WO2002012722A1 - Flying disk shaped flying/space vehicle with the use of a new technic of thrust through the rolling of a wheel - Google Patents
Flying disk shaped flying/space vehicle with the use of a new technic of thrust through the rolling of a wheel Download PDFInfo
- Publication number
- WO2002012722A1 WO2002012722A1 PCT/GR2001/000032 GR0100032W WO0212722A1 WO 2002012722 A1 WO2002012722 A1 WO 2002012722A1 GR 0100032 W GR0100032 W GR 0100032W WO 0212722 A1 WO0212722 A1 WO 0212722A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- wheel
- airwheel
- rolling
- main body
- thrust
- Prior art date
Links
- 238000005096 rolling process Methods 0.000 title claims abstract description 110
- 239000002887 superconductor Substances 0.000 claims abstract description 7
- 238000012423 maintenance Methods 0.000 claims abstract description 5
- 239000007789 gas Substances 0.000 claims description 75
- 230000003247 decreasing effect Effects 0.000 claims description 6
- 230000007613 environmental effect Effects 0.000 claims description 6
- 238000002485 combustion reaction Methods 0.000 claims description 4
- 238000006243 chemical reaction Methods 0.000 claims description 3
- 238000010276 construction Methods 0.000 claims description 3
- 239000000446 fuel Substances 0.000 claims description 3
- 230000006698 induction Effects 0.000 claims description 2
- 239000013598 vector Substances 0.000 claims description 2
- 238000005192 partition Methods 0.000 claims 1
- 210000002683 foot Anatomy 0.000 description 15
- 238000000034 method Methods 0.000 description 9
- 239000007788 liquid Substances 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 4
- 206010049119 Emotional distress Diseases 0.000 description 3
- 230000009429 distress Effects 0.000 description 3
- 230000003993 interaction Effects 0.000 description 3
- 239000000463 material Substances 0.000 description 2
- 230000005610 quantum mechanics Effects 0.000 description 2
- 230000029058 respiratory gaseous exchange Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 101100492584 Caenorhabditis elegans ast-1 gene Proteins 0.000 description 1
- 241000272470 Circus Species 0.000 description 1
- 239000006096 absorbing agent Substances 0.000 description 1
- 230000037406 food intake Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H99/00—Subject matter not provided for in other groups of this subclass
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/001—Flying saucers
Definitions
- This invention concerns of a new flying disk shaped flying/space vehicle which uses a new technic of thrust through the rolling of a wheel.
- This new vehicle using basic principles of the physics is able to travel with tremendous higher speeds than the speeds of the prior state of art flying vehicles, avoid/face air pockets, get back to the horizontal level from every slope as well as fly under every slope, change altitude and direction at will, land vertical and maintain a steady flight for the whole time of flight.
- airwheel For the shake of shortness from now on we will refer to this vehicle with the name "airwheel”.
- the prior state of art consists of vehicles that use basically the lift force on wings (planes & helicopters) to maintain their height during the flight. This force in case of an air pocket or sudden winds could cause some flaws on the trajectory of the flight.
- Airwheel comes here to introduce a better way of steady flight through the use of air outflow and rotating wheels.
- the prior state of art flying vehicles also use helicoid means which deal with the 'pushing' of air to get their thrust and thus they have some limitations in the speed they are able to achieve.
- Airwheel comes to introduce a new technic of thrust through the rolling of a wheel and the speeds airwheel is capable to achieve through the use of this new technic are limited only by the durability of the material the rolling wheel is constructed in distresses.
- Helicopters are not able to fly under great slopes and achieve great speeds but are able to change the direction of flight as well as their flight height at will (in a rather short period of time & poky space) and at last are able to land vertical.
- airplanes are able to fly under great slopes (at least the fighters) with high speeds but are not able to change their flight height and direction at will (in a rather short period of time & poky space) and at last are not able to land vertical (except the harriers).
- Airwheel comes to fill an empty position, which will combine the good features of the helicopters & airplanes and add some new good features too.
- This invention concerns of a new flying/space vehicle which maintains its height with the outflow of under great pressure gases and the use of lift due to the containment of hot gas and/or hot light gases.
- the outflow of the gases is materialized through the nozzles (k) that can take different slopes related to the main body (a) (fig.l & fig.5) on a radius level of symmetry of the main body (f ⁇ g.2b). Thus they are able to change the direction of the force that is exercised on the outflowing point (the base of the nozzle mounted on the main body). Also by changing the pressure of the outflowing gas the meter of the foresaid force also changes proportionally.
- the nozzles are provided with gas through connoid tubes that are placed in the main body and are divided in subrooms.
- the volume of the subrooms from the first to the last is scalable decreased causing a scalable increment of the pressure of the gas as it flows between the subrooms from the first ( ⁇ j - delta one) to the last ( ⁇ ⁇ - delta kappa where kappa is a positive integer greater than ten).
- the connoid tubes are provided with gas by the rooms (4) where the atmospheric gas is consolidated by turbines that ingests it and divert it there.
- the nozzles are provided with gas from the Air Storage Tanks (from now on ASTs) (fig.1-7) which are tanks that store atmospheric air under really high pressure (liquidized).
- the horizontal movement of airwheel in height 'h' is achieved by using a new technic of thrust through the rolling of the wheel.
- this technic by exercising a force (here this force is achieved by outflowing under great pressure gases) in the edge of the rolling wheel (b) (force's direction is opposite to the linear speed's direction of the edge) from a fixed point related to the main body of the vehicle we simulate the way a car moves by giving torsion from the engine to the wheel which through the braking force of the tire rolls instead of just rotating and thus moves the car.
- Airwheel takes advantage of the enviromnental magnetic fields created by the solar wind and the magnetosphere of the earth. Due to the magnetic fields of solar wind being extremely weak it extends telescopic devices from the tubelike stands that mount rolling wheel (b) to the main body to get the torsion the rolling wheel needs. These devices extend and open creating a 'T' in which upper part are located pairs of superconductor bobbins located in such a way that the magnetic field of each bobbin of the pair is opposite oriented to the other's. By taking advantage of the interaction between the magnetic field the bobbins create and the environmental magnetic field the rolling wheel as it rolls takes the torsion it needs to simulate the rolling of the wheel of a car, as it was mentioned before. Airwheel is comprised by three constitutional units and these are : • The main body (a)
- the airwheel is seen as a whole structure in figure 5 where we can see in crosscut each of the foresaid structural units.
- Airwheel as disclosed before has the following advantages in relation to the prior state of art air vehicles.
- Fig.2b The movement of a nozzle in ground plan and side plan Fig.2c - Air Storage Tank (AST 1 -upper AST or AST 2-lower AST)
- Fig. ⁇ c Pair of superconductor bobbins with their inner magnetic fields
- X Fig.7 - Showing of the way of turning (with angle degrees) using the rolling wheel (seen as a ring on the thinkable trigonometric circle).
- the materializing of this invention is divided to the detailed analysis of materializing of each of the stuctural units of the airwheel.
- the analysis of the materialization starts with the main body and then goes to the materialization of the rolling & AMM wheels.
- the main body in three dimentions has the same shape as a yo-yo as seen in fig.1 . It contains all the parts needed by airwheel to maintain its height of flight and some parts that support its horizontal movement (flight).
- Each of these accessions contains a turbine which ingests atmospheric air and diverts it to the rooms 4 through the funnels (3).
- the rooms 4 have some vents on their walls. These are the vents that provide with atmospheric gas the radial connoid tubes (fig.1-8, 11,12) as well as the Air Storage Tanks (ASTs).
- the rooms 4 also provide with atmospheric gas the ASTs .
- the ASTs (7) are tanks where airwheel stores gas in order to use it in case of an air pocket.
- the ASTs (f ⁇ g.2c) are divided in concentric ringlike subrooms with decreasing volume from the first (near room 4) to the last (in the border of the AST).
- the decrement of the volume between two neighboring subrooms is given by the factor 'n' which gives the result of the volume of the outer subroom divided by the volume of the inner subroom.
- the increment of the pressure is given again by the factor 'm' as before (in the connoid tubes) due to the quantum mechanics phenomena that appear (due to high pressure).
- the ASTs and the connoid tubes are two of the three devices which will make sure airwheel will fly.
- the third device is a set of airbags (fig.1-13) filled with hot atmospheric gas and/or hot light gases in order to decrease the total weight of the airwheel. This will make it easier to the nozzles to lift to a height 'h' and keep there the airwheel during the flight.
- the lasers (fig.1-25) . There will be 72 lasers located as seen in fig.l, one every five degrees. That's to say that the angle between the axes of two neighboring lasers will be 5° (angle degrees). The lasers will define the 'level' where the rolling wheel will outflow. To understand the formation of the lasers better see the seconds in a non-digital watch and mentally replace the seconds with lasers.
- the room 26 is a ringlike room which will contain the fuels (if internal combustion engines are used) or batteries/electric generators (if electric engines are used).
- the room 27 will be used for the engines which in case of internal combustion engines will take air from the upper room 4 and outflow the exhausts in lower room 4. In case of electrical engines it will take the energy need from the batteries/generators in room 26 as mentioned before. There could by hybrid engines which they use internal combustion engines used in slow speed to provide mechanical energy to electric generators which will give the energy needed to electrical engines.
- the room 29 will be used for carrying baggage and merchandise by 60% and by 40% to carry compressed atmospheric air needed for breathing.
- the engines will give torsion to a gearbox device, which will give the torsion needed to a formation of six gears located on the tops of an hexagon. These gears will give motion to the rolling & the AMM wheels (six gears per wheel) as seen in fig.l (31 & 31).
- the gears 30 will give torsion to the AMM wheel & the gears 31 will give torsion to the rolling wheel.
- the lowest airbags 13 (seen in fig. l behind the pistons (36) will be replaced by a ringlike tank (28) which will contain a liquid easily volatilizable (the use of this tank will be explained in The airwheel as a space vehicle paragraph). Also the room 29 will be used by 100% for storing compressed atmospheric gas for breathing.
- the landing device which is a formation of six foots (d) extending when airwheel lands.
- the foot consists of three structural units which are : the piston (36), the supporting device (35) and the main foot (34).
- the main foot is steady mounted on the one side as seen in fig.l .
- the supporting device is mounted on the one side on a sliding device which slides on a driver steady mounted on a piece of the shell and on the other side the supporting device is mounted on the main foot (in the 3/5 of the main foot's length).
- the piston (fig.1-36) is used to puss the sliding part of the supporting device in order to extend the foot.
- the piston empties from air and is pulled mechanically back pulling the sliding part of the supporting device and thus pulling the main foot up.
- a sliding cover covers the entire device and gives to the lower side of the lower part of the main body the cylindrical symmetry (cylindrical symmetry with the mathematical meaning).
- the piston gets the air it needs from the lower AST.
- the feet are also used as shock absorbers when the airwheel lands.
- the rolling wheel is the structural unit of the airwheel, which is responsible for the horizontal movement in height 'h' (flight) of the whole structure. It is shown in fig.3a in ground 'ghost' plan.
- the rolling wheel consists of three structural units which are : the inner part (shown in highlighted black line in fig.3 a) , the tubelike stands (fig.3a-20) and the outer part as seen in fig.3a.
- the inner part is the device that sets up the rolling wheel on the corresponding stands (rails) of the main body. As seen in fig.3c the inner part hangs on the rail and then a sliding part comes out and locks the inner part on the rail.
- the outer side of the inner part (left of the sliding part - fig.3 c) has a surface which looks like a gear in order to take torsion from the gears (30).
- the tubelike stands (20) mount the outer part on the inner part. These stands are mounted to each other for greater stability with crossed stands as seen in fig.3a (in fig.3a the crossed stands are seen only between three tubelike stands but all the tubelike stands are mounted to each other with crossed stands).
- the tubelike stands will contain telescopic devices which extend (the use of these devices is explained later in 'The airwheel as a space vehicle' paragraph).
- the outer part of the airwheel is the part that is used for rolling.
- the rolling wheel as seen in cross cut (in a half plane starting with the axis of symmetry of the rolling wheel) shows in cross cut the outer part.
- the 'snags' (14) which mount the rolling wheel on the accessions of the main body (where the connoid tubes 12 end - fig.l), the sensors (f) and the electrical generators (15) in the lower 'snag' which give to the rolling wheel the needed energy to perform its function.
- the crosscut of the outflow device (17) can also be seen in figure 3c as a triangle (under the "b" without a number).
- the outer part of the rolling wheel contains the spiral devices (16) which are spiral connoid tubes divided in subrooms (as seen in zoom in fig.3b). Their shape is spiral because this shape combined with the rotation of the rolling wheel subserves the ingestion of the gas provided by the connoid tubes (12) of the main body.
- the volume of the subrooms follows the same rule as the volume of the connoid tubes' subrooms increasing that way the pressure until the outflow device.
- the outflow device (17) has nozzles steady mounted, connected each with a corresponding sensor (f). When the sensor passes (as seen in fig.3 a) in front of a laser beam the nozzle starts outflowing and when it passes in front of a second laser beam it stops.
- the direction the nozzles of the outflow device (17) outflow is the same with the linear speed's direction of the edge of the outflow device (the edge of the rolling wheel) creating that way an opposite direction force which will simulate as mentioned before the braking force of the tire causing the rolling of it and through this the horizontal movement of the car.
- the two lasers (25) define a level (24) (actually an angle) in which the nozzles of the outflow device outflow. Lighting up different lasers we change this level causing the airwheel to turn. If we identify the level (23) with the direction of flight and light up the right lasers making the level (24) exactly the same with level (23) then airwheel will turn smoothly to the left as described in 'An imaginable flight of the airwheel in Earth's atmosphere ' paragraph.
- the AMM Wheel is a high inertia torsion wheel that rotates opposite to the rolling wheel's rotation to maintain the angular momentum of the whole structure constant equal to zero. It is shown in figure 4.
- the discontinuous line in the ground plan identifies with a level of symmetry seen in the lower left as side plan.
- the materialization of the AMM wheel is really simple. It consists of three structural units which are : the inner part, the tubelike stands and the outer part.
- the inner part is the same as before with the exception that the gear-like surface is located on the upper vertical surface of the outer side of the inner part (right over the mounting of the tubelike stands on the inner part). That way the AMM wheel gets its torsion from the gears 31 (fig.7a-31).
- the tubelike stands that mount the outer part on the inner part are constructed this way for increased tensile strength.
- the outer part is a high mass ring that is mounted on the inner part with the tubelike stands. Its specific angular speed rotation (opposite to the rolling wheel's) due to the high mass cancels the angular momentum of the rolling wheel and maintains that way the angular momentum of the whole structure constant equal to zero.
- the stands 32 ⁇ (thirty two-beta) that hang the AMM wheel on the stands 32 ⁇ (thirty two-alpha) of the main body.
- the telescopic devices are used by airwheel to draft the torsion it needs to move in space.
- airwheel When airwheel is used in space, it will use the magnetic fields of the magnetosphere or the magnetic fields (from now on MFs) of solar wind which will interact with MFs it creates in order to draft the torsion the rolling wheel needs to roll (create a corresponding force to the braking force of a tire which makes the tire roll and not just rotate & thus moves the car).
- the interaction consists in pairs of superconductor bobbins with opposite directed inner MFs which interact with the environmental MFs (the MF of each bobbin is opposite directed to the MF of the other in each pair - see the vectors of the magnetic induction of the inner and the environmental MFs in fig.6c).
- the interaction occurs under the following principle.
- the poles of the magnetic fields are as seen further down (between the '
- each of the bobbins expels the other but they are steady mounted to each other.
- the formation of the poles causes the 'push' from the left and the 'pull' of the pair from the right (as seen here).
- There won't be any magnetic torsion because each time one pair of bobbins will be working and even though the magnetic energy of the left bobbin is higher than the one of right bobbin there won't be any torsion because the mass of the whole structure of the airwheel will prevent that (it will be impossible for the pair of bobbins to turn the whole airwheel from the torsion the pair gets from the environmental MFs).
- the superconductors the bobbins are made of, will have unfold its superconductivity due to the temperature of the interplanetary space.
- the telescopic devices When airwheel leaves the atmosphere and gets in the magnetosphere the telescopic devices will extend from the tubelike stands of the rolling wheel as mentioned before and will open creating a 'T (see fig.6b) in which top the pairs of the superconductor bobbins are located.
- the telescopic devices extend because the magnetic fields of the solar wind are extremely weak and by greatening its radius the airwheel will be capable of drafting the needed torsion from these weak magnetic fields. This might not be needed for use in the magnetosphere but this shall be decided by experimental measurements.
- the airwheel When the airwheel is used as a space vehicle it is launched from the earth before midnight to take advantage of the magnetosphere. In the magnetosphere airwheel will be using the outer regions of it (the magnetosphere) where there is not high energy hot plasma.
- Airwheel is standing on the ground on its six feet (d) (fig.6a) which are located on the lower side of the main body (a).
- the airbags (13) are fully filled with hot/atmospheric gas and/or hot light gases, decreasing that way the total weight of the airwheel and the tanks 26 are fully filled with fuels.
- the airwheel engages the engines of the turbines in the accessions 1 & 2 and ingests that way atmospheric gas to the rooms 4 (upper & lower).
- the gases which are collected at this time in the rooms 4 are used to fully fill the ASTs.
- the gas is forwarded to the connoid tubes 8,11,12 from the rooms 4.
- the gas fully fills the connoid tubes until the nozzle which doesn't outflow at this time.
- the gas flows between the subrooms of the tube and outflows to the rolling wheel (see fig. l & fig.5).
- the rolling wheel with its rotation and the shape of its spiral connoid tubes (16) is subserving the 'sucking ' of the outflowing gas from the connoid tubes 12.
- the outflow device (17) doesn't outflow but is filled with gas under high pressure at this point.
- the lower jets are pointed towrds the ground and start outflowing giving a vertical thrust to the airwheel which in conjuction with the decrement of airwheel's weight with the use of the airbags (13) it provides lift to the airwheel.
- the airwheel When the airwheel is on the air, it pulls its landing feet in the main body (a).
- the piston's container (36) will empty the air and the piston will be pulled back and pull that way the supporting device (35) which will pull inside the main body the foot (34).
- the airwheel lights up two neightbouring lasers (25) which will define the area where the rolling wheel's outflow device (17) will outflow (fig.3 a).
- This outflow will create a force which will simulate the braking force between the tyre of a car and the road and move that way the airwheel (i.e. the tyre gets torsion from the car's engine and through the braking force - friction - it doesn't just rotate but it rolls moving that way the car).
- the outflow from device (17) will occur only in the area that is defined by the two lasers (see fig.3 a).
- the sensors (f) sense the light and the corresponding jets start outflowing and when the sensors (f) pass in front of the second laser the same way the corresponding jets stop outflowing. That way the airwheel will start 'rolling' - flying in height 'h'.
- the pilot desires to increase the speed of the airwheel, he will increase the pressure in the connoid tubes 12 providing more gas to the rolling wheel (b).
- the rolling wheel (b) as well as the AMM wheel (c) will start rotating faster to maintain the angular momentum of the whole sturcture constant equal to zero.
- the increased flow of gases from the connoid tubes 12 will increase the pressure in the outflow device 17 which will outflow gases with greater pressure.
- the airwheel wishes to turn there are two ways to do it. If its speed is low it can use the jets which will be properly pointed and by outflowing will cause airwheel to turn. If its speed is high then the following procedure will be followed :
- the outflowing point of the rolling wheel keeps changing so that it is constantly identified with the 270° point of the imaginable trigonometric circle (the direction of flight is constantly identified as foresaid with the 90° point).
- the outflowing point becomes again the 0° point in the imaginable trigonometric circle. If the airwheel wishes to turn left, it will light up the proper lasers (25) so that the outflowing point will be identified with the 90° point as seen in fig.7c. This will make the arwheel start turning left.
- the airwheel wishes to turn in a 'smooth' way under high speed flight. If it doesn't wish to turn in a 'smooth' way, it can also turn (under high speed flight) by pointing its jets properly and by ordering them to outflow, turn in a less 'gliding' way causing an extreme distress of G's to the passengers as a result.
- the ASTs are fully filled once again with gas and so is the tank 28 (seen as the lowest devices 13 in fig.l) fully filled with a liquid easy to volatilize.
- the jets are pointed in such a way that turn the airwheel upwards and provide him with lift in that upgoing flight.
- Airwheel will follow the magnetic lines of the Earth's magnetosphere and then get out of it and follow the magnetic lines of the magnetotail. Following the magnetotail it will get out of it and then follow the magnetic fields of the solar wind. Although solar wind's fields are really weak the combination of the high magnetic fields the T-like devices create with the length itself of these T-like devices should be capable to counterbalance the torsion that the rolling wheel gets from the engines.
- the engines will be electroengines powered by nuclear energy.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Tires In General (AREA)
- Control Of Vehicles With Linear Motors And Vehicles That Are Magnetically Levitated (AREA)
Abstract
Description
Claims
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2001279985A AU2001279985A1 (en) | 2000-08-08 | 2001-08-07 | Flying disk shaped flying/space vehicle with the use of a new technic of thrust through the rolling of a wheel |
EP01958261A EP1307655A1 (en) | 2000-08-08 | 2001-08-07 | Flying disk shaped flying/space vehicle with the use of a new technic of thrust through the rolling of a wheel |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GR20000100278A GR1003698B (en) | 2000-08-08 | 2000-08-08 | Flying/space vehicle in the shape of a flying saucer using a new thrust technique involving rolling a wheel |
GR20000100278 | 2000-08-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2002012722A1 true WO2002012722A1 (en) | 2002-02-14 |
Family
ID=10944353
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/GR2001/000032 WO2002012722A1 (en) | 2000-08-08 | 2001-08-07 | Flying disk shaped flying/space vehicle with the use of a new technic of thrust through the rolling of a wheel |
Country Status (5)
Country | Link |
---|---|
US (1) | US20020153449A1 (en) |
EP (1) | EP1307655A1 (en) |
AU (1) | AU2001279985A1 (en) |
GR (1) | GR1003698B (en) |
WO (1) | WO2002012722A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007033200A1 (en) * | 2007-07-17 | 2009-07-02 | Kunst, Ernst K. | Material object weight partial or complete decontrolling and lift and drive generating method for e.g. aircraft, involves converting kinetic energy into stored electrical energy by low-speed lifting gyroscope during stationary application |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7802755B2 (en) * | 2004-03-10 | 2010-09-28 | Poltorak Alexander I | Rotating wing aircraft with tip-driven rotor and rotor guide-ring |
US20050210862A1 (en) * | 2004-03-25 | 2005-09-29 | Paterro Von Friedrich C | Quantum jet turbine propulsion system |
US20050230525A1 (en) * | 2004-03-30 | 2005-10-20 | Paterro Von F C | Craft with magnetically curved space |
US7185848B2 (en) * | 2004-06-21 | 2007-03-06 | Ltas Holdings, Llc | Mass transfer system for stabilizing an airship and other vehicles subject to pitch and roll moments |
US20070262198A1 (en) * | 2004-11-18 | 2007-11-15 | Avudainayagam Subbiah | Flying machine |
US9284959B2 (en) * | 2011-09-26 | 2016-03-15 | Charles Ronald Grigg | Propulsion turbine |
CN104192309A (en) * | 2014-08-26 | 2014-12-10 | 魏伯卿 | Aerodynamic force, shape and weapon layout of modern flying saucer |
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DE3734811A1 (en) * | 1987-10-14 | 1988-06-23 | Theo Diedrich | Giro flying object |
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GB2312709A (en) * | 1996-04-30 | 1997-11-05 | David Johnston Burns | Flying craft with magnetic field/electric arc vertical thrust producing means |
US5730390A (en) * | 1992-05-14 | 1998-03-24 | Klaus Kunkel | Reusable spacecraft |
-
2000
- 2000-08-08 GR GR20000100278A patent/GR1003698B/en unknown
-
2001
- 2001-08-07 US US10/089,908 patent/US20020153449A1/en not_active Abandoned
- 2001-08-07 EP EP01958261A patent/EP1307655A1/en not_active Withdrawn
- 2001-08-07 WO PCT/GR2001/000032 patent/WO2002012722A1/en not_active Application Discontinuation
- 2001-08-07 AU AU2001279985A patent/AU2001279985A1/en not_active Abandoned
Patent Citations (9)
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FR1107257A (en) * | 1954-06-18 | 1955-12-29 | Circular wing supersonic gyroscopic helicopter and astronautics | |
DE2439608A1 (en) * | 1974-08-19 | 1976-03-04 | Horst Hanschmann | Turbine heated and driven balloon - has reinforced fabric container and jet engine to provide flow over external surfaces |
DE2800975A1 (en) * | 1978-01-11 | 1979-07-12 | Schmidt Klieber Alexander | Flying machine obtaining lift by dynamics of rotation - has flywheel combined with lift surface driven by jets rotating about cylindrical fuselage |
DE3734811A1 (en) * | 1987-10-14 | 1988-06-23 | Theo Diedrich | Giro flying object |
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DE4123709A1 (en) * | 1991-03-06 | 1992-09-10 | Blazquez Jose Maria Roncero | AIRCRAFT |
US5730390A (en) * | 1992-05-14 | 1998-03-24 | Klaus Kunkel | Reusable spacecraft |
FR2707248A1 (en) * | 1993-07-05 | 1995-01-13 | Thomson Csf | Self-propelled and remotely controlled flying machine fitted with a payload |
GB2312709A (en) * | 1996-04-30 | 1997-11-05 | David Johnston Burns | Flying craft with magnetic field/electric arc vertical thrust producing means |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007033200A1 (en) * | 2007-07-17 | 2009-07-02 | Kunst, Ernst K. | Material object weight partial or complete decontrolling and lift and drive generating method for e.g. aircraft, involves converting kinetic energy into stored electrical energy by low-speed lifting gyroscope during stationary application |
Also Published As
Publication number | Publication date |
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AU2001279985A1 (en) | 2002-02-18 |
US20020153449A1 (en) | 2002-10-24 |
GR1003698B (en) | 2001-10-19 |
EP1307655A1 (en) | 2003-05-07 |
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