An analysis method for integrated heat and electricity of radome

Abstract

The present invention proposes a radome force thermoelectric integration analysis method, the method mainly includes the following steps: S1: establish the finite element model of the mechanical calculation of the radome, and the undeformed finite element model of the electromagnetic calculation; S2: the mechanical finite element model established for S1 The element model is used to solve the aerodynamic and thermal loads; S3: the mechanical finite element model established by S1 is used to solve the aerodynamic loads; S4: the calculation results of S2 and S3 are post-processed to extract the node displacement. S5: Complete reconstruction of the S4 finite element model based on Python language; S6: Reconstruct the deformed finite element model in S5 based on HyperMesh software to obtain the electromagnetic calculation finite element model, and complete the analysis of the wave transmission performance of the radome under aerodynamic load; S7 : Complete the electromagnetic medium parameter setting and antenna modeling of the electromagnetic calculation finite element model established in S1, complete the wave transmission performance analysis of the original state radome, and compare with the calculation results of S6.

Description

technical field [0001] The invention belongs to the interdisciplinary field of computational electromagnetic structural strength, and in particular relates to an analysis method for integrated analysis of radome force, heat and electricity. Background technique [0002] With the continuous development of aerospace technology, the performance of various aircraft has made breakthroughs in different fields. The game between major powers is now not just a game between hard power. The strength gap between aircraft is also an important point that cannot be ignored. In the design of the aircraft, the aircraft radome, because it is located at the forefront, undertakes the important task of protecting key electronic systems such as the aircraft radar guidance system. Therefore, the electromagnetic check and strength check of the aircraft radome are very important for the design of the composite material structure and even the design of the entire aircraft. The radome in the aircra...

AI Technical Summary

Problems solved by technology

[0003] Purpose of the invention: The present invention proposes an integrated analysis method for radome force, heat and electricity, which solves the problem of the electrical and mechanical properties of the radome caused by the long research and development cycle, high iteration cost, and no cross-discipline between mechanics and electromagnetics in the current radome development process. Issues such as inability to optimize at the same time

Images