EP 1765669 A1 20070328 - MULTI-ENGINE AIRCRAFT
Title (en)
MULTI-ENGINE AIRCRAFT
Title (de)
FLUGZEUG MIT MEHREREN TRIEBWERKEN
Title (fr)
AVION MULTIMOTEUR
Publication
Application
Priority
- FR 2005001649 W 20050629
- FR 0407863 A 20040715
Abstract (en)
[origin: WO2006016031A1] The invention relates to a multi-engine aircraft whose at least two engines (2, 3) are fixed to the fuselage wings symmetrically with respect to the longitudinal vertical plane of symmetry thereof, respectively and the third engine (7) is provided for the tail of the fuselage which comprises tail-planes in the view of said longitudinal plane. The tail-planes (9, 10) define a channel (11) symmetrical with respect to the longitudinal plane of the fuselage and the third engine (7) is disposed on the plane of symmetry of the channel corresponding to the longitudinal plane and mounted on the top part of the fuselage in an elevated manner and before the tail-planes in such a way that output of said third engine is arranged substentially upon the input of the channel (11) defined by said tail-planes.
IPC 8 full level
B64D 27/20 (2006.01); B64D 27/40 (2024.01); B64D 33/04 (2006.01)
CPC (source: EP US)
B64C 5/06 (2013.01 - EP US); B64D 27/20 (2013.01 - EP US); Y02T 50/40 (2013.01 - EP US)
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU MC NL PL PT RO SE SI SK TR
DOCDB simple family (publication)
FR 2873096 A1 20060120; FR 2873096 B1 20071123; BR PI0510912 A 20071113; CA 2563815 A1 20060216; CA 2563815 C 20120807; CN 1984812 A 20070620; EP 1765669 A1 20070328; JP 2008506576 A 20080306; JP 4823222 B2 20111124; RU 2006141347 A 20080527; RU 2352500 C2 20090420; US 2008073459 A1 20080327; US 7905449 B2 20110315; WO 2006016031 A1 20060216
DOCDB simple family (application)
FR 0407863 A 20040715; BR PI0510912 A 20050629; CA 2563815 A 20050629; CN 200580023640 A 20050629; EP 05783890 A 20050629; FR 2005001649 W 20050629; JP 2007520855 A 20050629; RU 2006141347 A 20050629; US 63222505 A 20050629