[go: up one dir, main page]

WO2008073069A3 - Véhicule aérien sans équipage - Google Patents

Véhicule aérien sans équipage Download PDF

Info

Publication number
WO2008073069A3
WO2008073069A3 PCT/US2006/032280 US2006032280W WO2008073069A3 WO 2008073069 A3 WO2008073069 A3 WO 2008073069A3 US 2006032280 W US2006032280 W US 2006032280W WO 2008073069 A3 WO2008073069 A3 WO 2008073069A3
Authority
WO
WIPO (PCT)
Prior art keywords
propulsion device
aerial vehicle
unmanned aerial
wing
assembly
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/US2006/032280
Other languages
English (en)
Other versions
WO2008073069A2 (fr
Inventor
James Alman
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.)
CYBER DEFENSE SYSTEMS Inc
Original Assignee
CYBER DEFENSE SYSTEMS Inc
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 CYBER DEFENSE SYSTEMS Inc filed Critical CYBER DEFENSE SYSTEMS Inc
Priority to PCT/US2006/032280 priority Critical patent/WO2008073069A2/fr
Publication of WO2008073069A2 publication Critical patent/WO2008073069A2/fr
Anticipated expiration legal-status Critical
Publication of WO2008073069A3 publication Critical patent/WO2008073069A3/fr
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • B64C15/12—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets the power plant being tiltable
    • 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
    • B64C29/0041—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 jet motors
    • B64C29/0066—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 jet motors with horizontal jet and jet deflector
    • 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
    • B64C29/0041—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 jet motors
    • B64C29/0075—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 jet motors the motors being tiltable relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/12—Canard-type aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/25—Fixed-wing aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/80—Vertical take-off or landing, e.g. using rockets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • B64U2101/31—UAVs specially adapted for particular uses or applications for imaging, photography or videography for surveillance
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Harvester Elements (AREA)
  • Toys (AREA)

Abstract

La présente invention concerne un véhicule aérien sans équipage comprenant un fuselage, un ensemble stabilisateur horizontal, un ensemble aile, un dispositif de propulsion avant et au moins un dispositif de propulsion arrière. Le fuselage a une partie d'extrémité avant et une partie arrière. L'ensemble stabilisateur horizontal a une aile gauche et une aile droite. L'ensemble aile a une aile sensiblement alignée avec l'ensemble stabilisateur horizontal et parallèle à celui-ci. Lors de son activation, le dispositif de propulsion avant fournit une poussée aidant à soulever le véhicule aérien sans équipage. Lors de leur activation, le ou les dispositifs de propulsion arrière sont tournés de façon sélective de quatre-vingt-dix degrés de façon à diriger la poussée provenant du ou des dispositifs de propulsion arrière vers le bas et vers l'arrière. Le dispositif de propulsion avant et le ou les dispositifs de propulsion arrière coopèrent pour fournir une poussée vers le bas entraînant le soulèvement du véhicule aérien sans équipage.
PCT/US2006/032280 2006-08-18 2006-08-18 Véhicule aérien sans équipage Ceased WO2008073069A2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/US2006/032280 WO2008073069A2 (fr) 2006-08-18 2006-08-18 Véhicule aérien sans équipage

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US60/709,210 2006-08-18
PCT/US2006/032280 WO2008073069A2 (fr) 2006-08-18 2006-08-18 Véhicule aérien sans équipage

Publications (2)

Publication Number Publication Date
WO2008073069A2 WO2008073069A2 (fr) 2008-06-19
WO2008073069A3 true WO2008073069A3 (fr) 2009-04-09

Family

ID=39512215

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2006/032280 Ceased WO2008073069A2 (fr) 2006-08-18 2006-08-18 Véhicule aérien sans équipage

Country Status (1)

Country Link
WO (1) WO2008073069A2 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8162253B2 (en) * 2009-08-19 2012-04-24 Seiford Sr Donald S Convertible vehicle for road, air, and water usage
CN103158871B (zh) * 2013-03-07 2015-07-29 杨义华 一种垂直起降的喷气式飞机
CN103612752A (zh) * 2013-03-07 2014-03-05 杨义华 一种垂直起降的喷气式飞机之垂直起飞技术
CN103612753A (zh) * 2013-03-07 2014-03-05 杨义华 一种垂直起降的喷气式飞机的降落方法
CN103921636A (zh) * 2013-12-02 2014-07-16 王庆忠 一种翼装快艇
CN105892480B (zh) * 2016-03-21 2018-12-11 南京航空航天大学 异构多无人机系统协同察打任务自组织方法
CN107512386A (zh) * 2017-08-19 2017-12-26 中国矿业大学 一种矿井空气动力高速飞行器及控制方法
CN111273678B (zh) * 2019-11-26 2021-07-02 成都飞机工业（集团）有限责任公司 一种大升阻比无人机边界保护方法
CN113110595B (zh) * 2021-05-12 2022-06-21 中国人民解放军陆军工程大学 面向目标核查印证的异构无人机群协同方法

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3454241A (en) * 1966-08-24 1969-07-08 Man Turbo Gmbh Swiveling lift engines for vtol aircraft
US3460783A (en) * 1966-08-11 1969-08-12 Bolkow Gmbh Apparatus for positioning of the thrust engines of a vertical take-off and landing aircraft
US4982914A (en) * 1966-05-18 1991-01-08 Karl Eickmann Aircraft with a plurality of propellers, a pipe structure for thereon holdable wings, for vertical take off and landing
US5407150A (en) * 1990-07-25 1995-04-18 Sandleir Vtol Aircraft Co., Ltd. Thrust unit for VTOL aircraft

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4982914A (en) * 1966-05-18 1991-01-08 Karl Eickmann Aircraft with a plurality of propellers, a pipe structure for thereon holdable wings, for vertical take off and landing
US3460783A (en) * 1966-08-11 1969-08-12 Bolkow Gmbh Apparatus for positioning of the thrust engines of a vertical take-off and landing aircraft
US3454241A (en) * 1966-08-24 1969-07-08 Man Turbo Gmbh Swiveling lift engines for vtol aircraft
US5407150A (en) * 1990-07-25 1995-04-18 Sandleir Vtol Aircraft Co., Ltd. Thrust unit for VTOL aircraft

Also Published As

Publication number Publication date
WO2008073069A2 (fr) 2008-06-19

Similar Documents

Publication Publication Date Title
USD592547S1 (en) Parallel hybrid three-wheel passenger vehicle with reconfigurable chassis and power systems
ATE467560T1 (de) Flugzeug mit vermindertem lärmpegel
BG111231A (en) ROAD-AIR VEHICLE
GB2469431B (en) Flying-wing aircraft
WO2016086066A8 (fr) Planche à roulettes motorisées
WO2007079306A3 (fr) Appareil pour reduire la trainee aerodynamique
WO2011066004A3 (fr) Véhicule transformable pour usage routier, aérien et aquatique
WO2009034805A1 (fr) Aéronef de type flottant à pression positive
WO2008129244A3 (fr) Véhicule aéroporté annulaire
WO2008081098A8 (fr) Avion a empennages arrieres annulaires
WO2006072960A3 (fr) Vehicules adav a soufflantes canalisees
WO2011066031A3 (fr) Système de commande d'élevon
WO2006073634A3 (fr) Aeronef a decollage et atterrissage verticaux (adav) a aile fixee en fleche negative
WO2008147484A3 (fr) Véhicule volant modulaire
EP2351607A3 (fr) Jouet volant
WO2015179122A3 (fr) Véhicule à double usage pour transport aérien et terrestre et procédés associés
WO2008073069A3 (fr) Véhicule aérien sans équipage
WO2008125868A3 (fr) Aéronef
ATE462645T1 (de) Flugzeug mit reduzierten umweltauswirkungen
WO2006133062A3 (fr) Aeronef jouet
WO2010026345A3 (fr) Structure d'ensemble siège pour aéronef et fuselage adapté
MX355578B (es) Sistema de carenado posterior aerodinámico para un remolque.
CA2896584A1 (fr) Structure de coffre de vehicule
WO2006022813A3 (fr) Avion a fuselage duel haute portance, faible trainee
WO2009016094A3 (fr) Empennage de queue pour aéronef

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 06851861

Country of ref document: EP

Kind code of ref document: A2

NENP Non-entry into the national phase

Ref country code: DE

NENP Non-entry into the national phase

Ref country code: RU

32PN Ep: public notification in the ep bulletin as address of the adressee cannot be established

Free format text: NOTING OF LOSS OF RIGHTS PURSUANT TO RULE 112(1) EPC (EPO FORM 1205A DATED 02-06-2009)

122 Ep: pct application non-entry in european phase

Ref document number: 06851861

Country of ref document: EP

Kind code of ref document: A2