EP 3090131 B8 20210407 - AIRFOIL, CORRESPONDING GAS TURBINE ENGINE AND METHOD FOR REDUCING AIRFOIL TIP LEAKAGE LOSSES
Title (en)
AIRFOIL, CORRESPONDING GAS TURBINE ENGINE AND METHOD FOR REDUCING AIRFOIL TIP LEAKAGE LOSSES
Title (de)
SCHAUFEL, ZUGEHÖRIGES GASTURBINENTRIEBWERK UND VERFAHREN ZUR REDUZIERUNG VON LECKVERLUSTEN AN SCHAUFELSPITZEN
Title (fr)
AUBE, MOTEUR À TURBINE À GAZ ET PROCÉDÉ DE RÉDUCTION DE PERTES DE FUITE EN BOUT D'AUBE ASSOCIÉS
Publication
Application
Priority
- US 201314143115 A 20131230
- US 2014069422 W 20141210
Abstract (en)
[origin: WO2015102827A1] An airfoil according to an exemplary aspect of the present disclosure includes, among other things, a suction sidewall and a pressure sidewall, each sidewall extending spanwise from an airfoil base and extending chordwise between a leading edge and a trailing edge. A tip wall extends chordwise from the leading edge to the trailing edge and joining respective outer spanwise ends of the suction and pressure sidewalls. A tip leakage control vane is formed with an outer surface of the tip wall and a winglet is formed at a junction between the suction sidewall and the tip leakage control vane.
IPC 8 full level
F01D 5/20 (2006.01)
CPC (source: EP US)
F01D 5/20 (2013.01 - EP US); F01D 9/02 (2013.01 - US); F01D 11/08 (2013.01 - US); F05D 2220/32 (2013.01 - US); F05D 2240/126 (2013.01 - EP US); Y02T 50/60 (2013.01 - EP US)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
DOCDB simple family (publication)
WO 2015102827 A1 20150709; EP 3090131 A1 20161109; EP 3090131 A4 20170201; EP 3090131 B1 20210127; EP 3090131 B8 20210407; US 2015330230 A1 20151119; US 9777582 B2 20171003
DOCDB simple family (application)
US 2014069422 W 20141210; EP 14877250 A 20141210; US 201314143115 A 20131230