EP 0913556 A2 19990506 - Turbine blade cooling
Title (en)
Turbine blade cooling
Title (de)
Turbinenschaufelkühlung
Title (fr)
Refroidissement d'une aube de turbine
Publication
Application
Priority
US 96212897 A 19971031
Abstract (en)
A blade (10) for a gas turbine engine is disclosed having several improved cooling features. The blade has a plurality of internal cooling passages. The blade has a tip cap aperture (46) and film cooling holes (20), arranged such that the rearmost cooling passage in the blade receives sufficient cooling in all areas to control local heating of the blade. The blade also has angled turbulence promoters to improve internal cooling and a specially shaped platform (14) to avoid heating of the blade platform edges. <IMAGE>
IPC 1-7
IPC 8 full level
F01D 5/18 (2006.01); F01D 5/20 (2006.01); F01D 5/30 (2006.01)
CPC (source: EP)
F01D 5/186 (2013.01); F01D 5/187 (2013.01); F01D 5/20 (2013.01)
Designated contracting state (EPC)
DE FR GB IT
DOCDB simple family (publication)
EP 0913556 A2 19990506; EP 0913556 A3 20000726; JP H11193701 A 19990721
DOCDB simple family (application)
EP 98308829 A 19981028; JP 30466498 A 19981027