高贵福,王刚,孙建亮,任杰安,王圣刚,周春燕,赵保平.飞行器环境适应性设计方法研究与实践[J].装备环境工程,2017,14(6):49-54. GAO Gui-fu,WANG Gang,SUN Jian-liang,REN Jie-an,WANG Sheng-gang,ZHOU Chun-yan,ZHAO Bao-ping.Research and Practice of Environmental Worthiness Design of Flying Object[J].Equipment Environmental Engineering,2017,14(6):49-54.
飞行器环境适应性设计方法研究与实践
Research and Practice of Environmental Worthiness Design of Flying Object
投稿时间:2017-04-22  修订日期:2017-06-15
DOI:10.7643/ issn.1672-9242.2017.06.011
中文关键词:  飞行器  环境适应性设计  诱发环境
英文关键词:flying object  environmental worthiness design  induced environmental
基金项目:
作者单位
高贵福 北京机电工程研究所,北京 100074 
王刚 北京机电工程研究所,北京 100074 
孙建亮 北京机电工程研究所,北京 100074 
任杰安 北京机电工程研究所,北京 100074 
王圣刚 北京机电工程研究所,北京 100074 
周春燕 北京机电工程研究所,北京 100074 
赵保平 北京机电工程研究所,北京 100074 
AuthorInstitution
GAO Gui-fu Beijing Mechanical-electronic Engineering Institute, Beijing 100074, China 
WANG Gang Beijing Mechanical-electronic Engineering Institute, Beijing 100074, China 
SUN Jian-liang Beijing Mechanical-electronic Engineering Institute, Beijing 100074, China 
REN Jie-an Beijing Mechanical-electronic Engineering Institute, Beijing 100074, China 
WANG Sheng-gang Beijing Mechanical-electronic Engineering Institute, Beijing 100074, China 
ZHOU Chun-yan Beijing Mechanical-electronic Engineering Institute, Beijing 100074, China 
ZHAO Bao-ping Beijing Mechanical-electronic Engineering Institute, Beijing 100074, China 
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中文摘要:
      目的 针对飞行器环境适应性设计不足的现状提出对策。方法 分析飞行器环境适应性设计的特点和当前存在的不足,以某电气设备为对象开展应用研究。结果 提出环境适应性设计工作内容、工作流程、设计原则和技术手段等方面的对策。环境适应性设计应采用环境仿真和验证试验相结合的手段,并逐步形成环境适应性设计准则。结论 飞行器环境适应性设计应采用系统工程的思路,覆盖产品层级、环境因素和研制阶段。技术手段方面应大力推进环境仿真研究和应用,建立产品环境适应性设计规范。
英文摘要:
      Objective To propose countermeasures for insufficient environmental worthiness design of flying object. Methods Certain electrical equipment was researched based on features and current shortages in environmental worthiness design of flying object. Results Countermeasures on work contents, procedures, principles and means of environmental worthiness design were given, and the work was performed by means of environmental simulation integrated with environmental test. And the design criterions were carried out gradually. Conclusion Environmental worthiness design of flying object must be performed in the thought of system engineering, and it must be involved in different product levels, environmental factors and development phases. With regard to technical means, great efforts must be made on environmental simulation study and application. And the design standards for environmental worthiness design should be made.
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