GB2434784A - A vehicle with a rotational mass providing lift - Google Patents

A vehicle with a rotational mass providing lift Download PDF

Info

Publication number
GB2434784A
GB2434784A GB0701837A GB0701837A GB2434784A GB 2434784 A GB2434784 A GB 2434784A GB 0701837 A GB0701837 A GB 0701837A GB 0701837 A GB0701837 A GB 0701837A GB 2434784 A GB2434784 A GB 2434784A
Authority
GB
United Kingdom
Prior art keywords
fan
vehicle
lift
rotatable mass
mass
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.)
Withdrawn
Application number
GB0701837A
Other versions
GB0701837D0 (en
Inventor
Philip Arthur Leeson
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.)
Bates Michael K
LEESON PHILIP A
Original Assignee
MICHAEL K BATES
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 MICHAEL K BATES filed Critical MICHAEL K BATES
Publication of GB0701837D0 publication Critical patent/GB0701837D0/en
Publication of GB2434784A publication Critical patent/GB2434784A/en
Withdrawn legal-status Critical Current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
    • 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
    • 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
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/001Flying saucers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/24Aircraft characterised by the type or position of power plants using steam or spring force
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Wind Motors (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A vehicle (10, figure 1) has a plurality of lift generating apparatuses (14) mounted thereon. Each lift generating apparatus comprises an annular array of electrical battery cells 36, with turbine blades 38 on the periphery, a fan or airscrew 21 concentrically and coaxially therewithin, and two interacting arrays of magnetic armatures 30, 32 between the array of battery cells 36 and the fan or airscrew 21, to provide electromagnetic coupling. The battery cells provide a rotational mass which is capable of being rotated at high speed to produce lift effects of the type associated with rotation of a fly wheel or gyroscope. An airstream from the fan 26 can be directed via ducts and directional nozzles so as to provide a propulsive force, and the turbine blades 38 are adjustable to control the rotational speed of the mass so as to act as a braking device.

Description

<p>* Vehicle Raving Novel Lift and Propulsion Apparatus and Lift and
Propulsion Apparatus Therefor This invention relates to a vehicle having a novel lift and propulsion apparatus, and to a lift and propulsion apparatus for the vehicle.</p>
<p>The majority of vehicles run with wheels, or in the case of sleds, runners, in contact with the surface of the ground. Except for specially adapted vehicles, using for example tracks or specially designed tyres, most of these vehicles are in practice restricted to operating on firm road surfaces. In order to provide a "go anywhere" capability, air-cushion vehicles were developed wherein fans providing a powerful down-draught are positioned under the vehicle to provide a cushion of air to provide a friction free support, propulsion of the vehicle then being provided by aircraft type :. engines such as airscrews, or turbo-fans. The limitation of air-cushion vehicles is that * *.. ***</p>
<p>the air cushion has to be confined by a surrounding skirt, and damage to the skirt can * . render the vehicle inoperative.</p>
<p> 15 Such vehicles are therefore generally used in an amphibious role, as ferries ::. and assault craft, and as runabouts in swampy terrain. *</p>
<p>S..... . . . . * * It is an object of the invention to provide a vehicle, and lift and propulsion apparatus for vehicles which will enable a vehicle to operate without the hindrances entailed by the necessity for a confining skirt as with air-cushion vehicles.</p>
<p>According to the invention, a vehicle is provided with a lift generating apparatus which incorporates a rotatable mass which is capable of being rotated at high speed to produce lift effects of the type associated with rotation of a fly wheel.</p>
<p>The rotatable mass preferably comprises an annular array of battery cells.</p>
<p>The apparatus preferably also includes a propulsion fan or airscrew which is mounted co-axially and concentrically of the rotatable mass, and which is preferably driven by being magnetically coupled to the rotatable mass.</p>
<p>The magnetic coupling may be achieved by an electromagnetic apparatus which may be mounted concentrically within the rotatable miss, and about the fan or a.u.i...i w.</p>
<p>The magnetic apparatus may comprise inner and outer concentric arrays of windings which interact respectively with permanent magnet armatures on the outer periphery of the fan casing, and with further permanent magnet armatures on the inner periphery of the annular battery cell array. The rotatable mass is thus cause to rotate by appropriate actuation of the outer array of windings, accelerating from rest to the rotational rate required to produce inertial flywheel or gyroscopic effects which lead to the production of lift. Similarly the fan propeller can be rotated to produce an air * stream of sufficient strength to be effective as a propulsion source, and means may be S..</p>
<p>* 15 provided to direct the air stream as required, which may be achieved by use of ducts and directable nozzles.</p>
<p>S.....</p>
<p>* The outer surface of the rotatable mass may be provided with adjustable turbine blades which are useable to control the rotational speed of the mass, acting as a braking device.</p>
<p>A vehicle according to the invention is preferably equipped with a plurality of such lift generating apparatuses, preferably symmetrically arranged to achieve an even distribution of effects. For example, a generally rectangular vehicle may be equipped with four lift generating apparatuses disposed towards the corners of the rectangle.</p>
<p>A preferred embodiment of vehicle according to the invention and of a lift and propulsion apparatus according to the invention for use in such a vehicle will now be described with reference to the accompanying drawings, wherein:-Figure 1 is a side elevation of a vehicle according to the invention; Figure 2 is a perspective view of a complete lift generating and propulsion apparatus for use in the vehicle of Figure 1; and Figure 3 is a perspective view of the apparatus of Figure 2 in its housing; and Figure 4 is a cross-sectional view of the apparatus of Figure 2, taken along a diameter thereof.</p>
<p>Referring first to Figure 1, a vehicle according to the invention comprises a base frame 10, and a body shell 11 the latter housing a forward control position, and a * . * I, passenger saloon, for use for example as a public service vehicle. The rear of the body shell mounts a ducted fan 12 which acts as a stabilising impeller. ***</p>
<p>Below the base frame 10 are mounted four nacelles 14 which each contain a * I lift and propulsion apparatus according to the invention which will be described more * fully below. The undersides of the nacelles 14 are provided with means for standing, when the vehicle is parked, such as skids or wheels. The nacelles 14 are located towards the four corners of the generally rectangular base plan of the vehicle and thus provide for an even distribution of the lifting effect of the drive apparatus.</p>
<p>One drive arid lift apparatus according to the invention, and as used in each of the nacelles 14 of the vehicle, is shown in more detail in Figures 2 to 4. The apparatus comprises an axial shaft 20 upon which an upper fan or airscrew 21 and a lower fan or airscrew 22 are rotatably mounted by means of hub bushes 23, 24 (see Figure 4). The fans comprise blades 25, the inner ends of which are joined to the respective hub bushes 23, 24 and the outer ends of which are connected to respective upper and lower peripheral rings 26, 27.</p>
<p>The peripheral rings 26, 27 carry on their outwards faces permanently magnetised plates 28, 29, spaced about the rings which form armatures which interact with inner electromagnets 30, 31. These in turn interact with outer eiectromanets 32, 33.</p>
<p>This double ring of electromagnets is surrounded by an annular rotatable body 34, which comprises a rotatable mass which when rotated rapidly, provides the gyroscope/flywheel effects which give rise to the lifting force. The body 34 comprises a ring of metal, in which is formed an array of cylindrical bores 35.</p>
<p>:... Each cylindrical bore 35 accommodates one or more battery cells 36. The *Ss* battery cells 36 provide the power required to energise the electromagnets 30, 31 and 32,33.</p>
<p>The inner face of the body 34 is provided with permanently magnetised plates * * 37 which act as armatures which interact with the outer electromagnets 32, 33 to ****** * provide rotational force to the annular body 34.</p>
<p>The outer face of the body 34 is provided with an array of turbine blades 38 which can be feathered to provide variable retardation to the body when rotating in order to control the spin rate of the body and act as a variable braking means.</p>
<p>Figure 2 shows that the rings of electromagnets are retained by a multi-armed spider 39 at each side, one above and one below, with radial arms 40 which extend from a hub ring 41 about the centre shaft 20.</p>
<p>* As shown in Figure 3, the entire assembly is contained within a housing comprising a peripheral wall 45 with openings 46 spaced thereabout to admit air to the space about the body 34 in which the turbine blade 38 are located, and a cover 47 (these also being a similar cover below the assembly) with a central aperture for the shaft 20, and elliptical apertures 48 which allow passage of air to or from the fan.</p>
<p> _-i. _..__.._ _1_._._.J..:...i.. 4t.</p>
<p>iu upcIauuII Ui uic appa.Lau ucpcuu vu uic uucivu LiUIIC uw a rotating body of high inertial mass, when rotated at a sufficient rotational rate, will exhibit gyroscopic precession effects which tend to act against gravity, producing so-called "fly wheel" effects and appearing to provide an antigravitational thrust.</p>
<p>In each of the units provided, one in each nacelle 14 of the vehicle, and according to the drawings, and above description, the body 34 provides a massive annular member due to the weight of the battery cells, and of the metal forming the **.* body enclosing the bores 35 in which the battery cells are located.</p>
<p>*.*. The body 34 can be rotated at between 100 to 500 rpm, whilst the * 15 electromagnets rotate at from 100 to 1900 rpm. The fans 21, 22 may rotate at from to 14 rpm.</p>
<p>****** * The electromagnets can conveniently be composed of laminar windings for compactness.</p>
<p>Suitable ducting arrangements may be provided to direct the air jet from the fans to a propulsion outlet at the rear of each respective nacelle 14.</p>
<p>Alternative or supplementary propulsion units, such as turbo-fans may be mounted elsewhere on the vehicle if required.</p>

Claims (1)

  1. <p>Claims 1. A vehicle provided with a lift generating apparatus which
    incorporates a rotatable mass which is capable of being rotated at high speed to produce lift effects of the type associated with rotation of a fly wheel.</p>
    <p>I hft vnrctiic fr g ii-I lnnar2tlI i1wnmArItinC, l -. -ri----, 1 0 -rotatable mass which is capable of being rotated at high speed to produce lift effects of the type associated with rotation of a fly wheel.</p>
    <p>3. Apparatus according to claim I or 2 wherein the rotatable mass comprises an annular array of batteiy cells.</p>
    <p>4. Apparatus according to claim 3 which also includes a propulsion fan or airscrew which is moulded coaxially and concentrically of the rotatable mass.</p>
    <p>5. Apparatus according to claim 4 wherein the propulsion fan or airscrew is driven by being magnetically coupled to the rotatable mass. S..</p>
    <p>* 15 6. Apparatus according to claim 5 wherein the magnetic coupling is achieved by an electromagnetic apparatus which is mounted concentrically within the * rotatable mass, and around the fan or airscrew.</p>
    <p>7. Apparatus according to claim 6 wherein the magnetic apparatus comprises inner and outer concentric arrays of windings which interact respectively with permanent magnet armatures on the outer periphery of the fan casing, and with further permanent magnet armatures on the inner periphery of the annular battery cell array.</p>
    <p>8. Apparatus according to claim 7 wherein means are provided to direct an airstream from the fan or propeller comprising ducts and directable nozzles.</p>
    <p>9. Apparatus according to any of claims 3 to 8 wherein the outer surface of the rotatable mass is provided with adjustable turbine blades which are useable to control the rotational speed of the mass, acting as a braking device.</p>
    <p>10. A vehicle according to claim 1, including lift generating apparatus according to any of claims 3 to 9 which vehicle is equipped with a plurality of such lift generating apparatus syzrmici icaily arranged to achicvc an even distribution of effects 11. A lift generating apparatus substantially as hereinbefore described with reference to and as illustrated in the accompanying drawings. * * * *.* **.. * * **. ** * * ** * ** * ***</p>
    <p>I * I * S I ***</p>
    <p>S III.. * *</p>
GB0701837A 2006-02-02 2007-01-31 A vehicle with a rotational mass providing lift Withdrawn GB2434784A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0602094.5A GB0602094D0 (en) 2006-02-02 2006-02-02 The arc

Publications (2)

Publication Number Publication Date
GB0701837D0 GB0701837D0 (en) 2007-03-14
GB2434784A true GB2434784A (en) 2007-08-08

Family

ID=36100906

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB0602094.5A Ceased GB0602094D0 (en) 2006-02-02 2006-02-02 The arc
GB0701837A Withdrawn GB2434784A (en) 2006-02-02 2007-01-31 A vehicle with a rotational mass providing lift

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GBGB0602094.5A Ceased GB0602094D0 (en) 2006-02-02 2006-02-02 The arc

Country Status (1)

Country Link
GB (2) GB0602094D0 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104787315A (en) * 2015-04-17 2015-07-22 何春旺 Duct power device and aircraft

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3220761A1 (en) * 1982-06-02 1984-03-15 Friedrich 7798 Pfullendorf Schuster Drive gyroscope
GB2207753A (en) * 1987-06-24 1989-02-08 David Raymond Morgan Force generating apparatus
GB2209832A (en) * 1987-09-12 1989-05-24 Harold Aspden Gyroscopic propulsion and levitation
GB2255152A (en) * 1991-04-26 1992-10-28 Roger William Seeley Flywheel and power unit
US20020148308A1 (en) * 2001-02-23 2002-10-17 Alvaro Rush Gyroscope based propulsion apparatus
US20060230847A1 (en) * 2005-04-19 2006-10-19 Hewatt Chris B Method and apparatus for gyroscopic propulsion

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3220761A1 (en) * 1982-06-02 1984-03-15 Friedrich 7798 Pfullendorf Schuster Drive gyroscope
GB2207753A (en) * 1987-06-24 1989-02-08 David Raymond Morgan Force generating apparatus
GB2209832A (en) * 1987-09-12 1989-05-24 Harold Aspden Gyroscopic propulsion and levitation
GB2255152A (en) * 1991-04-26 1992-10-28 Roger William Seeley Flywheel and power unit
US20020148308A1 (en) * 2001-02-23 2002-10-17 Alvaro Rush Gyroscope based propulsion apparatus
US20060230847A1 (en) * 2005-04-19 2006-10-19 Hewatt Chris B Method and apparatus for gyroscopic propulsion

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104787315A (en) * 2015-04-17 2015-07-22 何春旺 Duct power device and aircraft

Also Published As

Publication number Publication date
GB0701837D0 (en) 2007-03-14
GB0602094D0 (en) 2006-03-15

Similar Documents

Publication Publication Date Title
EP3205577B1 (en) Magnetic orientation detent
US3437290A (en) Vertical lift aircraft
US20050082421A1 (en) Flying machine
US3633849A (en) Flying craft
EP1775214A1 (en) Rapid air quantity generating and wind direction changing device and aircraft having the device mounted on side face of airframe
US20220380029A1 (en) Self propelled thrust-producing controlled moment gyroscope
CN112469969B (en) Thrust-producing split flywheel gyroscope method and apparatus
US20170361930A1 (en) Flying vehicle
CN105711824A (en) ROTARY WING DRONE provided with accessory enabling amphibious type rotary wing drone
KR20210048534A (en) Electromagnetic gyroscopic stabilization propulsion system method and apparatus
WO2021117054A1 (en) Electric flying vehicle with outer rotor in wheel motor
US20180272856A1 (en) Ducted Fan Propulsion System
JP2006021733A (en) Vertical taking-off and landing machine installing rapid wind quantity generation wind direction changing device of double inversion two-axis tilt as device for lift and propulsion of machine body and using it as steering means
GB2434784A (en) A vehicle with a rotational mass providing lift
WO2021111097A1 (en) An unmanned aerial vehicle
GB2371684A (en) Lift generating means for aircraft
WO2021216241A2 (en) Hubless propulsion unit
EP1247737B1 (en) Lift generating means for aircraft
JP2003212190A (en) Manned airship
JP2004168276A (en) Lift generating device
US20230257111A1 (en) Self propelled thrust-producing controlled moment gyroscope
EP0020569A1 (en) Thrusters for airship control
GB2578083A (en) An unmanned aerial vehicle
US11909279B1 (en) Prime mover with integral drivers for providing multiple modes of locomotion
EP4069586B1 (en) An unmanned aerial vehicle

Legal Events

Date Code Title Description
COOA Change in applicant's name or ownership of the application

Owner name: BATES, MICHAEL K

Free format text: FORMER APPLICANT(S): LEESON, PHILIP A

Owner name: LEESON, PHILIP A

Free format text: FORMER APPLICANT(S): LEESON, PHILIP A

WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)