EP 2582959 A1 20130424 - AIRCRAFT TURBO JET ENGINE FAN CASING
Title (en)
AIRCRAFT TURBO JET ENGINE FAN CASING
Title (de)
LÜFTERGEHÄUSE FÜR EINEN FLUGZEUG-TURBOJETMOTOR
Title (fr)
CARTER DE SOUFFLANTE DE TURBOREACTEUR D'AERONEF
Publication
Application
Priority
- FR 1054845 A 20100618
- FR 2011051382 W 20110616
Abstract (en)
[origin: WO2011157965A1] Aircraft turbo jet engine fan casing, notable in that it is in the form of a box section (6), the radially interior wall (6a) of which is able to form the internal skin of the cold air flow duct (17) of a nacelle in which said turbo jet engine is intended to be mounted, and the radially exterior wall (6b) of which is able to form the external skin of said nacelle.
IPC 8 full level
F02K 3/06 (2006.01); B64D 33/02 (2006.01)
CPC (source: EP US)
B64D 33/02 (2013.01 - EP US); F01D 21/045 (2013.01 - EP US); F02K 3/06 (2013.01 - EP US); F05D 2240/14 (2013.01 - EP US); F05D 2300/433 (2013.01 - EP US); F05D 2300/603 (2013.01 - EP US); Y02T 50/60 (2013.01 - EP US)
Citation (search report)
See references of WO 2011157965A1
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)
WO 2011157965 A1 20111222; BR 112012030320 A2 20160809; CA 2802398 A1 20111222; CN 102985677 A 20130320; EP 2582959 A1 20130424; FR 2961483 A1 20111223; FR 2961483 B1 20130118; RU 2013101090 A 20140727; US 2013111873 A1 20130509
DOCDB simple family (application)
FR 2011051382 W 20110616; BR 112012030320 A 20110616; CA 2802398 A 20110616; CN 201180025938 A 20110616; EP 11735897 A 20110616; FR 1054845 A 20100618; RU 2013101090 A 20110616; US 201213718532 A 20121218