EP 2556237 A1 20130213 - AIRCRAFT PROPULSION SYSTEM PROVIDED WITH REVERSE THRUST MEANS
Title (en)
AIRCRAFT PROPULSION SYSTEM PROVIDED WITH REVERSE THRUST MEANS
Title (de)
FLUGZEUGANTRIEBSSYSTEM MIT BREMSSCHUBMITTELN
Title (fr)
ENSEMBLE PROPULSIF POUR AÉRONEF MUNI DE MOYENS D'INVERSION DE POUSSÉE
Publication
Application
Priority
- FR 1052689 A 20100409
- FR 2011050483 W 20110310
Abstract (en)
[origin: WO2011124793A1] The invention relates to a propulsion system including a nacelle and, inside said nacelle, a dual flow turbojet engine that itself includes a fan casing (10) in which a fan and a flow-rectifying vane assembly (15) are located. Said propulsion system includes a reverse thrust means (17) that is located between said fan and said vane assembly (15).
IPC 8 full level
F02K 1/70 (2006.01)
CPC (source: EP US)
F02K 1/64 (2013.01 - US); F02K 1/70 (2013.01 - EP US); F02K 1/72 (2013.01 - US); Y02T 50/60 (2013.01 - EP US)
Citation (search report)
See references of WO 2011124793A1
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 2011124793 A1 20111013; BR 112012022437 A2 20160705; CA 2792288 A1 20111013; CN 102792001 A 20121121; EP 2556237 A1 20130213; FR 2958688 A1 20111014; FR 2958688 B1 20130222; RU 2012146860 A 20140520; US 2013025260 A1 20130131; US 9133790 B2 20150915
DOCDB simple family (application)
FR 2011050483 W 20110310; BR 112012022437 A 20110310; CA 2792288 A 20110310; CN 201180013879 A 20110310; EP 11712982 A 20110310; FR 1052689 A 20100409; RU 2012146860 A 20110310; US 201113640070 A 20110310