Design Desk Inc.
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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