EP 2625413 A1 20130814 - AIRCRAFT PROPULSION ASSEMBLY
Title (en)
AIRCRAFT PROPULSION ASSEMBLY
Title (de)
FLUGZEUGANTRIEBSANORDNUNG
Title (fr)
ENSEMBLE PROPULSIF D'AÉRONEF
Publication
Application
Priority
- FR 1057998 A 20101004
- FR 2011052298 W 20111003
Abstract (en)
[origin: WO2012045965A1] The invention relates to an aircraft propulsion assembly comprising at least one nacelle (2) having at least one intermediate housing (7) and a front frame (25) that is to be mounted downstream of an outer envelope (12) of said intermediate housing (7), said front frame (25) comprising a deviation edge and at least one element forming a direct or indirect support for at least one flow deviation means (22), characterised in that the deviation edge and said support-forming element are built into the outer envelope (12) of the intermediate housing (7).
IPC 8 full level
F02K 1/60 (2006.01); F01D 5/00 (2006.01); F02K 1/62 (2006.01); F02K 1/72 (2006.01); F02K 1/76 (2006.01)
CPC (source: EP US)
F01D 5/005 (2013.01 - EP US); F02K 1/566 (2013.01 - US); F02K 1/605 (2013.01 - EP US); F02K 1/625 (2013.01 - EP US); F02K 1/72 (2013.01 - EP US); F02K 1/766 (2013.01 - EP US); F05D 2230/80 (2013.01 - EP US); F05D 2240/14 (2013.01 - EP US); Y02T 50/60 (2013.01 - EP US)
Citation (search report)
See references of WO 2012045965A1
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)
FR 2965588 A1 20120406; FR 2965588 B1 20150501; BR 112013006465 A2 20170404; CA 2811481 A1 20120412; CN 103154489 A 20130612; EP 2625413 A1 20130814; RU 2013119476 A 20141120; US 2013277454 A1 20131024; WO 2012045965 A1 20120412
DOCDB simple family (application)
FR 1057998 A 20101004; BR 112013006465 A 20111003; CA 2811481 A 20111003; CN 201180048123 A 20111003; EP 11779780 A 20111003; FR 2011052298 W 20111003; RU 2013119476 A 20111003; US 201313856038 A 20130403