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Design, preparation and properties of non-oxide CMCs for application in engines and nuclear reactors: an overview

机译:用于发动机和核反应堆的非氧化物CMC的设计,制备和性能:概述

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摘要

SiC-based ceramic matrix composites, consisting of carbon or SiC fibers embedded in a SiC-matrix, are tough ceramics when the fiber/matrix bonding is properly optimized through the use of a thin interphase. They are fabricated according to different processing routes (chemical vapor infiltration, polymer impregnation/pyrolysis, liquid silicon infiltration or slurry impregnation/hot pressing) each of them displaying advantages and drawbacks which are briefly discussed. SiC-matrix composites are highly tailor-able materials in terms of fiber-type (carbon fibers of SiC-based fibers such as Si-C-O, SiC+C or quasi-stoichiometric SiC reinforcements), interphase (pyrocarbon or hexagonal BN. as well as (PyC-SiC)_n or (BN-SiC)_n multilayered interphases), matrix (simple SiC or matrices with improved oxidation resistance, such as self-healing matrices) and coatings (SiC or engineered multilayered coatings). The potential of SiC-matrix composites for application in advanced aerojet engines (after-burner hot section), gas turbine of electrical power/steam cogeneration (combustion chamber) and inner wall of the plasma chamber of nuclear fusion reaction, all of them corresponding to very severe conditions is discussed.
机译:SiC基陶瓷基复合材料由嵌入SiC基质中的碳或SiC纤维组成,当通过使用稀薄的相间适当地优化纤维/基质键合时,它们是坚韧的陶瓷。它们是根据不同的加工路线(化学气相渗透,聚合物浸渍/热解,液体硅渗透或浆料浸渍/热压)制造的,它们各自都有优点和缺点,下面将简要讨论。 SiC基复合材料在纤维类型(SiC基纤维的碳纤维,例如Si-CO,SiC + C或准化学计量SiC增强材料),相间(热碳或六角BN)方面都是高度可定制的材料。如(PyC-SiC)_n或(BN-SiC)_n多层中间相),基体(简单SiC或具有改进的抗氧化性的基体,例如自修复基体)和涂层(SiC或工程多层涂层)。 SiC基复合材料在先进航空发动机(后燃烧器热段),电力/蒸汽热电联产燃气轮机(燃烧室)和等离子室内壁核聚变反应中的应用潜力,它们全部对应于讨论了非常恶劣的条件。

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