Study on Interruption Treatment Method of Low-temperature Test of Complete Civil Aircraft
Received:September 21, 2020  Revised:October 23, 2020
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DOI:10.7643/issn.1672-9242.2021.02.008
KeyWord:low-temperature test of the complete civil aircraft  interruption treatment method  process framework establishment
           
AuthorInstitution
YANG Xin-lei China Electronic Product Reliability and Environment Testing Research Institute, Guangzhou , China
WU Jing-tao Aviation Industry Aircraft Strength Research Institute, Xi’an, , China
TANG Yang-gang Aviation Industry Aircraft Strength Research Institute, Xi’an, , China
WANG Qun-wei China Electronic Product Reliability and Environment Testing Research Institute, Guangzhou , China
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Abstract:
      According to the engineering requirements and technical characteristics of the low-temperature test of the climate laboratory conducted for the complete civil aircraft, the possible interruptions during the test are summarized, and the corresponding laboratory interruption treatment methods are given to form a laboratory operating procedure system. Based on main interruption causes summarized according to relevant test standards, as well as the interruptions caused by over-tests, under-tests, responsible faults, non-responsible faults, etc., the possible impacts are clarified, and the treatment methods after interruption are studied. According to the summarized standard interruption conditions, and relying on the low-temperature laboratory environmental test of a certain type of complete civil aircraft, the interruption conditions and corresponding treatment methods were studied separately, and a laboratory treatment method system was established based on the basic process of interruption. According to the research on the corresponding treatment methods for the interruption of the low-temperature test of the complete civil aircraft, a corresponding interruption treatment method process framework is established, which helps the test unit to carry out the large-scale climate test work for the complete civil aircraft in a quality manner, and provides emergency measures and safeguard ideas for the rationality and effectiveness of the test process.
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