航改燃气轮机总体性能与排气装置的一体化设计 |
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引用本文: | 周亚峰,谢业平,李泳凡.航改燃气轮机总体性能与排气装置的一体化设计[J].航空发动机,2008,34(1):7-9,45. |
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作者姓名: | 周亚峰 谢业平 李泳凡 |
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作者单位: | 沈阳发动机设计研究所,沈阳,110015 |
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摘 要: | 分析了舰用航改燃气轮机的设计特点,提出了在总体性能设计中采用排气装置一体化设计技术的合理性;对某型舰用燃气轮机排气装置的一体化设计进行的理论分析表明:排气装置达到了一体化的设计目的,燃气轮机整体性能得到了最佳的性能匹配。
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关 键 词: | 航改燃气轮机 性能计算 排气装置 引射器 |
修稿时间: | 2007年5月30日 |
Integrated Design of Aero-Derivative Gas Turbine and Exhaust System |
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Authors: | ZHOU Ya-feng XIE Ye-ping LI Yong-fan |
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Abstract: | The design features of the aero-derived marine gas turbine were analyzed and the rationality of integrated design technology of exhaust system adopted in the overall performance design was presented.The theoretical analysis of integrated design of a marine gas turbine exhaust system shows that the purpose of the integrated design of the exhaust system is achieved and the optimum performance matching is obtained in the gas turbine overall performance. |
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Keywords: | aero-derived gas turbine performance calculation exhaust system injector |
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