A Dynamic Monitoring Method for Measurement Data of Aircraft Structure Fatigue Test
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
- Publication Date
- 2022-04-19
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Abstract
Description
technical field
[0001] The invention belongs to the field of aviation fatigue damage tolerance test, in particular to a data dynamic monitoring method of aircraft structure fatigue test. Background technique
[0002] Aircraft structural fatigue tests generally have a long test period, a large amount of measurement data, difficult to monitor the test status, real-time monitoring and analysis of measurement data, and it is difficult to draw conclusions about whether the fatigue test is effective, continuous and stable.
[0003] In the fatigue test, for the analysis of measurement data, the conventional practice is to stop the test after a period of time is completed, and set aside time to analyze and judge the validity and stability of the measured strain and displacement in the past period. However, due to the huge amount of data, only relying on naked eye analysis and observation, many human factors are involved, the operability is not strong, and it takes too long. [0004...