EP 2238031 A1 20101013 - AIR INTAKE FOR AIRCRAFT NACELLE, AND PROPULSION ASSEMBLY INCLUDING SUCH AIR INTAKE
Title (en)
AIR INTAKE FOR AIRCRAFT NACELLE, AND PROPULSION ASSEMBLY INCLUDING SUCH AIR INTAKE
Title (de)
LUFTEINLASS FÜR EINE FLUGZEUGGONDEL UND ANTRIEBSANORDNUNG MIT EINEM SOLCHEN LUFTEINLASS
Title (fr)
ENTREE D'AIR POUR NACELLE D'AERONEF, ET ENSEMBLE PROPULSIF COMPRENANT UNE TELLE ENTREE D'AIR
Publication
Application
Priority
- FR 2009000061 W 20090121
- FR 0800471 A 20080129
Abstract (en)
[origin: WO2009109712A1] The invention relates to an air intake for an aircraft nacelle that comprises a shroud (19) that can be mounted on the fan casing (15) of a turbojet engine (1). The shroud (19) is sized so as to define a circumferential gap (J) relative to the casing (15). Punctual linking means (27, 33) between the shroud (19) and the casing (15) are discretely distributed at the periphery of said shroud (19).
IPC 8 full level
B64D 29/00 (2006.01); B64D 33/02 (2006.01)
CPC (source: EP US)
B64D 33/02 (2013.01 - EP US); F01D 21/00 (2013.01 - EP US); F02C 7/045 (2013.01 - EP US); B64D 2033/0206 (2013.01 - EP US); B64D 2033/0286 (2013.01 - EP US); F05D 2220/36 (2013.01 - EP US)
Citation (search report)
See references of WO 2009109712A1
Designated contracting state (EPC)
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 SE SI SK TR
Designated extension state (EPC)
AL BA RS
DOCDB simple family (publication)
FR 2926791 A1 20090731; FR 2926791 B1 20100528; BR PI0906953 A2 20150714; CA 2708106 A1 20090911; CN 101918276 A 20101215; CN 101918276 B 20131009; EP 2238031 A1 20101013; RU 2010134976 A 20120310; RU 2494015 C2 20130927; US 2010320316 A1 20101223; US 8985506 B2 20150324; WO 2009109712 A1 20090911
DOCDB simple family (application)
FR 0800471 A 20080129; BR PI0906953 A 20090121; CA 2708106 A 20090121; CN 200980102533 A 20090121; EP 09716599 A 20090121; FR 2009000061 W 20090121; RU 2010134976 A 20090121; US 86490109 A 20090121