EP 2763897 A1 20140813 - AIRCRAFT PROPULSION ASSEMBLY
Title (en)
AIRCRAFT PROPULSION ASSEMBLY
Title (de)
FLUGZEUGANTRIEBSANORDNUNG
Title (fr)
ENSEMBLE PROPULSIF D'AÉRONEF
Publication
Application
Priority
- FR 1159010 A 20111006
- FR 2012052259 W 20121005
Abstract (en)
[origin: WO2013050714A1] The invention concerns an aircraft propulsion assembly of which the suspension assembly comprises the following upstream suspension fasteners mounted on a blower housing (34) and/or on said intermediate housing (30) of the turbojet engine: at least one main upstream suspension fastener (130), configured in such a way as to absorb at least a moment (Mx) along the longitudinal axis (X) of the turbojet engine and the forces (Fy and Fz) in a plane perpendicular to the longitudinal axis, and at least one pair (120, 140, 200) of additional upstream suspension fasteners (120a, 120b, 140a, 140b, 121a, 121b, 200a, 200b) separate from the main suspension fastener (130) and configured in such a way as to absorb at least a moment (Mz) according to the vertical axis of the turbojet engine and, associated with a device for absorbing thrust forces (110), a moment (My) along the transverse axis of the turbojet engine and forces (Fx) along the longitudinal axis of the turbojet engine.
IPC 8 full level
B64D 27/26 (2006.01)
CPC (source: EP US)
B64D 27/10 (2013.01 - US); B64D 27/40 (2024.01 - EP US); B64D 27/404 (2024.01 - EP); B64D 27/406 (2024.01 - EP); B64D 27/404 (2024.01 - US); B64D 27/406 (2024.01 - US)
Citation (search report)
See references of WO 2013050714A1
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 2013050714 A1 20130411; BR 112014006998 A2 20170411; CA 2849239 A1 20130411; CN 103874633 A 20140618; EP 2763897 A1 20140813; FR 2981047 A1 20130412; FR 2981047 B1 20131025; RU 2014117114 A 20151120; US 2014217234 A1 20140807
DOCDB simple family (application)
FR 2012052259 W 20121005; BR 112014006998 A 20121005; CA 2849239 A 20121005; CN 201280049371 A 20121005; EP 12775819 A 20121005; FR 1159010 A 20111006; RU 2014117114 A 20121005; US 201414245843 A 20140404