FR3113399B1 - Dispositif aérodynamique pour aéronef et aéronef muni d’un tel dispositif - Google Patents

Dispositif aérodynamique pour aéronef et aéronef muni d’un tel dispositif Download PDF

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Publication number
FR3113399B1
FR3113399B1 FR2008477A FR2008477A FR3113399B1 FR 3113399 B1 FR3113399 B1 FR 3113399B1 FR 2008477 A FR2008477 A FR 2008477A FR 2008477 A FR2008477 A FR 2008477A FR 3113399 B1 FR3113399 B1 FR 3113399B1
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France
Prior art keywords
aircraft
wings
landing
taking
vtol
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
Application number
FR2008477A
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English (en)
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FR3113399A1 (fr
Inventor
Ponnat Arnaud De
Mischa Masson
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Fleasy
Original Assignee
Fleasy
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
Application filed by Fleasy filed Critical Fleasy
Priority to FR2008477A priority Critical patent/FR3113399B1/fr
Priority to PCT/FR2021/051040 priority patent/WO2022034272A1/fr
Publication of FR3113399A1 publication Critical patent/FR3113399A1/fr
Application granted granted Critical
Publication of FR3113399B1 publication Critical patent/FR3113399B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

Dispositif permettant à un aéronef pouvant décoller et atterrir verticalement de le faire dans des conditions de vent fort.L’invention concerne un dispositif permettant à un aéronef en vol pouvant décoller et atterrir verticalement VTOL et dont les ailes sont orientées verticalement lors de ces phases (par exemple aéronef « tail sitter » ou « tilt wing ») de réaliser des décollages et atterrissage dans des conditions de vent fort.Le dispositif est constitué d’ailes (1), de plans liés aux ailes (2) par une liaison de type pivot (3), d’un servo moteur ou actionneur (4) permettant de modifier l’angle entre l’aile (1) et le plan (2), d’un automate ou calculateur (5). L’ensemble permet de maintenir l’aéronef VTOL en position « vent de travers » lors des phases de décollage, montée, descente et atterrissage. Figure pour l’abrégé : Fig 3
FR2008477A 2020-08-13 2020-08-13 Dispositif aérodynamique pour aéronef et aéronef muni d’un tel dispositif Active FR3113399B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR2008477A FR3113399B1 (fr) 2020-08-13 2020-08-13 Dispositif aérodynamique pour aéronef et aéronef muni d’un tel dispositif
PCT/FR2021/051040 WO2022034272A1 (fr) 2020-08-13 2021-06-10 Aeronef a decollage et a atterrissage vertical

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2008477 2020-08-13
FR2008477A FR3113399B1 (fr) 2020-08-13 2020-08-13 Dispositif aérodynamique pour aéronef et aéronef muni d’un tel dispositif

Publications (2)

Publication Number Publication Date
FR3113399A1 FR3113399A1 (fr) 2022-02-18
FR3113399B1 true FR3113399B1 (fr) 2023-03-31

Family

ID=74183221

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2008477A Active FR3113399B1 (fr) 2020-08-13 2020-08-13 Dispositif aérodynamique pour aéronef et aéronef muni d’un tel dispositif

Country Status (2)

Country Link
FR (1) FR3113399B1 (fr)
WO (1) WO2022034272A1 (fr)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130206921A1 (en) * 2012-02-15 2013-08-15 Aurora Flight Sciences Corporation System, apparatus and method for long endurance vertical takeoff and landing vehicle
US9821909B2 (en) * 2016-04-05 2017-11-21 Swift Engineering, Inc. Rotating wing assemblies for tailsitter aircraft
CN108502183A (zh) * 2017-02-25 2018-09-07 原熙 折叠翼直升飞机

Also Published As

Publication number Publication date
WO2022034272A1 (fr) 2022-02-17
FR3113399A1 (fr) 2022-02-18

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