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| Tailoring Method of High Temperature Test Conditions of a Certain Type of Aircraft Laboratory |
| Received:January 09, 2020 Revised:February 13, 2020 |
| View Full Text View/Add Comment Download reader |
| DOI：10.7643/issn.1672-9242.2020.05.011 |
| KeyWord:high temperature test test procedure tailoring method test conditions |
| Author | Institution |
| ZHANG Ya-juan |
Aircraft Strength Research Institute of China, Xi¢an , China |
| GONG Yun-zhao |
Aircraft Strength Research Institute of China, Xi¢an , China |
| WANG Hong-bin |
Aircraft Strength Research Institute of China, Xi¢an , China |
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| Abstract: |
| The paper aims to more truly simulate the high-temperature environment conditions on the ground of aircraft through high-temperature verification laboratory test of the whole aircraft.By analyzing the latest climate test standards at home and abroad such as GJA150A, MIL-STD-810G and RTCA/DO-160G, the high temperature test program of a certain aircraft laboratory was determined. Based on this test procedure, combined with the requirements of aircraft temperature adaptability, the envelope of civil aircraft operating environment and the experience of foreign aircraft laboratory temperature tests, the high temperature test conditions of a certain type of aircraft laboratory were obtained by analysis and tailoring. The high temperature test condition tailoring method for the aircraft laboratory are formed, and the research results can provide a reference for the high temperature laboratory test design of the whole aircraft . |
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