Development of a new alloy for directional solidification of large industrial gas turbine blades

Proceedings of the International Symposium on Superalloys

Volumn , Issue , 2004, Pages 25-34

  Burgel R ^a   Grossmann, J ^b   Lusebrink O ^b   Mughrabi, H ^c   Pyczak, F ^c   Singer, R F ^c   Volek, A ^c  

^a UNIVERSITY OF APPLIED SCIENCES OSNABRÜCK   (Germany)

^b Doncasters Precision Castings Bochum GmbH   (United Kingdom)

^c UNIVERSITY OF ERLANGEN NUREMBERG   (Germany)

Author keywords

Cobalt; Directional solidification; Hot corrosion; Industrial gas turbine; Nickel base superalloy; Phase stability; Rhenium; Stress rupture

Indexed keywords

COATINGS; COBALT; CORROSION RESISTANCE; GAS TURBINES; NICKEL ALLOYS; RUTHENIUM; SOLID SOLUTIONS; SOLIDIFICATION; TURBOMACHINE BLADES;

HOT CORROSION; INDUSTRIAL GAS TURBINE; NICKEL-BASE SUPERALLOY; PHASE STABILITY; STRESS-RUPTURE;

SUPERALLOYS;

EID: 22744456209     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.7449/2004/superalloys_2004_25_34     Document Type: Conference Paper

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