HSR/EPM combustor materials development program

被引：206

作者：

Brewer, D ^{[1
]}

机构：

[1] NASA, Lewis Res Ctr, Cleveland, OH 44135 USA

来源：

MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 1999年 / 261卷 / 1-2期

关键词：

SiC/SiC ceramic matrix; combustor; thermal conductivity;

D O I：

10.1016/S0921-5093(98)01079-X

中图分类号：

TB3 [工程材料学];

学科分类号：

0805 ; 080502 ;

摘要：

Significant progress has been made developing a SiC/SiC ceramic matrix composite material for aeronautic combustor liner applications. Improvements in material processing technology have resulted in improved thermal conductivity and fatigue durability. A material characterization effort is underway to assess material behavior and direct material development efforts. The effects of the aggressive combustion environment continue to be a material system development challenge. (C) 1999 Published by Elsevier Science S.A. All rights reserved.

引用

页码：284 / 291

页数：8