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Publishing Language: Chinese

Anti-bird impact design of aircraft structure via bulding block approach

Tao SUO1,2,3,4( )Yulong LI4,5,6
School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China
Institute of Extreme Mechanics, Northwestern Polytechnical University, Xi'an 710072, China
National Key Laboratory of Aircraft Configuration Design, Xi'an 710072, China
Joint International Research Laboratory of Impact Dynamics and its Engineering Application, Xi'an 710072, China
School of Civil Aviation, Northwestern Polytechnical University, Xi'an 710072, China
National Key Laboratory of Strength and Structural Integrity, Xi'an 710072, China
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Abstract

In the field of aerospace engineering, aircraft inevitably encounter bird strikes during their service life, posing a direct threat to flight safety and potentially leading to catastrophic accidents involving the loss of aircraft and human lives. Due to the complexity of impact dynamics, bird strike resistance design for aircraft structures necessitates an integrated approach combining design analysis, numerical simulation, and experimental validation. However, the lack of dynamic performance and constitutive parameters for structural materials, as well as limitations in experimental methods and instrumentation, resulted in lengthy and inefficient impact resistance design. In recent years, the Impact dynamics research team at Northwestern Polytechnical University has conducted a series of innovative studies focusing on bird strike resistance design for aircraft structures, based on building block approach. This work addresses the determination of dynamic properties and constitutive parameters of structural materials and bird, the dynamic failure behavior of riveted joints, and the development of a novel anti-bird strike design concept and its application in the bird strike resistance design of a civil aircraft.

CLC number: V215;0347;0316 Document code: A Article ID: 1000-6893(2025)05-531524-23

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
SUO T, LI Y. Anti-bird impact design of aircraft structure via bulding block approach. Acta Aeronautica et Astronautica Sinica, 2025, 46(5). https://doi.org/10.7527/S1000-6893.2025.31524

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Received: 12 November 2024
Revised: 02 December 2024
Accepted: 10 January 2025
Published: 10 March 2025
© 2025 The Journal of Acta Aeronautica et Astronautica Sinica