EP 2564050 A1 20130306 - TURBOJET ENGINE NACELLE
Title (en)
TURBOJET ENGINE NACELLE
Title (de)
TURBOSTRAHL-TRIEBWERKSGONDEL
Title (fr)
NACELLE DE TURBORÉACTEUR
Publication
Application
Priority
- FR 1053373 A 20100430
- FR 2011050924 W 20110421
Abstract (en)
[origin: WO2011135238A1] The invention relates to a bypass turbojet engine nacelle equipped with a thrust reverser device (20) comprising a cowl (30), diversion means (40) supported by a front frame (50) upstream of the cowl (30), said cowl (30) having translational mobility in a direction substantially parallel to a longitudinal axis of the nacelle and being able alternately to move from a closed position in which it ensures the aerodynamic continuity of the nacelle and covers the diversion means (40), into an open position in which it opens up a passage in the nacelle and uncovers the diversion means (40), said cowl (30) being extended by at least one variable-geometry jet pipe nozzle (60) mounted at a downstream end of said cowl (30), and in which at least part of the front frame (50), the diversion means (40) and the jet pipe nozzle (60) have translational mobility in a direction substantially parallel to a longitudinal axis of the nacelle with respect to the cowl (30) towards a position that causes a variation in the cross section of the jet pipe nozzle.
IPC 8 full level
CPC (source: EP US)
Citation (search report)
See references of WO 2011135238A1
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 2011135238 A1 20111103; BR 112012026719 A2 20160712; CA 2796743 A1 20111103; CN 102859168 A 20130102; CN 102859168 B 20151216; EP 2564050 A1 20130306; FR 2959532 A1 20111104; FR 2959532 B1 20130104; RU 2012149588 A 20140620; US 2013228635 A1 20130905
DOCDB simple family (application)
FR 2011050924 W 20110421; BR 112012026719 A 20110421; CA 2796743 A 20110421; CN 201180021748 A 20110421; EP 11731443 A 20110421; FR 1053373 A 20100430; RU 2012149588 A 20110421; US 201213663652 A 20121030