Aircraft strength test debugging method and system

Abstract

The invention belongs to the technical field of aircraft strength tests, and particularly relates to an aircraft strength test debugging method and system. The method comprises the following steps: S1, acquiring a test debugging task of a server, wherein the test debugging task comprises a debugging manual, debugging contents and matters needing attention for debugging the aircraft strength test equipment; S2, projecting the test debugging task to a test machine or a test facility to form an information virtual image; S3, reading a two-dimensional code label preset on the surface of each test device, and uploading test device information carried by the two-dimensional code label to the server; S4, collecting real-time picture information of test equipment debugging performed by a user wearing the debugging terminal, uploading the real-time picture information to the server, and sharing the real-time picture information with remote equipment control personnel at the same time; and S5, obtaining a debugging picture of a remote equipment controller. According to the invention, the digital recording of the test equipment fault in the whole aircraft strength test debugging is realized, and the debugging efficiency is improved.

Description

technical field [0001] The application belongs to the technical field of aircraft strength testing, and in particular relates to an aircraft strength testing debugging method and system. Background technique [0002] The full-scale aircraft strength test is an important ground test in the process of aircraft research and development. The ground equipment simulates the aerodynamic force, engine thrust and other loads and other environmental conditions in the flight of the aircraft, and studies the static state of the aircraft structure and components under different degrees of tension or compression. The distribution of strength, stiffness, stress and deformation under load, and verifying whether the aircraft meets the structural strength required for flight is an important means to ensure the flight safety of the aircraft. [0003] In the whole machine strength laboratory, the test equipment control room has high environmental requirements, so it should be set up separately ...

AI Technical Summary

Problems solved by technology

[0004] In order to solve the above technical problems, this application provides a visual debugging method that can effectively improve the efficiency and quality of the strength test debugging of the whole aircraft, build a test debugging system based on 5G+MR in a complex aviation test environment, and at the same time have the ability to digitize the debugging results The storage is convenient for retrieval and inspection, and realizes the data accumulation of test equipment failure problems in the aircraft strength test and debugging, thereby forming a big data control and knowledge model of laboratory equipment, and improving the intelligence level of aviation strength laboratories

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