A low temperature test method for aircraft braking system
A technology for braking system and low temperature test, applied in the field of low temperature test of civil aircraft braking system, can solve the problems of inability to verify low temperature adaptability and low temperature life, and achieve the effect of avoiding low temperature failure
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[0078] In this embodiment, a low-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. The low-temperature storage and low-temperature working test profiles shall be formulated according to the life requirements.
[0079] This embodiment uses the test equipment shown in Table 1.
[0080] Table 1 Summary of Low Temperature Test Equipment for Civil Aircraft Braking System
[0081]
[0082] The matching products of the civil aircraft braking system described in this embodiment are shown in Table 2.
[0083] Table 2 Supporting Products of Civil Aircraft Braking System
[0084]
[0085]
[0086] The concrete process of this embodiment is:
[0087] Step 1. Determine the sampling principle and the treatment method for low temperature faults during the test.
[0088] One set of brake system is randomly selected to represent the model for low temperature test. If no fail...
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