EP 2563665 A1 20130306 - STRUCTURE FOR A NACELLE OF AN AIRCRAFT ENGINE
Title (en)
STRUCTURE FOR A NACELLE OF AN AIRCRAFT ENGINE
Title (de)
BAUTEIL FÜR EINE GONDEL EINES FLUGZEUGTRIEBWERKS
Title (fr)
STRUCTURE POUR NACELLE DE MOTEUR D'AÉRONEF
Publication
Application
Priority
- FR 1053338 A 20100429
- FR 2011050505 W 20110314
Abstract (en)
[origin: WO2011135213A1] The present invention relates to a support half structure for a nacelle of an aircraft engine, which half structure includes at least one longitudinal beam (1 b) and a front half frame (3b). Said half structure is characterized in that said beam (1 b) and said half frame (3b) are made from composite materials, in that said half frame (3b) has an open cross-section, and in that said half structure has one of the following three characteristics: said beam (1 b) and said front half frame (3b) form a one-piece part, or said beam (1 b) has an extension having an open cross-section, the shape of which corresponds to that of said front half frame (3b), said extension being attached to said half frame (3b), or said half frame has an open extension, the shape of which corresponds to that of said beam, said extension being attached to said beam.
IPC 8 full level
B64D 29/06 (2006.01)
CPC (source: EP US)
B64D 29/06 (2013.01 - EP US)
Citation (search report)
See references of WO 2011135213A1
Citation (examination)
FR 2959487 A1 20111104 - AIRCELLE SA [FR]
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 2011135213 A1 20111103; BR 112012023770 A2 20160823; CA 2796630 A1 20111103; CN 102858635 A 20130102; EP 2563665 A1 20130306; FR 2959486 A1 20111104; FR 2959486 B1 20120413; RU 2012150133 A 20140610; US 2013062462 A1 20130314; US 9010681 B2 20150421
DOCDB simple family (application)
FR 2011050505 W 20110314; BR 112012023770 A 20110314; CA 2796630 A 20110314; CN 201180020770 A 20110314; EP 11712999 A 20110314; FR 1053338 A 20100429; RU 2012150133 A 20110314; US 201213662905 A 20121029