Geomagnetic Field Amplifier


The following design system is intended to assist in the increase of the geomagnetic field of the Earth.  The device then able to break gravity and maintain electrical production to "transmit" a magnetic field increasing the total field strength. Currently the Earth's populations common knowledge contains the observed failing geomagnetic field.



































































The Earth's polar ice melt due to Global warming produced by Carbon Dioxide (CO2), fossil fuel emissions, has impact upon the rotation of the Earth possibly affecting the Geomagnetic field. Earth Mantel flow produces the Magnetic field and  an inclining "wobble" might disrupt the Magnetic field intensity causing higher radiation permeation at ground level from the Sun itself. Mechanical supplements as magnetic field amplifier satellites is a good idea.


NO (nitric oxide), N2O (nitros oxide), and NO2 ( Nitrogen Dioxide), production from permeating ultraviolet solar radiation and rising Methane (CH4) with tandem inclining CO2 emissions causes equatorial atmospheric altitude incline as the gas (Atmospheric envelope elongates factoring planetary rotation ). The atmosphere equatorial altitude then increases when heated to then sluff off O3 (Ozone) to Outer Space (gravimetric proxi / molecular specific physical weight of gas composition at altitude).


This would then cause the Sun itself to convert high altitude Nitrogen to Nitrogen Di-oxide,  Nitros Oxide, and Nitric Oxide at enormous rates due to greater Ultraviolet Light permeation, with the thermal retention of N2O then a greenhouse gas ... Nitros Oxide traps MORE heat and the compound incline is like car exhaust fossil fuel emissions from the Sun 24/7/365 days a year..... at Planetary hemisphere area of effect! Changing the shape of the equatorial high altitude also produces a "Lens Effect" like a magnifying glass concentrating Sunlight causing a feedback in the Albedo thermal retention as the focusing of Sunlight increases heat a factor in the greater equation changing the production rate of Nitros Oxide.


The melting ice caps might cause inclined planet wobble effecting the magnetic field of the Earth increasing the effect of N2O production... an incline factor that causes incline effect of temperature rise into WATER REACTIVITY.... the CO2 (carbon dioxide) then retaining greater thermal gain from the btu of the N2O time vs. heat dissipation factoring altitude and O3 loss due to molecular specific density at altitude factoring gravity in the high altitude conditions... heat is conductive..... a molecule that retains a higher "heat" heats adjacent molecules of other compound (CO2/CH4) - ie... thermal conductivity..... increased fresh water on the ground is a solve to yield higher plant respiration increasing ground level O2 that naturally forms High Level O3. Fresh water solve at https://www.designdeskinc.com/gravity-desalination-plant.html


The magnetic turbulence of modern equipment then producing electromagnetic eddies in the greater Magnetosphere causing magnetic flow turbulence. The radioactive decay rate of Planetary core elements then is also a factor as the  radioactive material that is producing planet core heat, allowing the planet's core geo-dynamo to cycle (mantle convection), causes heat loss over long time spans (radioactive half life),  this effects the Earth's magnetic shielding from the Sun itself.  The convection rate might have varying degrees of effectivity due to the current volume of heat producing material factoring pressure and Earth's rotation.


 The design described then is placed in low Earth orbit to increase the magnetic polarization of the North and South magnetic poles of the Earth.

The design polarity then with variance to correspond with the transmitted magnetic field, ie... north polarity then above the north pole geographic then the "transmitted" south pole above the south pole geographic. The design below then depicting the north pole alignment format.


Multiple device then placed above each pole of the Earth to then "re-Gauss" the planet "juicing" the geomagnetic field to "re-align" and increase the magnetic flow. The design has application to clean orbital space debris or control re-enter defunct satellites. The system also could be adapted to serve as an emergency aircraft landing system demonstrating slow descent vertical vector displacement to "hover land" the aircraft as a redundant flight safety tool.



Parts List


1. mono-pole electromagnet  array multiple electromagnets about 360 degrees sum of 24

    (only one pole emitting the opposite magnetic pole then magnetically insulated)


2. open bore hole


3. upper mounting structural frame bracket placed at unit circular quadrant points (also containing electrical transference wires

    within the structural member)


4. hollow bracket


5. toriod electromagnet outer casing


6. microwave transmitter "ring"


7. transmitter wave divider also as a mounting "union bracket" to stabilize the upper electromagnets circular ring" to the core electromagnet


8. hollow core electromagnet (only one pole exposed - opposite pole magnetically sealed - heavy load diodes upon the electrical

    wire + and resistor upon the - "return" electric wire protects the control electronics from environmental over induction ie... solar flare

    safety circuit)


9. high gain microwave transmitter


10. encased toroid electromagnet (lower "magnetic pole" magnetically insulated)


11. outer lamp ring casing - translucent


12. lamps


13. core hinge "bay" through bolt


14. connecting servo "arm" bushing - heavy gasket


15. union bolt


16. toroid electromagnet casing open bore - circular pattern about 360 degrees


17. shielded core electromagnet "also encased by hard encasement


18. union bolt


19. mounting bolts


20. lock nut


21.  rotating oil and air pressure "tumbler" pressure storage vessel ( sum of two total system within letter "B" for redundancy cross wired so

       that both "tumblers" can feed, oil or air pressure to the system's  generator system Letter "C" [ fluid oil pressure / air pressure] )


22. thru bore pressure transference slip ring - multiple exhaust oil / or air also with generator Letter "C" send or return oil pressure with

      pneumatic fill valve as one way valve "letter "G" also upon a "tee" union upon the exterior to "fill" the "tumbler" via one way valve, with

      air pressure and or oil "outer plate also as a mounting union point to the structural frame to stabilize the "tumbler"


23. revolutions per minute sensor (r.p.m. sensor) and electric drive motor unit causing the "tumbler to be able to "spin up" even in zero

      gravity to align the oil / air pressure for the hydraulic draft generator system to function correctly.


24. bearing race - pressure retaining mounting bore so that the electric motor's drive shaft then driving the "tumbler mount" bearing race

      mounting bracket and the half of the bearing race (closed to the electric motor), then used to mount the system to the structural frame

      of the housing.


25. thru bore current transfer slip ring and positional sensor used when rotating the oil jet with the electric servo motor


26. servo electric positional electric motor


27. thru bore current transfer slip ring and positional sensor used when rotating the oil jet with the electric servo motor


28. lamps


29. hydraulic impeller (hydraulic fluid "oil" impeller) causes union rotation with number 35


30. translucent lamp "dome"


31. venturi max pressure safety discharge valve and temperature sensor - safety vents oil pressure to the core thrust chamber via oil flow pipe


32. oil exhaust flow pipe


33. oil flow guide and max pressure safety vent system - the flow guide contains ports to direct over pressure to the max pressure safety valve


34. oil exhaust flow pipe


35. oil compressor and permanent magnet magneto (electricity generator), with current feed to the circumference mounted

      electromagnets upon the oil compressor (incline electrical current the directed through number 36 connecting unit "slip ring system"

      contained within number 53)


36. oil impeller and circumference electric drive motor "brush less" advances by hydraulic draft " fluid suction"


37. oil compressor and circumference "brush less" electric motor


38. oil drive impeller advances the "drive line assembly" by oil flow speed


39. main venturi max pressure / over pressure safety vent valve flow "coil" oil flow pipe


40.  external mechanical oil pump oil flow pipe


41. main oil flow coil type oil flow pipe


42. electric oil displacement "oil discharge" / system throttle valve


43. air pressure filled oil displacement "thrust chamber" oil injects into air pressure


44. external inline oil filter with speed of flow by pass


45. oil intake assembly


46. air pressure valve - one way valve


47. one way valve


48. electric actuation pneumatic pressure control valve


49. dual component air pressure / oil pressure tank - air pressure causes oil pressure. A high pressure vessel to then in math surpass the

      required work capacity factoring all mechanical and electromagnetic resistance produced within the total system.


50. one way valve


51. air pressure flow pipe


52. air pressure coupling


53. lubricated 1:10 ratio gear set aligned so that the output rotation then tandem to the permanent magnet Magneto oil pump number 35

      and the input rotation then tandem with number 36 - contains thru bore current transfer slip ring to increase the magnetic field emanating

      from the permanent magnet electromagnetic about the circumference of the generating oil compression fan yields higher electricity output

      from number 35


54. mechanical oil pump


55. oil jet mounting bracket


56. main venturi over pressure safety valve vents over pressure


57. main throttle valve shutter valve


58. one way valve


59. baffle diffuser with open bore holes


60. external oil fill plug threaded screw bolt uses safety lock washer


61. diffuser "baffle" divider cone sends the oil flow perpendicular


62. heated (electric heating resistor) electric oil injector - heats system's oil


63. electric pneumatic pressure valve


64. oil flow chamber "fill" oil flow pipe


65. electric oil flow valve


66. oil pressure chamber - pressurized by air pressure


67. plate piston moves by air pressure - contains ring and gland bushing hydraulic fluid pressure rated piston plate ring system


68. communications electronics


69. transmitter / antenna system


70. lubricated 1:10 ratio gear set aligned so that the output rotation then tandem with number 37 and input rotation then tandem with

      number 38 - contains r.p.m. ( revolutions per minute ) sensor to "regulate" oil jet speed reports to main logic electronic circuit paths


71.  external venturi over pressure valve discharge oil flow pipe directs oil to the hydraulic fluid / oil impeller number 29 union joined by

       external mount oil pressure compression couplings


72. system - oil jet chamber divider plate separated the wick assembly from the thrust assembly


73. electricity transfer multi wire "bus" clip


74. oil fill cap threaded


75. large sprocket


76. drive chain tension sprocket


77. receiving sprocket


78. drive chain and sprocket encasement oil retainer case - non flammable non electrically conductive lubrication


79. voltage regulator


80. permanent magnet "wound electromagnet" magneto "stepper" tilt system also "reacting from the oil jets electrical output to cause

      increased total system electricity availability - base root" cyclical pressure p.s.i. then to compound in electrical generation level of total cycle


81. oil pressure "start cycle" control valve


82. oil impeller


83. oil flow speed regulator inlet dampener valve - maintains oil flow pipe structural integrity


84. pneumatic "start" impeller


85. high volume oil pump - causes system advancement by the hydraulic draft of a pressurized fluid - system accelerator of drive lined union

      joined components in tandem with the reintroduction of produced electrical current


86. 1:10 ratio gear set output rotation tandem with number 85's internal pump wheel and input rotation tandem with

      fixed union drive line assembly containing number 88


87. r.p.m. sensor system speed control regulates the position of the oil flow valve and the logic mapping electronics potentiometer feeding

      current to the system "advancer" electric motor number 88


88. drive line electric motor dual shaft


89. oil pump union joined drive shaft to number 77 and, internal pump wheel number 89 and input coupling to number 86


90. oil filter


91. electric valve control solenoid


92. drive chain


93. oil flow pipe


94. high voltage electricity generator


95. pneumatic flow pipe


96. pneumatic "start valve" electric actuation


97. avionics main logic electronic circuit "box" flight control circuit boards and electricity management electronics thermal regulation

      system not to over heat the electronics inductance cage encased


98. lock washer


99. carbon foam radiation and electromagnetic pulse shielding insulation ( induction cage system  upon the inner surface of the outer hull )


100. magnetic oil plug / oil drain plug


101. external oil pressure injection fitting compression coupling directs hot oil from the oil injector into the chamber




Letter "A" = oil jet


Letter "B" = dual tumbler oil / air pressure chamber contains battery and battery charging system to "Start" the generator system and

                   electrify the logic electronic circuit boards - system on / off communications via transmitter and remote control logic electronic

                   circuit board reports system parameters to the remote control unit for safe functioning


Letter "C" = electricity generator / generator "bay" contents - inductance cage encased


Note - The geomagnetic field satellite may be used in tandem with https://www.designdeskinc.com/solar-radiation-diffuser-satellite.html to

           slow and cool  a coronal mass ejection  prior to impalement with the Solar Radiation Diffuser Satellite. Turbulence traversing a "wave"

           slows the  wave... magnetic  interference then produced by the geomagnetic field amplifier to slow / redirect solar flare...... spreading it

           apart dropping the thermal properties to then not cause excessive thermal fatigue upon the outer surface of the Solar Radiation

           Diffuser Satellite.  A cost effective method!


Note - electric components required for the system to operate then connect to the main logic logic mapping circuit control board.


Note - the system physical scale may be small to allow for cost effective implementation 36" (inches) - 96" (inches)


Note - for long range asteroid mitigation and or using the geomagnetic field amplifier to slow / re-direct solar flares the center core Letter "A" then

          may use https://www.designdeskinc.com/cold-plasma-drive-toroid-static-compressor.html


Note - the system may be placed at greater altitude in redundant systems ie. higher placement than for just feeding the Magnetosphere. The

           higher orbital placement then to act a as a primary deflection system to prevent low level (ground level) magnetic "storms".

           Effectively a satellite shielding system.


Note - the system may be placed to stop the recoil that causes the ground level geomagnetic storm using multiple satellites to "magnetic field

           direct"  the snap back / recoil, of high energy level  results of solar storm (requires induction dissipation units) .

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Geoengineering - Climate Change Mitigation

Design Desk Inc.