WO2003099653A1 - Aeronef a decollage et atterrissage verticaux - Google Patents

Aeronef a decollage et atterrissage verticaux Download PDF

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Publication number
WO2003099653A1
WO2003099653A1 PCT/RU2003/000058 RU0300058W WO03099653A1 WO 2003099653 A1 WO2003099653 A1 WO 2003099653A1 RU 0300058 W RU0300058 W RU 0300058W WO 03099653 A1 WO03099653 A1 WO 03099653A1
Authority
WO
WIPO (PCT)
Prior art keywords
landing
vertical take
machine
radius
flying machine
Prior art date
Application number
PCT/RU2003/000058
Other languages
English (en)
Russian (ru)
Inventor
Boris Kirillovich Smirnov
Original Assignee
Boris Kirillovich Smirnov
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 Boris Kirillovich Smirnov filed Critical Boris Kirillovich Smirnov
Priority to AU2003227384A priority Critical patent/AU2003227384A1/en
Publication of WO2003099653A1 publication Critical patent/WO2003099653A1/fr

Links

Classifications

    • 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
    • B64C11/006—Paddle wheels
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/003—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
    • B64C39/005—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a horizontal transversal axis

Definitions

  • the flying machine is a vertical take-off and landing.
  • a field of technology is available for a short time.
  • the invention is available to flying devices, to short-range flying machines and to take off, and also may be used for food.
  • Le ⁇ a ⁇ elnaya machine ve ⁇ i ⁇ alnym vzlo ⁇ m and ⁇ sad ⁇ y m ⁇ zhe ⁇ by ⁇ is ⁇ lz ⁇ vana for ⁇ e ⁇ ev ⁇ z ⁇ i ⁇ assazhi ⁇ v and g ⁇ uz ⁇ v in sil ⁇ vy ⁇ s ⁇ u ⁇ u ⁇ a x, ⁇ CHS, s ⁇ i ⁇ eln ⁇ - ⁇ em ⁇ n ⁇ ny ⁇ ⁇ ab ⁇ a ⁇ , ⁇ smiches ⁇ y ⁇ sli and ⁇ . d.
  • T REDUCE the mechanism of vertical take-off and landing. Increase the coefficient of usefulness.
  • the lifting force arises in the following way.
  • the vehicle is driven by centrifugal force, while the air is generated by the air. If you take two corner discs in the middle of a hole. Radius of the disc. , the radius of the response * £, the distance between the disks ( Figure 1, 2). These two disks are connected by blades, as many as the blades ⁇ . For ⁇ chn ⁇ s ⁇ i l ⁇ as ⁇ i nuzhn ⁇ sdela ⁇ ⁇ my ⁇ ⁇ ⁇ uga and za ⁇ e ⁇ i ⁇ on dis ⁇ a ⁇ ⁇ a ⁇ , ⁇ a ⁇ ⁇ azan ⁇ on ⁇ igu ⁇ e 3.
  • the 2nd area was located on the horizontal area.
  • SIGNIFICANT FOX (DR. 26)
  • a flying machine in a cosmic environment, it is necessary to supply it with a jet engine.
  • Le ⁇ a ⁇ elnaya machine ve ⁇ i ⁇ aln ⁇ g ⁇ vzlo ⁇ a and ⁇ sad ⁇ i ⁇ dnimae ⁇ sya on d ⁇ s ⁇ a ⁇ chn ⁇ b ⁇ lshuyu vys ⁇ u not vy ⁇ lyuchaya us ⁇ ys ⁇ v ⁇ ve ⁇ i ⁇ aln ⁇ g ⁇ vzlo ⁇ a and ⁇ sad ⁇ i, v ⁇ lyuchae ⁇ sya ⁇ ea ⁇ ivny dviga ⁇ el, ⁇ em most nabi ⁇ ae ⁇ more b ⁇ ly ⁇ e vys ⁇ y and za ⁇ em vy ⁇ lyuchayu ⁇ us ⁇ ys ⁇ v ⁇ ve ⁇ i ⁇ aln ⁇ g ⁇ vzlo ⁇ a and ⁇ sad ⁇ i not
  • Landing is produced in the home. Turning off the motors, in the case of close proximity to the vehicle, turn on the silent and 2.7. Information supporting the possibility of carrying out the invention. When you move the body, you will experience a valuable running force. This force is equal - *

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Emergency Lowering Means (AREA)
  • Feedback Control In General (AREA)

Abstract

L'aéronef à décollage et atterrissage verticaux est constitué d'un propulseur comprenant deux disques comportant en leur milieu un orifice et reliés par des pales. Les disques et les pales forment une turbine. Vu de haut, cette turbine est recouverte d'une aile semi-rigide, immobile par rapport au corps de l'aéronef. Pour assurer la stabilité de l'aéronef on utilise un nombre pair de turbines et la contre-rotation des turbines.
PCT/RU2003/000058 2002-05-23 2003-02-20 Aeronef a decollage et atterrissage verticaux WO2003099653A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2003227384A AU2003227384A1 (en) 2002-05-23 2003-02-20 Aircraft for vertical take of and landing

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2002113467 2002-05-23
RU2002113467/28A RU2002113467A (ru) 2002-05-23 2002-05-23 Летательная машина с вертикальным взлётом и посадкой

Publications (1)

Publication Number Publication Date
WO2003099653A1 true WO2003099653A1 (fr) 2003-12-04

Family

ID=29580129

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2003/000058 WO2003099653A1 (fr) 2002-05-23 2003-02-20 Aeronef a decollage et atterrissage verticaux

Country Status (3)

Country Link
AU (1) AU2003227384A1 (fr)
RU (1) RU2002113467A (fr)
WO (1) WO2003099653A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2899118A1 (fr) 2014-01-27 2015-07-29 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Hélicoptère comprenant un fuselage et au moins un rotor principal

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1344283A (en) * 1918-10-22 1920-06-22 John W Webb Flying-machine
US4269135A (en) * 1977-11-14 1981-05-26 Michelino Labonia Hydroplanes
DE4320625A1 (de) * 1992-05-26 1995-01-05 Eberhard Bach Schwingenrotor
US5454530A (en) * 1993-05-28 1995-10-03 Mcdonnell Douglas Helicopter Company Canard rotor/wing
RU2090454C1 (ru) * 1995-03-17 1997-09-20 Ким Петрович Белошапкин Летательный аппарат тарельчатый планетного и межпланетного плавания
RU2097311C1 (ru) * 1995-08-29 1997-11-27 Александр Тимофеевич Андреев Летательное устройство для подъема и перемещения груза

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1344283A (en) * 1918-10-22 1920-06-22 John W Webb Flying-machine
US4269135A (en) * 1977-11-14 1981-05-26 Michelino Labonia Hydroplanes
DE4320625A1 (de) * 1992-05-26 1995-01-05 Eberhard Bach Schwingenrotor
US5454530A (en) * 1993-05-28 1995-10-03 Mcdonnell Douglas Helicopter Company Canard rotor/wing
RU2090454C1 (ru) * 1995-03-17 1997-09-20 Ким Петрович Белошапкин Летательный аппарат тарельчатый планетного и межпланетного плавания
RU2097311C1 (ru) * 1995-08-29 1997-11-27 Александр Тимофеевич Андреев Летательное устройство для подъема и перемещения груза

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2899118A1 (fr) 2014-01-27 2015-07-29 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Hélicoptère comprenant un fuselage et au moins un rotor principal
US9527577B2 (en) 2014-01-27 2016-12-27 Airbus Helicopters Deutschland GmbH Rotorcraft with a fuselage and at least one main rotor

Also Published As

Publication number Publication date
RU2002113467A (ru) 2004-01-27
AU2003227384A1 (en) 2003-12-12

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