EP 2181041 A1 20100505 - NACELLE WITH AN ADAPTABLE OUTLET SECTION
Title (en)
NACELLE WITH AN ADAPTABLE OUTLET SECTION
Title (de)
GONDEL MIT EINSTELLBAREM AUSLASSTEIL
Title (fr)
NACELLE A SECTION DE SORTIE ADAPTABLE
Publication
Application
Priority
- FR 2008000859 W 20080619
- FR 0705920 A 20070820
Abstract (en)
[origin: WO2009024660A1] The present invention relates to a jet engine nacelle (1) comprising an aft section (5) having an internal structure (9) intended to surround an aft portion of an engine compartment and to define, with an exhaust nozzle (6), a calibrated outlet section for the ventilation of the engine compartment by way of spacing means arranged in the outlet section, characterized in that the spacing means are divided into rigid spacing means (11) designed to provide a constant spacing and into compensating means (13) designed so as to be able to adapt to the relative movements of the jet engine with respect to the nacelle.
IPC 8 full level
B64D 33/04 (2006.01)
CPC (source: EP US)
B64D 29/06 (2013.01 - EP US); B64D 33/04 (2013.01 - EP US); F02K 1/08 (2013.01 - US); F02K 1/085 (2013.01 - US); Y10T 137/0536 (2015.04 - EP US)
Citation (search report)
See references of WO 2009024660A1
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 MT NL NO PL PT RO SE SI SK TR
Designated extension state (EPC)
AL BA MK RS
DOCDB simple family (publication)
FR 2920146 A1 20090227; FR 2920146 B1 20091030; BR PI0813603 A2 20141230; CA 2696792 A1 20090226; CA 2696792 C 20151006; CN 101784449 A 20100721; CN 101784449 B 20150107; EP 2181041 A1 20100505; RU 2010109801 A 20110927; RU 2469923 C2 20121220; US 2011214747 A1 20110908; US 8875518 B2 20141104; WO 2009024660 A1 20090226
DOCDB simple family (application)
FR 0705920 A 20070820; BR PI0813603 A 20080619; CA 2696792 A 20080619; CN 200880102592 A 20080619; EP 08828022 A 20080619; FR 2008000859 W 20080619; RU 2010109801 A 20080619; US 67423708 A 20080619