Failure due to structural degradation in turbine blades

Engineering Failure Analysis

Volumn 13, Issue 3 SPEC. ISS., 2006, Pages 452-463

  Ejaz, Noveed ^a   Tauqir, A ^a  

^a Dr A Q Khan Research Laboratories   (Pakistan)

Author keywords

Hot corrosion; Intergranular corrosion; Microstructural degradation; Turbine blade; U 500

Indexed keywords

CHEMICAL ANALYSIS; CORROSION; CRACK INITIATION; CRACKS; DEGRADATION; FATIGUE OF MATERIALS; FRACTURE; GRAIN BOUNDARIES; HIGH PRESSURE TURBOMACHINERY; HIGH TEMPERATURE EFFECTS; OXIDATION; TURBOMACHINE BLADES;

HOT CORROSION; INTERGRANULAR CORROSION; MICROSTRUCTURAL DEGRADATION; TURBINE BLADE; UDIMET 500;

FAILURE ANALYSIS;

FAILURE ANALYSIS;

EID: 28344435497     PISSN: 13506307     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.engfailanal.2004.12.041     Document Type: Article

References (5)

1. Willium F. Smith Structure and properties of engineering material 1981 McGraw Hill, Inc. USA p. 47
2. D. Coursourdis P. Felix H. Fischmeister Y. Lindblom M.O. Speidel Creep and structural stability of high temperature materials, high temperature alloys for gas turbines 1978 Applied Science Publisher Ltd. UK 313
3. (a) Joseph R. Davis, editor. Fractography, metal handbook, vol. 12, USA: ASM, March 1987, p. 126, 142.
4. (b) George F. Vander Voort, Carpenter Technology Corporation.
5. P.H. Floyd W. Wallace J.-P.A. Immarigeon Rejuvenation of properties in turbine engine hot section components by HIPing 1981 The Metals Society p. 97-102