the bottom end of the air guide rail, castruty holes are formed in the permeable plate, an air guide rail cavity is sealed between the permeable plate and the air guide rail, the air guide railcavity is communicated with a pressurizing air pump through an air conveying pipeline, and a one-way valve is further arranged on the air conveying pipeline; an impact head is arranged at the front end of the take-off platform, a front check block and a rear check block are fixed to the top end of the take-off platform, and a blocking mechanism is further arranged on the lower guide rail. 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 an arresting mechanism. 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 provides an...
Claims
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IPC IPC(8): B64F1/06
CPCB64F1/06
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