FLYMORTON

FLYMORTON

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FLYMORTON WEARABLE BIOMECHANICAL POWER ARMOR POWERED BIOMECHATRONIC COMMUTATIVE ORTHOPEDIC BIOMECTRIC RANGE REST BIAXIAL ARMATURE ROM STATOR MOTOR ESC MANNED UAV BRACE HUMANOID SUIT MACHINE DRONE 

Diagram drawing

METHOD OR APPROACH
COOLING MAGNET WIRE COPPER MAGNETIC LEVITATION COIL 
TRANSDUCTOR  
TWO OR ONE (DC) PHASE AUDIO WIRE METHOD (MAGNETIC REFRIGERATION) OF AWG# 24 INDUCTOR WIRE CATHODE ANODE CURRENT CARRYING TWO OR ONE PHASE WIRE JUNCTION TYPE SEEBECK EFFECTS, PELTIER EFFECTS COOLING INDUCTOR WIRE BARING
THERMOCOUPLE CURRENT CARRYING
FUNCTIONAL LIKENESSES AS AN BRUSH ROTARY THERMOCOUPLE CURRENT CARRYING
JUNCTION PHASE WIRE
 BYPASS
JUNCTION MATERIALS
SILICON BRUSH BLOCK FILAMENT BISMUTH CORE STAINLESS STEEL BARING MAGNET COPPER AUDIO WIRING ACTION CURRENT CARRYING
BLOCK BRUSH GENERATOR CHARGE
JUNCTION BYPASS TYPE
ROTARY SHAPE SPHERICAL MATERIAL
 SILICON CORE CONTAINS BISMUTH FILAMENT
BARING STAINLESS STEEL BARING COPPER COATED AUDIO WIRING CURRENT CARRYING PHASE BY 
JUNCTION BYPASS 
THERMOCOUPLE
 CURRENT CARRYING
MATERIALS
SILICON BRUSH BLOCK BISMUTH FILAMENT CORE STAINLESS STEEL BARING MAGNET COPPER AUDIO WIRING ACTION CURRENT CARRYING BLOCK BRUSH. 

THERMOCOUPLE SPHERICAL ROTARY JUNCTION 
 MAGNETIC REFRIGERATION APPROACH
SOLENOID PULL PUSH GADOLINIUM BORE
APPLICATION INTRODUCED SILICON SPHERICAL ROTARY REACTOR TYPE THERMOELECTRIC EFFECT REFRIGERATION SEEBECK EFFECTS PELTIER EFFECTS COOLING
JUNCTION SILICON BRUSH BARING STAINLESS STEELS SUBZERO TEMPERATURE to -269°C (-452°F . SYNCHRONOUS AC CHARGED VOLTAGE TRANSFORMER TRANSDUCTOR 
DIAMAGNETIC REPULSIVE ACTUATOR SELF SUSPENSION SELF LEVITATION ANTI-GRAVITY
UAV MACHINES

Electronic (HFC) (MCE) ELECTRODYNAMICS (EMS) (EDS) DIAMAGNETIC repulsive ORTHOSIS BOOT MANACLE Suspension SELF LEVITATION engine subsystem materials are Awg 18 silicon 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 Of Eddy currents against the aluminum block exterior surfaces Watts converted into horsepower Therefore electric potential energy of 746 Watts maybe equivalent to 1 horsepower. The diamagnetic boot emits 5 kilowatts of electrical potential energy related within british mechanical horsepowers are equivalent to 6,705 horsepowers. Here's Intuitive intelligence My weight 183lbs this may not include the body armor Inertial weighs at 140lbs However this must not be excluded Let's include weight of gravity whatsoever maybe connected to the diamagnetic electrical circuit. Equivalent scale weighs at 324lbs. Problem solved by the weight of electrical solenoid circuit weight of turns. Audio wire Turns Maybe spun tightly around the diamagnetic element given weight to equal weight of mass. WHENSOEVER the phase wire received a signal to establish a charge current carrying electrical energy winding Eddy currents repulsive FORCES against the diamagnetic horn baring within the center or the coil emissions, VELOCITY, 6,382lbs repulsive weighs more than the diamagnetic element weight forces the central repulsive element away from the electrical energy winding field of VECTORING, VELOCITIES, displacing the diamagnetic element, weighs less than the electrical energy EMITTING against the weight of it's gravity, or inertial Mass potential energy speed in constant force per second displacing diamagnetic repulsive element lifted up into the air against The human users body 183lbs weight of gravitational weight, this may also include 140lbs weight or inertial mass actuated by electrical energy EMITTING. subject not limiting to additional structure potential metric range inventor Jermaine Morton design furthermore the boot SUBSYSTEM CYLINDRICAL HOLLOW LIQUID CHAMBER BARING PERMANENT MAGNET OPERATES ROTATIONING SELF COOLING PERMANENT MAGNET EMITTER MOTORIZED FLUIDS SPEED OF 40,000RPM FUNCTIONAL LIKENESSES AS AN MCE SUBSYSTEM PISTON MOTORIZED LIQUID PUMP TYPE HFC ROTARY REFRIGERANT FLUIDS EMISSIONS PARAMAGNETIC COOLER MICROWAVES. THE PERMANENT MAGNET FLUID CHAMBER BARING COPPER AUDIO WIRING SPUN TIGHTLY INTO HELIX SHAPE AROUND THE EXTERIOR OF THE HFC LIQUID REFRIGERANT COOLING CHAMBER MOUNTED ALONGSIDE UNDERNEATH THE DIAMAGNETIC BOOT FOOT MOUNT STRUCTURE. BARING ELECTRICAL AUDIO WIRING MODULATED PERMANENT MAGNETIC THERMOELECTRIC EFFECTS REFRIGERATION PURPOSE FOR ELECTRICAL WIRING HEAT DISSIPATION ENVIRONMENT 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, TYPE TRANSFORMER, ELECTROMOTIVE, SEPARATE ELECTRIC CIRCUIT, TRANSFERS 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 electric 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 CHARACTERIZED AS IN WEARABLE  BIOMECHATRONIC TITANIUM MODULATION TRANSLATED VIBRANIUM MODIFIED TRANSDUCTION LINEAR MOTOR ARRANGED DELIBERATELY  ELECTRODYNAMICS REPULSIVE DIAMAGNETIC SUSPENSION SOLENOID TYPE DIAMAGNETIC ORTHOSIS BIOMETRIC RANGE MANACLE REST ENCLOSURES ARE MODULATED MICRO MINIATURE MOTOR VIBRATOR DC TWO PHASE WIRE VIBRATES PIEZOELECTRIC EFFECT PYROELECTRIC EFFECTIVE ENERGY CRYSTAL CELL CHARGE AWG#24 INDUCTOR TYPE VOLTAGE TRANSFORMER (DC) OUTPUT PHASE WIRING AC SYNCHRONOUS WIRELESS OR WIRED POWER TRANSFER TYPE TRANSDUCTOR SPUN TIGHTLY HELIX SHAPED WIRING PHASE CATHODE OR ANODE SEPARATELY CONNECTIONS TO 3V LITHIUM CELL BUTTON COIN BATTERY SERIES CURRENT CARRYING PHASE WIRE CONNECTIONS TO (DC) ULTRA CAPACITIVE FOIL SCROLLED SEPARATED BY WAX SHEET PAPER FLATTENED AND DEFORMED SHAPED ONE HALF OF AN OCTAGON RECTANGLE CUT SCROLL ENDS ARRANGED DELIBERATELY STACKED ALONGSIDE THE TITANIUM SHEET METAL  SEPARATED BY HIGH TEMPERATURE PLASTIC COUPLE TO TITANIUM PERMANENTLY MOUNTED TO THE TITANIUM FRAME ALONGSIDE METRIC RANGE. TITANIUM MODIFICATION ARE AN ELECTRIC CIRCUIT FUNCTIONAL LIKENESSES AS AN ELECTROMAGNETICS TYPE TRANSDUCTOR LINEAR MOTOR EMITTING A TRAVELING ELECTROMAGNETIC FIELD, AS AN ELECTRODYNAMICS WIRELESS POWER CHARGE INDUCTOR WITHIN THE DIAMAGNETIC COCKPIT BEFORE IT'S INTERIOR CORE. DIAMAGNETIC REPULSIVE FORCES TRANSMITTED BY THE BIOMETRIC SHAPED TRANSDUCTOR TITANIUM EMISSIONS AGAINST THE DIAMAGNETIC ALUMINUM BLOCK BARING INDUCTOR COILS SPUN TIGHTLY AROUND THE DIAMAGNETIC MECHANICAL ORTHOSIS EXSOFRAME REPULSIVE EMISSIONS  AGAINST THE DIAMAGNETIC BIOMETRIC ORTHOSIS EXSOFRAME EXTERIOR SIMULTANEOUSLY THE SUBSYSTEM BELOW DIAMAGNETIC EXSOFRAME BARING TRANSDUCTOR LINEAR MOTOR TRAVELING REPULSIVE DIAMAGNETIC ACTUATOR DEFINES AS MOVER FOR MOVEMENT REPULSIVE FORCES LEVITATION AS TO FLY SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE MODULATED ULTRASONIC OSCILLATING ELECTRICAL ENERGY GENERATING  AC/DC PIEZOELECTRIC EFFECT DEFORMATION LEVER HIGH VOLTAGE BALLISTIC PROOF DEFLECTION DC non-magnetic energy CHARGE parallel projectile electrocution ENCLOSURES

FLYMORTON CHARACTERIZED AS IN WEARABLE BIOMECHATRONIC TITANIUM MODULATION TRANSLATED VIBRANIUM MODIFIED TRANSDUCTION LINEAR MOTOR ARRANGED DELIBERATELY ELECTRODYNAMICS REPULSIVE DIAMAGNETIC SUSPENSION SOLENOID TYPE DIAMAGNETIC ORTHOSIS BIOMETRIC RANGE MANACLE REST ENCLOSURES ARE MODULATED MICRO MINIATURE MOTOR VIBRATOR DC TWO PHASE WIRE VIBRATES PIEZOELECTRIC EFFECT PYROELECTRIC EFFECTIVE ENERGY CRYSTAL CELL CHARGE AWG#24 INDUCTOR TYPE VOLTAGE TRANSFORMER (DC) OUTPUT PHASE WIRING AC SYNCHRONOUS WIRELESS OR WIRED POWER TRANSFER TYPE TRANSDUCTOR SPUN TIGHTLY HELIX SHAPED WIRING PHASE CATHODE OR ANODE SEPARATELY CONNECTIONS TO 3V LITHIUM CELL BUTTON COIN BATTERY SERIES CURRENT CARRYING PHASE WIRE CONNECTIONS TO (DC) ULTRA CAPACITIVE FOIL SCROLLED SEPARATED BY WAX SHEET PAPER FLATTENED AND DEFORMED SHAPED ONE HALF OF AN OCTAGON RECTANGLE CUT SCROLL ENDS ARRANGED DELIBERATELY STACKED ALONGSIDE THE TITANIUM SHEET METAL SEPARATED BY HIGH TEMPERATURE PLASTIC COUPLE TO TITANIUM PERMANENTLY MOUNTED TO THE TITANIUM FRAME ALONGSIDE METRIC RANGE. TITANIUM MODIFICATION ARE AN ELECTRIC CIRCUIT FUNCTIONAL LIKENESSES AS AN ELECTROMAGNETICS TYPE TRANSDUCTOR LINEAR MOTOR EMITTING A TRAVELING ELECTROMAGNETIC FIELD, AS AN ELECTRODYNAMICS WIRELESS POWER CHARGE INDUCTOR WITHIN THE DIAMAGNETIC COCKPIT BEFORE IT'S INTERIOR CORE. DIAMAGNETIC REPULSIVE FORCES TRANSMITTED BY THE BIOMETRIC SHAPED TRANSDUCTOR TITANIUM EMISSIONS AGAINST THE DIAMAGNETIC ALUMINUM BLOCK BARING INDUCTOR COILS SPUN TIGHTLY AROUND THE DIAMAGNETIC MECHANICAL ORTHOSIS EXSOFRAME REPULSIVE EMISSIONS AGAINST THE DIAMAGNETIC BIOMETRIC ORTHOSIS EXSOFRAME EXTERIOR SIMULTANEOUSLY THE SUBSYSTEM BELOW DIAMAGNETIC EXSOFRAME BARING TRANSDUCTOR LINEAR MOTOR TRAVELING REPULSIVE DIAMAGNETIC ACTUATOR DEFINES AS MOVER FOR MOVEMENT REPULSIVE FORCES LEVITATION AS TO FLY SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE MODULATED ULTRASONIC OSCILLATING ELECTRICAL ENERGY GENERATING AC/DC PIEZOELECTRIC EFFECT DEFORMATION LEVER HIGH VOLTAGE BALLISTIC PROOF DEFLECTION DC non-magnetic energy CHARGE parallel projectile electrocution ENCLOSURES

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