EA201491529A1 - Механизм регулировки крыльев - Google Patents

Механизм регулировки крыльев

Info

Publication number
EA201491529A1
EA201491529A1 EA201491529A EA201491529A EA201491529A1 EA 201491529 A1 EA201491529 A1 EA 201491529A1 EA 201491529 A EA201491529 A EA 201491529A EA 201491529 A EA201491529 A EA 201491529A EA 201491529 A1 EA201491529 A1 EA 201491529A1
Authority
EA
Eurasian Patent Office
Prior art keywords
wing
around
wing structure
rotation
longitudinal axis
Prior art date
Application number
EA201491529A
Other languages
English (en)
Inventor
Иоганнес Райтер
Original Assignee
Иоганнес Райтер
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 Иоганнес Райтер filed Critical Иоганнес Райтер
Publication of EA201491529A1 publication Critical patent/EA201491529A1/ru

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
    • B64C29/0033—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
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/001—Vibration damping devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B64C27/16—Drive of rotors by means, e.g. propellers, mounted on rotor blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B64C27/16—Drive of rotors by means, e.g. propellers, mounted on rotor blades
    • B64C27/18—Drive of rotors by means, e.g. propellers, mounted on rotor blades the means being jet-reaction apparatus
    • 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
    • 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
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/385—Variable incidence wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10—Wings
    • B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
    • 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
    • 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
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/12—Propulsion using turbine engines, e.g. turbojets or turbofans
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U60/00—Undercarriages
    • B64U60/40—Undercarriages foldable or retractable

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

Настоящее изобретение относится к устройству для генерирования аэродинамической подъемной силы и, в частности, воздушному летательному аппарату (100) вертикального взлета и посадки. Крыльевая конструкция (110) содержит по меньшей мере одну силовую установку (111), при этом силовая установка (111) содержит вращающуюся массу, которая выполнена с возможностью вращения вокруг оси (117) вращения. Крыльевая конструкция (110) установлена на фюзеляж (101) таким образом, чтобы крыльевая конструкция (110) могла быть повернута вокруг продольной оси (112) крыла крыльевой конструкции (110) и чтобы крыльевая конструкция (110) могла вращаться относительно фюзеляжа (101) и вокруг дополнительной оси вращения, которая отличается от продольной оси (112) крыла. Механизм регулировки регулирует угол поворота крыльевой конструкции (110) вокруг продольной оси (112) крыла под воздействием прецессионной силы (Fp), которая вызывает поворот крыльевой конструкции (110) вокруг продольной оси (112) крыла.
EA201491529A 2012-02-13 2013-02-13 Механизм регулировки крыльев EA201491529A1 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB1202441.0A GB201202441D0 (en) 2012-02-13 2012-02-13 Wing adjustment mechanism
PCT/EP2013/052911 WO2013120918A1 (en) 2012-02-13 2013-02-13 Wing adjusting mechanism

Publications (1)

Publication Number Publication Date
EA201491529A1 true EA201491529A1 (ru) 2015-04-30

Family

ID=45930023

Family Applications (2)

Application Number Title Priority Date Filing Date
EA201491529A EA201491529A1 (ru) 2012-02-13 2013-02-13 Механизм регулировки крыльев
EA201491528A EA201491528A1 (ru) 2012-02-13 2013-02-13 Воздушный летательный аппарат вертикального взлета и посадки с двумя крыльевыми конструкциями

Family Applications After (1)

Application Number Title Priority Date Filing Date
EA201491528A EA201491528A1 (ru) 2012-02-13 2013-02-13 Воздушный летательный аппарат вертикального взлета и посадки с двумя крыльевыми конструкциями

Country Status (9)

Country Link
US (2) US20150232178A1 (ru)
EP (2) EP2814735A1 (ru)
CN (1) CN104470800A (ru)
BR (1) BR112014020090A8 (ru)
CA (1) CA2864580A1 (ru)
EA (2) EA201491529A1 (ru)
GB (2) GB201202441D0 (ru)
IN (1) IN2014DN07628A (ru)
WO (2) WO2013120918A1 (ru)

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Also Published As

Publication number Publication date
EP2814734A1 (en) 2014-12-24
EA201491528A1 (ru) 2015-01-30
BR112014020090A8 (pt) 2017-07-11
BR112014020090A2 (ru) 2017-06-20
US20150028155A1 (en) 2015-01-29
US20150232178A1 (en) 2015-08-20
GB201202441D0 (en) 2012-03-28
WO2013120912A1 (en) 2013-08-22
GB201214887D0 (en) 2012-10-03
EP2814735A1 (en) 2014-12-24
CN104470800A (zh) 2015-03-25
CA2864580A1 (en) 2013-08-22
WO2013120918A1 (en) 2013-08-22
IN2014DN07628A (ru) 2015-05-15

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