FR3041991B1 - Aeronef avec un moyen de propulsion a soufflante deportee - Google Patents
Aeronef avec un moyen de propulsion a soufflante deportee Download PDFInfo
- Publication number
- FR3041991B1 FR3041991B1 FR1559452A FR1559452A FR3041991B1 FR 3041991 B1 FR3041991 B1 FR 3041991B1 FR 1559452 A FR1559452 A FR 1559452A FR 1559452 A FR1559452 A FR 1559452A FR 3041991 B1 FR3041991 B1 FR 3041991B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- fixed
- propulsion
- remote blower
- blower propulsion
- Prior art date
- 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
Links
- 230000000712 assembly Effects 0.000 abstract 2
- 238000000429 assembly Methods 0.000 abstract 2
Classifications
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- 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
- B64D35/00—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions
- B64D35/04—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
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- 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
- B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/001—Shrouded propellers
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/182—Stringers, longerons
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/32—Wings specially adapted for mounting power plant
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- 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
- B64D27/10—Aircraft characterised by the type or position of power plant of gas-turbine type
- B64D27/12—Aircraft characterised by the type or position of power plant of gas-turbine type within or attached to wing
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- B64D27/40—
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- 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
- B64D35/00—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions
- B64D35/02—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions characterised by the type of power plant
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/077—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type the plant being of the multiple flow type, i.e. having three or more flows
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- B64D27/404—
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
La présente invention porte sur un aéronef comportant un fuselage, deux ailes (3) de part et d'autre du fuselage, au moins deux ensembles de propulsion, chacun fixé à une des ailes. Il est caractérisé par le fait que les ensembles de propulsion comprennent au moins un turbomoteur (5) et une hélice (9), l'un des deux étant fixé sous l'aile (3), l'autre fixé sur l'aile. En particulier les axes du turbomoteur et de l'hélice sont situés dans un même plan vertical.
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1559452A FR3041991B1 (fr) | 2015-10-05 | 2015-10-05 | Aeronef avec un moyen de propulsion a soufflante deportee |
FR1561014A FR3041992B1 (fr) | 2015-10-05 | 2015-11-16 | Aeronef avec un moyen de propulsion a soufflante deportee |
US15/284,895 US10850859B2 (en) | 2015-10-05 | 2016-10-04 | Aircraft with a propulsion unit with offset fan |
US15/765,404 US11015521B2 (en) | 2015-10-05 | 2016-10-05 | Aircraft propulsion assembly equipped with a main fan and with at least one offset fan |
PCT/FR2016/052569 WO2017060629A1 (fr) | 2015-10-05 | 2016-10-05 | Ensemble de propulsion d'un aeronef equipe d'une soufflante principale et d'au moins une soufflante deportee |
US15/764,864 US11174781B2 (en) | 2015-10-05 | 2016-10-05 | Aircraft propulsion assembly equipped with a main fan and with a least one offset fan |
PCT/FR2016/052567 WO2017060628A1 (fr) | 2015-10-05 | 2016-10-05 | Ensemble de propulsion d'un aéronef equipé d'une soufflante principale et d'au moins une soufflante déportée |
GB1616883.3A GB2544625B (en) | 2015-10-05 | 2016-10-05 | Aircraft with a propulsion unit with offset fan |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1559452A FR3041991B1 (fr) | 2015-10-05 | 2015-10-05 | Aeronef avec un moyen de propulsion a soufflante deportee |
FR1559452 | 2015-10-05 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3041991A1 FR3041991A1 (fr) | 2017-04-07 |
FR3041991B1 true FR3041991B1 (fr) | 2020-05-01 |
Family
ID=54366471
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1559452A Active FR3041991B1 (fr) | 2015-10-05 | 2015-10-05 | Aeronef avec un moyen de propulsion a soufflante deportee |
FR1561014A Active FR3041992B1 (fr) | 2015-10-05 | 2015-11-16 | Aeronef avec un moyen de propulsion a soufflante deportee |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1561014A Active FR3041992B1 (fr) | 2015-10-05 | 2015-11-16 | Aeronef avec un moyen de propulsion a soufflante deportee |
Country Status (2)
Country | Link |
---|---|
US (1) | US10850859B2 (fr) |
FR (2) | FR3041991B1 (fr) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3042010B1 (fr) * | 2015-10-05 | 2018-07-13 | Safran Aircraft Engines | Aeronef avec un ensemble propulsif a soufflantes multiples fixe sous aile |
US10618667B2 (en) * | 2016-10-31 | 2020-04-14 | Rolls-Royce Corporation | Fan module with adjustable pitch blades and power system |
FR3065031B1 (fr) * | 2017-04-11 | 2019-06-14 | Airbus Operations | Groupe motopropulseur a plusieurs soufflantes pour aeronef. |
US11142330B2 (en) * | 2018-08-30 | 2021-10-12 | Aurora Flight Sciences Corporation | Mechanically-distributed propulsion drivetrain and architecture |
US11926410B2 (en) * | 2018-12-31 | 2024-03-12 | Jetzero, Inc. | Drag recovery scheme for nacelles |
US11619192B2 (en) * | 2020-07-21 | 2023-04-04 | The Boeing Company | Synergistic hybrid propulsion |
US20220350348A1 (en) * | 2021-04-29 | 2022-11-03 | General Electric Company | Aircraft with a multi-fan propulsion system for controlling flight orientation transitions |
CN113060291A (zh) * | 2021-05-25 | 2021-07-02 | 复旦大学 | 一种固定翼无人机用发动机安装支架及固定翼无人机 |
Family Cites Families (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2526941A (en) * | 1948-06-10 | 1950-10-24 | Northrop Aircraft Inc | Gas turbine system for aircraft propulsion |
US2910254A (en) * | 1955-07-27 | 1959-10-27 | Razak Charles Kenneth | Boundary layer control apparatus relating to aircraft |
US2973165A (en) * | 1957-02-04 | 1961-02-28 | Power Jets Res & Dev Ltd | Aircraft with jet engines in wings |
US3054577A (en) * | 1961-02-27 | 1962-09-18 | Forschungszentrums Der Luftfah | Power plant for jet propelled aircraft |
US3089666A (en) * | 1961-04-13 | 1963-05-14 | Boeing Co | Airplane having changeable thrust direction |
GB1157822A (en) * | 1965-08-21 | 1969-07-09 | Boelkow Gmbh | VTOL Aircraft |
US3592412A (en) * | 1969-10-03 | 1971-07-13 | Boeing Co | Convertible aircraft |
DE2641468C2 (de) * | 1976-09-15 | 1985-06-13 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Flugzeug mit oberhalb der Tragflügel angeordneten Triebwerken |
GB1599730A (en) * | 1978-05-30 | 1981-10-07 | Greenmeadow Engs Ltd | Attachment of masses to aircraft and spacecraft |
GB2268138B (en) * | 1981-06-20 | 1994-05-04 | Rolls Royce | Multi-engined VTOL aircraft |
US4437627A (en) * | 1982-03-12 | 1984-03-20 | The Boeing Company | Integrated power plant installation system |
GB2203105B (en) * | 1987-04-06 | 1990-11-28 | Rolls Royce Plc | Wing mounted ducted fan gas turbine powerplant |
US4821980A (en) * | 1987-09-29 | 1989-04-18 | The Boeing Company | Vibration isolating engine mount |
US5085315A (en) * | 1989-05-05 | 1992-02-04 | Sambell Kenneth W | Wide-range blade pitch control for a folding rotor |
US5065959A (en) * | 1989-11-21 | 1991-11-19 | The Boeing Company | Vibration damping aircraft engine attachment |
US5149016A (en) * | 1991-01-25 | 1992-09-22 | John Huhn | Prop jet airplane propelling system |
FR2698068B1 (fr) * | 1992-11-16 | 1995-02-03 | Airbus Ind | Avion et autre aéronef à moteur pourvu d'ailes. |
US7540450B2 (en) * | 2004-07-16 | 2009-06-02 | Pratt & Whitney Canada Corp. | Aircraft propulsion system |
ES2341514B1 (es) * | 2007-10-03 | 2011-04-18 | Airbus España S.L. | Configuracion estructural para el montaje de un motor sobre la estructura de una aeronave. |
DE102008011643A1 (de) * | 2008-02-28 | 2009-09-03 | Rolls-Royce Deutschland Ltd & Co Kg | Flugzeugantriebseinheit mit Multi-Fan-Ausgestaltung |
WO2010038922A1 (fr) * | 2008-10-04 | 2010-04-08 | Chaeho Lim | Aéronef capable d’atterrir ou de décoller au moyen de voilures tournantes variables |
DE102012106869A1 (de) * | 2012-07-27 | 2014-01-30 | Jonathan Hesselbarth | Senkrecht startendes Flugzeug |
RU2567914C2 (ru) * | 2013-11-07 | 2015-11-10 | Владимир Тарасович Шведов | Самолёт с газотурбинной силовой установкой, содержащей вихревые эжекторные движители |
GB201405388D0 (en) * | 2014-03-26 | 2014-05-07 | Rolls Royce Plc | Turbomachine fan casing assembly |
US9878796B2 (en) * | 2014-03-27 | 2018-01-30 | United Technologies Corporation | Hybrid drive for gas turbine engine |
US9475585B2 (en) * | 2014-06-25 | 2016-10-25 | The Boeing Company | Tilt-rotor vertical-lift aircraft |
GB201412188D0 (en) * | 2014-07-09 | 2014-08-20 | Rolls Royce Plc | Two-part gas turbine engine |
US9533768B2 (en) * | 2014-08-12 | 2017-01-03 | The Boeing Company | Aircraft engine mounting system |
US9950800B2 (en) * | 2014-11-26 | 2018-04-24 | The Boeing Company | Integrated pusher turbofan for aircraft |
-
2015
- 2015-10-05 FR FR1559452A patent/FR3041991B1/fr active Active
- 2015-11-16 FR FR1561014A patent/FR3041992B1/fr active Active
-
2016
- 2016-10-04 US US15/284,895 patent/US10850859B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3041992B1 (fr) | 2019-05-10 |
US20170240286A1 (en) | 2017-08-24 |
US10850859B2 (en) | 2020-12-01 |
FR3041992A1 (fr) | 2017-04-07 |
FR3041991A1 (fr) | 2017-04-07 |
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Legal Events
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Year of fee payment: 2 |
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Effective date: 20170407 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20180809 |
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