Aircraft brake system low temperature test method
A brake system and low-temperature test technology, which is applied in the low-temperature test field of civil aircraft brake systems, can solve the problems of inability to verify low-temperature adaptability and low-temperature life
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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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