An investigation on the failed blades in a locomotive turbine

Engineering Failure Analysis

Volumn 14, Issue 7, 2007, Pages 1322-1328

  Xu, Xiaolei ^a   Yu, Zhiwei ^a  

^a DALIAN MARITIME UNIVERSITY   (China)

Author keywords

Multiple origin fatigue fracture; Over heat damage; Turbo blades

Indexed keywords

BENDING (DEFORMATION); CRACK INITIATION; EUTECTICS; FATIGUE OF MATERIALS; FRACTOGRAPHY; FRACTURE; GRAIN BOUNDARIES; MORPHOLOGY; NICKEL ALLOYS;

EUTECTIC MELTING; METALLOGRAPHIC MORPHOLOGY; MULTIPLE-ORIGIN FATIGUE FRACTURE; OVER-HEAT DAMAGE;

TURBOMACHINE BLADES;

BENDING (DEFORMATION); CRACK INITIATION; EUTECTICS; FATIGUE OF MATERIALS; FRACTOGRAPHY; FRACTURE; GRAIN BOUNDARIES; MORPHOLOGY; NICKEL ALLOYS; TURBOMACHINE BLADES;

EID: 34247557517     PISSN: 13506307     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.engfailanal.2006.11.041     Document Type: Article

References (2)

1. Mazur Z., Lina-Ramírez A., Juárez-Islas J.A., and Campos-Amezcua A. Failure analysis of a gas blade of Inconel 738LC alloy. Eng Fail Anal 12 3 (2005) 474-486
2. Carter T.J. Common failure in gas turbine blades. Eng Fail Anal 12 2 (2005) 237-247