| 核能航空发动机技术方案初探 |
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| 引用本文： | 张军峰,苏桂英.核能航空发动机技术方案初探[J].航空发动机,2010,36(3):45-49. |
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| 作者姓名： | 张军峰 苏桂英 |
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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： | 在对核反应堆、发动机和传热系统进行概要分析的基础上,初步探讨了核能航空发动机的技术方案。经分析认为:基于目前的技术水平,采用高温气冷堆、双回路传热系统的双布雷顿循环核能涡扇发动机相对可行。
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| 关 键 词： | 核能航空发动机 核反应堆 传热系统 |
Preliminary Investigation of Technical Proposals for Nuclear Aeroengine |
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| Authors: | ZHANG Jun-feng SU Gui-ying |
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| Institution: | (Shenyang Aeroengine Research Institute,Shenyang 110015,China) |
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| Abstract: | The preliminary investigatiaon of the technical proposals for nuclear aeroengine were presented based on the technological analyses of nuclear reactor,aeroengine and heat transfer system.The analysis results show that the technical proposals are relatively feasible which are the Bi-Brayton nuclear turbofan combined with high temperature gas cooled reactor and double-loop heat transfer system based on the present tecnology capability. |
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| Keywords: | nuclear aeroengine nuclear reactor heat transfer system |
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