Rejuvenation of degraded first stage gas turbine nozzle by heat treatment

Journal of Alloys and Compounds

Volumn 497, Issue 1-2, 2010, Pages 360-368

  Zangeneh, Sh ^a   Farhangi, H ^a   Lashgari, H R ^a  

^a UNIVERSITY OF TEHRAN   (Iran)

Author keywords

Cobalt base superalloy; First stage gas turbine nozzle; Heat treatment

Indexed keywords

AGING TREATMENT; AIR COOLING; BASE MATERIAL; COBALT-BASE SUPERALLOY; COBALT-BASE SUPERALLOYS; CONTINUOUS FILMS; CONTROLLED PRECIPITATION; CRACK INITIATION AND PROPAGATION; FIRST-STAGE NOZZLES; GAS TURBINE NOZZLES; HEAT TREATMENT PROCESS; INITIAL VALUES; INTERNAL SERVICES; MICROSTRUCTURAL INVESTIGATION; MICROSTRUCTURE AND MECHANICAL PROPERTIES; PRECIPITATE COARSENING; PRIMARY CARBIDES; SECONDARY CARBIDES; SOLUTION TREATMENTS;

CARBIDES; COBALT; ENDOCRINOLOGY; GAS TURBINES; GASES; GRAIN BOUNDARIES; GRAIN SIZE AND SHAPE; HEAT TREATMENT; MECHANICAL PROPERTIES; METAL ANALYSIS; MICROSTRUCTURE; NOZZLES; SUPERALLOYS; TURBOMACHINERY;

PHASE INTERFACES;

EID: 77950960402     PISSN: 09258388     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jallcom.2010.03.070     Document Type: Article

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