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WO2004065208A3 - Quiet vertical takeoff and landing aircraft using ducted, magnetic induction air-impeller rotors - Google Patents

Quiet vertical takeoff and landing aircraft using ducted, magnetic induction air-impeller rotors Download PDF

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Publication number
WO2004065208A3
WO2004065208A3 PCT/US2004/001689 US2004001689W WO2004065208A3 WO 2004065208 A3 WO2004065208 A3 WO 2004065208A3 US 2004001689 W US2004001689 W US 2004001689W WO 2004065208 A3 WO2004065208 A3 WO 2004065208A3
Authority
WO
WIPO (PCT)
Prior art keywords
ducted
magnetic induction
rotors
vertical takeoff
landing aircraft
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/US2004/001689
Other languages
French (fr)
Other versions
WO2004065208A2 (en
Inventor
John K Sanders Jr
J Kenneth Sanders
Arturo Aviles Jr
Arturo F Aviles
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.)
UFOZ LLC
Original Assignee
UFOZ LLC
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 UFOZ LLC filed Critical UFOZ LLC
Publication of WO2004065208A2 publication Critical patent/WO2004065208A2/en
Anticipated expiration legal-status Critical
Publication of WO2004065208A3 publication Critical patent/WO2004065208A3/en
Ceased legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/20Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/12Rotor drives
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016Aircraft 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
    • B64C29/0025Aircraft 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 fixed relative to the fuselage
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016Aircraft 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
    • B64C29/0033Aircraft 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
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
  • Toys (AREA)

Abstract

A VTOL aircraft with magnetic linear induction powered impeller rotors (21b). The craft may have many configurations of multiple or single rotors. Directional control is included through the use of vanes or thrust tilting of the rotors.
PCT/US2004/001689 2003-01-23 2004-01-22 Quiet vertical takeoff and landing aircraft using ducted, magnetic induction air-impeller rotors Ceased WO2004065208A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US29/175,100 USD543928S1 (en) 2003-01-23 2003-01-23 Hovercraft with stacked rotor thruster and winglets
US29/175,100 2003-01-23

Publications (2)

Publication Number Publication Date
WO2004065208A2 WO2004065208A2 (en) 2004-08-05
WO2004065208A3 true WO2004065208A3 (en) 2005-10-13

Family

ID=32769809

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2004/001689 Ceased WO2004065208A2 (en) 2003-01-23 2004-01-22 Quiet vertical takeoff and landing aircraft using ducted, magnetic induction air-impeller rotors

Country Status (2)

Country Link
US (1) USD543928S1 (en)
WO (1) WO2004065208A2 (en)

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USD846440S1 (en) * 2016-10-18 2019-04-23 Samsung Electronics Co., Ltd. Drone
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USD847021S1 (en) * 2016-10-18 2019-04-30 Samsung Electroncis Co., Ltd. Drone
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USD846438S1 (en) * 2016-10-18 2019-04-23 Samsung Electronics Co., Ltd. Drone
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USD843305S1 (en) * 2016-10-25 2019-03-19 Aeromobil R&D, S. R. O. Flying car
USD844537S1 (en) * 2016-10-25 2019-04-02 Aeromobil R&D, S. R. O. Body of a flying car
USD843304S1 (en) * 2016-10-25 2019-03-19 Aeromobil R&D, S. R. O. Tail section of flying car
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USD816581S1 (en) * 2016-12-06 2018-05-01 Jianjia Zhao Quadcopter
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EP3354559B1 (en) * 2017-01-26 2019-04-03 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A thrust producing unit with at least two rotor assemblies and a shrouding
EP3366586B1 (en) 2017-02-27 2020-08-19 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A thrust producing unit with at least two rotor assemblies and a shrouding
RU179110U1 (en) * 2017-06-07 2018-04-26 Азрет Рамазанович Аслануков Winged Aircraft
USD830897S1 (en) * 2017-09-19 2018-10-16 Hyunhwan CHOI Unmanned aerial vehicle
JP2020536016A (en) * 2017-10-02 2020-12-10 カリフォルニア インスティチュート オブ テクノロジー Autonomous flight ambulance
US10988245B2 (en) 2017-11-13 2021-04-27 Bell Textron Inc. Segmented duct for tilting proprotors
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106809376A (en) * 2017-02-16 2017-06-09 武汉八维时空信息技术股份有限公司 Helicopter based on gyroscope principle
CN106809376B (en) * 2017-02-16 2019-03-29 武汉八维时空信息技术股份有限公司 Helicopter based on gyroscope principle

Also Published As

Publication number Publication date
WO2004065208A2 (en) 2004-08-05
USD543928S1 (en) 2007-06-05

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