EP 2268910 A2 20110105 - BYPASS TURBOJET ENGINE NACELLE
Title (en)
BYPASS TURBOJET ENGINE NACELLE
Title (de)
BYPASSGASTURBINENGONDEL
Title (fr)
NACELLE DE TURBORÉACTEUR À DOUBLE FLUX
Publication
Application
Priority
- FR 2009050643 W 20090409
- FR 0802036 A 20080414
Abstract (en)
[origin: WO2009136096A2] The invention relates to a bypass turbojet engine nacelle comprising a downstream section equipped with a thrust reverser device comprising a moving cowl (6) mounted such that it can move in translation in a direction substantially parallel to a longitudinal axis of the nacelle and able to move alternately from a closed position in which it ensures the aerodynamic continuity of the nacelle and covers deflection means (70) and an open position in which it opens a passage in the nacelle and uncovers the deflection means, the said moving cowl also being extended by at least one nozzle section (7) mounted at a downstream end of the said moving cowl, characterized in that the nozzle section comprises at least one panel (10) mounted such that it can rotate about at least one pivot about an axis substantially perpendicular to a longitudinal axis of the nacelle, the said panel further being connected to a fixed fairing structure (2) of the turbojet engine by at least one link rod (11) mounted such that it can rotate about anchor points on the panel of the nozzle section and on the fixed structure, respectively.
IPC 8 full level
CPC (source: EP US)
F02K 1/1261 (2013.01 - EP US); F02K 1/72 (2013.01 - EP US); F05D 2260/50 (2013.01 - EP US)
Citation (search report)
See references of WO 2009136096A2
Citation (examination)
FR 1164936 A 19581015 - BERTIN ET CIE SOC
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 2929998 A1 20091016; FR 2929998 B1 20110812; BR PI0910935 A2 20151006; CA 2719155 A1 20091112; CN 102007284 A 20110406; EP 2268910 A2 20110105; RU 2010145242 A 20120520; RU 2499904 C2 20131127; US 2011030338 A1 20110210; WO 2009136096 A2 20091112; WO 2009136096 A3 20100107
DOCDB simple family (application)
FR 0802036 A 20080414; BR PI0910935 A 20090409; CA 2719155 A 20090409; CN 200980113052 A 20090409; EP 09742294 A 20090409; FR 2009050643 W 20090409; RU 2010145242 A 20090409; US 93746209 A 20090409