EP 1693572 B1 20151104 - Bleeding air from the tip of the rotating blades in a high pressure compressor of a turbine engine
Title (en)
Bleeding air from the tip of the rotating blades in a high pressure compressor of a turbine engine
Title (de)
Luftentnahme bei den rotierenden Schaufelspitzen eines Hochdruckverdichters eines Turbinentriebwerks
Title (fr)
Prélèvement en tête des roues mobiles de compresseur haute pression de turboréacteur
Publication
Application
Priority
FR 0501567 A 20050216
Abstract (en)
[origin: EP1693572A2] The compressor (10) has several stator vanes (18) and moving blades (16) which are spaced apart in axial direction relative to a central longitudinal axis. The blades are surrounded by a stationary casing (14). The stationary casing has several bleed holes (24) which are centered in a range of 5-50% of the blade chord length. The diameter of the bleed hole is 30% of the blade chord length. The bleed hole is inclined at two different angles relative to the longitudinal axis. An independent claim is also included for turbomachine.
IPC 8 full level
F04D 29/68 (2006.01); F04D 27/02 (2006.01)
CPC (source: EP US)
F04D 27/023 (2013.01 - EP US); F04D 29/526 (2013.01 - EP US); F04D 29/682 (2013.01 - EP US); F04D 29/685 (2013.01 - EP US); Y10S 415/914 (2013.01 - EP US)
Designated contracting state (EPC)
DE FR GB
DOCDB simple family (publication)
EP 1693572 A2 20060823; EP 1693572 A3 20110518; EP 1693572 B1 20151104; CA 2536132 A1 20060816; CA 2536132 C 20130618; CN 1840864 A 20061004; CN 1840864 B 20100526; FR 2882112 A1 20060818; FR 2882112 B1 20070511; JP 2006226285 A 20060831; JP 5004476 B2 20120822; RU 2006104789 A 20070927; RU 2395010 C2 20100720; US 2006182623 A1 20060817; US 7549838 B2 20090623
DOCDB simple family (application)
EP 06100669 A 20060120; CA 2536132 A 20060213; CN 200610008206 A 20060216; FR 0501567 A 20050216; JP 2006021844 A 20060131; RU 2006104789 A 20060215; US 34912306 A 20060208