Aircraft Structural Test Load System Integration And Interaction Techniques

In this paper, a method of using computer software technology in the field of structure test design is discussed. The main work is the study of how to describe the test load system and the implementation of system design. The binary tree forest data structure is used to describe the lever load system of structure test. On the basis of this description, a optimum method of load system design is studied.Integration of the load system design and human computer interactive technology and graphics user interface technology facing aircraft structure test is discussed. By using human computer interactive design technology and graphics user interface technology in the field of structure test design, complicated problems in designing the aircraft structure test load system is solved and efficient interactive design to the structure test load system is realized.Integration of structure test load system and parameterized drawing system is discussed. Having designed the load system, the binary tree forest disk storage structure and arithmetic is used to realize disk storage of the lever system. The parameterized drawing system reads data from the file that the loading system builds and automatically draws on AutoCAD platform.