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Failure assessment of the first stage high-pressure turbine blades in an aero-engine turbine

  • Published:2017-05-26 Issue:12 Volume:40 Page:2092-2106
  • ISSN:8756-758X
  • Container-title:Fatigue & Fracture of Engineering Materials & Structures
  • language:en
  • Short-container-title:Fatigue Fract Engng Mater Struct

Author:

Shi D.12,Wang C.1,Yang X.123ORCID,Li S.1

Affiliation:

1. School of Energy and Power Engineering; Beihang University; Beijing 100191 China

2. Collaborative Innovation Center of Advanced Aero-Engine; Beijing 100191 China

3. School of Aircraft Engineering; Nanchang Hangkong University; Nanchang 330063 China

Funder

National Basic Research Program of China

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference51 articles.

1. Investigation progress on aeroengine structural integrity;Li;Aeroengine,2014

2. Li , A. 2013 Research on key techniques of aeroengine wear fault intelligent diagnosis

3. Failure of a low pressure turbine rotor blade of an aeroengine;Bhaumik;Eng. Fail. Anal.,2006

4. Failure analysis of gas turbine last stage bucket made of Udimet 500 superalloy;Mazur;J. Fail. Anal. Prev.,2002

5. Applications of fractography for aircraft defect causal analysis;Conor;Fatigue Fract. Eng. Mater. Struct.,2012

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