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WO2003066429A3 - Vehicules de decollage et d'atterrissage verticaux ameliores - Google Patents

Vehicules de decollage et d'atterrissage verticaux ameliores Download PDF

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Publication number
WO2003066429A3
WO2003066429A3 PCT/US2003/003730 US0303730W WO03066429A3 WO 2003066429 A3 WO2003066429 A3 WO 2003066429A3 US 0303730 W US0303730 W US 0303730W WO 03066429 A3 WO03066429 A3 WO 03066429A3
Authority
WO
WIPO (PCT)
Prior art keywords
vertical take
improved vertical
nacelles
landing vehicles
additional
Prior art date
Application number
PCT/US2003/003730
Other languages
English (en)
Other versions
WO2003066429A2 (fr
Inventor
Paul S Moller
Original Assignee
Moller Int Inc
Paul S Moller
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 Moller Int Inc, Paul S Moller filed Critical Moller Int Inc
Priority to EP03709001A priority Critical patent/EP1478570A4/fr
Priority to AU2003212957A priority patent/AU2003212957A1/en
Publication of WO2003066429A2 publication Critical patent/WO2003066429A2/fr
Publication of WO2003066429A3 publication Critical patent/WO2003066429A3/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C37/00—Convertible aircraft
    • 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
    • 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
    • B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
    • B64C11/48—Units of two or more coaxial propellers
    • 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
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/04—Aircraft characterised by the type or position of power plants of piston type
    • B64D27/06—Aircraft characterised by the type or position of power plants of piston type within, or attached to, wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically
    • 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
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Wind Motors (AREA)
  • Motorcycle And Bicycle Frame (AREA)

Abstract

L'invention concerne un véhicule VTOL comprenant un fuselage doté de deux ailes pliables, deux fuseaux moteurs basculants fixés aux ailes, un stabilisateur vertical, un stabilisateur horizontal et deux propulseurs auxiliaires. Chaque fuseau moteur contient un système d'aubes placés à l'arrière de l'ouverture et des actionneurs s'étendant et rétractant les aubes avec des mécanismes de bascule de fuseau moteur permettant de dévier l'écoulement d'air sur une fourchette prédéterminée d'angles partant de l'horizontal. Chaque fuseau horaire contient également deux moteurs rotatifs, chacun commandant directement un ventilateur, des ventilateurs sont placés en regard et fonctionnent dans les sens contraires à la rotation à la même vitesse rotative. Dans un mode de réalisation, on prévoit deux fuseaux moteurs supplémentaires fixés au fuselage au lieu des propulseurs auxiliaires. Un système de commande de vol informatisé redondant maintient la stabilité du véhicule à mesure qu'il passe d'un mode de vol à un autre mode.
PCT/US2003/003730 2002-02-08 2003-02-06 Vehicules de decollage et d'atterrissage verticaux ameliores WO2003066429A2 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP03709001A EP1478570A4 (fr) 2002-02-08 2003-02-06 Vehicules de decollage et d'atterrissage verticaux ameliores
AU2003212957A AU2003212957A1 (en) 2002-02-08 2003-02-06 Improved vertical take-off and landing vehicles

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US35527002P 2002-02-08 2002-02-08
US60/355,270 2002-02-08

Publications (2)

Publication Number Publication Date
WO2003066429A2 WO2003066429A2 (fr) 2003-08-14
WO2003066429A3 true WO2003066429A3 (fr) 2004-02-05

Family

ID=27734494

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2003/003730 WO2003066429A2 (fr) 2002-02-08 2003-02-06 Vehicules de decollage et d'atterrissage verticaux ameliores

Country Status (3)

Country Link
EP (1) EP1478570A4 (fr)
AU (1) AU2003212957A1 (fr)
WO (1) WO2003066429A2 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2864029B1 (fr) * 2003-12-23 2006-04-07 Eurocopter France Aeronef convertible pourvu de deux "tilt fan" de part et d'autre du fuselage et d'un "fan" fixe insere dans le fuselage
CN102582828A (zh) * 2012-02-02 2012-07-18 刘长亮 一种双涵道复合尾舵垂直起降飞行器
RU2534112C1 (ru) * 2013-05-14 2014-11-27 Алексей Борисович Моров Аппарат вертикального взлёта и посадки
FR3065399A1 (fr) * 2017-04-25 2018-10-26 Jonas Popelin Aeronef a propulsion-combinee
DE102019210007A1 (de) * 2019-07-08 2021-01-14 Volkswagen Aktiengesellschaft Vertikal start- und landefähiges Flugobjekt und Mantelkörper
CN115335609A (zh) * 2019-08-19 2022-11-11 顶峰推进有限责任公司 增强推力的提升和推进系统
RU2765892C1 (ru) * 2021-02-04 2022-02-04 Александр Трофимович Осинин Система поворота движителя летательного аппарата вертикального взлета и посадки
JP7723886B1 (ja) * 2024-11-14 2025-08-15 アラセ・アイザワ・アエロスパシアル合同会社 無人航空機の制御方法

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5115996A (en) * 1990-01-31 1992-05-26 Moller International, Inc. Vtol aircraft
US5419514A (en) * 1993-11-15 1995-05-30 Duncan; Terry A. VTOL aircraft control method
US5505407A (en) * 1993-09-09 1996-04-09 Fran Rich Chi Associates Air-land vehicle

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3083936A (en) * 1959-02-18 1963-04-02 Scott C Rethorst Aircraft
US4358074A (en) 1979-05-24 1982-11-09 The Boeing Company Propulsion system for V/STOL aircraft
US5839691A (en) 1996-05-22 1998-11-24 Lariviere; Jean Soulez Vertical takeoff and landing aircraft

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5115996A (en) * 1990-01-31 1992-05-26 Moller International, Inc. Vtol aircraft
US5505407A (en) * 1993-09-09 1996-04-09 Fran Rich Chi Associates Air-land vehicle
US5419514A (en) * 1993-11-15 1995-05-30 Duncan; Terry A. VTOL aircraft control method

Also Published As

Publication number Publication date
AU2003212957A1 (en) 2003-09-02
EP1478570A4 (fr) 2008-04-09
AU2003212957A8 (en) 2003-09-02
EP1478570A2 (fr) 2004-11-24
WO2003066429A2 (fr) 2003-08-14

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