Aircraft fly-by-wire braking system capable of automatic braking and braking method
A technology of automatic braking and braking system, applied in the direction of aircraft braking arrangement, braking regulator, etc., can solve problems such as difficulty in troubleshooting and positioning, low reliability in use, and potential safety hazards, and achieve shortened landing distance and reliable Sexual height, effect of reducing physical and mental load
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[0026] The front landing gear wheels of modern aircraft generally do not have brakes, and brake devices are equipped on the wheels of the two main landing gears. The two aircraft main landing gears are usually arranged symmetrically on both sides of the aircraft fuselage. In this embodiment, one of the main landing gear and one wheel is installed as an example to illustrate the fly-by-wire hydraulic braking system of an aircraft with automatic braking capability according to the present invention.
[0027] In this embodiment, the automatic brake is set to one level; the automatic brake anti-skid valve adopts an independent anti-skid valve, and the electro-hydraulic servo valve is used as the anti-skid valve; the pressure supply of the automatic brake is separately provided by the decompression valve.
[0028] This embodiment is an aircraft braking system with automatic braking, including: a braking command sensor 1 , a control box 4 , a first electro-hydraulic servo valve 3 , ...
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