Conduction impedance-based construction method for electromagnetic prototype of aircraft fuel tank

By constructing an electromagnetic prototype based on conduction impedance and gradually adjusting the electromagnetic model of the fuel tank, the problem of insufficient electromagnetic modeling accuracy in the existing technology was solved, and high-precision lightning current distribution simulation was achieved, supporting the efficient lightning protection design of the fuel tank.

WO2026113038A1PCT designated stage Publication Date: 2026-06-04SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA

Patent Information

Authority / Receiving Office
WO · WO
Patent Type
Applications
Current Assignee / Owner
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
Filing Date
2024-12-04
Publication Date
2026-06-04

AI Technical Summary

Technical Problem

Existing technologies make it difficult to efficiently and accurately perform electromagnetic modeling of aircraft fuel tanks, which leads to difficulties in the rapid evaluation and iteration of lightning protection designs and makes it impossible to realistically simulate the distribution of lightning current.

Method used

By constructing an electromagnetic prototype based on conduction impedance, the simplified electromagnetic model is gradually adjusted to match the test data, including the conduction impedance simulation of adjacent fastening bolts, components, and individual parts, until a high-precision electromagnetic prototype of the fuel tank is obtained.

Benefits of technology

It achieves high-precision electromagnetic modeling of aircraft fuel tanks, enabling realistic simulation of lightning current distribution, providing a reliable basis for lightning protection design of fuel tanks, and is applicable to electromagnetic prototyping of various types of fuel tanks and internal components.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present application relates to the field of aircraft electromagnetic compatibility and lightning protection, and in particular to a conduction impedance-based construction method for an electromagnetic prototype of an aircraft fuel tank. The method is applicable to the construction of electromagnetic prototypes for various types of aircraft fuel tanks, is also applicable to the construction of electromagnetic prototypes for components such as piping and wiring harnesses inside the fuel tanks, and can lay a foundation for high-precision electromagnetic prototype construction of the aircraft fuel tanks and for lightning protection simulation and design based on the electromagnetic prototypes of the fuel tanks.
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