Development of CMC vane for gas turbine engine

被引：0

作者：

Watanabe, K ^{[1
]}

Suzumura, N ^{[1
]}

Nakamura, T ^{[1
]}

Murata, H ^{[1
]}

Araki, T ^{[1
]}

Natsumura, T ^{[1
]}

机构：

[1] Ishikawajima Harima Heavy Ind Co Ltd, 3-5-1 Mukodai Cho, Tokyo 1888555, Japan

来源：

27TH INTERNATIONAL COCOA BEACH CONFERENCE ON ADVANCED CERAMICS AND COMPOSITES: B | 2003年 / 24卷 / 04期

关键词：

D O I：

暂无

中图分类号：

TQ174 [陶瓷工业]; TB3 [工程材料学];

学科分类号：

0805 ; 080502 ;

摘要：

CMCs (Ceramic Matrix Composites) are attractive material for structural component applications in gas turbine engines because of their excellent high temperature properties and lower specific weight by comparison with Ni base super alloy. In ESPR (Research and Development of Environmentally. Compatible Propulsion System for Next-Generation Supersonic Transport project), turbine stator vane was selected to be applied SiC/SiC (SiC fiber reinforced SiC). In this study, development of fabrication process and improvement of material process has been carried out. In addition, vane element evaluation tests using trial vane product was accomplished.

引用

页码：599 / +

页数：2