EP 3315721 B1 20220302 - LEADING-EDGE REINFORCEMENT OF A TURBINE ENGINE BLADE
Title (en)
LEADING-EDGE REINFORCEMENT OF A TURBINE ENGINE BLADE
Title (de)
VERSTÄRKUNG DER VORDERKANTE EINER LAUFRADSCHAUFEL EINER STRÖMUNGSMASCHINE
Title (fr)
RENFORT DE BORD D'ATTAQUE D'UNE AUBE DE TURBOMACHINE
Publication
Application
Priority
FR 1660479 A 20161028
Abstract (en)
[origin: US2018119551A1] A turbine engine blade comprising an aerodynamic surface that extends in a first direction between a leading edge and a trailing edge, and in a second direction substantially perpendicular to the first direction between a root and a tip of the blade, and a leading-edge reinforcement comprising a fin partly covering the aerodynamic surface of the blade, characterised in that the fin has a radially outer edge arranged in the vicinity of the tip of the blade and extending between the leading edge and the trailing edge, this radially outer edge comprising an upstream point fitting flush with the tip of the blade at the leading edge and a so-called downstream point separated from the tip of the blade.
IPC 8 full level
F01D 5/14 (2006.01); F01D 5/28 (2006.01); F04D 29/32 (2006.01)
CPC (source: CN EP US)
F01D 5/147 (2013.01 - CN EP US); F01D 5/282 (2013.01 - EP US); F01D 5/288 (2013.01 - CN US); F01D 21/045 (2013.01 - US); F04D 29/324 (2013.01 - EP US); F04D 29/388 (2013.01 - US); F05D 2220/36 (2013.01 - US); F05D 2240/303 (2013.01 - EP US); F05D 2250/711 (2013.01 - US); F05D 2300/133 (2013.01 - US); F05D 2300/174 (2013.01 - CN)
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)
EP 3315721 A1 20180502; EP 3315721 B1 20220302; CN 108005730 A 20180508; CN 108005730 B 20220708; FR 3058181 A1 20180504; FR 3058181 B1 20181109; US 10316669 B2 20190611; US 2018119551 A1 20180503
DOCDB simple family (application)
EP 17197595 A 20171020; CN 201711019798 A 20171027; FR 1660479 A 20161028; US 201715794765 A 20171026