| 层板发汗冷却在液体火箭发动机中的应用与发展综述 |
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| 引用本文： | 张峰,刘伟强.层板发汗冷却在液体火箭发动机中的应用与发展综述[J].火箭推进,2007,33(6):43-48. |
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| 作者姓名： | 张峰 刘伟强 |
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| 作者单位： | 国防科技大学航天与材料工程学院,湖南,长沙,410073 |
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| 摘 要： | 较系统地介绍了应用于液体火箭发动机推力室冷却的层板技术,指出了层板发汗冷却的技术优势。介绍了一内壁全部由层板构成的液体火箭发动机推力室结构及其层板发汗冷却单元的设计和加工工艺问题。总结了国内外关于层板发汗在火箭推力室冷却方面的研究进展,并简要论述了其应用前景。
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| 关 键 词： | 层板 发汗冷却 液体火箭发动机 推力室 |
| 收稿时间： | 2006-10-30 |
| 修稿时间： | 2007-10-18 |
Application and development of platelet transpiration cooling technology in LRE |
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| Zhang Feng,Liu Weiqiang.Application and development of platelet transpiration cooling technology in LRE[J].Journal of Rocket Propulsion,2007,33(6):43-48. |
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| Authors: | Zhang Feng Liu Weiqiang |
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| Abstract: | Platelet technology and its advantages are introduced in detail. A thrust chamber structure with whole inner wall consisting of platelets and its manufacture process are presented. Progresses in platelet technology applications to LRE's thrust chamber both in domestic and abroad are summarized. Its future application prospect is discussed. |
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| Keywords: | platelet transpiration cooling LRE thrust chamber |
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