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 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

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

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


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
















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, 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


















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







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 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 energy repulsive forces phase diamagnetic element ESC AGAINST THE DIAMAGNETIC WEIGHT OF GRAVITY couple to the diamagnetic element emissions phases underneath the diamagnetic element suspended within the vector field tractor beam within proximity solenoid hold sensory


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



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 wirecoil 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
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


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










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


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





































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

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 EMS ENERGY VELOCITY Subject not limiting to additional structure potential metric range inventor Jermaine Morton design


































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ALJ.Hearings@SSA.gov If I could work Minimum wage is $8.75 700$ every two weeks after taxes 691$.6¢ Monthly 1,383.2 Social security administration claims dispute JERMAINE MORTON claims argued that Jermaine Morton can work without getting disability income social security discontinued JERMAINE MORTON'S social security benefits as of May 2025 Social security administration decision discontinues Jermaine Morton social security administration claims jermaine morton is not eligible for social security benefits in no respect or regards or accountability cause by social security administration any Damages of the following social security administration acknowledge their decision that shall effects JERMAINE MORTON lifestyle For example Jermaine Morton only owns 1 pants 1 t-shirt 1 Jean pants 1 pair socks 1 underwear 1 pair sneakers 1 hat 1 bookbag Social security administration acknowledges their decision that discontinues Jermaine Morton social security claims for assistance jermaine morton is not eligible for social security benefits in no respect or regards or accountability cause by social security administration however social security administration suggest made to jermaine morton in writing that he is able to work! Following social security administration decision Social security administration acknowledges in their decision that Jermaine Morton has no source of income banking account and no savings account And no cash jermaine morton acknowledges the impact the decision the social security administration has caused though its final decision action completed effectively without referrals or verbal suggestions for forwarding an assistance the final decision is from or by the social security administration in person or by phone or letter Jermaine Morton must be fully responsible for survival financial expenses or living expenses or any children that are beneficiarys which was receiving a financial fraction of optional by or from jermaine mortons discontinued financial benefits Leaving Jermaine Morton with 0$0¢ Generally, a high school diploma or equivalent (like a GED) is considered the minimum level of education for many entry-level positions at the DOL and in the federal government. This is because it serves as a basic level of education that employers often use as a hiring criteria. Specific Job Requirements: The specific educational requirements will vary depending on the particular job you're applying for. Some roles, particularly those in professional and scientific fields, may require a specific college degree. You should carefully review the job announcement for the specific qualifications needed. Jermaine Morton has an 4th grade education Level Being in and out of detention center at 11 years of age until Jermaine Morton aged 15 years old Jermaine Morton has not attended school until he was 16 years of age 1 suspensions that lead to a total refusal of his mother not signing him back in school Jermaine Morton has attended Coney Island Brooklyn hospital physiatry center from 16years of age until 17 years of age and at the age of 18years old JERMAINE MORTON became homeless in the state of New York City Brooklyn Coney Island now resides In the United States of America within Florida State Jacksonville Duval county at the age of 47 whereas the cost of rapid bus traveling or traveling financial expenses and must take full responsibility of his actions cost of rapid public Transit $1.75 per ride note that jermaine morton has 0$0¢ To not limiting the cost of bus and transfer to an additional bus traveling toward work of $1.75¢+$1.75¢ And from work $1.75¢+$1.75¢ In the amount for 10 days of rapid bus traveling Cost of rapid bus traveling 70$ 3$.50¢ to and from work 3$.50¢=7$ daily for 20days of work=140$ monthly expenses Jermaine Morton acknowledges that he has not saved 0$.0¢ Having no financial income Hourly income 0$.0¢ Daily income 0$.0¢ Monthly income 0$.0¢ Yearly income 0$.0¢ no cash No savings account 0$0¢ Jermaine Morton has no financial support or financial assistance for transportation to and from work or the qualifications in order to get a job Social security administration acknowledges the effects that by decision Jermaine Morton having responsibilities 5 children ages female born 1991~2025 34 years old Male son 1995~2025 30 years old Female daughter 2003~2025 22 years old Male son 2006~2025 19 year's old Female daughter 2010~2025 15 years old Assuring Jermaine Morton social security administration shall not be held to accountability claims or neglect laws following any events leading to any failures of responsibilities effected apon of social security administration decision Rental payments expenses that are bill monthly Child care rental payments expenses that are bill monthly Child care food supply expenses that are bill monthly Child care travel financial expenses that are bill monthly Medical payments financial expenses that are bill monthly Medication payment financial expenses that are bill monthly Phone payment financial expenses that are bill monthly Food supply payment financial expenses that are bill monthly Public rapid Transit financial payment expenses that are bill monthly Clean clothing maintenance financial payment expenses that are bill monthly Cosmetic payment financial financial expenses that are bill monthly Toiletry payment financial expenses that are bill monthly laundry payment financial expenses that are bill monthly Social security administration decision claim they shall not be subject to accountability act or neglect crime apon our decision caused or Damages locked out of rental storage monthly bill unpaid loss of clothing Loss of cosmetic Loss of personal government documents Loss of personal government receits Loss of storage property Loss of patentable material Loss of patent documents Loss of copyright documents Loss of copyrightable material Loss of rare material Loss of Rental storage Loss of Child care rental Loss of Child care food supply Loss of Child care travel Loss of financial benefits child neglect Loss of Medical Loss of Medication Loss of being contacted by Phone Loss of Food supply Loss of Public rapid Transit Loss of Clean clothing Loss of Cosmetic Loss of Toiletry Loss of laundry Loss of Rental Homeless Cause by Social security administration Cancellation social security benefits Social security agent failure contact Jermaine Morton, Social security administration agent Failure to access updated address information Social security administration agent decision neglect accountability cause Damages JERMAINE MORTON has no secondary clothing Jermaine Morton only owns 1 pants 1 t-shirt 1 Jean pants 1 pair socks 1 underwear 1 pair sneakers 1 hat 1 bookbag No permanent address Social security administration written statements Denied jermaine morton disability claim and discontinued his monthly benefits Of 1,610$.0¢ Social security administration agent suggests Jermaine Morton can work without a referral from social security administration records claims that Jermaine Morton has no high school diploma no GED diploma, No long range work history no training or skill no medical benefits, No medical coverage, no other means of income, no relatives local No means of contacting Jermaine Morton or locating jermaine morton has No home or apartment address jermaine morton is considered homeless Jermaine Morton has No clothing and is not allowed to panhandle solicitate help or financial assistance No place of residence not allowed to panhandle solicitate or trespass No food not allowed to panhandle not allowed solicitate not allowed to trespass No water not allowed to panhandle not allowed to solicitate or trespass No medicine not allowed to panhandle not allowed to solicitate or trespass No home or no apartment not allowed to panhandle solicitate or trespass No contact cellular phone operational devices by mean that jermaine morton maybe contacted Jermaine Morton can not connect with any online services No bathhouse or means of bathing not allowed panhandle solicitate or trespass No toilet or wipes paper to keep skin tissue clean or healthy not allowed to solicitate or trespass no place to sleep not allowed on anyone property not allowed to solicitate or trespass No place to rest not allowed on anyone property not allowed to solicitate or trespass No place to stand not allowed on anyone property not allowed to solicitate not allowed to panhandle or trespass Policies against panhandling, or begging for money, often involve restricting where and how begging can occur, rather than banning it outright. Many cities and counties have ordinances that limit panhandling in specific areas, during certain hours, or if it's considered aggressive or disruptive. Restricted areas: Many jurisdictions prohibit panhandling near businesses, ATMs, bus stops, and other public spaces. Time restrictions: Some cities limit panhandling to daylight hours. Permits and licensing: In some cases, panhandlers may be required to obtain permits or licenses. solicitation policy in the workplace defines the rules around employees soliciting or distributing materials to other employees or non-employees. These policies aim to maintain a professional and distraction-free environment, prohibiting activities like selling items, soliciting donations, or distributing political materials during work hours or in work areas. Surface area of the lot boundary in square feet or meters, geographical information system (GIS) map, which is a similar map and is available on government sites as well. It also delineates the legal boundaries of your property. This information should also be located on your property deed trespass in a structure or conveyance is a misdemeanor of the second degree, punishable as provided not been authorized, licensed, or invited, is warned by the owner or lessee of the premises, or by a person authorized by the owner or lessee, to depart and refuses to do so, commits the offense of trespass in a structure or conveyance. (2)(a) Except as otherwise provided in this subsection, trespass in a structure or conveyance is a misdemeanor of the second degree, punishable as provided in s. 775.082 or s. 775.083. (b) If there is a human being in the structure or conveyance at the time the offender trespassed, attempted to trespass, or was in the structure or conveyance, the trespass in a structure or conveyance is a misdemeanor of the first degree, punishable as provided in s. 775.082 Social security administration agent decision of neglect holding no accountability In no respect or regards to standing policies or rules in limitations of case manager's failure to properly assess, Failure to plan, failure to connect with Jermaine Morton needed resources, However social security administration decision to discontinue Jermaine Morton financial or medical benefits can contribute to situations where people are at risk of harm. can Jermaine Morton survive without money. Jermaine Morton Survival depends on various factors like access to food, water, and shelter, all of which typically require money in modern society. Without these necessities, a jermaine morton's health would rapidly deteriorate, and survival would be short-lived. social security agents are case managers that can contribute to situations where neglect occur: failing to provide the necessary care, attention, or support that they require or deserve. It can involve ignoring their needs, disregarding their well-being, or not fulfilling obligations towards them. Neglect can manifest in various ways, including emotional, physical, or financial inadequacies. 1. Failure to Properly Assess Needs: Glucose as Fuel: The brain relies heavily on glucose, a simple sugar, for energy. Unlike other body parts, the brain cannot store glucose, so it needs a constant supply No, the human brain cannot work properly without a steady supply of glucose, its primary fuel source. The brain needs a constant supply of glucose to perform functions like thinking, memory, and learning. Without enough glucose, neurotransmitters, the brain's chemical messengers, are not produced, and communication between brain cells (neurons) breaks down. A social security administration decision failure with no accountability has no adequately assess an individual's needs (physical, emotional, social) may not identify vulnerabilities or risks for example social security administration decision acknowledging that jermaine morton has no other source of income, social security administration Acknowledging that jermaine morton has no other source of food assistance, medical assistance or insurance, no living residents, no bathing resources, no sleep or resting resources, social security administration decision acknowledged the material fact on oath and affidavit. Jermaine Morton is concerned a human being having a mortal body, which has a Brain's Dependence: The brain cannot operate without glucose, as it's the primary fuel source for brain cells (neurons) and the production of neurotransmitters. Glucose and Brain Function: Brain functions like thinking, memory, and learning are directly linked to glucose levels and the brain's ability to use it efficiently This can lead to a failure to connect them with appropriate support services or interventions for Jermaine Morton's survival 2. Lack of Proper contacting Planning and Follow-Through: Consequences of Low Glucose: If the brain doesn't receive enough glucose, it can lead to a variety of problems, including impaired cognitive function, poor attention, and difficulty with communication between neurons A social security agent case manager who doesn't develop a comprehensive plan or follow through on commitments may fail to ensure the individual receives the necessary support. This could result in a lack of supervision, inadequate care, or neglect of JERMAINE MORTON that is a homeless black man disabile adult that was denied opportunities for assistance from SOCIAL security administration has not given JERMAINE MORTON no referral No Inadequate Connections to any other agencies or Resources: A social security agent case manager who doesn't connect individuals with appropriate resources (e.g., housing, food, medical care) may leave them vulnerable to neglect. This could include failing to provide referrals, advocate for their needs, or ensure they receive necessary support. Social security administration by decision-making believe that they shall not be held to an accountability laws or punishment against neglect foreknowning the impact our decision may effect jermaine morton benefits for survival or mental or physical health give or take the maximum survival time for the entire body, having no financial support assistance jermaine morton's brain cellular process neurologic of the brain's may be effected by an hypothalamus process known as autophagy (literally self-eating.) 4. Lack of Proper Documentation and Communication: A case manager who doesn't adequately document their interactions or communicate effectively with other professionals social security agent case manager may create gaps in care. Social Security case managers are accountable for a variety of responsibilities, including documenting case management activities, ensuring timely referrals, and working with clients to achieve their goals. Accountability extends to following rules of conduct, avoiding delays in claim processing, and ensuring client confidentiality. The Social Security Administration (SSA) also has internal systems and processes to ensure accountability for improper payments and fraud prevention. Elaboration: Documentation: Case managers must meticulously document their interactions and actions with clients, ensuring all case management activities are recorded in a timely manner, according to NASW. Referrals: Case managers are accountable for ensuring clients receive appropriate referrals to other agencies or resources, such as food banks or other organizations that can address specific needs. Client Goals: Case managers work collaboratively with clients to develop and achieve personalized goals, often involving a mix of counseling, support, and guidance. Rules of Conduct: Case managers are subject to rules of conduct that prohibit threatening, coercing, or misleading clients, as well as other actions that could compromise the integrity of the process. Claim Processing: Case managers should avoid actions that would unreasonably delay the processing of claims or cause them to be delayed without a legitimate reason. Client Confidentiality: Case managers must protect the confidentiality of client information and avoid disclosing it without proper consent. Internal Systems: The SSA has implemented systems, such as the Unified Measurement System/Managerial Cost Accountability System (SUMS/MCAS), to track and manage costs and resources, ensuring accountability for financial matters Social Security crimes committed by agents include misusing benefits intended for others, working under another person's Social Security number, and filing claims using a false name or SSN. Additionally, it can involve providing false information on benefits claims, concealing facts affecting eligibility, and mismanaging a beneficiary's funds. Here's a more detailed breakdown: Misusing benefits (by a representative payee): A representative payee is someone assigned to handle financial affairs for a benefits recipient. They can misuse the funds by spending them on personal expenses instead of the beneficiary's needs. Working under someone else's Social Security number (SSN): This involves using another person's SSN to get a job or work for wages, potentially impacting the real owner's benefits and tax record. Filing claims under another person's SSN: This includes using another person's SSN to apply for Social Security benefits, which is a form of identity theft and fraud. Providing false information on benefits claims: This involves intentionally misrepresenting facts or omitting information to qualify for or increase benefits. Concealing facts or events that affect eligibility: This includes hiding information that could disqualify a person from receiving benefits or reduce their benefit amount. Mismanaging a beneficiary's funds: This can involve a representative payee failing to properly manage funds, spending them inappropriately, or failing to account for them. Making false statements on claims: This includes making false or misleading statements in application forms, or providing false information during investigations social security administration records claims Jermaine Morton history involuntary psychiatric hospitalization Year 1991~1992 concurrent 30days at Coney Island Brooklyn New York City hospital concurrent 1~year and 5 months at South Beach state psychiatric hospital Year 1994~1996 concurrent Jermaine Morton involuntary psychiatric hospitalization Kings county hospital Brooklyn New York for 2 years concurrent and 6 months Year 1997 Jermaine Morton involuntary psychiatric hospitalization Coney Island Brooklyn New York City hospital served 30days Year 2000~2003 concurrent Jermaine Morton involuntary psychiatric hospitalization to lower Manhattan New York City hospital transfer to wards Island 10035 New York state hospitals stair program 6th floor b dorm Year 2003 Jermaine Morton involuntary psychiatric hospitalization presbyterian hospital transfer to state hospital outside of new york city area to Connecticut state hospital stay 6 months Year 2004 Jermaine Morton involuntary psychiatric hospitalization to Bronx hospital 6 months Year 2005 Jermaine Morton involuntary psychiatric hospitalization to Wards Island state hospital 4floor Mira 4 b 8 months Year 2005 Jermaine Morton involuntary psychiatric hospitalization at Brooklyn New York City hospita

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FLYMORTON CHARACTERIZED AS IN WEARABLE SPIDER-MAN ELECTRODYNAMICS REPULSIVE EDF EMS EDS AERODYNAMIC MANNED UAV ACROBATIC EDF SOLENOID HOLD SUIT BLEND WEARABLE MAN OF STEEL ELECTRODYNAMICS REPULSIVE EDF EMS EDS MANNED UAV AERODYNAMIC SUIT DRONE WEARABLE IRON MAN ELECTRODYNAMICS REPULSIVE EDF EMS EDS MANNED UAV AERODYNAMIC SUIT DRONE WEARABLE FANTASTIC FOUR TORCH METALLIC CARBON RUBBERMAID TRANSDUCTOR TRANSDUCER ENCLOSURES MODULATED HARMONIC SONIC SPIKE STUDDED ELECTRON BEAM ENCLOSURES ELECTRODYNAMICS REPULSIVE THRUST PRESSURES LINEAR HORIZONTAL PLASMA FLAME EMITTER BIOMETRIC RANGE VECTOR FIELD IONIC ORBITAL ATMOSPHERIC ELECTROPHORESIS ELECTROMOTIVE RADIATION LEPTON ELECTRON OR ELECTRON DECAY FORCES GYROSCOPE PRECESSION ION COUNTERCLOCKWISE LIQUID ROTATION WITHIN A PARTICLE ENCLOSURES DUE TO SUBATOMIC UPWARD MOVEMENT AGAINST THE WEIGHT OF GRAVITY, ION ATOMIC DECAY SUBATOMIC RADIATION COLLISIONS FORCES COUNTERCLOCKWISE ATOMIC MASS PHASE CENTRAL SUBATOMIC AREA RESONATE ELECTROLYTE RESERVOIR ROTATION COUNTERCLOCKWISE ELECTROMOTIVE TYPE ELECTROLUX LENZ'S LAW SUBATOMIC ACTIVITY KINETIC ENERGY UPWARD FORCES ATOMIC MASS ELECTRODYNAMICS COLLISION PHASE METALLIC GAUGE ENCLOSURES PRISM RESONATE HELIUM-4 DECAY ORBITAL UPWARD KINETIC ENERGY AGAINST THE WEIGHT OF MASS METALLIC GAUGE GRAVITY ARC ORBITAL TORQUE RESONATE FORCES SUBATOMIC MASS EEG RADIATION PRESSURES UPWARD FORCE CONSTANT ENERGY WAVELENGTH PULSE PHASE AC INDUCTION LENZ'S LAW IONS FARADAY'S LAW OF INDUCTION GAUSS FARADAY'S CAGE BUOYANCY ENCLOSURES ESC AERODYNAMIC MANNED UAV FLIGHT SUIT DRONE ALL-IN-ONE POTENTIOMETRIC RANGE SYSTEM COMPONENTS LENZ'S LAW ELECTRICAL TRANSDUCTION FARADAY 'S LAW OF INDUCTION CIRCUIT MODULATED INDUCTOR DC/AC 7V PULSE PHASE EMI FILTER INDUCED CURRENT CARRYING DIAMAGNETIC COPPER WIRE BIOMETRIC RANGE ARRANGED 319,056TESLA'S COIL OF WIRE TURNS DESIGN VOLTAGE TRANSFORMER BARING MAGNETIC FLUX TYPE FERROMAGNETIC IRON COIL 319,056TURNS OF WIRE WEBER ELECTROMOTIVE (EMT) MFD (EMI)SEPARATE CIRCUIT TYPE SOLENOID BARING IRON FLUX WIRE CURRENT CARRYING COIL ELEMENT FERROMAGNETIZED TRANSDUCTOR HALL EFFECT SPLIT EDDY CURRENTS EMITTER VECTOR FIELD PHASE POLARIZED PERMANENT MAGNET REPULSIVE VECTOR FIELD ARRANGED TESLA'S MOTOR TYPE LINEARLY MAGLEV WAY ISOTROPIC RADIATION PRESSURES FORCES AGAINST SYNCHRONIZATION (EMI) IRON VECTOR FIELD MODULATED DC/AC 350V 50HZ+PULSE PHASE FERROMAGNETISM TEMPORARY MAGNETISM PULSE PHASE DC/AC EDF FARADAY'S CAGE ALUMINUM SOLID BLOCK DEFORM BIOMETRIC BACK SIDE RANGE DESIGN ELECTRICAL CIRCUIT ENCLOSURES MODULATED DC/AC 350W 50HZ/60HZ PULSE PHASE PARAMAGNETISM EMT AC PHASE VOLTAGE TRANSFORMER SEPARATE CIRCUITS PULSE PHASE AC EDF FARADAY'S CAGE ENCLOSURES DIAMAGNETIC DC/ 350V 50hz/60hz PULSE PHASE COPPER SHEET BLOCK CURRENT CARRYING SOLID METALLIC DEFORM BIOMETRIC FRONTAL RANGE STRUCTURE DESIGN CURRENT CARRYING AC PULSE PHASE CENTRAL ELECTRICAL WIRE CIRCUIT VOLTAGE TRANSFORMER EDS ESC MANNED UAV DRONE SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON

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