Airplane hydraulic brake system
A braking system and hydraulic technology, applied in the direction of aircraft braking arrangement, control mechanism, vehicle components, etc., can solve problems such as unreasonable layout and potential safety hazards, and achieve the effect of eliminating hidden dangers of accidents, rational structure and lightening burden.
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[0022] 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. This embodiment takes one of the main landing gear and one wheel installed as an example to illustrate the control process of the aircraft hydraulic brake system main landing gear braking the wheel normally and the take-off line braking. Since emergency braking is not involved, the aircraft emergency braking system is not shown in the figure. The emergency braking system is prior art.
[0023] The components of the aircraft hydraulic braking system in this embodiment include: a hydraulic braking valve 1 , a hydraulic control switching valve 2 , an electro-hydraulic servo valve 3 , an anti-skid control box 4 , and a speed sensor 5 .
[0024] The hydraulic brake valve 1 is installed near the pedal mechanism b...
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