EP 0475428 B1 19980107 - Gas turbine, gas turbine blade used therefor and manufacturing method for gas turbine blade
Title (en)
Gas turbine, gas turbine blade used therefor and manufacturing method for gas turbine blade
Title (de)
Gasturbine, für diese Gasturbine verwendete Schaufel und Verfahren zur Herstellung dieser Schaufel
Title (fr)
Turbine à gaz, aube pour cette turbine à gaz et méthode de fabriction de l'aube
Publication
Application
Priority
JP 24521090 A 19900914
Abstract (en)
[origin: EP0475428A1] A heavy-duty gas turbine includes a compressor; a combustion liner; a turbine blade (7) in a single stage or multi-stages; and a turbine nozzle provided in correspondence to the turbine blade (7). The turbine blade (7) has a dovetail (10) secured to a turbine disk and has an overall length of not less than 180 mm, and it is made of a single-crystal Ni-base alloy whose gamma phase is a single crystal. Operating gas temperature is not less than 1400 DEG C, and metal temperature of a first blade is not less than 1000 DEG C under working stress. <IMAGE>
IPC 1-7
IPC 8 full level
B22D 27/04 (2006.01); C22C 19/03 (2006.01); C22C 19/05 (2006.01); C30B 21/02 (2006.01); F01D 5/28 (2006.01); F01D 5/30 (2006.01)
CPC (source: EP KR)
B22D 3/00 (2013.01 - KR); F01D 5/28 (2013.01 - EP); F05D 2300/607 (2013.01 - EP)
Designated contracting state (EPC)
CH DE FR GB IT LI
DOCDB simple family (publication)
EP 0475428 A1 19920318; EP 0475428 B1 19980107; CA 2051133 A1 19920315; CA 2051133 C 20000829; CN 1034828 C 19970507; CN 1060890 A 19920506; DE 69128580 D1 19980212; DE 69128580 T2 19980430; JP 2729531 B2 19980318; JP H04124237 A 19920424; KR 0185206 B1 19990401; KR 920006057 A 19920427
DOCDB simple family (application)
EP 91115542 A 19910913; CA 2051133 A 19910911; CN 91109581 A 19910914; DE 69128580 T 19910913; JP 24521090 A 19900914; KR 910015986 A 19910913