材料科学
复合材料
航空发动机
陶瓷
复合数
围带
机械工程
陶瓷基复合材料
燃气轮机
涡轮叶片
喷气发动机
工程类
涡轮机
作者
Gregory S. Corman,Krishan L. Luthra
出处
期刊:Elsevier eBooks
[Elsevier BV]
日期:2017-02-20
卷期号:: 325-338
被引量:30
标识
DOI:10.1016/b978-0-12-803581-8.10001-3
摘要
The General Electric Company (GE) has been actively involved in the development of ceramic matrix composite (CMC) materials for use in industrial gas turbines and jet engines for over 40 years. The fruition of this work will come with the commercial introduction of the CFM leading edge aviation propulsion (LEAP) engine in 2016, which will include first stage high pressure turbine (HPT) shroud components made of GE’s prepreg melt infiltrated CMC material. This introduction will mark the world’s first commercial use of ceramic composite structural components in a gas turbine engine. This chapter will describe the history of the development of this material from early conception, process development, rig and engine test validations, to scale-up, and commercialization.
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