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1. WO2006016031 - MULTI-ENGINE AIRCRAFT

Publication Number WO/2006/016031
Publication Date 16.02.2006
International Application No. PCT/FR2005/001649
International Filing Date 29.06.2005
IPC
B64D 27/20 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
27Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
02Aircraft characterised by the type or position of power plant
16of jet type
20within, or attached to, fuselage
B64D 27/26 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
27Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
26Aircraft characterised by construction of power-plant mounting
CPC
B64C 5/06
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
5Stabilising surfaces
06Fins
B64D 27/20
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
27Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
02Aircraft characterised by the type or position of power plant
16of jet type
20within or attached to fuselage
Y02T 50/40
YSECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
50Aeronautics or air transport
40Weight reduction
Applicants
  • AIRBUS FRANCE [FR]/[FR] (AllExceptUS)
  • CAZALS, Olivier [FR]/[FR] (UsOnly)
  • GENTY DE LA SAGNE, Jaime [FR]/[FR] (UsOnly)
  • RITTINGHAUS, Denis [FR]/[FR] (UsOnly)
Inventors
  • CAZALS, Olivier
  • GENTY DE LA SAGNE, Jaime
  • RITTINGHAUS, Denis
Agents
  • BONNETAT, Christian
Priority Data
040786315.07.2004FR
Publication Language French (fr)
Filing Language French (FR)
Designated States
Title
(EN) MULTI-ENGINE AIRCRAFT
(FR) AVION MULTIMOTEUR
Abstract
(EN) 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.
(FR) L'invention concerne un avion multimoteur, dont au moins deux moteurs (2, 3) sont associés aux ailes du fuselage respectivement symétriquement par rapport au plan longitudinal vertical de symétrie de ce dernier et dont un troisième (7) est prévu au niveau de la queue dudit fuselage, qui comporte les empennages arrière, selon ledit plan longitudinal.les empennages arrière (9, 10) définissent un canal (11), symétrique par rapport audit plan longitudinal du fuselage, et le troisième moteur (7) est agencé dans le plan de symétrie dudit canal correspondant audit plan longitudinal et est monté sur la partie supérieure dudit fuselage de façon surélevée et devant les empennages, pour que la sortie de ce troisième moteur se trouve sensiblement à l'entrée du canal (11) défini par lesdits empennages.
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