EP 0924384 A2 19990623 - Airfoil with leading edge cooling
Title (en)
Airfoil with leading edge cooling
Title (de)
Kühlung der Anströmkante einer Turbomaschinenschaufel
Title (fr)
Refroidissement de l'arête amont d'une aube pour une turbomachine
Publication
Application
Priority
US 99232397 A 19971217
Abstract (en)
A hollow airfoil (16) is provided which includes a body, a trench (30), and a plurality of cooling apertures (36) disposed within the trench (30). The body extends chordwise between a leading edge (26) and a trailing edge (29), and spanwise between an outer radial surface and an inner radial surface, and includes an exterior wall surrounding a cavity (20). The trench (30) is disposed in the exterior wall along the leading edge (26), extending in a spanwise direction. <IMAGE>
IPC 1-7
IPC 8 full level
CPC (source: EP)
F01D 5/187 (2013.01); F05D 2240/121 (2013.01); F05D 2240/303 (2013.01); F05D 2260/202 (2013.01)
Designated contracting state (EPC)
DE FR GB
DOCDB simple family (publication)
EP 0924384 A2 19990623; EP 0924384 A3 20000823; JP H11247611 A 19990914; KR 19990063131 A 19990726
DOCDB simple family (application)
EP 98310191 A 19981211; JP 37577998 A 19981217; KR 19980055495 A 19981216