直升机性能与RMS综合一体化设计的研究 |
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引用本文: | 陈圣斌,郝宗敏.直升机性能与RMS综合一体化设计的研究[J].直升机技术,2006(4). |
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作者姓名: | 陈圣斌 郝宗敏 |
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作者单位: | 中国直升机设计研究所,中国直升机设计研究所 景德镇,333001,景德镇,333001 |
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摘 要: | 本文根据以往直升机型号研制中存在的性能或图样设计与RMS分析设计脱节的问题,提出了实现性能与RMS综合一体化的技术方法,以期满足使用部门的要求,实现直升机RMS新的跨越。
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关 键 词: | 直升机 可靠性 维修性 保障性 |
Investigation About the Integrated Design of the Performance and RMS for the Helicopter |
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Authors: | CHEN Sheng-bin HAO Zong-min |
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Abstract: | In this paper based on the problems occurred in the helicopter design,integrated Design process of the performance and Reliability/Maintainability/Supportability (RMS) for the helicopter are provided to meet user requirement and to achieve great-step forward of the RMS. |
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Keywords: | helicopter reliability maintainability supportability |
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