FLYMORTON.COM: FLYMORTON WEARABLE ELECTRONIC EMS EDS DIAMAGNETIC ESC BOOTS SOFTWARE BASE PROCESSING SIGNALS HARDWARE CHARGE INDUCTOR ELECTROMAGNETIC LEVITATION COIL or LINEAR MOTOR DIRECT CURRENT PHASE WIRE POINT IONS electrodynamics winding ENERGY TRAVELING REPULSIVE FORCE permanently connected to COMMON MATERIAL against the weight of its gravity against its inertial weight of gravity having FREEDOM OF MOVEMENT horizontally or AC CHARGE INDUCTOR ELECTROMAGNETIC LEVITATION COIL or LINEAR MOTOR ALTERNATIVE CURRENT PHASE WIRE POINT ION electrodynamics repulsive energy winding REPULSIVE FORCE emitter permanently connected to COMMON MATERIAL mount against the unified magnitude weight of gravity from the direction of its emitting ions velocity greater than the aluminum having FREEDOM OF MOVEMENT traveling vertically or horizontally Acoustic encoder 100hz ultrasonic drive phase wire p type n type bus connections to three separated coils separated by group stacked graphite to silicon to aluminum to bismuth starlight fireproof coated block type baring linear motor coil between magnetic suspension coils all of which are enclosed within epoxy resin crystal clear harder waterproof enclosure microwave coil Thermal phase Graphite thermal electric effect phase Silicon Thermal electric effect refrigeration phase aluminum common repulsive element force phase Bismuth crystalloid coated starlight materials phase aluminum block bottom side cooler. electromagnetic ultrasonic pulse phase 2 levitation boot bottom

FLYMORTON CHARACTERIZED AS IN WEARABLE BIOMECHATRONIC MANNED UAV LEVITATION LINEAR MOTOR BOOT SUBSYSTEM BIOMETRIC FOOT RANGE SHAPED STRUCTURE FUNCTIONAL LIKENESSES AS AN COPPER TUBE LIQUID COOLER STACK RECTANGULAR SILICON ELECTROMAGNET MAGNETRON THERMOELECTRIC EFFECT HEATSINK ELECTRODYNAMICS THERMOELECTRIC EFFECT REFRIGERATION COOLER VERTICAL METALLOID STACKED SILICON MODULATED ALUMINUM ELECTRON ULTRACAPACITOR ELECTROMAGNETIC REPULSIVE PIEZOELECTRIC EFFECTS PYROELECTRIC EFFECTS SILICON THERMOELECTRIC EFFECT HEATSINK BARING SWIRL COPPER TUBING CYCLE FLUIDS CHAMBER hydrofluorocarbon (HFC) COOLING LIQUID REFRIGERAN magnetocaloric effect (MCE) magnetohydrodynamics MODULATED ELECTROMOTIVE ULTRASONIC COOLER
ELECTRODYNAMICS SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIAL METRIC RANGE INVENTOR JERMAINE MORTON DESIGN

FLYMORTON CHARACTERIZED AS IN WEARABLE BIOMECHANICAL ESC POWER FOOT BOTTOM HFC LIQUID COOLER MCE MAGNETOCALORIC EFFECT ELECTROMAGNET COMMUTATIVE CAGE ELECTRODYNAMICS LINEAR MOTOR ARMATURE ROTOR FOOT SUBSYSTEM SUBJECT NOT LIMITING TO ADDITIONAL STRUCTURE POTENTIAL METRIC RANGE INVENTOR JERMAINE MORTON DESIGN

FLYMORTON CHARACTERIZED AS IN WEARABLE BIOMECHATRONIC SELF-SUSPENSION LEVITATION MANNED UAV BOOT PAIR SUBSYSTEM MULTI ROTOR PROPELLER SERIES OPERATES SPLIT ROTATING DIVERSE DRIVE WITHIN COMMUTATOR LEFT FOOT BOTTOM FRONT CAGE THREE SET OF FREEDOM ROTARY BLADE MOTION COUNTERCLOCKWISE SIMULTANEOUSLY ALONGSIDE THE RIGHT FOOT HEEL COMMUTATOR CAGE THREE SET OF FREEDOM ARMATURE ROTARY 4 BLADE PROPELLER MOTION CLOCKWISE SIMULTANEOUSLY LEFT FOOT HEEL COMMUTATOR CAGE ELECTRODYNAMICS DRIVE THREE SET SERIES OF FREEDOM ARMATURE ROTARY 4 BLADE MOTION DRIVE ALONGSIDE THE RIGHT FOOT BOTTOM FRONT ROTARY PROPELLER SET SERIES SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIAL METRIC RANGE INVENTOR JERMAINE MORTON DESIGN

https://youtu.be/oWiYsRi2Dss

Examples WEARABLE MANNED UAV BODY ARMOR ELECTRODYNAMICS PROPULSION

FLYMORTON CHARACTERIZED AS IN WEARABLE BIOMECHANICAL TRANSDUCTION MOTORIZED ELECTRONIC BOOT MANNED UAV ORTHOSIS FOOT BIOFRINGENT BIOMETRIC FOOT SHAPED RANGE ELEMENT PIEZOELECTRIC EFFECTS PYROELECTRIC EFFECTS THERMOELECTRIC EFFECT SILICON ELECTROMAGNET HALL EFFECT HORN BASE MODULATED AUDIO ENCODER ELECTROMOTIVE HARMONIC SONIC COMMUTATOR CAGE STRUCTURE LINEAR MOTOR ELECTRODYNAMICS SPLIT SOLENOID PULL PUSH DIVERSE ROTATING DRIVE BALL BARING BRACKET ROTOR PERMANENT MAGNET 4 PROPELLER BLADE ARMATURE CONNECTIONS TO GRAPHITE FOOT FRAME PROPELLER CHAMBER SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIAL METRIC RANGE INVENTOR JERMAINE MORTON DESIGN

Method or approach cooler microwaves vector field the image 19AWG copper coil 500T tightly spun helix shape alongside silicon element round hollow block ring structure functional likenesses as an Electromagnetic Suspension coil Electromagnetic hall effects solenoid pull push hold sensory four phase wire coil separated by silicon element hollow block cage coil silicon thermal positive charge thermoelectric effects refrigeration negative charge heat dissipate Seebeck effects Peltier effects cooler semiconductor High Purity 4N 99.99% Bismuth element block cage superconductor 52N 600LBS pulling rate Nickel Neodymium magnet repeat within series alongside the silicon copper tubing liquid cooling spun within the silicon heatsink block bladed ring coil helix shape alongside around the ring modification enable the copper tubing fluid cooling Suspension coil 19AWG mounted to an aluminum element biometric foot range block bottom surface commutator cage electrodynamics BLOCK subject not limiting to additional structure inventor Jermaine Morton design

FLYMORTON WEARABLE ELECTRONIC FLIGHT BOOTS, EXHIBITING aluminum block housing. THE ALUMINUM HOLLOW BLOCK BARING PERMANENT MAGNET CORE OF STRUCTURE EXSOFRAME. THE PERMANENT MAGNET EXSOFRAME MODULATED ELECTRONIC BOOT ION ENGINE COOLING SYSTEM. CYLINDRICAL tubing liquid cooling. SPUN INTO HELIX SHAPE ALONGSIDE 19 AUDIO WIRE GAUGE. SPUN INTO SOLENOID TYPE ELECTROMAGNETIC LEVITATION INDUCTION MOTOR STRUCTURE. EXHIBITS 5000 TURNS INDUCTION WIRE CORE. ALONGSIDE THE ELECTRICAL TRANSDUCTION WIRE COPPER LIQUID COOLING TUBING TUBING SPUN ALONGSIDE THE METRIC CIRCULAR RANGE. DIRECT CURRENT PHASE THE INDUCTOR WIRE ELECTROMOTIVE rectifier CIRCUIT ALTERNATIVE CURRENT CONVERT INTO DIRECT CURRENT PHASE WIRE MODULATED ELECTROMOTIVE DRIVEN AUDIO ULTRASONIC ENCODER OUTPUT AC CHARGE ELECTROMAGNETIC PULSE PHASE TWO SUSPENSION MODULATED GYROSCOPIC PITCH AXIS SWITCH CHANNEL LEVITATION COIL EMITTER Or gravity proximity distance sensory switch channel controls charge coil spun series type electromagnetic linear MOTOR SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIAL METRIC RANGE INVENTOR JERMAINE MORTON DESIGN

COOLING DIAMAGNETIC EXOSKELETRONIC BOOT ENGINE ORTHOSIS LEG FOOT BOTTOM BRACE SUBSYSTEM STRUCTURE OR MATERIAL
PARAMAGNETIC MCE THERMAL RESISTANCE ELECTRICAL WIRING
Gd2(SO4)3·8H2O, 20°C 68°F THERMAL HYSTERESIS COOLING COIL TUBING ALONGSIDE CIRCLE COPPER COIL SURFACES
COPPER COIL cage BARING silicon hollow chamber operates HFC 134a LIQUID cooling tube Pump liquid refrigerant's vapor temperature is between 40° and 50°F; and without changing its temperature; it absorbs heat as it changes state from a liquid to a zero degree low temperature vapor .subject not limiting to additional structure potential metric range inventor Jermaine Morton design

FLYMORTON BIOMECHATRONIC BOOTS, RECTANGULAR CYLINDRICAL BARING MAGNET BIOFRINGENT EXOSKELETRONIC CALF SHIN BIAXIAL ANKLE ROM HEEL FOOT TOE COMMUTATOR CAGE INDUCTION COIL HELIX SHAPED SPUN ELECTROMOTIVE ELECTROMAGNETIC PULSE PHASE TWO SOLENOID PULL PUSH SENSORY ELECTROMAGNETIC LEVITATION HALL EFFECTS SENSE TRACTOR BEAM ELECTROSTATIC VECTORING PROXIMITY HOLD SENSE SUSPENSION AND LINEAR MOTOR ELECTROSTATIC repulsive forces against aluminum boot FRAME having freedom of movement AND MINIMUM WEIGHT RESISTANCE SELF repulsive AGAINST THE WEIGHT OF ITS GRAVITY AGAINST ITS INERTIAL WEIGHT OF THE MATERIAL COMMON HAVING NOT OPPOSITES THAT MAY ATTRACT ION however forces MATERIAL AWAY FROM THE ELECTROMAGNETIC SONIC PULSE VECTOR FIELD WHILE TRAVELING both COIL EMITTER AND HOUSING ARE carried AWAY OPPOSITE DIRECTION OF THE HALL EFFECT EMITTER PHASE POINT moving BOTH THE COIL ENGINE AND aluminum EXO FRAME SIMULTANEOUSLY CHARGE INDUCTOR ELECTROMAGNETIC LEVITATION COIL or LINEAR MOTOR DIRECT CURRENT PHASE WIRE POINT IONS electrodynamics winding ENERGY TRAVELING REPULSIVE FORCE permanently connected to COMMON MATERIAL against the weight of its gravity against its inertial weight of gravity having FREEDOM OF MOVEMENT horizontally or AC
CHARGE INDUCTOR ELECTROMAGNETIC LEVITATION COIL or LINEAR MOTOR ALTERNATIVE CURRENT PHASE WIRE POINT ION electrodynamics repulsive energy winding REPULSIVE FORCE emitter permanently connected to its COMMON MATERIAL mount against the unified magnitude weight of gravity from the direction of its emitting ions velocity greater than the aluminum having FREEDOM OF MOVEMENT traveling vertically or horizontally modulated by gyroscopic MCU and gravity sensors distance center switch self suspension levitation controls, subject not limiting to additional system or structure potential metric range inventor Jermaine Morton designed

Electromagnetic
References and examples
https://youtu.be/r0bGQVB2y3M
https://youtu.be/oWiYsRi2Dss

https://youtu.be/OI_HFnNTfyU

Electronic boot repulsive engine subsystem

materials are

Awg 18 copper wire

Diameter 0.0403

Resistance per 1000 ft (ohms) 6.385

over 1,000 volts.

Resistance per 5000 ft (ohms) 31.925

18 AWG 5,000 ft divided by 3inch wire turns= 60,003 times 3inch turns

5 kilowatts =5000 watts

746 Watts equivalent to 1 horsepower

5 kilowatts =6.705 british horsepowers

My weight 183lbs

Body armor weight 140lbs

Inertial weight 320lbs

Eddy currents are

6,382lbs electrostatic Paramagnetic energy winding Repulsive forces against diamagnetic lift up into the air against 183lbs human users body weight of gravity includes 140lbs diamagnetic manned human users body armor inertial weight 320lbs of gravity Eddy currents force of emissions 6,382lbs repulsive forces against diamagnetic 320lbs manned body armor lifted into the air subject not limiting to additional structure potential metric range inventor Jermaine Morton design furthermore the boot engine

PARAMAGNETIC MCE COPPER REFRIGERANT COOLING TUBING SPUN TIGHTLY INTO HELIX SHAPE ALONGSIDE ELECTRICAL WIRING PURPOSE FOR HEAT DISSIPATION METHOD

Gd2(SO4)3·8H2O, thermal hysteresis 20°C 68°F

REFRIGERANT LIQUID COOLING TUBING SPUN ALONGSIDE THE ELECTRICAL EXTERIOR COPPER COIL SURFACES, THE ELECTRICAL

HELIX SHAPE SPUN COPPER COIL EXHIBITS HOLLOW cage silicon TUBING operates (HFC 134a) REFRIGERANT COOLING TUBING CONNECTIONS TO DC ROTOR MOTOR Pump liquid refrigerant's vapor temperature is between 40° and 50°F; and without changing its temperature; it absorbs heat as it changes state from a liquid to a vapor.subject not limiting to additional structure potential metric range inventor Jermaine Morton design,

coil turns are spun helix shaped alongside or within aluminum block interface introduced to the same metric range virtually equal in area Electrically induce phase wire point. charge inductor coil Transfer potential energy creates electrostatic paramagnetic particle density effects the aluminum block with a higher repulsive force of matter in a given space underneath aluminum block surfaces modulated electronic circuit electromotive (EMS) damping vibrations axis stability eddy currents allowing stability alternating current magnetic fields given potential energy attractive current field vector proximity and opposing current field vector proximity (EDS). Repulsive forces against diamagnetic weight of gravity simultaneously carrying the electromagnetic emissions source having a lower weight the Electrodynamics potential energy repulsive forces both emission source and the diamagnetic Element against it's inertial weight of gravity lifted into the air as to levitate as to fly

Acoustic encoder 100hz ultrasonic drive phase wire p type n type bus connections to three separated coils separated by group stacked graphite to silicon to aluminum to bismuth starlight fireproof coated block type baring linear motor coil between magnetic suspension coils all of which are enclosed within epoxy resin crystal clear harder

waterproof enclosure

Thermal dynamics phase Graphite thermal electric effect phase

Silicon Thermal electric effect refrigeration phase common effect aluminum repulsive energy phase Bismuth semiconductor Peltier effect cooler side coated by fireproof starlight materia

I'm

ALUMINUM BLOCK BARING RECTIFIER MODULE AC/DC ELECTROMAGNETIC PULSE PHASE TWO WIRE 19AWG COPPER WIRE SPUN THROUGHOUT ALUMINUM BLOCK OPEN CLEARANCE SURFACE BASE CROSS THREADED 19AWG SOLENOID PULL PUSH ELECTROMAGNETIC PULSE PHASE TWO LINEAR MOTOR VERTICAL OR HORIZONTAL SELF SUSPENSION ELECTRODYNAMICS PROPULSION MANNED UAV ESC ORTHOSIS FOOT BRACE ARMOR SUBJECT NOT LIMITING TO ADDITIONAL STRUCTURE INVENTOR JERMAINE MORTON DESIGN

Electronic boot repulsive engine subsystem

materials are

Awg 18 copper wire

Diameter 0.0403

Resistance per 1000 ft (ohms) 6.385

over 1,000 volts.

Resistance per 5000 ft (ohms) 31.925

18 AWG 5,000 ft divided by 3inch wire turns= 60,003 times 3inch turns

5 kilowatts =5000 watts

746 Watts equivalent to 1 horsepower

5 kilowatts =6.705 british horsepowers

My weight 183lbs

Body armor weight 140lbs

Inertial weight 320lbs

Eddy currents are

PARAMAGNETIC MCE COPPER REFRIGERANT COOLING TUBING SPUN TIGHTLY INTO HELIX SHAPE ALONGSIDE ELECTRICAL WIRING PURPOSE FOR HEAT DISSIPATION METHOD

Gd2(SO4)3·8H2O, thermal hysteresis 20°C 68°F

REFRIGERANT LIQUID COOLING TUBING SPUN ALONGSIDE THE ELECTRICAL EXTERIOR COPPER COIL SURFACES, THE ELECTRICAL

FLYMORTON WEARABLE BIOMECHATRONIC MANNED UAV SUIT MACHINES DESIGN ORTHOSIS BIOMETRIC RANGE ELECTROMAGNETIC ELECTRON CAPACITOR STATOR THERMOCOUPLE BIOFRINGENT MAGNETRONS STRUCTURE THERMOELECTRIC EFFECTS COOLER HALL EFFECTS REFRIGERATION PHASE ANTI-GRAVITY ESC BOOT ELECTRODYNAMICS REPULSIVE TECHNOLOGY SUBJECT NOT LIMITING TO ADDITIONAL STRUCTURE INVENTOR JERMAINE MORTON DESIGN

CHARGE INDUCTOR ELECTROMAGNETIC LEVITATION COIL or LINEAR MOTOR ALTERNATIVE CURRENT PHASE WIRE POINT ION electrodynamics repulsive energy winding REPULSIVE FORCE emitter permanently connected to its COMMON MATERIAL mount against the unified magnitude weight of gravity from the direction of its emitting ions velocity greater than the aluminum having FREEDOM OF MOVEMENT traveling vertically or horizontally modulated by gyroscopic MCU and gravity sensors distance center switch self suspension levitation controls, Acoustic encoder 100hz ultrasonic drive phase wire p type n type bus connections to three separated coils separated by group stacked graphite to silicon to aluminum to bismuth starlight fireproof coated block type baring linear motor coil between magnetic suspension coils all of which are enclosed within epoxy resin crystal clear harder waterproof enclosure

coil microwave Thermal dynamics phase Graphite thermal electric effect phase

Amount copper wire
coil turns are spun helix shaped alongside or within aluminum block interface introduced to the same metric range virtually equal in area Electrically induce phase wire point
charge inductor coil Transfer potential energy creates electrostatic paramagnetic particle density effects the aluminum block with a higher repulsive force of matter in a given space underneath aluminum block surfaces modulated electronic circuit electromotive (EMS) damping vibrations axis stability eddy currents allowing stability alternating current magnetic fields given potential energy attractive current field vector proximity and opposing current field vector proximity (EDS). Repulsive forces against diamagnetic weight of gravity simultaneously carrying the electromagnetic emissions source having a lower weight the Electrodynamics potential energy repulsive forces both emission source and the diamagnetic Element against it's inertial weight of gravity lifted into the air as to levitate as to fly

Amount copper wire

coil turns are spun helix shaped alongside or within aluminum block interface introduced to the same metric range virtually equal in area Electrically induce phase wire point

charge inductor coil Transfer potential energy creates electrostatic paramagnetic particle density effects the aluminum block with a higher repulsive force of matter in a given space underneath aluminum block surfaces modulated electronic circuit electromotive (EMS) damping vibrations axis stability eddy currents allowing stability alternating current magnetic fields given potential energy attractive current field vector proximity and opposing current field vector proximity (EDS). Repulsive forces against diamagnetic weight of gravity simultaneously carrying the electromagnetic emissions source having a lower weight the Electrodynamics potential energy repulsive forces both emission source and the diamagnetic Element against it's inertial weight of gravity lifted into the air as to levitate as to fly

FLYMORTON WEARABLE BIOMECHATRONIC MANNED UAV SUIT MACHINES DESIGN THERMOCOUPLES MAGNETRONS STRUCTURE THERMOELECTRIC EFFECTS HALL REFRIGERATION ANTI-GRAVITY ESC BOOT ELECTRODYNAMICS

FLYMORTON CHARACTERIZED AS IN WEARABLE LINEAR MOTOR MANNED UAV ROTOR COMMUTATOR CAGE ORTHOSIS BIOMETRIC RANGE SHAPE MODULATED HARD SUIT SIGNALS SOFTWARE BASE PROCESSOR ELECTROMOTIVE BRAINWAVES SENSORY HUMAN MAGNETO ELECTROPHYSICAL RADAR BIOMETRIC RANGE NAVIGATION LANDING SWITCH CONTROLS GRIPPING VERTICAL WALL CLIMBING CROSS CRAWLING UNIGRAVITY ANTIGRAVITY ELECTRODYNAMICS ION PROPELLANT ENGINE ROCKET ELECTROMAGNETIC SELF- SUSPENSION SELF LEVITATION BIOMECHATRONIC POWERED FLIGHT SUIT MACHINE BODY ARMOR SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIAL METRIC RANGE INVENTOR JERMAINE MORTON DESIGN

https://www.flymorton.blogspot.com

https://www.flymorton.com

Unigravity anti-gravity

How is it possible

18 peace Magnetic levitation Copper coils

100T+ spun around stainless steel

liquid cooling tubing both localized

connected on to an aluminum block surfaces,

whenever the current carrying

group of induction coil receives a charge

the charge inductor maybe above 737watts

of electrical energy repulsive forces

away the aluminum block simultaneously the coils couple to the aluminum block are

carried by the aluminum being lifted

up away into the air by electromagnetic repulsive Forces aluminum away phase by coil energy winding emitting electrostatic repulsive energy Gus translated microwaves measured attack Force more than 550lbs maybe measured translated into one mechanical horsepower of microwaves forces against the aluminum block away up into the air carried the intense radiation microwave energy vectoring constant Forces against the aluminum block gravitational weight and inertial weight of gravity subject not limited to additional structure inventor Jermaine Morton design

FLYMORTON WEARABLE MANNED UAV THERMOCOUPLE BIOMECHATRONIC MAGNETRON ESC ANTI-GRAVITY BOOT ELECTRODYNAMICS PROPULSION REPULSIVE TECHNOLOGY

Electronic boot repulsive engine subsystem
materials are
Awg 18 copper wire
Diameter 0.0403
Resistance per 1000 ft (ohms) 6.385
over 1,000 volts.
Resistance per 5000 ft (ohms) 31.925
18 AWG 5,000 ft divided by 3inch wire turns= 60,003 times 3inch turns
5 kilowatts =5000 watts
746 Watts equivalent to 1 horsepower
5 kilowatts =6.705 british horsepowers
My weight 183lbs
Inertial weight 140lbs
6,382lbs electrostatic Paramagnetic energy winding Repulsive forces diamagnetic lift up into the air against 183lbs users body weight gravity includes 140lbs additional inertial weight of gravity subject not limiting to additional structure potential metric range inventor Jermaine Morton design furthermore the boot engine
PARAMAGNETIC MCE THERMAL RESISTANCE ELECTRICAL WIRING
Gd2(SO4)3·8H2O, COOLING TUBING ALONGSIDE CIRCLE COPPER COIL SURFACES
COPPER COIL cage BARING silicon hollow chamber operates HFC 134a LIQUID cooling tube Pump liquid refrigerant's vapor temperature is between 40° and 50°F; and without changing its temperature; it absorbs heat as it changes state from a liquid to a vapor.subject not limiting to additional structure potential metric range inventor Jermaine Morton design

The magnetic levitation coil fixed underneath the aluminum block whenever received a charge electrodynamics Repulsive FORCES against the aluminum considered as an diamagnetic element FORCES the aluminum block to ESC from electrostatic field vector proximity hall effects coil are permanently mounted to the aluminum block surfaces emissions forces the aluminum block away simultaneously the hall effects coil are being lifted into the air Carried upwards by the aluminum block moving away from the emissions 1000+ times greater than the weight of the gravity and 1000+ times greater than the initial weight

The boot bottom HOLLOW aluminum block cage ball baring bracket freedom for rotation armature mount. The upper stacked metalloid thermocouple baring diamagnetic aluminum block baring coated 18awg copper magnetIc coated induction wire coil type solenoid magnetic levitation helix shape spun around the refrigeration MCE HFC liquid cooling silicon tubing connected to the aluminum block surfaces the aluminum block enclosed within Bismuth element to silicon housing the tubing baring alongside around the exterior CHARGE Electrical copper wire coil emits SYNCHRONOUS ALTERNATIVE CURRENT electrostatic energy winding wireless power current carrying charge thermocouple element Bismuth current carrying silicon Metalloid thermoelectric effects refrigeration Seebeck effects electrodynamics Electromagnetic electrostatic Paramagnetic hall effects solenoid push pull 1100Newton+ energy repulsive forces phase diamagnetic element ESC AGAINST THE DIAMAGNETIC WEIGHT OF GRAVITY Initial weight of gravity couple to the diamagnetic element emissions phases underneath repulsive microwaves movement alongside the surfaces of the diamagnetic element between the emission source repulsive FORCES away the diamagnetic element carrying the emission source repulsive FORCES on or above 1100newtons suspending both the the source and the diamagnetic element in the case is the orthosis calf shin ankle heel foot toe metalloid brace suspended within vector solenoid pull tractor solenoid hall effects beaming repulsive FORCES against the diamagnetic EXOSKELETRONIC solenoid held within proximity solenoid hold sensory subject not limiting to additional structure potential metric range inventor Jermaine Morton design


	Amount copper wire	coil turns are spun helix shaped alongside or within aluminum block interface introduced to the same metric range virtually equal in area Electrically induce phase wire point	charge inductor coil Transfer potential energy creates electrostatic paramagnetic particle density effects the aluminum block with a higher repulsive force of matter in a given space underneath aluminum block surfaces modulated electronic circuit electromotive (EMS) damping vibrations axis stability eddy currents allowing stability alternating current magnetic fields given potential energy attractive current field vector proximity and opposing current field vector proximity (EDS). Repulsive forces against diamagnetic weight of gravity simultaneously carrying the electromagnetic emissions source having a lower weight the Electrodynamics potential energy repulsive forces both emission source and the diamagnetic Element against it's inertial weight of gravity lifted into the air as to levitate as to fly

The boot bottom HOLLOW aluminum block cage ball baring bracket freedom for rotation armature mount. The upper stacked metalloid thermocouple baring diamagnetic aluminum block baring coated 18awg copper magnetIc coated induction wire coil type solenoid magnetic levitation helix shape spun around the refrigeration MCE HFC liquid cooling silicon tubing connected to the aluminum block surfaces the aluminum block enclosed the tubing baring CHARGE Electrical copper wire coil emits SYNCHRONOUS ALTERNATIVE CURRENT electrostatic energy winding wireless power current carrying charge thermocouple element Bismuth current carrying silicon Metalloid thermoelectric effects refrigeration Seebeck effects electrodynamics Electromagnetic electrostatic Paramagnetic hall effects solenoid push pull 1100Newton+ energy repulsive forces phase diamagnetic element ESC AGAINST THE DIAMAGNETIC WEIGHT OF GRAVITY Initial weight of gravity couple to the diamagnetic element emissions phases underneath repulsive microwaves movement alongside the surfaces of the diamagnetic element between the emission source repulsive FORCES away the diamagnetic element carrying the emission source repulsive FORCES on or above 1100newtons suspending both the the source and the diamagnetic element in the case is the orthosis calf shin ankle heel foot toe metalloid brace suspended within vector solenoid pull tractor solenoid hall effects beaming repulsive FORCES against the diamagnetic EXOSKELETRONIC solenoid held within proximity solenoid hold sensory subject not limiting to additional structure potential metric range inventor Jermaine Morton design

FLYMORTON WEARABLE INDUCTION SUSPENSION ARMOR REPULSIVE FORCES DIAMAGNETIC BODY ARMOR ESC MANNED UAV ORTHOSIS BIOMETRIC RANGE BIOFRINGENT BODY ARMOR FLIGHT SUIT MACHINES.

18awg current carrying cross threaded sewing throughout diamagnetic body armor RECTIFIED AC/DC 18AWG 5000ft length divided 3inch 60,000T suspension coil charge 5kw 6,705hp 4400lbs+Eddy currents electrostatic Paramagnetic forces SELF-repulsive against weight of gravity forces against inertial weight of gravity lifted into the air.

EXAMPLES OF INDUCTION MOTORS

https://youtu.be/OI_HFnNTfyU

WEARABLE BIOMECHATRONIC BIOFRINGENT MCE HFC REFRIGERATION TRANSDUCTION EMS SUBSYSTEM EDS SELF-REPULSIVE SELF SUSPENSION DIAMAGNETIC MANNED UAV LINEAR MOTOR ORTHOSIS CALF BRACE ESC SUBJECT NOT LIMITING TO ADDITIONAL STRUCTURE INVENTOR JERMAINE MORTON DESIGN

RAW BIOMECHANICAL DIAMAGNETIC

biometric calf DESIGN

100 OF THE WEIGHT OF THE ALUMINUM BLOCK FRAME cut SUBSTRACTION LEAVING 60%aluminum BLOCK frame weight metric REPLACED BY ADDING 40% WEIGHT OF 24 AWG copper SPUN HELIX SHAPED ALONGSIDE THE ALUMINUM BLOCK FRAME UNTIL THE WEIGHT OF ALUMINUM BLOCK 100% OF SOLID WEIGHT. ESC MOTOR CONTROLS 50 AMPHERE MODULATED ELECTROLUX ELECTROMOTIVE METALLIC BOND MFD 1000ft 1KW PER CHARGE 24AWG SPUN AROUND THE ALUMINUM BLOCK FRAME VERTICALLY ALONGSIDE SPACERS UNDERNEATH CONNECTIONS TO FLAT TITANIUM SHEET METAL FRAME USED TO INCREASE THE MAGNETIC REPULSIVE STRENGTH VECTORING VELOCITY ELECTROSTATIC EMISSIONS

Typical Wire Chemistry
Zn 1.0
Sn 1.0
Mn 1.5
Fe 0.50
Si 2.8 - 4.0
Al 0.01
Pb 0.02
Cu (including Ag) REM
OTHER 0.50
Coated wire Epoxy resin cryonic liquid waterproof protection

SILICON COPPER SPOOL WIRE 200T COIL COMMONLY USED FOR TIG WELDING DCEN. THE SILICON COPPER WIRE SHALL BE SPUN TIGHTLY AROUND ABOUT THE 24 AWG 1000T MAGNETIC COPPER WIRE SURFACES WHENSOEVER THE ELECTRICAL ENERGY GENERATED SIGNALS WIRE TO ESTABLISH A CHARGE SOLENOID COIL ELECTRICAL ENERGY WINDING THERMAL DYNAMICS PHASE SILICON COPPER SPUN SOLENOID COIL PHASE THERMOELECTRIC EFFECTS REFRIGERATION WIRE HEAT PHASE POINT TOWARDS LENGTH OF WIRE REACTIVE HEAT DISSIPATION PHASE SEEBECK EFFECTS SILICON COPPER COIL PHASES THE CENTER MAGNETIC COIL SURFACES HEAT DISSIPATION WITHIN SILICON COPPER COIL THERMOELECTRIC EFFECTS CAGE

IRONMAN MARK42 EMS DIAMAGNETIC SELF-REPULSIVE LEVITATION MANNED ORTHOSIS BIOMETRIC RANGE BRACE UAV ELECTROMAGNETIC BODY ARMOR EDTS ENGINE BOOT THRUSTERS BOTTOM GAUNTLET HANDHELD PALMER ENGINE EDTS THRUSTERS COOLER THERMIONIC EMISSIONS ELECTRODYNAMICS SUBJECT NOT LIMITING TO ADDITIONAL STRUCTURE PROGRESSIVE DEVELOPMENT INVENTOR JERMAINE MORTON DESIGN

WEARABLE BIOMECHATRONIC EMS EE EDS REPULSIVE FORCES DIAMAGNETIC ORTHOSIS BOOT ESC

The induction ESC MOTOR EMS 4000KW there are four Audio wire solenoid coils 1000turns per coil 1kw per charge, there are six solenoid push pull coil within the boot bottom. 2 solenoid coils audio wire are only 400turns, But and the other four solenoid audio wire coils are 1000Turns audio wire , enumerates 4000 watts divided by 240volts is 16.6 amps.

4000 watts =5.364 british horsepowers

Reminder

1 hp motor lift, about 550 lbs (250 kg) at a rate of 1 ft/sec, 1100 lbs at a rate of 0.5 ft/sec, 225 lb at a rate of 2 ft/sec, 1 lb at a rate of 550 ft/sec, and so on.

However

550 lbs times 7= 3,850lbs REPULSIVE lift forces against diamagnetic boot bottom ESC however limited to one single boot bottom not as of a pair. EMS ENERGY VELOCITY

The difference in this magnetic suspension I have connected both the Repulsive emission source to lift together couple to the diamagnetic aluminum block. the phase wire electromagnetic suspension coil emits electrical winding electrostatic repulsive 3.850lbs of energy psi forces against the common element away from the direction of the electrical energy winding lifted into the air yanking both the emission source against the weight of gravity and inertial Mass ANTI-GRAVITY not emitting against the Earth surfaces no contrary against the aluminum block weight of gravity or inertial mass the aluminum block in this case is couple to the coil wiring crossed sewing coil wiring are threaded between the open clearance aluminum block gauge

https://youtu.be/OI_HFnNTfyU

CERAMIC & silicon carbide powder solid

WEARABLE BIOMECHATRONIC EMS EE EDS REPULSIVE FORCES DIAMAGNETIC ORTHOSIS BOOT ESC

4000 watts =5.364 british horsepowers

Reminder

1 hp motor lift, about 550 lbs (250 kg) at a rate of 1 ft/sec, 1100 lbs at a rate of 0.5 ft/sec, 225 lb at a rate of 2 ft/sec, 1 lb at a rate of 550 ft/sec, and so on.

However

550 lbs times 7= 3,850lbs REPULSIVE lift forces against diamagnetic boot bottom ESC EMS ENERGY VELOCITY Subject not limiting to additional structure potential metric range inventor Jermaine Morton design

FLYMORTON.COM

Wednesday, December 22, 2021

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