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[1]王凯,王东方,刘友强,等.变形高温合金在液体火箭发动机中的应用进展及展望[J].火箭推进,2024,50(01):57-66.[doi:10.3969/j.issn.1672-9374.2024.01.005]
　WANG Kai,WANG Dongfang,LIU Youqiang,et al.Application and prospect of wrought superalloy in liquid rocket engine[J].Journal of Rocket Propulsion,2024,50(01):57-66.[doi:10.3969/j.issn.1672-9374.2024.01.005]
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变形高温合金在液体火箭发动机中的应用进展及展望

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 50 期数: 2024年01期 页码: 57-66 栏目: 目次 出版日期: 2024-02-28
Title:
Application and prospect of wrought superalloy in liquid rocket engine
文章编号:
1672-9374(2024)01-0057-10
作者:
王凯; 王东方; 刘友强; 杨卫鹏; 张鹏
西安航天发动机有限公司,陕西 西安 710100
Author(s):
WANG Kai;  WANG Dongfang;  LIU Youqiang;  YANG Weipeng;  ZHANG Peng
Xi'an Space Engine Company Limited, Xi'an 710100, China
关键词:
变形高温合金;  液体火箭发动机;  推力室;  涡轮盘;  热加工技术
Keywords:
wrought superalloy;  liquid rocket engine;  thrust chamber;  turbine;  thermal processing technology
分类号:
V434
DOI:
10.3969/j.issn.1672-9374.2024.01.005
文献标志码:
A
摘要:
变形高温合金以其良好的耐高温、抗氧化、抗热腐蚀性能和较好的冷、热加工性,在液体火箭发动机推力室身部、涡轮壳体、涡轮转子等热端部件中得到了广泛的应用。通过查阅文献,综述了国内外变形高温合金及热加工技术发展现状、液体火箭发动机热端构件对高温合金性能需求、变形高温合金在国内外著名液体火箭发动机中的应用情况。结合液体火箭发动机可回收、高性能、轻量化、低成本的发展趋势,总结了变形高温合金在液体火箭发动机领域的主要发展趋势,包括研发针对液体火箭发动机服役工况的高温合金材料、改进热加工工艺,从而提升高温合金性能、降低高温合金构件制造成本; 研发和推广耐高温轻质金属间化合物、降低热端构件质量。
Abstract:
Wrought superalloy has been widely used in hot section parts such as liquid rocket engine thrust chambers, turbine shells and turbine rotors because of its excellent high-temperature resistance, oxidation resistance, thermal corrosion resistance as well as good cold and hot workability. The development status of wrought superalloy and thermal processing technology, the performance requirements of wrought superalloy for hot section components of liquid rocket engines, and the application of wrought superalloy in well-known liquid rocket engines are reviewed based on domestic and foreign literature. Based on the development trend of reusability, high performance, light weight and low cost of liquid rocket engines, the main development trends of wrought superalloy in liquid rocket engines have been summarized. To improve the performance of superalloy and reduce the cost of manufacturing by investigating superalloy materials aiming at service conditions of liquid rocket engines and improving the hot working processes. On the other hand, more attention can be paid to developing and promoting high-temperature resistant lightweight intermetallic compounds to reduce the weight of hot section components.

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备注/Memo

收稿日期:2023- 07- 17 修回日期:2023- 08- 23
基金项目:装备预先航天科技联合基金(6141B06310101)
作者简介:王凯(1991—),男,硕士,高级工程师,研究领域为液体火箭发动机制造。

更新日期/Last Update: 1900-01-01