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Patent Searching and Data


Title:
STATOR OF AN AIRCRAFT TURBINE ENGINE
Document Type and Number:
WIPO Patent Application WO/2016/055715
Kind Code:
A3
Abstract:
The invention relates to a stator (40) of an aircraft turbine engine, comprising an annular row of stationary vanes (44) and an annular row of arms (48), characterised in that the trailing edges (42) of the stationary vanes are located substantially in a first transverse plane (P1) downstream from a second transverse plane (P2) which passes substantially through the leading edges (46) of the arms.

Inventors:
CHARBONNIER SIMON PIERRE CLAUDE (FR)
PERRIER MATTHIEU YOANN (FR)
Application Number:
FR2015/052583
Publication Date:
December 29, 2016
Filing Date:
September 29, 2015
Export Citation:
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Assignee:
SAFRAN AIRCRAFT ENGINES (FR)
International Classes:
F01D25/16; F01D5/14; F01D9/04; F01D17/16; F02C9/18
Domestic Patent References:
WO2005119028A12005-12-15
Foreign References:
EP0942150A21999-09-15
EP1298286A22003-04-02
DE102007035726A12009-02-05
US5207054A1993-05-04
GB2226600A1990-07-04
US5672047A1997-09-30
Attorney, Agent or Firm:
BARBE, Laurent et al. (Gevers & Orès, 41 avenue de Friedland, Paris, 75008, FR)
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