A high temperature test method for aircraft braking system
A braking system and high temperature test technology, which is applied in the high temperature test field of civil aircraft braking system, can solve problems such as hidden dangers of high temperature faults of products, and achieve the effect of eliminating high temperature faults and avoiding high temperature faults.
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[0080] In this embodiment, a high-temperature test is carried out on a brake system of a civil aircraft. The service life of the brake system is 5000 landings / 10 years, whichever comes first. According to the life requirements, the high temperature storage and high temperature working test profiles are formulated.
[0081] This embodiment uses the test equipment shown in Table 1.
[0082] Table 1 Summary of High Temperature Test Equipment for Civil Aircraft Brake System
[0083]
[0084]
[0085] The matching products of the civil aircraft braking system described in this embodiment are shown in Table 2.
[0086] Table 2 Supporting Products of Civil Aircraft Braking System
[0087] serial number name model Function 1 Linear Displacement Sensor DW-1 Provide displacement signal to control box 2 Anti-skid brake control box FH-2 Provide 0~20mA control current to the servo valve 3 servo valve SF-3 Output 0~10MPa pressure 4 ...
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