航空结构轮胎爆破喷流载荷下的结构损伤分析及试验研究

周昌伟,张利娟,张陈力子

振动与冲击 ›› 2023, Vol. 42 ›› Issue (8) : 334-340.

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PDF(2740 KB)
振动与冲击 ›› 2023, Vol. 42 ›› Issue (8) : 334-340.
论文

航空结构轮胎爆破喷流载荷下的结构损伤分析及试验研究

  • 周昌伟,张利娟,张陈力子
作者信息 +

Structural damage analysis and experimental study of aviation structure under tire blasting jet load

  • ZHOU Changwei, ZHANG Lijuan, ZHANG Chenlizi
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文章历史 +

摘要

在飞行中,起落架收起后出现的爆胎是由于先前的轮胎损伤而产生的,在轮胎的外露表面上任何一处都有可能发生。为了研究舱内轮胎爆破的喷流载荷对飞机结构的影响,采用了一种可以反映瞬时气流场压力分布的工程拟合方法,建立了工程计算模型。利用该计算模型,观察了典型大尺寸结构在瞬时喷流载荷下的动力学响应过程,得到了结构损伤。结果表明爆破点附近结构弹性变形很大,刚度最大的结构(如缘条)是危险部位;舱内轮胎爆破对结构破坏更严酷;该模型的计算结果与试验数据吻合较好,能够正确预测喷流载荷的压力场分布和结构的动态响应过程。该方法为航空结构的抗轮胎爆破冲击设计与损伤分析提供了一种可靠的手段。

Abstract

In flight, the tire burst of the retracted landing gear is caused by previous tire damage, which may occur anywhere on the exposed surface of the tire.In order to study the influence of tire blasting jet load on aircraft structure in the cabin, an engineering fitting method was adopted to reflect the instantaneous air field pressure distribution, and an engineering calculation model was established.Using this calculation model, the dynamic response process of typical large-size structures under instantaneous jet load was observed, and the structural damage was obtained. It was shown that the elastic deformation of the structure near the blasting point is very large, and the structure with the highest stiffness (such as edge strip) is the dangerous part;tire blasting in cabin causes more severe damage to structure;the computed results with the proposed model agree well with the test data,so the calculation model can correctly predict the pressure field distribution of jet load and the dynamic response process of the structure.This method can provide a reliable means for anti-tire blasting impact design and damage analysis of aviation structures.

关键词

轮胎爆破 / 喷流载荷 / 冲击动力学

Key words

tire blasting / jet load / impact dynamics

引用本文

导出引用
周昌伟,张利娟,张陈力子. 航空结构轮胎爆破喷流载荷下的结构损伤分析及试验研究[J]. 振动与冲击, 2023, 42(8): 334-340
ZHOU Changwei, ZHANG Lijuan, ZHANG Chenlizi. Structural damage analysis and experimental study of aviation structure under tire blasting jet load[J]. Journal of Vibration and Shock, 2023, 42(8): 334-340

参考文献

[1] 章飞, 原磊. 飞机轮胎爆破安全性分析[C]// 第八届中国航空学会青年科技论坛.
Zhang Fei, Yuan Lei. Safety Analysis of aircraft Tire blasting [C] / the eighth Youth Science and Technology Forum of the Aeronautical Society of China.
[2] 张建敏. 飞机轮胎爆破模式浅析[J]. 力学季刊, 2014, 35(1):10.
Zhang Jianmin. A brief study on damaging effects of aeroplane tire and wheel failures [J]. Chinese Quarterly of Mechanics, 2014, 35 (1): 10.
[3] 王曦瑶. 运输类飞机轮胎爆破适航条款追踪分析[J]. 科技创新与应用, 2015(26):1.
Wang Xiyao. Tracking and analysis of explosion airworthiness clause of transport aircraft tire [J]. S Technology Innovation and Application, 2015 (26): 1.
[4] Airworthiness standards: transport category airplanes: 14 CFR Parts 25 [S].Washington: Federal Aviation Administration, 2015.
[5] Certification specifications for large airplanes CS-25 [S] .European Aviation SafetyAgency,2008.
[6] 张建敏, 岳珠峰, 耿小亮,等. 航空轮胎爆破气流场测试方法[J]. 工程爆破, 2016, 22(3):6.
Zhang Jianmin, Yue Zhufeng, Geng Xiaoliang, et al. Blasting air flow of aircraft tire test [J]. Engineering blasting, 2016, 22 (3): 6.
[7] 王佩艳, 张建敏, 岳珠峰,等. 航空轮胎爆破防护设计研究[J]. 力学季刊, 2017, 38(1):8.
Wang Peiyan, Zhang Jianmin, Yue Zhufeng, etc. Study on protection design of aircraft tyre blowout [J]. Chinese Quarterly of Mechanics, 2017, 38 (1): 8.
[8] 张建敏, 耿小亮, 姚世乐,等. 飞机起落架舱内轮胎爆破压力场测试研究[J]. 应用力学学报, 2016, 33(3):5.
Zhang Jianmin, Geng Xiaoliang, Yao Shile, et al. Test method for blasting air flow of aircraft tyre in aircraft landing gear chamber [J]. Chinese Journal of Applied Mechanics, 2016, 33 (3): 5.
[9] 陈凯帆,马建.飞机轮胎爆破喷流模式下管路的强度计算方法[J].民用飞机设计与研究,2021( 3) : 21-25.
Chen Kaifan, Ma Jian. Calculation method of pipeline strength in jet mode of aircraft tire burst [J]. Civil aircraft Design and Research, 2021 (3): 21-25.
[10] 霍志勤,罗帆. 近十年中国民航事故及事故征候的统计分析[J]. 中国安全科学学报, 2006, 16(12):7.
Huo Zhiqin, Luo Fan. Statistic analysis on accidents and incidents in the last decade in China civil aviation [J]. China Safety Science Journal, 2006, 16 (12): 7.
[11] 毛可毅, 牟浩蕾, 巩天琛,等. 欧美损伤容限与疲劳评定适航符合性方法差异分析[J]. 航空标准化与质量, 2016(2):3.
Mao Keyi, Mou Haolei, Gong Tianchen, et al. Analysis of the difference of airworthiness compliance methods between damage tolerance and fatigue assessment in Europe and America [J]. Aviation Standardization and quality, 2016 (2): 3.
[12] 谢灿军, 童明波, 刘富,等. 7075-T6铝合金动态力学试验及本构模型研究[J]. 振动与冲击, 2014, 33(18):6.
Xie Canjun, Tong Mingbo, Liu Fu, et al. Dynamic tests and constitutive model for 7075-T6 aluminum alloy [J]. Vibration and shock, 2014, 33 (18): 6.

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