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Airplane electromagnetic environment effect simulation method

A technology of electromagnetic environment and simulation method, applied in design optimization/simulation, geometric CAD, configuration CAD, etc., can solve the problem of difficult to achieve rapid calculation ability of mixed material structure of electric power, lack of ability to quantify the electromagnetic environment effect of aircraft, and lack of electromagnetic environment. Parameter library, etc.

Pending Publication Date: 2020-02-11
中航通飞华南飞机工业有限公司
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AI Technical Summary

Benefits of technology

This technology allows engineers to easily simulate how complex structures behave when exposed to different types of radiation such as lightning or gamma rays during flight without having access too much detail about their physical properties like density. It also includes an electric field model with multiple scales and various parameters stored within it which helps them calculate more accurate results compared to traditional methods based on specific material characteristics.

Problems solved by technology

This patented describes an issue where current commercially available simulations cannot effectively simulate complex composites (such as those used by military forces) without causing damage or malfunctions due to their unique characteristics. Current simulators are limited because they only work at certain frequencies within these environments. Therefore there needs a new approach called Electromagnetism Simulation Programming (EMP), which allows engineers to easily create customized models based upon different types of conductive elements found inside them.

Method used

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  • Airplane electromagnetic environment effect simulation method
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  • Airplane electromagnetic environment effect simulation method

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Embodiment Construction

[0025] The present invention proposes a simulation method for aircraft electromagnetic environment effects, see figure 1 , which is characterized in that: importing the aircraft CAD model, and performing model repair and multi-scale subdivision on the aircraft CAD model to form an aircraft grid model; using the aircraft composite material electromagnetic parameter library to set the aircraft material electromagnetic parameters; combining the material electromagnetic parameters to The aircraft grid model is subjected to regional decomposition numerical simulation modeling to obtain the aircraft electromagnetic model; combined with the preset electromagnetic excitation source, the adaptive cross approximation algorithm ACI or multi-layer The fast multipole algorithm MLFMA calculates the electromagnetic field strength value in the interior area of ​​the aircraft. Set the cable harness path and electrical characteristic information, use the aircraft harness modeling model library ...

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Abstract

The invention provides an aircraft electromagnetic environment effect simulation method, which comprises the steps of importing an aircraft CAD model, and performing mold repairing and multi-scale subdivision on the aircraft CAD model to form an aircraft grid model; setting airplane material electromagnetic parameters by utilizing the airplane composite material electromagnetic parameter library;performing regional decomposition numerical simulation modeling on the aircraft grid model in combination with material electromagnetic parameters to obtain an aircraft electromagnetic model; and in combination with a preset electromagnetic excitation source, calculating an electromagnetic field intensity value of the internal area of the aircraft by adopting an adaptive cross approximation algorithm ACI or a multilayer fast multipole algorithm MLFMA on the basis of a moment method MoM for the aircraft electromagnetic model; setting a cable harness path and electrical characteristic information, and establishing a harness electromagnetic model in the aircraft electromagnetic model by utilizing the aircraft harness modeling model library; and in combination with the electromagnetic field intensity value, adopting a high-frequency field line coupling analysis algorithm for the wire harness electromagnetic model to calculate an induced current value on an aircraft cable harness.

Description

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Claims

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Application Information

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Owner 中航通飞华南飞机工业有限公司
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