董军超,王凤金,朱重阳.基于多失效模式的弹上舱段结构件贮存寿命验证方法[J].装备环境工程,2022,19(10):80-85. DONG Jun-chao,WANG Feng-jin,ZHU Chong-yang.Missile Cabin Storage Life Verification and Assessment MethodBased on Multiple Failure Modes[J].Equipment Environmental Engineering,2022,19(10):80-85.
基于多失效模式的弹上舱段结构件贮存寿命验证方法
Missile Cabin Storage Life Verification and Assessment MethodBased on Multiple Failure Modes
  
DOI:10.7643/issn.1672-9242.2022.10.011
中文关键词:  多失效模式  弹上舱段结构件  贮存寿命  验证与评估  防热材料  激活能中图分类号:TJ760 文献标识码:A 文章编号:1672-9242(2022)10-0080-06
英文关键词:multiple failure modes  missile cabin  storage life  verification and assessment  thermal protection material  activation energy
基金项目:
作者单位
董军超 北京强度环境研究所,北京 100076 
王凤金 北京航天发射技术研究所,北京 100076 
朱重阳 北京强度环境研究所,北京 100076 
AuthorInstitution
DONG Jun-chao Beijing Institute of Structure and Environment Engineering, Beijing 100076, China 
WANG Feng-jin Beijing Institute of Space Launch Technology, Beijing 100076, China 
ZHU Chong-yang Beijing Institute of Structure and Environment Engineering, Beijing 100076, China 
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中文摘要:
      目的 验证多失效模式下弹上舱段结构件的贮存寿命。方法 通过开展贮存条件下失效模式分析,确定复合材料贮存薄弱环节,依此制定高温摸底试验方案。开展高温极限应力试验,确定不改变复合材料失效机理的高温贮存极限应力,并据此开展加速因子试验,基于阿伦尼兹模型,计算不同失效模式的激活能,并以激活能最小的性能参数作为贮存薄弱环节,计算舱段结构件加速因子,设计舱段结构件加速贮存寿命验证试验,评估其贮存寿命。结果 计算了某防热材料各失效模式下的激活能,确定了其性能参数的薄弱环节,根据薄弱环节的激活能计算了舱段结构件加速因子和加速贮存试验时间,验证了其贮存寿命。结论 通过确定防热材料的贮存薄弱环节,开展了加速贮存试验,验证了舱段贮存寿命。
英文摘要:
      The paper intends to verify the storage life of missile cabin based on multiple failure modes. Through the failure mode analysis under storage conditions, the paper determines the weak links of composite materials and formulates the high-temperature test scheme. Carry out high temperature ultimate stress test to determine the high temperature storage ultimate stress that does not change the failure mechanism of composite materials, and conduct the acceleration factor test accordingly. Calculate the activation energy of different failure modes based on Arrhenius model, and take the performance parameter with the minimum activation energy as the storage weak link to calculate the cabin acceleration factor, design the cabin accelerated storage life verification test and evaluate the storage life of the cabin. The activation energy of thermal protection material under different failure modes is calculated and the weak links based on its performance parameters are identified. The cabin’s acceleration factor and acceleration storage test time are calculated and the storage life is verified. By identifying the storage weaknesses of thermal protection materials,an accelerated storage test is carried out to verify storage life of the cabin.
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