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空天防御  2024, Vol. 7 Issue (6): 38-45    
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  研究进展 本期目录 | 过刊浏览 | 高级检索 |
高声速飞行器用高温钛合金研究进展与发展趋势
陈志勇
中国科学院金属研究所,辽宁 沈阳 110016
Research and Development of High-Temperature Titanium Alloys for Hypersonic Aircraft
CHEN Zhiyong
Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, Liaoning, China
全文: PDF(1510 KB)  
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摘要 高温钛合金在高声速飞行器领域具有广阔的应用前景。高温钛合金能够提高高声速飞行器在极端飞行环境下的性能和可靠性,是实现其更高速度和更远飞行距离的理想耐高温轻质金属材料。针对我国高声速飞行器中热结构的服役工况特点,从高温钛合金特性出发,梳理高温钛合金的国内外发展现状,重点阐述我国高声速飞行器用550~650 ℃高温钛合金的自主研发和应用情况;针对高声速飞行器用高温钛合金面临的更高使用温度需求,介绍一种700~750 ℃新型高温钛合金Ti750S 的研发现状,并展望未来高声速飞行器用高温钛合金的研发方向和应用前景。
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关键词 高声速飞行器高温钛合金轻质结构Ti750S 钛合金    
Abstract:High-temperature titanium alloys allow broad application prospects in hypersonic aircraft. They have ideal lightweight and heat-resistant metallic materials, enhancing the performance and reliability of hypersonic aircraft in extreme flight environments, thus achieving higher speeds and longer flight distances. Considering the services of thermal structures in China’s hypersonic aircraft, starting from the characteristics of high-temperature titanium alloys, this paper has reviewed the latest development status of high-temperature titanium alloys domestically and abroad. It focused on introducing China’s independent research, development and application of 550-650 °C high-temperature titanium alloys. To achieve higher operating temperature requirements, the research and development of a new 700-750 °C high-temperature titanium alloy Ti750S was proposed, and the respective application directions and prospects of high-temperature titanium alloys for future hypersonic aircraft were prospected.
Key wordshypersonic aircraft    high-temperature titanium alloy    lightweight structure    Ti750S titanium alloy
收稿日期: 2024-05-16      出版日期: 2025-01-16
ZTFLH:  TJ 760. 4  
基金资助:国家部委基础科研计划项目(JCKY2021204A004)
作者简介: 陈志勇(1977—),男,博士,研究员。
引用本文:   
陈志勇. 高声速飞行器用高温钛合金研究进展与发展趋势[J]. 空天防御, 2024, 7(6): 38-45.
CHEN Zhiyong. Research and Development of High-Temperature Titanium Alloys for Hypersonic Aircraft. Air & Space Defense, 2024, 7(6): 38-45.
链接本文:  
https://www.qk.sjtu.edu.cn/ktfy/CN/      或      https://www.qk.sjtu.edu.cn/ktfy/CN/Y2024/V7/I6/38

参考文献
[1] 陈雪, 朱龙宇, 薛钦洋, 王柯翔, 韩志林, 罗楚养. 防空导弹用树脂基复合材料研究进展[J]. 空天防御, 2024, 7(6): 76-95.
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