Volume 26 Issue 3
Aug.  2012
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Article Contents
ZHANG Li-tong, CHENG Lai-fei, XU Yong-dong, LIU Yong-sheng, ZENG Qing-feng, DONG Ning, LUAN Xin-gang. Progress on Self-Healing Silicon Carbide Ceramic Matrix Composites and Its Applications[J]. Journal of Aeronautical Materials, 2006, 26(3): 226-232.
Citation: ZHANG Li-tong, CHENG Lai-fei, XU Yong-dong, LIU Yong-sheng, ZENG Qing-feng, DONG Ning, LUAN Xin-gang. Progress on Self-Healing Silicon Carbide Ceramic Matrix Composites and Its Applications[J]. Journal of Aeronautical Materials, 2006, 26(3): 226-232.

Progress on Self-Healing Silicon Carbide Ceramic Matrix Composites and Its Applications

  • Received Date: 2006-02-20
  • Rev Recd Date: 2006-03-20
  • Publish Date: 2006-06-01
  • Continuous fiber reinforced silicon carbide ceramic matrix composites were developing towards possessing self-healing properties for the need of high thrust mass ratio aerospace-engine working in thermal oxidizing environment.The microstructure and properties of a self-healing silicon carbide matrix composite were introduced.The mechanism of toughness and stiffness of the composite and the self-healing behaviors were commented.The application progress of self-healing silicon carbide component was summarized.Manufacturing method and technique feature were reviewed.Multi-component and multi-layer microstructure was the key point for this composite possessing self-healing and toughing properties,and oxidation resistant system which exhausted O2 and sealed crack in each layer.This self-healing silicon carbide matrix composite coule not only meet the requirements of for aerospace-engine service but decreased weight remarkably,increased thrust-weight ratio in return.


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  • [1] OHNABE H,Masaki S,Onozuka M,et al.Potential application of ceramic matrix composites to aero-engine components[J].Composites:Part A,1999,30:489-496.
    [2] 张立同,成来飞,徐永东.新型碳化硅陶瓷基复合材料的研究进展[J].航空制造技术,2003(1):23-32.
    [3] AKASHI T,TAKESHI N,KOOUN T.Research of CMC application to tube components[J].IHI Engineering Review,2005,38 (2):58-63.
    [4] XU Y D,ZHANG L T,CHENG L F,et al.Microstructure and mechanical properties of three-dimensional carbon/silicon carbide composites fabricated by chemical vapor infiltration[J].Carbon,1998,36 (7-8):1051-1056.
    [5] CHENG L F,XU Y D,ZHANG L T,et al.Oxidation and defect control of CVD SiC coating on three-dimensional C/SiC composites[J].Carbon,2002,40 (12):2229-2234.
    [6] YIN X W,CHENG L F,ZHANG L T,et al.Microstructure and oxidation resistance of carbon/ silicon carbide composites infiltrated with chromium silicide[J].Materials Science and Engineering A,2000,29 (1-2):89-94.
    [7] CHENG L F,XU Y D,ZHANG L T,et al.Effect of glass sealing on the oxidation behavior of three dimensional C/SiC composites in air[J].Carbon,2001,39 (8):1127-1133.
    [8] WU S J,CHENG L F,ZHANG L T,et al.Oxidation behavior of 2D C/SiC with a multi-layer CVD SiC coating[J].Surface and Coatings Technology,2005,In Press,Available online.
    [9] TSOU H T,KOWBEL W.A hybrid PACVD SiC/CVD-Si3N4/SiC multi-layer coating for oxidation protection of composites[J].Carbon,1995,33 (9):1279-1288.
    [10] CAMERON G C,JAMES E.Oxidative and hydrolytic stability of boron nitride-a new approach to improving the oxidation resistance of carbonaceous structures[J].Carbon,1995,33(4):389-395
    [11] REBILLAT F,GUETTE A,ESPITALIER L.Oxidation resistance of SiC/SiC micro and mini-composites with a highly crystallized BN interphase[J].Journal of the European Ceramic Society,1998,18:1809-1819.
    [12] JAMES M S,LARRY P Z.Performance of four ceramic matrix composite divergent tlap inserts following ground testing on an F110 turbofan engine[J].Journal of the American Ceramic Society,2000,83 (7):1727-1738.
    [13] KIYOSHI S,HIROKI M,OSAMU F,et al.Developing interfacial carbon-boron-silicon coatings for silicon nitride-fiber-reinforced composites for improved oxidation resistance[J].Journal of the American Ceramic Society,2002,85(7):1815-1822.
    [14] SCHULTE J F,SCHMIDT J,TAMME R,et al.Oxidation behaviour of C/C-SiC coated with SiC-B4C-SiC-cordierite oxidation protection system[J].Materials Science and Engineering A,2004,386 (1-2):428-434.
    [15] ASLAIN R,PAILLER R,BOURRAT X,et al.Synthesis of highly tailored ceramic matrix composites by pressure-pulsed CVI[J].Solid State Ionics,2001,141-142:541-548.
    [16] AGUCHI T,NAZAWA T,IAGAWA N.Fabrication of advanced SiC fiber/F-CVI SiC matrix composites with SiC/C multi-layer interphase[J].Journal of Nuclear Materials,2004,329-333:572-576.
    [17] IRICELLE J P,GOURSAT P,BAHLOUL H D.Oxidation behaviour of a multi-layer ceramic-matrix composite (SiC)f/C/(Si-B-C)m[J].Composites Science and Technology,2001,61:607-614.
    [18] ASLAIN R.Design,preparation and properties of non-oxide CMCs for application in engines and nuclear reactors:an overview[J].Composites Science and Technology,2004,64:155-170.
    [19] AUMOUROUX F,BERTRAND S,PAILLER R,et al.Oxidation-resistant carbon-fiber-reinforced ceramic-matrix composites[J].Composites Science and Technology,1999,59:1073-1085.
    [20] ERTRAND S.Lifetime improvement in SiC/SiC composites with nanosequenced (PyC/SiC)n and (BN/SiC)n interphases[D].Univ.Bordeaux 1,1998.No.1927.
    [21] CHMIDT S,BEYER S,KNABE H,et al.Advanced cramic matrix composite materials for current and future propulsion technology applications[J].Acta Astronautica,2004,55:409-420.
    [22] ASLAIN R,LAMON J,PAILLER R,et al.Micro/minicomposites:a useful approach to the design and development of nonoxide CMCs[J].Composites:Part A,1999,30:537-547.
    [23] 长瑞,郝元恺.陶瓷基复合材料-原理、工艺、性能与设计[M].长沙:国防科技大学出版社,2001.
    [24] HRISTIN F.A global approach to fiber nD architectures and self-sealing matrices-from research to production[A].5th International Conference on High:Temperature Ceramic Matrix Composites[C].2004.477-483.
    [25] HAO J C,WESTBROOK J H.Ultrahigh-temperature materials for jet engines[J].MRS Bulletin,2003,622-630.
    [26] ASLAIN R,CHRISTIN F.SiC-matrix composite materials for advanced jet engines[J].MRS Bulletin,2003,654-658.
    [27] NASLAIN R,GUETTE A,REBILLAT F,et al.Boron-bearing species in ceramic matrix composites for long-term aerospace applications[J].Journal of Solid State Chemistry,2004,177:449-456.
    [28] IMMEL J,MIRIYALA N,PRICE J,et al.Evaluation of CFCC liners with EBC after field testing in a gas turbine[J].Journal of the European Ceramic Society,2002,22:2769-2775.
    [29] ARRY Z,GEORGE R,PATRICK S.Ceramic matrix composites for aerospace turbine engine exhaust nozzles[A].5th International Conference on High-Temperature Ceramic Matrix Composites[C].2004.491-498.
    [30] ICHAEL V,ANTHONY C,ROBINSON R C.Characterization of ceramic matrix composite vane sub-elements subjected to rig testing in a gas turbine environment[A].5th International Conference on High-Temperature Ceramic Matrix Composites[C].2004.499-505.
    [31] HRISTIN F.Design,fabrication and application of C/C,C/SiC and SiC/SiC composites[A].4th International Conference on High-Temperature Ceramic Matrix Composites[C].2001.731-743.
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