WO2014021798A3 - Vertical take off/landing and balance system for aerial vehicles - Google Patents

Vertical take off/landing and balance system for aerial vehicles Download PDF

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Publication number
WO2014021798A3
WO2014021798A3 PCT/TR2013/000229 TR2013000229W WO2014021798A3 WO 2014021798 A3 WO2014021798 A3 WO 2014021798A3 TR 2013000229 W TR2013000229 W TR 2013000229W WO 2014021798 A3 WO2014021798 A3 WO 2014021798A3
Authority
WO
WIPO (PCT)
Prior art keywords
landing
aerial vehicles
vertical take
electric motor
take
Prior art date
Application number
PCT/TR2013/000229
Other languages
French (fr)
Other versions
WO2014021798A2 (en
Inventor
Oran BULENT
Original Assignee
Bulent Oran
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 Bulent Oran filed Critical Bulent Oran
Publication of WO2014021798A2 publication Critical patent/WO2014021798A2/en
Publication of WO2014021798A3 publication Critical patent/WO2014021798A3/en

Links

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
    • B64C29/0008—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
    • B64C29/0025—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 fixed relative to the fuselage
    • 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
    • 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
    • B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
    • 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
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/03—Annular blade-carrying members having blades on the inner periphery of the annulus and extending inwardly radially, i.e. inverted rotors
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)

Abstract

The invention relates to a system providing vertical take off and landing for military aircrafts or civilian airplanes, unmanned aerial vehicles and so on. The rotating fans working with electric motor taking electricity from the very powerful generator integrated with the main motor, provides balance and take off-landing of aerial vehicle. The rotors, which haven't axis shafts, belonging to special designed electric motors, rotates with the spiral fan blades integrated with the rotor in the magnetic shell supporting with bearings. The system uses the advantages of direct driver technology and brushless electric motor together. This system doesn't cause an environmental pollution and a noise pollution and works with high efficiency for years. Both production and also maintenance of this system are very easy. The project relates to a system providing a feature of vertical take off and landing as well as to remain in the air without motion for hours at the point determined beforehand. This feature enables all aerial vehicles used for search and rescue operations and also special military missions successfully.
PCT/TR2013/000229 2012-07-31 2013-07-24 Vertical take off/landing and balance system for aerial vehicles WO2014021798A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
TR2012/08854 2012-07-31
TR2012/08854A TR201208854A2 (en) 2012-07-31 2012-07-31 Vertical take off and landing system for aircraft

Publications (2)

Publication Number Publication Date
WO2014021798A2 WO2014021798A2 (en) 2014-02-06
WO2014021798A3 true WO2014021798A3 (en) 2014-04-03

Family

ID=47679847

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/TR2013/000229 WO2014021798A2 (en) 2012-07-31 2013-07-24 Vertical take off/landing and balance system for aerial vehicles

Country Status (2)

Country Link
TR (1) TR201208854A2 (en)
WO (1) WO2014021798A2 (en)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITAR20130041A1 (en) * 2013-10-14 2015-04-15 Navis S R L AUXILIARY PROPULSION SYSTEM FOR TAKE OFF AND VERTICAL LANDING OF AIRPLANES THAT USES RECHARGEABLE ENERGY STORAGE SYSTEMS
ITMI20132018A1 (en) * 2013-12-03 2015-06-04 Navis S R L PROPULSION SYSTEM FOR VERTICAL OR SUBSTANTIALLY VERTICAL FLYING AIRCRAFT
WO2015056124A1 (en) * 2013-10-14 2015-04-23 Navis S.R.L. Propulsion system for vertical or substantially vertical takeoff aircraft
FR3018768B1 (en) * 2014-03-19 2016-03-04 Andre Chaneac VERTICAL TAKE-OFF AND VERTICAL AIRCRAFT COMPRISING AT LEAST ONE PROPULSIVE ASSEMBLY AND A PROPULSIVE MEDIUM
WO2015191017A1 (en) 2014-06-13 2015-12-17 Oran Bülent Propeller with super conductive electrical motor for air vehicles
IL233942B (en) 2014-08-04 2020-01-30 Israel Aerospace Ind Ltd Propulsion system assembly
CN104503459A (en) * 2014-11-25 2015-04-08 深圳市鸣鑫航空科技有限公司 Multi-rotor unmanned aerial vehicle recycling system
FR3033363B1 (en) * 2015-03-04 2017-04-07 Andre Chaneac TURBOJET ENGINEERING WHETHER A BLOWER IS A GENERATOR AND ITS MOUNTING ON A VERTICAL TAKE-OFF AND VERTICAL AIRCRAFT AIRCRAFT
CN104843181B (en) * 2015-04-10 2017-10-20 桂林航龙科讯电子技术有限公司 A kind of oil electric mixed dynamic fixed-wing VUAV system
DE102015209673A1 (en) * 2015-05-27 2016-12-01 Siemens Aktiengesellschaft Drive unit for an aircraft, aircraft with a drive unit and use of a double coil actuator motor
FR3037038A1 (en) * 2015-06-08 2016-12-09 Andre Chaneac TURBO REACTOR DRIVING A BLOWER AND A GENERATOR, ITS MOUNTING ON A VERTICAL LANDING AEROFEF AND LANDFILLING
US9714090B2 (en) 2015-06-12 2017-07-25 Sunlight Photonics Inc. Aircraft for vertical take-off and landing
US11034443B2 (en) 2015-06-12 2021-06-15 Sunlight Aerospace Inc. Modular aircraft assembly for airborne and ground transport
CN105015760A (en) * 2015-07-07 2015-11-04 西北工业大学 Propeller-type lift-enhancing structure for symmetric wing
US9950788B2 (en) 2015-07-14 2018-04-24 Northrop Grumman Systems Corporation Magrail, bleed air driven lift fan
EP3124379B1 (en) * 2015-07-29 2019-05-01 Airbus Defence and Space GmbH Hybrid-electric drive train for vtol drones
CN105366049A (en) * 2015-11-24 2016-03-02 中国航空工业集团公司沈阳飞机设计研究所 Vertical takeoff and landing unmanned aerial vehicle
CN105487093B (en) * 2015-12-29 2018-04-13 湖南云顶智能科技有限公司 For recovering the device and method for the unmanned plane that falls
US10183744B2 (en) 2016-02-10 2019-01-22 Lockheed Martin Corporation Magnetic orientation detent
WO2017200504A1 (en) * 2016-05-16 2017-11-23 Oran Avci Elif Shaftless multi blade wind turbine
EP3290334B1 (en) * 2016-08-31 2021-08-11 Sunlight Aerospace Inc. Aircraft for vertical take-off and landing
RU2634609C1 (en) * 2016-09-09 2017-11-01 Федеральное государственное бюджетное образовательное учреждение высшего образования "Московский авиационный институт (национальный исследовательский университет)" Unmanned aerial vehicle control method and flight control actuating unit for method actualization
US10479496B2 (en) 2016-10-31 2019-11-19 Lockheed Martin Corporation Magnetic orientation detent with motor assist
CN107632617B (en) * 2017-09-28 2020-02-14 深圳市道通智能航空技术有限公司 Control method and device for unmanned aerial vehicle
DE102018120200A1 (en) * 2018-08-20 2020-02-20 Dr. Ing. H.C. F. Porsche Aktiengesellschaft aircraft
GB201814869D0 (en) 2018-09-03 2018-10-31 Rolls Royce Plc Aircraft Propulsion System
GB201814255D0 (en) 2018-09-03 2018-10-17 Rolls Royce Plc Aircraft propulsion system
FR3094955B1 (en) * 2019-04-12 2022-06-03 Safran Aircraft thruster
US11661183B2 (en) 2020-03-16 2023-05-30 D. Anthony Windisch Small light vertical take-off and landing capable delta wing aircraft

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2509442A (en) * 1945-04-17 1950-05-30 Matheisel Rudolph Inverse rotor
WO2006113877A2 (en) * 2005-04-20 2006-10-26 Lugg Richard H Hybrid jet/electric vtol aircraft
US20090121073A1 (en) * 2006-04-03 2009-05-14 The Boeing Company Aircraft having a jet engine, an adjustable aft nozzle, and an electric vertical fan

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2509442A (en) * 1945-04-17 1950-05-30 Matheisel Rudolph Inverse rotor
WO2006113877A2 (en) * 2005-04-20 2006-10-26 Lugg Richard H Hybrid jet/electric vtol aircraft
US20090121073A1 (en) * 2006-04-03 2009-05-14 The Boeing Company Aircraft having a jet engine, an adjustable aft nozzle, and an electric vertical fan

Also Published As

Publication number Publication date
TR201208854A2 (en) 2012-12-21
WO2014021798A2 (en) 2014-02-06

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