EP 2076438 A2 20090708 - BYPASS TURBOJET ENGINE NACELLE
Title (en)
BYPASS TURBOJET ENGINE NACELLE
Title (de)
BYPASSGASTURBINENGONDEL
Title (fr)
NACELLE POUR TURBORÉACTEUR DOUBLE FLUX
Publication
Application
Priority
- FR 2007001633 W 20071005
- FR 0608892 A 20061011
- FR 0701899 A 20070316
Abstract (en)
[origin: WO2008043903A2] The nacelle (1) comprises an air intake (5) upstream of the turbojet engine (2), a middle section (6) an internal casing (6a) of which is intended to surround a fan (3) of the turbojet engine (2), and a downstream section (7) comprising an external structure (7a) which is rigidly connected to a downstream part of the casing (6a) of the fan (3) so as to support the turbojet engine (2) and has means of attachment to a strut (12) intended to be connected to a fixed structure (13) of an aeroplane.
IPC 8 full level
B64D 27/18 (2006.01)
CPC (source: EP US)
B64D 27/18 (2013.01 - EP US); B64D 27/40 (2024.01 - EP US); B64D 27/402 (2024.01 - EP); B64D 27/404 (2024.01 - EP); B64D 29/08 (2013.01 - EP US); B64D 33/04 (2013.01 - EP US); F02C 7/20 (2013.01 - EP US); F02K 1/72 (2013.01 - EP US); F02K 3/06 (2013.01 - EP US); B64D 27/402 (2024.01 - US); B64D 27/404 (2024.01 - US); F05D 2300/603 (2013.01 - EP US); Y02T 50/40 (2013.01 - EP US); Y02T 50/60 (2013.01 - EP US)
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR
DOCDB simple family (publication)
WO 2008043903 A2 20080417; WO 2008043903 A3 20080703; BR PI0717730 A2 20131022; CA 2665425 A1 20080417; EP 2076438 A2 20090708; RU 2009117418 A 20101120; RU 2453477 C2 20120620; US 2010040466 A1 20100218; US 8523516 B2 20130903
DOCDB simple family (application)
FR 2007001633 W 20071005; BR PI0717730 A 20071005; CA 2665425 A 20071005; EP 07858402 A 20071005; RU 2009117418 A 20071005; US 44542107 A 20071005