| 航空发动机设计体系的建设与发展 |
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| 引用本文： | 王永明,卫刚,兰发祥,黄顺洲. 航空发动机设计体系的建设与发展[J]. 燃气涡轮试验与研究, 2007, 20(3): 1-7 |
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| 作者姓名： | 王永明 卫刚 兰发祥 黄顺洲 |
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| 作者单位： | 中国燃气涡轮研究院,四川,成都,610500 |
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| 摘 要： | 本文对航空发动机设计体系的定义、基本内涵、作用和发展特点进行了探讨,分析了航空发动机设计体系的基本要求,提出了设计体系建设、发展的方法及途径,对设计体系的整体规划、关键技术分解、设计体系集成、发展等问题进行了初步探讨。
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| 关 键 词： | 航空发动机 技术验证 设计体系 |
| 文章编号： | 1672-2620（2007）03-0001-07 |
| 修稿时间： | 2007-07-26 |
Constructing and Developing of Aeroengine Design System |
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| WANG Yong-ming,WEI Gang,LAN Fa-xiang,HUANG Shun-zhou. Constructing and Developing of Aeroengine Design System[J]. Gas Turbine Experiment and Research, 2007, 20(3): 1-7 |
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| Authors: | WANG Yong-ming WEI Gang LAN Fa-xiang HUANG Shun-zhou |
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| Affiliation: | China Gas Turbine Establishment, Chengdu 610500, China |
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| Abstract: | In this paper,the definitions,basic connotation,effects and developing characters of aeroengine design system were discussed.We analyzed the basic demands of aeroengine design system,gave the methods of constructing and developing the design system,and discussed the whole layout,the decomposing of key technology,the integration and development of design system primarily. |
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| Keywords: | aeroengine technology validation design system |
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