A Multi-Combination Aircraft Brake System Selected and Controlled According to Taxi Speed
A braking system and aircraft technology, applied in the direction of aircraft braking arrangement, control mechanism, etc., can solve the problems of heat generation, unfavorable deceleration effect during the taxiing process of the aircraft, etc.
Active Publication Date: 2020-04-03
桐乡乐维新材料有限公司
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Problems solved by technology
[0003] However, as far as the current research status of the aircraft braking system is concerned, most of them use a single, integral brake pad to decelerate the aircraft, which easily causes the entire brake pad of the aircraft to generate heat after a period of contact, which is harmful to the aircraft taxiing process. Therefore, it is particularly important to research and develop an aircraft brake device that can decelerate the aircraft through different brake pads in different time periods, and can be selected and controlled according to the speed of the aircraft. It greatly improves the adaptability and safety of the aircraft's flight environment, and can prolong the life of the aircraft's braking device
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[0022] The present invention is realized through the following technical solutions:
[0023] A multi-combination aircraft braking system that is selected and controlled according to the taxiing speed, including a vertical support rod 1, a brake pad connecting rod 2, an aircraft taxiing wheel 3, a braking device 4, a lateral support rod 5, a brake pad support rod 6, an aircraft Wheel hub 7, brake device wall 8, brake pad stretch rod 9, brake pad 10, rotation shaft through hole 11, main stretch rod 12, rotation shaft I13, auxiliary stretch rod 14, rotation shaft II15, rotation shaft III16, brake Brake rotation shaft 17, auxiliary support rod 18, brake pad tension rod through hole 19, elastic device auxiliary support plate 20, upper convex body 21, lower convex body 22, brake pad mounting plate 23, brake pad backing plate 24, elastic device 25, brake pad support rod rod body 26, connecting rod adjusting teeth 27, connecting rod adjusting slideway 28, adjusting hole 29, adjusting ...
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The invention relates to a multiple-combination airplane braking system performing selection and control according to a taxiing speed, belonging to the technical field of aeronautical facilities. Speed reduction and braking after an airplane lands can be achieved through airplane taxiing wheels, braking devices, auxiliary supporting bars, elastic device auxiliary supporting plates, elastic devices, adjusting bolts, and the like. In addition, according to different speeds after different periods of time after the airplane lands, the number of locked airplane brake pads and locking positions ofthe airplane brake pads are autonomously controlled, thus prolonging the service lifetime of the airplane brake pads to a great degree, and intervening the brake effect to a certain degree to improveflight comfort of passengers and the flight crew on an airplane. The system is of great practical significance for actual airplane control and airplane riding comfort.
Description
technical field [0001] The invention relates to an aircraft brake system, in particular to a multi-combination aircraft brake system selected and controlled according to taxiing speed, which belongs to the technical field of aviation equipment. Background technique [0002] As a kind of aircraft, the aircraft has been used in more and more occasions. In recent years, with the continuous progress and development of social science and technology, and based on the needs of different environments and uses, various aircraft have been continuously developed. , which has also prompted the continuous research and development of aircraft parts and related supporting devices. As an indispensable and important part of the aircraft, the braking system of the aircraft has extraordinary significance in the process of the aircraft taxiing to stop, and its deceleration effect will directly affect the environmental adaptability and safety of the aircraft. [0003] However, as far as the cur...
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IPC IPC(8): B64C25/42B64C25/44
CPCB64C25/42B64C25/44
Inventor 冯琴
Owner 桐乡乐维新材料有限公司