FR3061146B1 - REAR-ENGINED AIRCRAFT CARRIED BY AT LEAST ONE ARM IN A POSITION OFFSET BACKWARDS AND AT A DISTANCE FROM A REAR END OF THE AIRCRAFT’S AIRCRAFT - Google Patents

REAR-ENGINED AIRCRAFT CARRIED BY AT LEAST ONE ARM IN A POSITION OFFSET BACKWARDS AND AT A DISTANCE FROM A REAR END OF THE AIRCRAFT’S AIRCRAFT Download PDF

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Publication number
FR3061146B1
FR3061146B1 FR1663356A FR1663356A FR3061146B1 FR 3061146 B1 FR3061146 B1 FR 3061146B1 FR 1663356 A FR1663356 A FR 1663356A FR 1663356 A FR1663356 A FR 1663356A FR 3061146 B1 FR3061146 B1 FR 3061146B1
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France
Prior art keywords
aircraft
arm
distance
rear end
engined
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Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1663356A
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French (fr)
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FR3061146A1 (en
Inventor
Olivier Cazals
Thierry Druot
Julien Guillemaut
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
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Airbus Operations SAS
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Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1663356A priority Critical patent/FR3061146B1/en
Publication of FR3061146A1 publication Critical patent/FR3061146A1/en
Application granted granted Critical
Publication of FR3061146B1 publication Critical patent/FR3061146B1/en
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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plant of jet type within or attached to fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/16—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like specially adapted for mounting power plant
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/04—Aircraft not otherwise provided for having multiple fuselages or tail booms

Abstract

Pour optimiser les performances d'un aéronef en maximisant la faculté d'ingestion de la couche limite par un moteur arrière, il est proposé un aéronef (10) comprenant une cellule (12) et au moins un moteur arrière (34), la cellule (12) étant prolongée par au moins un bras (30A, 30B) qui porte le moteur arrière (34) et le maintient décalé en arrière et à distance d'une extrémité arrière (32) de la cellule (12) définie sur un axe longitudinal (37) du moteur arrière (34).To optimize the performance of an aircraft by maximizing the ability to ingest the boundary layer by a rear engine, an aircraft (10) is proposed comprising an airframe (12) and at least one rear engine (34), the airframe (12) being extended by at least one arm (30A, 30B) which carries the rear motor (34) and keeps it offset rearward and at a distance from a rear end (32) of the cell (12) defined on an axis longitudinal (37) of the rear engine (34).

FR1663356A 2016-12-23 2016-12-23 REAR-ENGINED AIRCRAFT CARRIED BY AT LEAST ONE ARM IN A POSITION OFFSET BACKWARDS AND AT A DISTANCE FROM A REAR END OF THE AIRCRAFT’S AIRCRAFT Active FR3061146B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1663356A FR3061146B1 (en) 2016-12-23 2016-12-23 REAR-ENGINED AIRCRAFT CARRIED BY AT LEAST ONE ARM IN A POSITION OFFSET BACKWARDS AND AT A DISTANCE FROM A REAR END OF THE AIRCRAFT’S AIRCRAFT

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1663356 2016-12-23
FR1663356A FR3061146B1 (en) 2016-12-23 2016-12-23 REAR-ENGINED AIRCRAFT CARRIED BY AT LEAST ONE ARM IN A POSITION OFFSET BACKWARDS AND AT A DISTANCE FROM A REAR END OF THE AIRCRAFT’S AIRCRAFT

Publications (2)

Publication Number Publication Date
FR3061146A1 FR3061146A1 (en) 2018-06-29
FR3061146B1 true FR3061146B1 (en) 2023-11-03

Family

ID=58162896

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1663356A Active FR3061146B1 (en) 2016-12-23 2016-12-23 REAR-ENGINED AIRCRAFT CARRIED BY AT LEAST ONE ARM IN A POSITION OFFSET BACKWARDS AND AT A DISTANCE FROM A REAR END OF THE AIRCRAFT’S AIRCRAFT

Country Status (1)

Country Link
FR (1) FR3061146B1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3043984B1 (en) * 2015-11-25 2017-12-22 Snecma PLANE PROPELLED BY TURBOMACHINE WITH ACOUSTIC SCREEN
FR3099138B1 (en) * 2019-07-23 2021-07-02 Safran Aircraft Engines Aircraft comprising a blower thruster at the rear of the fuselage and a mounting structure for this thruster
EP3904202B1 (en) * 2020-04-29 2023-06-07 Airbus Operations, S.L. A rear end section for an aircraft

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2359052B (en) * 2000-02-09 2003-09-17 Rolls Royce Plc Engine arrangement
US6808140B2 (en) * 2002-02-08 2004-10-26 Moller Paul S Vertical take-off and landing vehicles
US7766275B2 (en) * 2006-06-12 2010-08-03 The Boeing Company Aircraft having a pivotable powerplant
FR2938823A1 (en) * 2008-11-26 2010-05-28 Aircelle Sa FLYING WING FOR AIRCRAFT
FR2993859B1 (en) * 2012-07-26 2015-08-21 Airbus Operations Sas MULTIPLAN PLANE WITH PROPULSION PUSHING AND PULLING
WO2014074143A1 (en) * 2012-11-12 2014-05-15 United Technologies Corporation Aircraft with forward sweeping t-tail
US10112696B2 (en) * 2012-11-12 2018-10-30 United Technologies Corporation Stabilizer sacrificial surfaces
WO2014074145A1 (en) * 2012-11-12 2014-05-15 United Technologies Corporation Angled core gas turbine engine mounting
RU2534676C1 (en) * 2013-05-27 2014-12-10 Дмитрий Сергеевич Дуров Cryogenic turbo-electric stol aircraft
US9505484B1 (en) * 2016-04-11 2016-11-29 Nasser M. Al-Sabah Modular aircraft system

Also Published As

Publication number Publication date
FR3061146A1 (en) 2018-06-29

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