%0 Journal Article
%T Comparative Study on the Friction and Wear Behaviors of C/C Composites and High-Strength Graphite at Elevated Temperature
C/C复合材料及高强石墨高温摩擦磨损性能对比研究
%A YI Mao-zhong
%A GE Yi-cheng
%A FENG Yi-lei
%A HUANG Qi-zhong
%A HUANG Bai-yun versity
%A Changsh
%A China
%A
易茂中
%A 葛毅成
%A 冯一雷
%A 黄启忠
%A 黄伯云
%J 摩擦学学报
%D 2004
%I
%X The friction and wear behaviors of two types of C/C composites with different structures sliding against W18Cr4V steel at elevated temperatures were investigated on an MG-2000 tester in a pin-on-disc configuration, using high-strength graphite which was supposed to be used to prepare the seal-ring of the main axis of an aviation engine as a control. The composition and morphology of the worn composite surface was analyzed by means of Raman spectroscopy and scanning electron microscopy. It was found that the C/C composite with a rough lamination and smooth lamination complex structure showed much better wear-resistance than the high-strength graphite at elevated temperature, thus it could be used as a promising candidate material to prepare the seal ring of the main axis of the aviation engine. The C/C composites were dominated by abrasive wear, adhesion wear, and oxidation wear, in the dry sliding against the steel at elevated temperatures.
%K C/C composites
%K high-strength graphite
%K turbo-engine
%K seal-ring
%K friction and wear behavior at elevated temperature
C/C复合材料
%K 高强石墨
%K 航空发动机
%K 密封材料
%K 高温摩擦磨损性能
%U http://www.alljournals.cn/get_abstract_url.aspx?pcid=6E709DC38FA1D09A4B578DD0906875B5B44D4D294832BB8E&cid=5D344E2AD54D14F8&jid=2F467A5C6371C830162AAA01D7DAD07A&aid=E60B2A69C7AEA5E2&yid=D0E58B75BFD8E51C&vid=B91E8C6D6FE990DB&iid=38B194292C032A66&sid=6CCE24D86D03D083&eid=1DF3F9D75A12D97B&journal_id=1004-0595&journal_name=摩擦学学报&referenced_num=12&reference_num=11