首页|期刊导航|航空学报|基于实测冲击响应谱的飞机结构炮振响应预计与验证

基于实测冲击响应谱的飞机结构炮振响应预计与验证OA

Prediction and validation of aircraft structure response to gunfire vibration based on measured shock response spectrum

中文摘要英文摘要

针对飞机炮振环境筛选试验中通用谱与实测数据偏差显著的问题,通过实测飞机设备舱炮振响应,发现其采用随机振动形式无法表征真实冲击脉冲特性,且幅值偏差达5倍以上,导致能量匹配失准与结构累积损伤评估失效.基于炮振实测数据构建冲击响应谱(SRS),并在实测受限时结合扩展工况传递路径分析(OPAX)方法进行响应预计,通过有限元仿真与实验室试验验证,结果表明:SRS合成波形与实测数据在脉冲形态、幅值趋势上高度一致(能量误差<15%),且其应变响应可有效包络实测波动范围.研究表明,SRS通过多脉冲能量统计与结构动力学耦合,精准复现了真实炮振环境的动态特性,结合OPAX方法对炮振高影响区响应的预计能力,推进了国内炮振响应预计、谱编制的工程化应用发展,为飞机结构与机载设备提供了科学、标准化的炮振试验方法,显著提升了装备环境适应性试验的精准性和工程实用性.

The widely adopted Program IV general spectrum in China's military aircraft gunfire environment screening tests has been found to exhibit significant discrepancies with real-world gunfire vibration environments.Practical appli-cations reveal substantial energy mismatch(amplitude differences exceeding fivefold)and failure in accurately evaluat-ing structural cumulative damage.To address these issues,this study conducted gunfire vibration measurements on an aircraft equipment cabin.The results demonstrate that the traditional random-vibration-based general spectrum can-not characterize the real shock pulse characteristics.Subsequently,a Shock Response Spectrum(SRS)was con-structed based on measured data.The Operational Path Analysis with eXogenous inputs(OPAX)method was further applied to predict responses in high-impact zones where direct measurement is restricted.Finite element simulations and laboratory experiments were employed to validate the SRS method.The findings reveal that the SRS-derived waveform exhibited high consistency with measured data in terms of pulse morphology and amplitude trends(energy matching error<15%);the SRS strain responses effectively enveloped the full range of transient shock test results.This study further shows that SRS,by integrating multi-pulse energy statistics with structural dynamics coupling,pre-cisely replicates the dynamic characteristics of real gunfire environments.Combined with OPAX predictions,the ap-proach promotes the development of domestic engineering applications for gunfire vibration spectra and response esti-mation,and provides a scientific,standardized testing methodology for evaluating the reliability of aircraft structures and airborne equipment.The proposed approach significantly enhances the precision and practicality of environmental adaptability verification for defense systems.

李益萱;陈英华;李凯翔;白春玉;刘小川

中国飞机强度研究所 航空声学与振动航空科技重点实验室,西安 710065||中国飞机强度研究所 强度与结构完整性全国重点实验室,西安 710065中国直升机设计研究所,景德镇 333001中国飞机强度研究所 航空声学与振动航空科技重点实验室,西安 710065||中国飞机强度研究所 强度与结构完整性全国重点实验室,西安 710065中国飞机强度研究所 航空声学与振动航空科技重点实验室,西安 710065||中国飞机强度研究所 强度与结构完整性全国重点实验室,西安 710065中国飞机强度研究所 航空声学与振动航空科技重点实验室,西安 710065||中国飞机强度研究所 强度与结构完整性全国重点实验室,西安 710065

航空航天

炮振环境试验炮振通用谱冲击响应谱(SRS)实测数据建模OPAX响应预计

gunfire vibration environment testinggunfire vibration general spectrumShock Response Spectrum(SRS)measured data modelingOPAX-based response prediction

《航空学报》 2026 (4)

75-85,11

10.7527/S1000-6893.2025.32327

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