Evolution of Rolls-Royce air-cooled turbine blades and feature analysis

被引:36
|
作者
Li Xu [1 ]
Sun Bo [1 ]
You Hongde [1 ]
Wang Lei [1 ]
机构
[1] AVIC Shenyang Engine Design & Res Inst, 1 Wanlian Rd, Shenyang 110015, Peoples R China
关键词
air-cooled turbine blade; turbine entry temperature; over-tip leakage; blade cooling;
D O I
10.1016/j.proeng.2014.12.689
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
During past few decades there has been significant increase in turbine entry temperature (TET) in order to improve gas turbine ability and efficiency, which represents a huge challenge to turbine blades. Rolls-Royce maintains world-leading technology and capability in gas turbines design and manufacture, this study mainly focuses on the evolution of air-cooled turbine blades fabricated by Rolls-Royce, which shows that turbine blade developments are increasingly dependent on the improvement of material science and blade cooling technology. Moreover, its unique blade tip designs which minimize over-tip leakage are also reviewed. Future developments to improve turbine blade ability and reliability including high temperature materials, blade cooling technology and CFD analyzing approach are discussed. (C) 2015 The Authors. Published by Elsevier Ltd.
引用
收藏
页码:1482 / 1491
页数:10
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