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WO2020201644A3 - Dispositif hypersustentateur - Google Patents

Dispositif hypersustentateur Download PDF

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Publication number
WO2020201644A3
WO2020201644A3 PCT/FR2020/000084 FR2020000084W WO2020201644A3 WO 2020201644 A3 WO2020201644 A3 WO 2020201644A3 FR 2020000084 W FR2020000084 W FR 2020000084W WO 2020201644 A3 WO2020201644 A3 WO 2020201644A3
Authority
WO
WIPO (PCT)
Prior art keywords
lift device
aerodyne
aeronautics
field
relates
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.)
Ceased
Application number
PCT/FR2020/000084
Other languages
English (en)
Other versions
WO2020201644A2 (fr
Inventor
Olivier Lamaille
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.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from FR1903467A external-priority patent/FR3085033B1/fr
Priority claimed from FR1903468A external-priority patent/FR3085030B1/fr
Application filed by Individual filed Critical Individual
Priority to US17/600,579 priority Critical patent/US20220177115A1/en
Priority to CA3135682A priority patent/CA3135682A1/fr
Publication of WO2020201644A2 publication Critical patent/WO2020201644A2/fr
Publication of WO2020201644A3 publication Critical patent/WO2020201644A3/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/04—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for blowing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/01—Boundary layer ingestion [BLI] propulsion
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/04—Boundary layer controls by actively generating fluid flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/06—Boundary layer controls by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Lift-Guide Devices, And Elevator Ropes And Cables (AREA)
  • Handcart (AREA)

Abstract

La présente invention concerne le domaine de l'aéronautique et plus particulièrement porte sur un dispositif hypersustentateur et un aérodyne comprenant un tel dispositif hypersustentateur.
PCT/FR2020/000084 2019-04-01 2020-04-03 Appareil pour la navigation aérienne et ses dispositifs Ceased WO2020201644A2 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US17/600,579 US20220177115A1 (en) 2019-04-01 2020-04-03 High-lift device
CA3135682A CA3135682A1 (fr) 2019-04-01 2020-04-03 Appareil pour la navigation aerienne et ses dispositifs

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
FR1903467A FR3085033B1 (fr) 2018-07-19 2019-04-01 Dispositif de securite avion
FR1903468A FR3085030B1 (fr) 2018-07-19 2019-04-01 Dispositif hypersustentateur pour avion
FR1903468 2019-04-01
FR1903467 2019-04-01

Publications (2)

Publication Number Publication Date
WO2020201644A2 WO2020201644A2 (fr) 2020-10-08
WO2020201644A3 true WO2020201644A3 (fr) 2021-03-18

Family

ID=70680529

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2020/000084 Ceased WO2020201644A2 (fr) 2019-04-01 2020-04-03 Appareil pour la navigation aérienne et ses dispositifs

Country Status (3)

Country Link
US (1) US20220177115A1 (fr)
CA (1) CA3135682A1 (fr)
WO (1) WO2020201644A2 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12296954B2 (en) * 2021-05-26 2025-05-13 The Boeing Company Thin wing drive mechanism
US12060155B2 (en) * 2022-01-25 2024-08-13 Electra Aero, Inc. System and method for lift augmentation of an aircraft tailplane
US12358634B2 (en) * 2023-02-08 2025-07-15 Anduril Industries, Inc. Assembly for dual engine vertical take off and landing collapsible fixed wing aircraft

Citations (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3104082A (en) * 1961-11-16 1963-09-17 Edward C Polhamus Variable sweep aircraft wing
GB1248450A (en) * 1967-12-27 1971-10-06 Saab Scania Aktiebolag Fomerly Improvements in and relating to a method of braking an aircraft during landing
US3658279A (en) * 1970-04-21 1972-04-25 Lockheed Aircraft Corp Integrated propulsion system
US3920203A (en) * 1974-12-23 1975-11-18 Boeing Co Thrust control apparatus for obtaining maximum thrust reversal in minimum time upon landing of an aircraft
FR2281875A1 (fr) * 1974-08-16 1976-03-12 Kaniut Herbert Perfectionnements aux empennages pour avions
US4326686A (en) * 1980-02-15 1982-04-27 Runge Thomas M Fan jet engine bypass air delivery system for blown wing aircraft lift augmentation device
US4354646A (en) * 1978-09-20 1982-10-19 Rockwell International Corporation Variable dihedral angle tail unit for supersonic aircraft
US5252068A (en) * 1991-12-31 1993-10-12 Flight Dynamics, Incorporated Weight-shift flight control transducer and computer controlled flight simulator, hang gliders and ultralight aircraft utilizing the same
DE4237873A1 (de) * 1992-11-10 1994-05-19 Hans Dipl Ing Wirtz Senkrechtstartflugzeug mit aktiver Auftriebserzeugung und aktiver Steuermomenterzeugung
EP1604900A1 (fr) * 2004-06-11 2005-12-14 Airbus France Aéronef muni d'un carénage ventral, et carénage ventral
US20060016930A1 (en) * 2004-07-09 2006-01-26 Steve Pak Sky hopper
WO2009083262A2 (fr) * 2007-12-30 2009-07-09 Airbus Deutschland Gmbh Composant structurel aile-fuselage permettant de relier deux ailes portantes et une section de fuselage à un avion
FR2935351A1 (fr) * 2008-08-29 2010-03-05 Airbus France Avion a fuselage suspendu sous l'aile.
US20100276538A1 (en) * 2004-11-23 2010-11-04 Helou Jr Elie Cargo aircraft system
US20120025006A1 (en) * 2010-07-29 2012-02-02 Luther David I In-line staged horizontal takeoff and landing space plane
CN104787306A (zh) * 2015-03-23 2015-07-22 顾一明 一种利用气动力控制飞行姿态的低速安全飞行器
US20160347443A1 (en) * 2013-12-23 2016-12-01 Sang-hyun Lee Multi-rotor flying object
EP3181443A1 (fr) * 2015-12-18 2017-06-21 The Boeing Company Structure de fuselage pour agencer des queues et des plans canard de différentes tailles et formes
US20180016027A1 (en) * 2016-07-18 2018-01-18 Elwha Llc System and method for payload management for an unmanned aircraft
US20180079485A1 (en) * 2016-09-21 2018-03-22 Bell Helicopter Textron Inc. Wing Pivot Structure for Tiltrotor Aircraft
CN207450249U (zh) * 2017-11-08 2018-06-05 沈阳旋飞航空技术有限公司 一种无人机旋翼变桨距机构
EP3366582A1 (fr) * 2017-02-28 2018-08-29 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Aéronef multirotor ayant une cellule et un agencement d'unités de production de poussée
CN108750103A (zh) * 2018-06-14 2018-11-06 广东伟力智能科技有限公司 一种可实现垂直定高飞行及水平定高飞行的飞行器
WO2018208652A1 (fr) * 2017-05-08 2018-11-15 Insitu, Inc. Aéronef modulaire à capacité de décollage et d'atterrissage verticaux
US20200094941A1 (en) * 2018-09-25 2020-03-26 The Boeing Company Articulated empennage with ruddervator

Patent Citations (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3104082A (en) * 1961-11-16 1963-09-17 Edward C Polhamus Variable sweep aircraft wing
GB1248450A (en) * 1967-12-27 1971-10-06 Saab Scania Aktiebolag Fomerly Improvements in and relating to a method of braking an aircraft during landing
US3658279A (en) * 1970-04-21 1972-04-25 Lockheed Aircraft Corp Integrated propulsion system
FR2281875A1 (fr) * 1974-08-16 1976-03-12 Kaniut Herbert Perfectionnements aux empennages pour avions
US3920203A (en) * 1974-12-23 1975-11-18 Boeing Co Thrust control apparatus for obtaining maximum thrust reversal in minimum time upon landing of an aircraft
US4354646A (en) * 1978-09-20 1982-10-19 Rockwell International Corporation Variable dihedral angle tail unit for supersonic aircraft
US4326686A (en) * 1980-02-15 1982-04-27 Runge Thomas M Fan jet engine bypass air delivery system for blown wing aircraft lift augmentation device
US5252068A (en) * 1991-12-31 1993-10-12 Flight Dynamics, Incorporated Weight-shift flight control transducer and computer controlled flight simulator, hang gliders and ultralight aircraft utilizing the same
DE4237873A1 (de) * 1992-11-10 1994-05-19 Hans Dipl Ing Wirtz Senkrechtstartflugzeug mit aktiver Auftriebserzeugung und aktiver Steuermomenterzeugung
EP1604900A1 (fr) * 2004-06-11 2005-12-14 Airbus France Aéronef muni d'un carénage ventral, et carénage ventral
US20060016930A1 (en) * 2004-07-09 2006-01-26 Steve Pak Sky hopper
US20100276538A1 (en) * 2004-11-23 2010-11-04 Helou Jr Elie Cargo aircraft system
WO2009083262A2 (fr) * 2007-12-30 2009-07-09 Airbus Deutschland Gmbh Composant structurel aile-fuselage permettant de relier deux ailes portantes et une section de fuselage à un avion
FR2935351A1 (fr) * 2008-08-29 2010-03-05 Airbus France Avion a fuselage suspendu sous l'aile.
US20120025006A1 (en) * 2010-07-29 2012-02-02 Luther David I In-line staged horizontal takeoff and landing space plane
US20160347443A1 (en) * 2013-12-23 2016-12-01 Sang-hyun Lee Multi-rotor flying object
CN104787306A (zh) * 2015-03-23 2015-07-22 顾一明 一种利用气动力控制飞行姿态的低速安全飞行器
EP3181443A1 (fr) * 2015-12-18 2017-06-21 The Boeing Company Structure de fuselage pour agencer des queues et des plans canard de différentes tailles et formes
US20180016027A1 (en) * 2016-07-18 2018-01-18 Elwha Llc System and method for payload management for an unmanned aircraft
US20180079485A1 (en) * 2016-09-21 2018-03-22 Bell Helicopter Textron Inc. Wing Pivot Structure for Tiltrotor Aircraft
EP3366582A1 (fr) * 2017-02-28 2018-08-29 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Aéronef multirotor ayant une cellule et un agencement d'unités de production de poussée
WO2018208652A1 (fr) * 2017-05-08 2018-11-15 Insitu, Inc. Aéronef modulaire à capacité de décollage et d'atterrissage verticaux
CN207450249U (zh) * 2017-11-08 2018-06-05 沈阳旋飞航空技术有限公司 一种无人机旋翼变桨距机构
CN108750103A (zh) * 2018-06-14 2018-11-06 广东伟力智能科技有限公司 一种可实现垂直定高飞行及水平定高飞行的飞行器
US20200094941A1 (en) * 2018-09-25 2020-03-26 The Boeing Company Articulated empennage with ruddervator

Also Published As

Publication number Publication date
US20220177115A1 (en) 2022-06-09
CA3135682A1 (fr) 2020-10-08
WO2020201644A2 (fr) 2020-10-08

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