Open AccessResearch Progress of Continuous Fiber Reinforced Ceramic Matrix Composite in Hot Section Components of Aero engine
Author(s) -
Mingwei Chen,
Hai Qiu,
Weihua Xie,
Bingyu Zhang,
Shanhua Liu,
Wendong Luo,
Xin Ma
Publication year - 2019
Publication title -
iop conference series. materials science and engineering
Language(s) - English
Resource type - Journals
eISSN - 1757-899X
pISSN - 1757-8981
DOI - 10.1088/1757-899x/678/1/012043
Subject(s) - reinforced carbon–carbon , section (typography) , ceramic matrix composite , materials science , aero engine , composite material , composite number , turbine blade , ceramic , nozzle , alloy , matrix (chemical analysis) , turbine , mechanical engineering , computer science , engineering , operating system
Continuous fiber reinforced ceramic matrix composite (CFRC CMC) possessed low density, high temperature resistance, high strength and high toughness, which have been identified as a key and promising military material for replacing the traditional super alloy. CFRC CMC had been used in some hot section components, such as nozzle, combustor and turbine stator on M88-2, F100-PW-229, CFM56-5B, F-135, GEnx, LEAP-X and other aeroengines. Manufacturing technologies of CFRC CMC were thought as the commanding elevation for hot section components of aeroengines, and therefore much attention was given in Europe, America, Russia and other developed countries and regions. The evaluation and application of CFRC CMC were introduced in detail. Further, the challenge and tendency in the future were also put forward in this study.