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Statements

Subject Item
n2:RIV%2F68081723%3A_____%2F02%3A07023149%21RIV%2F2003%2FAV0%2FA07003%2FN
rdf:type
skos:Concept n13:Vysledek
dcterms:description
Increases in the operating temperature of industrial gas turbines are driving the requirement for high temperature, single crystal nickel alloys for turbine blade applications. A candidate for this application is the aerospace alloy CM186LC, and this is being investigated as part of a COST 522 programme WP1.1. The creep behaviour of the SX CM186LC has been studied to assess its suitability for use in the industrial gas turbine environment. A fully quantitative microscopic characterisation of cast SX CM186LC has been made which provides details of the complex microstructure of this alloy without any heat treatment. Creep tests have been conducted at a variety of stresses and temperatures relevant to operating conditions in a typical industrial gas turbine and the results are compared to other single crystal nickel alloys. Similarly, the effect of crystal orientation on the creep behaviour of CM186LC single crystals has also been assessed. Increases in the operating temperature of industrial gas turbines are driving the requirement for high temperature, single crystal nickel alloys for turbine blade applications. A candidate for this application is the aerospace alloy CM186LC, and this is being investigated as part of a COST 522 programme WP1.1. The creep behaviour of the SX CM186LC has been studied to assess its suitability for use in the industrial gas turbine environment. A fully quantitative microscopic characterisation of cast SX CM186LC has been made which provides details of the complex microstructure of this alloy without any heat treatment. Creep tests have been conducted at a variety of stresses and temperatures relevant to operating conditions in a typical industrial gas turbine and the results are compared to other single crystal nickel alloys. Similarly, the effect of crystal orientation on the creep behaviour of CM186LC single crystals has also been assessed.
dcterms:title
The creep behaviour of as-cast SX CM186LC at industrial gas turbine operating conditions. The creep behaviour of as-cast SX CM186LC at industrial gas turbine operating conditions.
skos:prefLabel
The creep behaviour of as-cast SX CM186LC at industrial gas turbine operating conditions. The creep behaviour of as-cast SX CM186LC at industrial gas turbine operating conditions.
skos:notation
RIV/68081723:_____/02:07023149!RIV/2003/AV0/A07003/N
n4:strany
1809
n4:aktivita
n8:Z n8:P
n4:aktivity
P(OC 522.80), Z(AV0Z2041904)
n4:dodaniDat
n6:2003
n4:domaciTvurceVysledku
n16:3109712
n4:druhVysledku
n18:D
n4:duvernostUdaju
n10:S
n4:entitaPredkladatele
n11:predkladatel
n4:idSjednocenehoVysledku
641889
n4:idVysledku
RIV/68081723:_____/02:07023149
n4:jazykVysledku
n17:eng
n4:klicovaSlova
creep; single crystals; industrial gas turbine
n4:klicoveSlovo
n15:industrial%20gas%20turbine n15:single%20crystals n15:creep
n4:kontrolniKodProRIV
[16C68A15037F]
n4:mistoKonaniAkce
Liege [BE]
n4:mistoVydani
Julich
n4:nazevZdroje
Materials for Advanced Power Engineering 2002.
n4:obor
n19:JL
n4:pocetDomacichTvurcuVysledku
1
n4:pocetTvurcuVysledku
6
n4:pocetUcastnikuAkce
0
n4:pocetZahranicnichUcastnikuAkce
0
n4:projekt
n5:OC%20522.80
n4:rokUplatneniVysledku
n6:2002
n4:tvurceVysledku
Henderson, M. B. Lukáš, Petr Klabbers, J. Dubiel, B. Maldini, M. Wilcock, I. M.
n4:typAkce
n12:WRD
n4:zahajeniAkce
2002-09-30+02:00
n4:zamer
n20:AV0Z2041904
s:numberOfPages
10
n7:hasPublisher
Forschungszentrum Julich