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综述了可用于2 200~3 000℃高温环境下难熔金属、陶瓷及碳/碳复合材料等研究进展和各种材料的优缺点;介绍了提高材料性能所采取的方法,指出了耐超高温材料研究的发展方向.

参考文献

[1] Kameleshwar Upahya;Yang J M;Hoffman W P .Materials for ultrahigh temperature structural application[J].Journal of the American Ceramic Society,1997,76(01):51-56.
[2] 宋桂明,孟庆昌,王玉金,周玉.TiC和ZrC颗粒增强钨基复合材料的烧蚀研究[J].固体火箭技术,2001(02):48-53.
[3] Sherman A;Tuffias R H;Kaplan R B .The properties and applications of rhenium produced by CVD[J].Journal of The Minerals,Metals & Materials Society,1991,20(07):20-23.
[4] Rosenbergq S D;Schoenman L .New generation of highperformance engines for spacecraft propulsion[J].Journal of Propulsion and Power,1994,10(01):40-46.
[5] 德K H;马图哈;丁道云.非铁合金的结构与性能[M].北京:科学出版社,1997:236-237.
[6] 萨姆索落夫Г B.难熔化合物手册[M].北京:中国工业出版社,1965:145-289.
[7] SHIMADA;Shiro Nakajima;Kenichiro Inagaki .MichioOxidation of single crystals of hafnium carbide in a temperature range of 600° to 900℃[J].Journal of the American Ceramic Society,1997,80:1749-1756.
[8] Bargeron C B;Benson R C;Jette A N;Phillips J E .Oxidation of hafnium carbide in the temperature range 1 400 ~2060℃[J].Journal of the American Ceramic Society,1993,76:1040-1046.
[9] Wang CR.;Yang JM.;Hoffman W. .Thermal stability of refractory carbide/boride composites[J].Materials Chemistry and Physics,2002(3):272-281.
[10] Courtright E L;Prater J T;Holcomb G R;Pierre St G R,Rapp R A .Oxidation of hafnium carbide and hafnium carbide with additions of tantalum and praseodymium[J].Oxidation of Metals,1991,36:423-437.
[11] Wunder V.;Wegner A.;Emig G.;Arnold W.;Popovska N. .Multilayer coatings on CFC composites for high-temperature applications[J].Surface & Coatings Technology,1998(1/3):329-332.
[12] 张长瑞;郝元恺.陶瓷基复合材料[M].长沙:国防科技大学出版社,2001:321-322.
[13] Melendez-Martnez J J;Nguez-Rodrguez A D;Monteverde F B;Melandri B C, Portu G D .Characterisation and high temperature mechnical properties of zirconium boride-based materials[J].Journal of the European Ceramic Society,2002,22:2543-2549.
[14] Monteverde F;Bellosi A;Guicciardi S .Processing and properties of zirconium-diboride-based materials[J].Journal of the European Ceramic Society,2002,22:279-288.
[15] TrippWC;DavisHH;GrahamHC .Effect of an SiC addition on the oxidation of ZrB2[J].Ceramic Bulletin,1973,52:612-616.
[16] Opeka mark M;Talmy G;Zaykoski;James A .Mechnical, thermal and oxidation properties of refractory hafnium and zirconium compounds[J].Journal of the European Ceramic Society,1999,19:2405-2414.
[17] Cecilia Bartuli;Teodoro Valente;Mario Tului .Plasma spray desposition and high temperature characterization of ZrB2-SiC protective coatings[J].Surface and Coatings Technology,2002,155:260-273.
[18] 贺福;王茂章.碳纤维极其复合材料[M].北京:科学出版社,1997:254-255.
[19] 张伟刚;成会明;沈祖洪;周本濂 .炭材料抗氧化研究进展[J].炭素,1997,20(02):1-6.
[20] Weiming Lu;D.D.L.Chung .Oxidation protection of carbon materials by acid phosphate impregnation[J].Carbon: An International Journal Sponsored by the American Carbon Society,2002(8):1249-1254.
[21] F. Smeacetto;M. Salvo;M. Ferraris .Oxidation protective multilayer coatings for carbon-carbon composites[J].Carbon: An International Journal Sponsored by the American Carbon Society,2002(4):583-587.
[22] Federico Smeacetto;Monica Ferraris;Milena Salvo .Multilayer coating with self-sealing properties for carbon-carbon composites[J].Carbon: An International Journal Sponsored by the American Carbon Society,2003(11):2105-2111.
[23] Joshi A;Lee J S .Coatings with particulate dispersions for high temperature oxidation protection of carbon and C/C composites[J].Composites Part A:Applied Science and Manufacturing,1997,28:181-189.
[24] Soo-Jin Park;Min-Kang Seo .The effects of MoSi_2 on the oxidation behavior of carbon/carbon composites[J].Carbon: An International Journal Sponsored by the American Carbon Society,2001(8):1229-1235.
[25] J.D.Webster;M.E.Westwood;F.H.Hayes .Oxidation protection coatings for C/SiC based on Y_2SiO_5[J].Key engineering materials,1997(3):1641-1644.
[26] [J].Nippon Kinzoku Gakkaishi-Journal of the Japan Institute of Metals,1999,63:118-125.
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