不同C/C复合材料飞机刹车盘基本性能的对比分析
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Release time:2021-07-17 DOI number:10.13801/j.cnki.fhclxb.2003.03.008 Affiliation of Author(s):中南大学 Journal:复合材料学报 Key Words:C/C复合材料;显微组织;摩擦磨损性能 Abstract:通过对比分析Dunlop、B.F.Goodrich、Missier、Bendix和中南大学粉末冶金研究所制备的几种炭/炭复合材料的显微组织、石墨化度、导热系数、洛氏硬度、抗压、抗弯、层间剪切强度、摩擦磨损性能后,得出如下结论:C/C复合材料作为一种性能优良的制动材料,必须具有合理的炭纤维骨架结构,一定比例的粗糙层气相沉积炭结构,较高的石墨化度和垂直摩擦面方向上的导热系数;我国具有自己知识产权的C/C复合材料飞机刹车盘的研制工作已取得了较大的进展和突破,其各项性能指标与国外同类产品性能相当 Discipline:Engineering First-Level Discipline:Materials Science and Engineering Document Type:J Volume:20 Issue:3 Page Number:35-40 Translation or Not:no Date of Publication:2003-06-16 Included Journals:EI -
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