On the design and structural analysis of jet engine fan blade structures

被引：116
作者：
Amoo, Leye M. [1 ]
机构：
[1] United Technol Corp UTC Pratt & Whitney, Aeromech Fan Blades, CSE, E Hartford, CT 06108 USA
来源：
PROGRESS IN AEROSPACE SCIENCES | 2013年 / 60卷
关键词：
Fan blade; Jet engine; Structures-design; Aerodynamics; Flutter; FEA;
D O I：
10.1016/j.paerosci.2012.08.002
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Progress in the design and structural analysis of commercial jet engine fan blades is reviewed and presented. This article is motivated by the key role fan blades play in the performance of advanced gas turbine jet engines. The fundamentals of the associated physics are emphasized. Recent developments and advancements have led to an increase and improvement in fan blade structural durability, stability and reliability. This article is intended as a high level review of the fan blade environment and current state of structural design to aid further research in developing new and innovative fan blade technologies. (C) 2012 Elsevier Ltd. All rights reserved.
引用
收藏
页码：1 / 11
页数：11
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