GB2368910A - A device to assist in the study of the earth's gravitaional field - Google Patents

A device to assist in the study of the earth's gravitaional field Download PDF

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Publication number
GB2368910A
GB2368910A GB0013315A GB0013315A GB2368910A GB 2368910 A GB2368910 A GB 2368910A GB 0013315 A GB0013315 A GB 0013315A GB 0013315 A GB0013315 A GB 0013315A GB 2368910 A GB2368910 A GB 2368910A
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United Kingdom
Prior art keywords
gyroscope
gravitational force
earth
way
velocity
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.)
Granted
Application number
GB0013315A
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GB0013315D0 (en
GB2368910B (en
Inventor
Dunstan Dunstan
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Individual
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Individual
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Priority to GB0013315A priority Critical patent/GB2368910B/en
Publication of GB0013315D0 publication Critical patent/GB0013315D0/en
Publication of GB2368910A publication Critical patent/GB2368910A/en
Application granted granted Critical
Publication of GB2368910B publication Critical patent/GB2368910B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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
    • F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G3/00—Other motors, e.g. gravity or inertia motors

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gyroscopes (AREA)

Abstract

The device (anti-gravitational force engine) has a body 1 in the form of a gyroscope to which permanent magnets 3 can be attached so that the body can be made to spin by an opposing fixed electro-magnetomotive force. The opposing fixed electro-magnetomotive force is in the form of an electrical stator winding 2 that can accelerate or decelerate the gyroscope from zero velocity up to the Earth's escape velocity. A laser 7 is provided to act as a frequency counter 14 input source and a velocity modulator by way of a photo-activated current source 17 connected to the stator windings 2. A mirror 6 and beam-splitter 16 are provided to control the laser beam 13. Frictionless magnetic bearings 10 and 12 and a vacuum pump 19 are provided in order to reduce gyroscope axis friction and air turbulence. A coolant piping system is used to stop overheating.

Description

Anti-Gravitational Force Engine This invention relates to an anti-gravitational force engine.
It is well known that the force of gravity is thought of either as a wave or a particle that can be nevertheless dealt with according to the known laws of Physics and Mechanical Engineering.
It is well known that the force of gravity on Earth causes it to be necessary for one to achieve an escape velocity of 11.18 km/s in order for one to escape from the planet's gravitational force. It is also well known that satellites in low earth orbit travel at approximately 8 km/s and that a velocity of the 2 times this 8 km/s achieves 11.18 km/s and the satellite can then escape from Earth orbit. It is further well known that the Earth's gravitational accelerational force must be balanced by the inertial force of the satellite in order for the satellite to maintain its altitude as it does in a geostationary orbit where it rotates once every Earth revolution.
However, a satellite cannot orbit the Earth along a line of latitude other than the Earth's equator and a stationary satellite positioned over either pole of the Earth would be pulled down, due to the force of the Earth's gravitation and such a satellite having no vector component of centripetal force as a satellite in an equatorial orbit. To be stationary over the Earth's poles a satellite would have to balance the Earth's gravitational accelerational force with a vector component of inertial force that would be equal to the vector component of centripetal force as such a satellite has when in an equatorial orbit. A satellite must then have a vector sum component of inertia in order for it to cancel out the force of the Earth's gravitational acceleration.
Currently there are no satellites that attempt to balance out the Earth's force of gravitational acceleration by having a component of inertia that is a function of the Earth's escape velocity.
According to the present invention there is provided a method to make an anti-gravitational force engine comprising a multi-spokewheeled gyroscope mounted within a body in the form of a box, an equatorial mounted tangentially firing electro-magneto-motive force stator winding capable of working at the Earth's escape velocity that is mechanically fixed to the box, an electrical power supply controlled by laser activated optics switches that are external to the box, and magnetic frictionless bearings for the spinning gyroscope that enable it to work at the Earth's escape velocity within a vacuum.
A specific embodiment of the invention will now be described by way of example with reference to the accompanying drawing in which :- Figure 1 shows the gyroscope in position within a box.
Referring to the drawing the anti-gravitational force engine comprises a multi-spoked wheel gyroscope 1 and frictionless magnetic bearings 10 and 12, mounted in a box 15. The gyroscope is forced to spin due to the magnetic repulsion of the fixed equatorially mounted electro-magnetomotive force stator windings 2 and the gyroscope-mounted magnetomotive force magnets 3.
In order to measure the velocity of the gyroscope a laser 7 is provided. The means for measuring the velocity is provided by a frequency counter 14 that registers laser light impulses as the laser beam 13 travels from the laser 7, is reflected by the mirror 6, and is cut by the spokes of the gyroscope 8.
In order to control the velocity of the gyroscope the laser beam 13 is split at the beamsplitter 16 and is registered by the switchbox 17 that sends a current down the wires 18 to the electro-magnetomotive force stator windings 2.
In order to measure the effect of the anti-gravitational force engine on the Earth's gravity a scale is placed over the main central spoked wheel of the gyroscope 4 and weight is placed upon the scale and the scale is visually observed as the gyroscope velocity of spin approaches the Earth's escape velocity.
In order to stop the spinning gyroscope means are provided for by the control box 17 for it to be switched off and the gyroscope is allowed to spin to a stop.
In order to counter effects of air turbulence as the gyroscope spins a vacuum pump 19 is used to simulate the atmospheric pressures of outer space.
In order to counter effects of overheating due to friction and electrical resistance within the components within the box means are provided for by way of cooling pipes so that the apparatus and method of anti-gravity simulation within the box are safe.

Claims (7)

  1. CLAIMS 1 An anti-gravitational force engine comprising a multi-spokedwheel gyroscope, within a body in the form of a box, means for balancing the gyroscope vertically with frictionless magnetic bearings being provided, the body of the gyroscope being adapted to spin at the Earth's escape velocity, and an adjustable electro-magnetomotive means for accelerating the gyroscope being provided.
  2. 2 An anti-gravitational force engine as claimed in Claim 1, wherein a magnetomotive reaction force to the electro-magnetomotive accelerational force in the form of a permanent magnet is provided by way of a permanent fitting on the perimeter of the main gyroscope multi-spoked wheel.
  3. 3 An anti-gravitational force engine as claimed in Claim1 and Claim 2, wherein an electro-magnetomotive force with which to repel the permanent magnet fixed onto the gyroscope is provided by way of an electrical stator winding that is fixed to the wall of the box.
  4. 4 An anti-gravitational force engine as claimed in Claim 3, wherein measurement of the gyroscope velocity is provided for by way of a laser-activated frequency counter.
  5. 5 An anti-gravitational force engine as claimed in any preceding claim, wherein means to control the acceleration and deceleration of the gyroscope is provided for by way of a laser activated current source mounted within a control panel external to the gyroscope box.
  6. 6 An anti-gravitational force engine as claimed in Claim 1 that spins at the Earth's escape velocity in a near vacuum by way of a vacuum pump being adapted to measurably reduce the atmospheric pressure within the gyroscope box to a near vacuum.
  7. 7 An anti-gravitational force engine substantially as described herein with reference to Figure 1 in the accompanying drawing.
GB0013315A 2000-06-02 2000-06-02 Anti-gravitational force engine Expired - Fee Related GB2368910B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0013315A GB2368910B (en) 2000-06-02 2000-06-02 Anti-gravitational force engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0013315A GB2368910B (en) 2000-06-02 2000-06-02 Anti-gravitational force engine

Publications (3)

Publication Number Publication Date
GB0013315D0 GB0013315D0 (en) 2000-07-26
GB2368910A true GB2368910A (en) 2002-05-15
GB2368910B GB2368910B (en) 2003-04-09

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ID=9892783

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0013315A Expired - Fee Related GB2368910B (en) 2000-06-02 2000-06-02 Anti-gravitational force engine

Country Status (1)

Country Link
GB (1) GB2368910B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007097711A1 (en) * 2006-02-21 2007-08-30 Soon Seng Sin Levitation and propulsion unit (lpu)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0566806A1 (en) * 1992-04-16 1993-10-27 Shinko Electric Co. Ltd. Magnetic bearing device
US5506459A (en) * 1995-09-15 1996-04-09 Ritts; Gary Magnetically balanced spinning apparatus
GB2299857A (en) * 1994-11-24 1996-10-16 Philip Frederick Stott Gyroscopic reactive propulsion unit
JP2000096647A (en) * 1998-09-24 2000-04-04 Natl Res Inst Of Agricultural Engineering Air breathing device for pipe line
US6057620A (en) * 1999-04-28 2000-05-02 Precision Instrument Development Center Geometrical structure configuration of maglev forces in a maglev rotational bearing apparatus

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0566806A1 (en) * 1992-04-16 1993-10-27 Shinko Electric Co. Ltd. Magnetic bearing device
GB2299857A (en) * 1994-11-24 1996-10-16 Philip Frederick Stott Gyroscopic reactive propulsion unit
US5506459A (en) * 1995-09-15 1996-04-09 Ritts; Gary Magnetically balanced spinning apparatus
JP2000096647A (en) * 1998-09-24 2000-04-04 Natl Res Inst Of Agricultural Engineering Air breathing device for pipe line
US6057620A (en) * 1999-04-28 2000-05-02 Precision Instrument Development Center Geometrical structure configuration of maglev forces in a maglev rotational bearing apparatus

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007097711A1 (en) * 2006-02-21 2007-08-30 Soon Seng Sin Levitation and propulsion unit (lpu)
CN101415941B (en) * 2006-02-21 2015-01-07 冼顺成 Levitation and propulsion unit
EP2134965A4 (en) * 2006-02-21 2016-01-20 Soon Seng Sin Levitation and propulsion unit (lpu)

Also Published As

Publication number Publication date
GB0013315D0 (en) 2000-07-26
GB2368910B (en) 2003-04-09

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PCNP Patent ceased through non-payment of renewal fee

Effective date: 20070602