EA200901189A1 - Летательный аппарат - Google Patents

Летательный аппарат

Info

Publication number
EA200901189A1
EA200901189A1 EA200901189A EA200901189A EA200901189A1 EA 200901189 A1 EA200901189 A1 EA 200901189A1 EA 200901189 A EA200901189 A EA 200901189A EA 200901189 A EA200901189 A EA 200901189A EA 200901189 A1 EA200901189 A1 EA 200901189A1
Authority
EA
Eurasian Patent Office
Prior art keywords
wing
fuselage
propulsion system
thrust
viewed
Prior art date
Application number
EA200901189A
Other languages
English (en)
Other versions
EA014867B1 (ru
Inventor
Харри Джордж Деннис Гоуслинг
Original Assignee
Гоу Сайнс Лимитед
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 Гоу Сайнс Лимитед filed Critical Гоу Сайнс Лимитед
Publication of EA200901189A1 publication Critical patent/EA200901189A1/ru
Publication of EA014867B1 publication Critical patent/EA014867B1/ru

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/06Aircraft not otherwise provided for having disc- or ring-shaped wings
    • B64C39/062Aircraft not otherwise provided for having disc- or ring-shaped wings having annular wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/25Fixed-wing aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • B64U30/26Ducted or shrouded rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/13Propulsion using external fans or propellers
    • B64U50/14Propulsion using external fans or propellers ducted or shrouded
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/18Thrust vectoring
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/30UAVs specially adapted for particular uses or applications for imaging, photography or videography

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Air-Flow Control Members (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • General Factory Administration (AREA)
  • Ink Jet Recording Methods And Recording Media Thereof (AREA)
  • Transmission Devices (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Air-Conditioning For Vehicles (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)

Abstract

Летательный аппарат, имеющий крыло-фюзеляж, которое определяет ось крыла-фюзеляжа и представляется, в основном, кольцевым, если смотреть на него вдоль оси крыла-фюзеляжа, внутреннее кольцевое пространство, определяющее канал, открытый на обоих концах. Система тяги имеет одну или несколько пар двигательных установок, при этом каждая пара имеет первую двигательную установку, установленную на крыле-фюзеляже и расположенную на первой стороне плоскости, включающей ось крыла-фюзеляжа, и вторую двигательную установку, установленную на крыле-фюзеляже и позиционированную на второй стороне плоскости, включающей ось крыла-фюзеляжа. Направление тяги первой двигательной установки может регулироваться независимо от направления тяги второй двигательной установки, и/или величина тяги первой двигательной установки может быть отрегулирована независимо от величины тяги второй двигательной установки. В некоторых примерах осуществления крыло-фюзеляж представляется крылом обратной стреловидности, если смотреть на него под первым углом обзора, и крылом прямой стреловидности, если смотреть на него со второй позиции просмотра под прямым углом к первому углу обзора.
EA200901189A 2007-04-18 2008-04-16 Летательный аппарат EA014867B1 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0707512.0A GB0707512D0 (en) 2007-04-18 2007-04-18 Annular airborne vehicle
PCT/GB2008/001329 WO2008129244A2 (en) 2007-04-18 2008-04-16 Annular airborne vehicle

Publications (2)

Publication Number Publication Date
EA200901189A1 true EA200901189A1 (ru) 2010-02-26
EA014867B1 EA014867B1 (ru) 2011-02-28

Family

ID=38135027

Family Applications (1)

Application Number Title Priority Date Filing Date
EA200901189A EA014867B1 (ru) 2007-04-18 2008-04-16 Летательный аппарат

Country Status (10)

Country Link
US (3) US8262016B2 (ru)
EP (3) EP2277775B1 (ru)
JP (1) JP5205447B2 (ru)
CN (1) CN101765540B (ru)
AT (3) ATE485218T1 (ru)
DE (1) DE602008003110D1 (ru)
EA (1) EA014867B1 (ru)
ES (1) ES2359455T3 (ru)
GB (1) GB0707512D0 (ru)
WO (1) WO2008129244A2 (ru)

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Also Published As

Publication number Publication date
GB0707512D0 (en) 2007-05-30
DE602008003110D1 (de) 2010-12-02
EA014867B1 (ru) 2011-02-28
CN101765540B (zh) 2013-03-27
US20120305714A1 (en) 2012-12-06
US8262016B2 (en) 2012-09-11
CN101765540A (zh) 2010-06-30
JP2010524765A (ja) 2010-07-22
WO2008129244A3 (en) 2008-12-11
JP5205447B2 (ja) 2013-06-05
US20100044496A1 (en) 2010-02-25
ES2359455T3 (es) 2011-05-23
EP2277775B1 (en) 2012-05-09
ATE556930T1 (de) 2012-05-15
EP2137069B1 (en) 2010-10-20
US8408489B2 (en) 2013-04-02
US8328131B2 (en) 2012-12-11
EP2308754B1 (en) 2012-05-09
ATE556931T1 (de) 2012-05-15
EP2308754A1 (en) 2011-04-13
US20120256043A1 (en) 2012-10-11
EP2137069A2 (en) 2009-12-30
ATE485218T1 (de) 2010-11-15
EP2277775A1 (en) 2011-01-26
WO2008129244A2 (en) 2008-10-30

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Legal Events

Date Code Title Description
PC4A Registration of transfer of a eurasian patent by assignment
MM4A Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s)

Designated state(s): AM AZ BY KZ KG MD TJ TM RU