| R0110重型燃气轮机的研制 |
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| 引用本文： | 崔荣繁,陈克杰,郭宝亭.R0110重型燃气轮机的研制[J].航空发动机,2011,37(3):8-11. |
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| 作者姓名： | 崔荣繁 陈克杰 郭宝亭 |
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| 作者单位： | 中航工业沈阳黎明航空发动机集团有限责任公司,沈阳,110015 |
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| 摘 要： | 通过阐述R0110重型燃气轮机的研制过程,总结了该燃气轮机的结构和性能特点。通过对各主要部件的设计、分析计算、试验研究,积累了大量的设计、试验和调试经验,解决了研发过程中所遇到的难点,初步掌握了重型燃气轮机研发的关键技术,基本建立了E＋级重型燃气轮机研发设计平台,为重型燃气轮机的系列化发展以及合成气燃气轮机研制奠定了坚实的基础。
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| 关 键 词： | R0110重型燃气轮机 产品研制 压气机 燃烧室 透平 |
Development of R0110 Heavy-duty Gas Turbine |
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| Authors: | CUI Rong-fan CHEN Ke-jie GUO Bao-ting |
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| Institution: | CUI Rong-fan,CHEN Ke-jie,GUO Bao-ting(AVIC Shenyang Liming Aero Engine(Gruop) Ltd.,Shenyang 110043,China) |
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| Abstract: | The characteristics of structure and performance were summarized by expatiating the development of R0110 heavy-duty gas turbine.The plenty of experience on design,test and adjusment for every main components was gathered by the design,analysis and experiment research.The difficulty was solved during the development.The key technologies for heavy-duty gas turbine were mastered preliminary.The design platform of E+ class heavy-duty gas turbine was built.It lay a good foundation for the derivative development ... |
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| Keywords: | R0110 heavy-duty gas turbine product development compressor combustor turbine |
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