Global Patent Index - EP 0916812 B1

EP 0916812 B1 20030305 - Final stage for an axial turbine

Title (en)

Final stage for an axial turbine

Title (de)

Endstufe für axialdurchströmte Turbine

Title (fr)

Etage final pour turbine axial

Publication

EP 0916812 B1 20030305 (DE)

Application

EP 97810873 A 19971117

Priority

EP 97810873 A 19971117

Abstract (en)

[origin: EP0916812A1] The end stage has a row of stator blades (10) and a row of narrowing rotor blades (20). The stator blades are swept forward axially at the rotor-side head end and swept back at the stator-side end, relative to the run of the rotor-side channel limit (2). The sweep-forward of the trailing edge (12) of the stator blades covers most of the radial extent parallel to the leading edge (21) of the rotor blades.

IPC 1-7

F01D 9/04; F01D 5/14

IPC 8 full level

F01D 5/14 (2006.01); F01D 9/04 (2006.01)

CPC (source: EP US)

F01D 5/141 (2013.01 - EP US); F01D 5/142 (2013.01 - EP US); F01D 9/041 (2013.01 - EP US)

Designated contracting state (EPC)

DE FR GB

DOCDB simple family (publication)

EP 0916812 A1 19990519; EP 0916812 B1 20030305; CN 1217419 A 19990526; CN 1250863 C 20060412; DE 59709447 D1 20030410; KR 19990045318 A 19990625; US 6099248 A 20000808

DOCDB simple family (application)

EP 97810873 A 19971117; CN 98123390 A 19981117; DE 59709447 T 19971117; KR 19980049088 A 19981116; US 19036698 A 19981112