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 Recent Development of New High Temperature Titanium Alloys for High Thrust Weight Ratio Aero Engines(PDF)

MATERIALS CHINA[ISSN:1674-3962/CN:61-1473/TG]

Issue:
2011年第6期
Page:
21-27
Research Field:
特约研究论文
Publishing date:

Info

Title:
 Recent Development of New High Temperature Titanium Alloys for High Thrust Weight Ratio Aero Engines
Author(s):
 HUANG Xu LI Zhenxi HUANG Hao
 Beijing Institute of Aeronautical Materials
Keywords:
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CLC:

PACS:
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DOI:
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DocumentCode:

Abstract:
    Development status of high temperature titanium alloys of aero engine in China was reviewed.Aimed at demands of low density and heat resistant structure materials for high thrust to weight ratio aero engine,recent developments and applications of TiAl alloys and SiC fiber reinforced titanium matrix composites were introduced....

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Last Update: 2011-08-09