材料工程2012,Issue(8) :92-100.

INCONEL 718(GH4169)高温合金的发展与工艺

Review of INCONEL 718 Alloy: Its History,Properties, Processing and Developing Substitutes

齐欢
材料工程2012,Issue(8) :92-100.

INCONEL 718(GH4169)高温合金的发展与工艺

Review of INCONEL 718 Alloy: Its History,Properties, Processing and Developing Substitutes

齐欢1
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作者信息

  • 1. 上海交通大学密西根学院,上海200240
  • 折叠

摘要

INCONEL 718合金(IN718)自从20世纪60年代初在美国的INCO Huntington Alloys(现为Special Metals Co.)被发明并应用于涡轮零部件制造后,已成为航空发动机历史上应用最为广泛的镍基高温合金材料.现代飞机发动机上超过30%(质量分数)的关键零部件由718合金制成.本文回顾了718合金在航空发动机上的应用历史,对该合金的基本力学性能、高温稳定性,以及目前国外应用的铸、锻制造工艺现状做了综述.对国外正在研究的新型IN718衍生替代合金的发展现状进行了介绍.

Abstract

Since its invention and initial application in gas turbine components in the early 60's of 20th century at INCO Huntington Alloys (now called Special Metals Co. ), INCONEL 718 alloy (IN718) has become the most widely used nickel based superalloy in the aircraft engine industry. It was used in many critical aircraft engine components, accounting for over 30% of the total finished component mass of a modern aircraft engine. This article reviews IN718 alloy development history, its mechanical properties, long-term thermal stabilities, industrial processing methods, and current developing substitute alloys for enhanced thermal stability.

关键词

INCONEL/718/镍基合金/718Plus/航空发动机

Key words

INCONEL 718/nickel-based superalloy/718Plus/aircraft engine

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出版年

2012
材料工程
中国航发北京航空材料研究院

材料工程

CSTPCDCSCD北大核心EI
影响因子:0.78
ISSN:1001-4381
被引量90
参考文献量23
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