FLYMORTON HYPERSONIC DETONANTION ENGINE

FLYMORTON CHARACTERIZED AS IN WEARABLE BIOMETRIC BIOMECHANICAL ACOUSTIC PERCUSSION BALLISTIC COMMULATOR BIOFRINGENT SOLENOID HYPERSONIC ORTHOPEDIC FULL BODY BRACE HALL EFFECT SOLENOID HOLD SENSORY POWERED REST BODY ARMOR BIAXIAL STEPPER ARMATURE EXOSKELETRONIC COMMULATOR MANNED HUMANOID BIOMEDIC AUTO RESIZER SELF CONFIGURATING ADDITIONAL STRUCTURE TRANSFORMER SELF BALANCING SELF RECHARGED HUMAN BODY ARMOR ENCLOSURES HUMAN RESIDENT MODIFIER COCKPIT CORE MANNED UAV COGNITIVE SUIT MACHINE

Theoretically.

Hand-held Electromagnetics hypersonic solenoid (HSDE) thrusters

The FLYMORTON CHARACTERIZED AS IN WEARABLE: biomechanical biometric biofringent exsoskeletronic motorized biaxial robotic orthopedic hand orthotic palma also-membraine metalliod commulator silicon pyro-graphene mixed metalliod palma Peltier effect electromagnet hall effect rotary commulator armature operates pneumatic cylinder gas laser autoignition hypersonic combustion detonation bomb compressor chamber thermal protection shaft thermoelectric effect photovoltaic coil modified Peltier effect exerts throughout the thermelectric effect refrigeration engine coil pipeline towards within gauntlet exerts throughout the second solenoid combustion chamber with increased thermo energy forces throughout the commulator palma motorized pneumatic rotary mechanism detonation forces torques and exerts thrust throughout metalliod percussion wheel blower blades from the hypersonic modified modulated open clearance metalliod harmonic antimatter thermal protection chamber thruster baring a center diode cylinder laser gas ignition bomb bleeder core.

Fuel energy

122milliliters 4.125 Fluid Ounces÷5=hydrogen liquid 0.825ml) aluminum powder 0.825mg)2coal powder 0.825mg) 2sodium alloy powder 0.825mg) 2potassium powder alloy (0.825mg) 2coal powder 0.825mg

Fuel thermal energy

Liquid Hydrogen energy fuel spontaneous autoignition is 500 °C (932 °F). 2/coal 0.825mg autoignition temperature above 450–650°C)2/aluminum themite powder oxide 0.825mg autoignition lower than 655 ° C (1215 ° F); 2425 ° C (4400 ° F)2Melting Point: 1,132° C (2,070° F) burns at temperatures above 2,200C), 2Sodium Oxide Powder autoignition 1,950° C (3,542°F) Potassium 63ºC

Split Ultrasonic mechanical oscillation solenoid piston autoignition detonation compressor combustable bomb bleeder engine method

Reciprocating 78.23400 times per second range within 0.106mm cylinder shaft length distance 4inch sonic modulated solenoid push solid mixed fuel energy compressor,

Compound solid metalliod chamber structure;

Silicon metalliod, 2sodium tungsten, 2(325)iron, 2(100)iron, 2cobolt magnet, 2yellow phosphorus, 2graphene,2 quartz crystalliod,

Thermal energy compound metalliod modulation engine structure operates;

Thermal energy-voltage booster-modulated-thermoelectric effect-voltage booster-electromagnetic hall effect shaft (EE) metalliod bond (MFD) voltage booster modulated shaft radiation energy method Magneto caloric effect-modulated-voltage booster-harmonic sonic solenoid compressor-modulated metalliod piston high voltage emitter head modulated ultrasonic transducer horn piston metalliod baring electron beam welding functional likenesses as in metalliod plunger having been thermoelectric effect cylinder piston head bleeder within the metalliod Pneumatic liquid energy fuel cell autoignition metalliod chamber fire detonation compressor combustible bomb cylinder chamber thermal energy thermoelectric effect refrigeration metalliod Peltier effect modulated impeller vacuum cylinder shaft cool exchanger liquid heating chamber parallel liquid tube vacuum rotary pump cylinder combustible bomb liquid energy fuel bleeder wearable hand-held thruster

Wearable (HSDE) Boot thrusters

Hydrogen2 2Aluminum 2,coal 2sodium, 2potassium
7000gr In one pound 42gr individual mach1 compressor velocity (4665 (ft / s) * (1422 (m / s)) =2 021 930.42 m2 / s2 *(mph) =
903 883.777 m3 / s3 *(joule)=2 021 930.42 m4 kg / s4 *(mm)=2 021.93042 m3 / s2* (mach 1) =693 522 135 m3 / s3hp) =1.50775326 × 109 m4 kg / s5 (Speeds velocity density constant discharge vertical however the electromagnetic solenoid engine hypersonic speeds are 10 to 25 Mach, 7,673 -19,183 mph, 12,348-30,870 km/h and 3,430-8,575 m/s Vertical dispatching thrusts. The body armor functional likenesses as an tractor beam transducer air horn body armor electromagnetic hypersonic vibrating body armor. 3d fraction of an area or area of fraction body armor enclosures are Electromagnetic cryonic metalliod Phosphores yellow crystalline enclosures Produces intense radiation full body armor cloaking mode.

FLYMORTON WEARABLE HYPERSONIC DETONATION ENGINE

$Moving consumable thermal solid liquid tin melt flow along with electrolytes liquid method magneto hydro caloric thermal dynamics. The shaft is powered by electrical energy charge non-comsumble electrode rail linear actuator liquid metal guide vacuum dispatch shaft. The AC charge shaft WHEREAS - CHARGE the thermal solid liquid metal principal The thermoelectric effect is the direct conversion of temperature differences to electric voltage and vice versa via a thermocouple.At the atomic scale, an applied temperature gradient causes charge carriers in the material to diffuse from the hot side to the cold side. The Gauntlet and Boot Pulse Detonation Engine (PDE) is an propulsive device that uses supersonic detonation waves as a combustion mechanism.Thrust exerts the wheel blower above 2,500 feet per second (above 1,700 mph) after hydrogen exerts autoignition with a temperature of around 1800 K (1500 °C electron beam piston compressor chamber with spontaneous Sonic's (speeds of sound) ignition in air, is 500 °C (932 °F). Air and hydrogen exerts speeds of sound at (1270 mph) of the elastic properties of hydrogen, contrary of the density that is less than that of air. While hydrogen exerts coil heat exchanger cool flame having maximal temperature below about 400 °C (752 °F). It is produced in a chemical reaction of the environment Peltier effect cooler thermoelectric refrigeration modulation combustion shaft Sound travels (about 4 times as faster in air. sonic velocity of sound speeds in that hydrogen fluid (a gas/vapor). maximum forces can be achieved by the hydrogen fluid charcoal powder substrate mixed Salt powder substrate combustion boiling temperature of sodium is 881 °C ; monoxide starts evaporation at 1350 °C, a value equal to the measured flame temperature. along with Aluminum powder substrate all of which is entrusted as it's fuel source fuel source within this propulsion machine. The aluminum temperatures reaches of 1000–1800 K. The Aluminum powders in air or Coal dust suspended in air is just explosive as area per unit weight of coal, coal can produce combustion gases as hot as 2,500 °C (4,500 °F) spontaneous combustion. As a result for,PDE SONIC SPEEDS DETONATION PULSE propulsion method. The design offers numerous advantages over traditional gas turbine engines Spontaneous combustion gauge cylinder silicon metaloid mixed sodium tungsten graphite metaloid thermoprotection copper 3mm gauge 1in 1/2 open clearence magnet Piston plunger magneto caloric cooler wafer modulated Peltier effect liquid cooler magnetic coil modulated actuator linear wafer modulated ultrasonic magnetic reciprocation compressor within the liquid inductor coil cooler shaft. 0.106mm shaft length reciprocating compressor returner speeds of sound 767mm per 1 second)electron beam welding 1,000,000v sparkgap arc fire plasma 78.23400 times within 0.106mm times the speeds of sound autoignition fires1 per second within 0.106mm shaft limited distance. piston plunger magnet wafer oscillating 78.23400mm returner 1mm /per second, fire flame flashpoint detonation hydrogen vapor/gas/coal/sodium/aluminum/temperature 48,441,4190°F combustion exerts heat exchanger coil thermoelectric effect refrigeration vacuum shaft compressor cylinder harmonic sonic modulated transducer air horn resonator detonation bleeder 3mm open clearence shaft vacuum parallel wheel blower harmonic ultrasonic rotary tube modulated cool exchanger dispatching thrusts. FLYMORTON CONCERT TO PROVIDE AUTO REFUELING SYSTEM The Vacuum system tube wheel blower structure operates as an liquid generator. The tube wheel blower center core blades functional likenesses as in propane torches the maximum temperature of 3,623 degrees F, or 1,995 degrees C, while thermal suctioning vapor compression particles within a medium vacuum vapor drip chamber vapor compressor liquid accumulator chamber vacuum within a localized thermoelectric effect refrigeration Peltier effect liquid cooler modulation electrolysis chamber. The wheel blower having functional likenesses as an xlyophone acoustic percussion blades are individual heating element action vacuum blade's that incorporates the wheel blower structure the wheel blower Metalliod heating elements capable of temperatures up to 1425°C (2600°F) Individually having a diverse acoustics drum gauges for manpowered drum percussion sounding. The wheel blower having individual blade gauges C, D, E, F, G, A, B, C scales and sequence of the wheel blower blade's MODULATED harmonic sonic piezoelectric effect buzzer core transducer horn enclosures heating element modulation ultrasonic ultrasound above C-major scale's, or above 20,000 hertz is the start of the ultrasound. The wheel blower Ultrasound rotary operates with frequencies from 20 kHz up to several gigahertz. the tube wheel blower transducer horn wheel blower percussion blade's metallic thermoprotection structure modulation Intense radiation pressure compression by ultrasound waves against particles within a medium three dimensional area fraction of liquid-filled enclosures in space thermal compression improved efficiency and reduced mechanical complexity.$

The Gauntlet and Boot Hypersonic Detonation Engine (HSDE) is an propulsive device that uses supersonic detonation waves as a combustion mechanism.Thrust exerts the wheel blower above 2,500 feet per second (above 1,700 mph) after hydrogen exerts autoignition with a temperature of around 1800 K (1500 °C electron beam piston compressor chamber with spontaneous Sonic's (speeds of sound) ignition in air, is 500 °C (932 °F). Air and hydrogen exerts speeds of sound at (1270 mph) of the elastic properties of hydrogen, contrary of the density that is less than that of air. While hydrogen exerts coil heat exchanger cool flame having maximal temperature below about 400 °C (752 °F). It is produced in a chemical reaction of the environment Peltier effect cooler thermoelectric refrigeration modulation combustion shaft Sound travels (about 4 times as faster in air. sonic velocity of sound speeds in that hydrogen fluid (a gas/vapor). maximum forces can be achieved by the hydrogen fluid charcoal powder substrate mixed Salt powder substrate combustion boiling temperature of sodium is 881 °C ; monoxide starts evaporation at 1350 °C, a value equal to the measured flame temperature. along with Aluminum powder substrate all of which is entrusted as it's fuel source fuel source within this propulsion machine. The aluminum temperatures reaches of 1000–1800 K. The Aluminum powders in air or Coal dust suspended in air is just explosive as area per unit weight of coal, coal can produce combustion gases as hot as 2,500 °C (4,500 °F) spontaneous combustion. As a result for,PDE SONIC SPEEDS DETONATION PULSE propulsion method. The design offers numerous advantages over traditional gas turbine engines

Spontaneous combustion

gauge cylinder silicon metaloid mixed sodium tungsten graphite metaloid thermoprotection copper 3mm gauge 1in 1/2 open clearence magnet Piston plunger magneto caloric cooler wafer modulated Peltier effect liquid cooler magnetic coil modulated actuator linear wafer modulated ultrasonic magnetic reciprocation compressor within the liquid inductor coil cooler shaft.

0.106mm shaft length reciprocating compressor returner speeds of sound 767mm per 1 second)electron beam welding 1,000,000v sparkgap arc fire plasma 78.23400 times within 0.106mm times the speeds of sound autoignition fires1 per second within 0.106mm shaft limited distance. piston plunger magnet wafer oscillating 78.23400mm returner 1mm /per second, fire flame flashpoint detonation hydrogen vapor/gas/coal/sodium/aluminum/temperature 48,441,4190°F combustion exerts heat exchanger coil thermoelectric effect refrigeration vacuum shaft compressor cylinder harmonic sonic modulated transducer air horn resonator detonation bleeder 3mm open clearence shaft vacuum parallel wheel blower harmonic ultrasonic rotary tube modulated cool exchanger dispatching thrusts.

FLYMORTON CONCERT TO PROVIDE AUTO REFUELING SYSTEM

The Vacuum system tube wheel blower structure operates as an liquid generator. The tube wheel blower center core blades functional likenesses as in propane torches the maximum temperature of 3,623 degrees F, or 1,995 degrees C, while thermal suctioning vapor compression particles within a medium vacuum vapor drip chamber vapor compressor liquid accumulator chamber vacuum within a localized thermoelectric effect refrigeration Peltier effect liquid cooler modulation electrolysis chamber. The wheel blower having functional likenesses as an xlyophone acoustic percussion blades are individual heating element action vacuum blade's that incorporates the wheel blower structure the wheel blower Metalliod heating elements capable of temperatures up to 1425°C (2600°F) Individually having a diverse acoustics drum gauges for manpowered drum percussion sounding. The wheel blower having individual blade gauges C, D, E, F, G, A, B, C scales and sequence of the wheel blower blade's MODULATED harmonic sonic piezoelectric effect buzzer core transducer horn enclosures heating element modulation ultrasonic ultrasound above C-major scale's, or above 20,000 hertz is the start of the ultrasound. The wheel blower Ultrasound rotary operates with frequencies from 20 kHz up to several gigahertz. the tube wheel blower transducer horn wheel blower percussion blade's metallic thermoprotection structure modulation Intense radiation pressure compression by ultrasound waves against particles within a medium three dimensional area fraction of liquid-filled enclosures in space thermal compression improved efficiency and reduced mechanical complexity, subject not limiting to additional system or structure

FLYMORTON WEARABLE BIOMECHANICAL CYLINDRICAL PYROELECTRIC EFFECT BIOMETRIC RANGE XYLOPHONE PERCUSSION VIBERPHONE BODY ARMOR EXOSKELETRONIC MANNED UAV ATMOSPHERICAL FUEL ENERGY RAILGUN ENGINE ROCKET PROPELLANT BODY ARMOR ORTHOSIS BIOMETRIC RANGE SOLENOID PUSH PULL BRACE PIEZOELECTRIC EFFECT ULTRASONIC LEEGGED STACKED DRAWER GUIDE ADDITIONAL COMMUTATOR BODY ARMOR BODY ARMOR STRUCTURE CAGE MULTI STATOR BIAXIAL ROTOR MAGNET ARMATURE ROM propeller BRACE FLIGHT SUIT MACHINE BODY ARMOR materials are METALLOID STRUCTURE YTTRIUM GADOLINIUM PYRO BISMUTH INDUCTOR TITANIUM PERCUSSION BODY ARMOR ATMOSPHERICAL WATER COMPRESSOR ELECTROLYSIS ELECTROPHORESIS CATHODE AC CHARGE RAIL ENGINE ROCKET POWER THRUSTER MANNED UAV ORTHOSIS BIOMETRIC RANGE BIAXIAL OR ROM BRACE FLIGHT SUIT MACHINE BODY ARMOR Secondary propulsion engine materials PVC spools TUBULAR ENGINE AC 5 MEGAJOULES SONIC MACH 2 &UP AUTOMATIC RECHARGED SUPER CAPACITOR RAIL ACOUSTOPHORESIS CHAMBER MAGNETO HYDROCALORIC THERMODYNAMICS THERMOELECTRIC EFFECTS Photovoltic chamber reaction SEEBECK Effects PELTIER EFFECTS COOLER OXIDATION COOLER THERMALDYNAMICS MODULATED BY ACOUSTIC RADIATION FORCES ATMOSPHERICAL COLLISION WITHIN THE RAIL LIQUID SOLID ICE PELLET TRAJECTORY CHAMBER SOLENOID PUSH PULL SENSORY LEED SPOOL TUBING FILLED COMPOUNDS ARE CHARCOAL, POTASSIUM NITRATE, ALUMINUM POWDER, AND SULFUR. Mechatronics STEPPER MOTOR LEED LONG LENGTH SPOOL TUBING ENGINE SPECIFICATIONS: ARTERIAL PVC MATERIAL, FLEXIBLE, PVC VINYL TUBING, MOTOR DIAMETER: 3/4", OD: 4/5", TUBULAR LENGTH 200.8 FEET, WALL THICKNESS: 1mm; Hardness: 73A (firm); TEMPERATURE RANGE : 23°F to 149°F (-5°C to 65°C); WORKING PRESSURE: 2500PSI+ TOTAL IMPULSE: 1100.8 N-sec BURN TIME: UNLIMITED THRUST: 2300 newtons+ Mechatronic oxidation processor: Delay Time: 3 seconds Propellant Weight: Motor Weight: Maximum Liftoff Weight: 1200Newtons (N)404.656 Pounds force (lb)1 N = 0.224809 lb1 lb = 4.448220 N Mechatronics oxidizer processor: transducer horn sonic oscillating intense radiation pressure micro cooler longitude wave vector Force temperature exchanger environment alongside transduce sonic oscillating intense micro heating longitude wave vector radiation pressures forces environment differential temperature exchanger, Subject not limiting to additional system or structure

FLYMORTON CHARACTERIZED AS IN WEARABLE DC BIOMECHATRONIC POWER ELECTROMAGNETIC BODY ARMOR INDUCTOR SYNCHRONOUS AC ELECTRICAL ENERGY CAPACITOR POWERED BODY ARMOR TYPE SOLENOID PULL PUSH DRAWER GUIDE ADDITIONAL PERMANENT MAGNET BODY ARMOR STRUCTURE ORTHOSIS BIOMETRIC RANGE NOT LIMITING TO ADDITIONAL STRUCTURE

Thermal PHOTONIC Photovoltic Thermal electric effect refrigeration sphere coefficient or violent isotopes SEEBECK effect PELTIER EFFECT COOLER sphere elements are silicon powder 2YTTRIUM powder 2NEODYMIUM powder 2siliver powder 2Strontium aluminate powder 2pyro 2gadolinium powder all of which are thermal mold formed shaped spherical type Crystalloid embedded within the cylindrical chamber operates combustible compression choke within the dispatch chamber functional likenesses as an pneumatics spherical rotary nozzle sprayer thrust increase compressed detonation vacuum chamber rotary pneumatic bomb Crank powered blower wheel rotary handwear solenoid pull push drawer engine electron capacitor armor guide high voltage capacitor RAILGUN SET CHAMBER ELECTRON BEAM WIGGLE THERMAL PHOTONIC BEAM PHASES CRYSTALLOID SPHERE THERMOELECTRIC ATMOSPHERICAL PARTICLE ACCUMULATION HIGH & LOW TEMPERATURE CYLINDRICAL CHAMBER OXIDATION BETWEEN HIGH VOLTAGE AC CHARGE RAIL CHAMBER OPERATES CALORICDYNAMICS THERMODYNAMICS MAGNETO HYDRO CALORIC THERMODYNAMICS

BIOMECHATRONIC electronic ELECTROPHORESIS engine microfluid polyamide hydro electrolyte ELECTROPHORESIS multiple channel chip MODIFIED modulated photovoltic magneto dynamics hertz sensory 1H (protium), 2H (deuterium), and 3H (tritium) nuclei energy fuel collector

Embedded within the powered body armor operates harmonisonic PELTIER effect radiation pressures cooler particle Freezing point lower than 1526 °C YTTRIUM SEEBECK effect solid environment enclosing the Copper tubing bearing ceramic piezoelectric buzzers modulated harmonic Sonic deformation intense radiation pressure forces against matter atmospherical liquid generator within the cylindrical chamber Cathode Anode high voltage charged harmonic sonic synchronous AC 5 megajoules rail chamber separated connections to the below series of harmonisonic transducer horn exterior cylindrical scramjet rotary gas sampler bomb bleeder embeddings within the separate segments of the body armor ion rocket biomechatronic solenoid push-pull body armor electromagnetic hold suit manned UAV suit machine system.

DIAMAGNETIC HIGH VOLTAGE CHARGE THERMAL REACTIVE CRYOGENIC METALLOID DIAMAGNETISM LIQUID MESH PUTTY 60%/40% METALLOID MESH ROTATING WITHIN HOLLOW QUARTZ ENERGY CRYSTAL CELL ROTARY HYPER ELECTROCHEMICAL CYCLING (EEG) NEWTRON ACCELERATOR STEP-UP ELECTROMAGNETISM JOULES INFINITE VOLTAGE BOOSTER INNOVATIVE SELF REPULSION HUMAN USER ACTUATOR ANTIGRAVITY ALUMINUM ALLOYS DEFORMED BIOMETRIC HAND SIDE PALMA RANGE STRUCTURE PARAMAGNETISM DIAMAGNETISM REPULSION VERTICAL ACTUATOR PYROELECTRIC EFFECT SODIUM TUNGSTATE (PI)(PO)DENSITY ENERGY CRYSTAL CELL CRYSTALLOID HOUSING DIAMAGNETIC THERMOELECTRIC EFFECTS REFRIGERATION THERMAL REACTIVE GLOW ELECTROCHEMICAL ELECTRON CAPACITIVE MESH NON-NEWTONIAN LIQUID VISCOSITY PUTTY FILAMENT (EEG) NEWTRON VORTEX ENERGY POWER TORQUE ION CRYSTALLOID GENERATOR ESCAPE ALUMINUM ALLOY METALLOID WEARABLE MOTOR MANNED UAV BODY ARMOR ELECTRODYNAMICS SELF REPULSIVE AWAY ENGINE REPELLENT VERTICALLY AWAY INVENTOR JERMAINE MORTON SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN FLYMORTON WEARABLE BIOMECHATRONIC SELF-(EEG) SELF-REPULSIVE FORCE AWAY-PHASE SELF-EMITTING METALLOID PYROTECHNIC (EEG)(EMF)(NPL) DOPPLER EFFECT BODY ARMOR SUIT MACHINE SELF- REPULSIVE SOLENOID PULL PUSH SENSORY SECTIONAL METALLIC BOND SYNCHRONOUS CHARGE METALLOID MAGNETIC REFRIGERATION NEWTON ENERGY ACCELERATOR SEEBECK EFFECT FEEDBACK CRYSTAL ENERGY CELL METALLOID CORE HYPERSONIC OSCILLATING ENERGY POWER GENERATOR ELECTRODYNAMICS DIAMAGNETIC REPULSIVE SELF ACOUSTOPHORESIS TRANSDUCTOR SELF LEVITATION AS TO FLY SELF-REPULSIVE (EMS) BODY ARMOR TRANSDUCTIVE THERMAL ELECTROMAGNETIC CONDENSATION MOISTURE LIQUID GENERATING THERMAL DYNAMICS POWER AIR BREATHING COOLER MAGNETIZED PYROTECHNIC GADOLINIUM CRYSTALLOID METALLOID BODY ARMOR MAGNETIC REFRIGERATION LOW TEMPERATURE PARAMAGNETIC AIR COMPRESSOR COMBUSTIBLE BOMB SAMPLER TRANSDUCER HORN BODY ARMOR BLEEDER ELECTROPHORESIS RADIATION PRESSURES MATTER BETWEEN THE MEDIUM RISE TRACTOR BEAM PHASE-(EDS) THREE DIMENSIONAL AREA OF FRACTION PROXIMITY FIELD SOLENOID HOLD SENSORY (UAV) BIOMECHATRONIC ORTHOTIC BIOMETRIC RANGE BIONIC DRONE STACKED LOW GAUGE METALLOID SHEET DEFORMED PENTAGON DESIGN FUNCTIONAL LIKENESSES AS AN COMMUTATOR MODIFIED PIEZOELECTRIC EFFECT METALLOID THERMOCOUPLE BEHAVIOR THERMOELECTRIC EFFECT PYROELECTRIC EFFECT HOLLOW OPEN CLEARANCE METALLOID PYROELECTRICITY CHARGE CAPACITOR OUTPUT SINGLE PHASE RECTIFIER FEEDBACK ENERGY POWER METALLOID SEEBECK EFFECTS CRYSTALLOID ENERGY CYCLOTRON HOLLOW OPEN CLEARANCE CAGE BALL BARING BRACKET ARMATURE PERMANENT MAGNET BLADED SYNCHRONOUS ROTOR HOLLOW CYLINDRICAL OPEN CLEARANCE ROTOR CENTRAL CORE CAGE TELESCOPIC SOLENOID SENSORY AC SYNCHRONOUS ENERGY CRYSTALLOID HYPER SONIC OSCILLATOR MAGNETRONIC PIEZOELECTRIC EFFECT GADOLINIUM BORE METALLIC BOND (MFD) ELECTROMAGNETIC PERMANENT MAGNETIC REFRIGERATION CHARGE CURRENT CARRYING ELECTRICAL ENERGY STEP-UP VOLTAGE TRANSDUCTOR ENERGY POWER ELECTROMAGNETISM ELECTRON CAPACITIVE ENERGY ACCELERATOR DIAMAGNETISM AMPLIFIER SELF REPULSIVE WEARABLE BIONIC BIOMECHATRONIC ALUMINUM ORTHOTIC HAND SIDE PALMER MOTORIZED SELF REPULSIVE FORCES SELF AWAY ION THRUSTER subject not limiting to additional system or structure potentiometric range inventor Jermaine Morton FLYMORTON WEARABLE ALUMINUM ORTHOSIS HAND SIDE PALMA BRACE LUMINESCENT QUARTZ ENERGY CRYSTAL CELL SPHERE ROTARY (EDS) ELECTROCHEMICAL POWER CRANK CATHODE BLADE CHARGE ELECTROCHEMICAL ELECTROMAGNETIC MESH TYPE (PIEZOELECTRIC EFFECTIVE) LUMINESCENT QUARTZ ENERGY CRYSTAL CELL (THERMAL MAGNETOCALORIC EFFECTS QUARTZ PYROELECTRICITY) CAPACITANCE CHARGE (SILICON) LOCAL TO NEODYMIUM PERMANENT MAGNETIC FLUX SILICON DENSITY (THERMOELECTRIC EFFECTIVE REFRIGERATION) THERMOCOUPLE BISMUTH (SEEBECK EFFECTIVE) THOMPSON EFFECTIVE PELTIER EFFECTS COOLER ALUMINUM SUB-ZERO DEGREE LOW TEMPERATURE ATMOSPHERIC HOLLOW HOUSING ENVIRONMENT BARING AND ELECTRICAL MOTOR CATHODE BLADE CURRENT CARRYING ELECTRICAL ALUMINUM MESH DIAMAGNETISM SPLIT CATHODE OR ANODE ELECTRON CAPACITOR POWER STORAGE (ENERGY POWER SUPPLYING ELECTROMAGNETISM CHARGED ELECTRODYNAMICS) VECTOR FIELD ALTERNATING CURRENT SYNCHRONOUS THERMAL MAGNETO CALORIC EFFECTIVE REFRIGERATION MESH AS IN MAGNETIC REFRIGERATION ( AC) SYNCHRONOUS ELECTRICAL ENERGY CHARGE MAGNETIC FLUX DENSITY THERMAL REACTIVE GLOW CRYSTAL PIEZOELECTRIC EFFECTIVE FILAMENT ELECTROCHEMICAL CONDUCTIVE LIQUID MIXED (HFC)-134A HYDROFLUOROCARBON THERMAL CYCLING HYPER HYSTERESIS MESH LOW TEMPERATURE COOLING COMPONENTS ENERGY POWER CAPACITOR SUPPLIER POWER CELL ENERGY GENERATOR PIEZOELECTRIC EFFECTIVE LUMINESCENT QUARTZ CRYSTAL CELL FILAMENT 1100BLS PULL RATE 52N NEODYMIUM MESH POWDER ALUMINUM MESH POWDER COPPER MESH POWDER SILICON MESH POWDER BISMUTH MESH POWDER QUARTZ MESH POWDER GADOLINIUM MESH POWDER LUMINESCENT GLOW ENERGY POWER PHOTOVOLTAIC CLEAR FOCAL QUARTZ ENERGY CRYSTAL CELL LIGHT EMITTING SPHERICAL ELECTROCHEMICAL ELECTROMAGNET DIAMAGNETIC REPULSIVE COMPONENTS WITHIN A HOLLOW OPEN CLEARANCE WITHIN THE ALUMINUM GAUGE DEFORMED BIOMETRIC HAND SIDE PALMER RANGE WEARABLE DEVICE CONCERTS TO PROVIDE ELECTROMOTIVE REPULSIVE FORCES AWAY ALUMINUM ACTUATOR DIAMAGNETIC REPULSION ELECTRODYNAMICS PRESSURES WITHIN VECTOR FIELD RADIATION LOW TEMPERATURE PARAMAGNETIC ENVIRONMENT BETWEEN THE HOLLOW OPEN CLEARANCE CAGE OF ALUMINUM GAUGE REPELS AWAY FROM THE VECTOR FIELD PUSHING AGAINST IT'S WEIGHT OF GRAVITY OR INERTIAL WEIGHT OF GRAVITY subject not limiting to additional system or structure potentiometric range design inventor Jermaine MortonFLYMORTON BIOMECHANICAL POWER ARMOR EXOSKELETRONIC POWERED BODY ARMOR BIOMECHATRONIC SUBSYSTEM ATMOSPHERIC COMPRESSOR AIR TRANSFER MICROFLUIDIC TELESCOPIC AIR BREATHING MICROCOSM LIQUID ENERGY FUEL ROCKET PROPELLANT ENGINE GENERATOR ACOUSTOPHORESIS ELECTROPHORESIS CHIP SET SHAPE BIOFRINGENT CYLINDRICAL MAZE TRANSDUCTION HORN WALL EXTERIOR BETWEEN BARING HELIX HEATING ELEMENT ELECTRODYNAMICS THERMALDYNAMICS OPEN CLEARANCE BARING CATHODE RAIL CENTER WITHIN THE HELIX COIL CHAMBER MICROFLUIDIC LINEAR MOTOR PIEZOELECTRIC EFFECTS CHAMBER PYROELECTRIC EFFECTS CHAMBER PELTIER EFFECTS MAZE WALL CHAMBER OPERATES ACOUSTOPHORESIS CHARGE ELECTRODYNAMICS ELECTROPHORESIS SONIC RADIATION PRESSURES COOLER ELECTROSTATIC AIR BREATHING BODY ARMOR CHAMBER PIEZOELECTRIC EFFECTS PYROELECTRIC EFFECTS THERMOELECTRIC EFFECTS PELTIER EFFECTS COOLER CYLINDRICAL TRANSDUCTION HORN BODY ARMOR EMITS COOLER ELECTROSTATIC RADIATION PRESSURES FORCES MATTER BETWEEN THE MEDIUM RISE WITHIN THE CYLINDRICAL OPEN CLEARANCE BODY ARMOR CHAMBER ELECTRODYNAMIC TYPE SOLENOID PULL PUSH MATTER ELECTROPHORESIS ACOUSTOPHORESIS TRANSDUCTOR CYLINDRICAL OPEN CLEARANCE MAZE BODY ARMOR AIR BREATHING ATMOSPHERIC ICE PELLET GENERATOR MAGNETO CALORICDYNAMICS ELECTRON CAPACITIVE ENERGY TRANSDUCTANCE BODY ARMOR 5-mega Joule 1 SECOND AC SYNCHRONOUS CAPACITOR AUTOMATIC ENERGY RECHARGE ELECTRODYNAMICS RAIL ENGINE magneto hydrochloric thermodynamics Subject not limiting to additional system or structure

CLAIM: FLYMORTON CHARACTERIZED AS IN WEARABLE BIOMECHATRONIC UAV ORTHOSIS BIOMETRIC RANGE MANACLE FLIGHT SUIT MACHINE OPERATES BY TELEKINESIS BRAIN EMISSIONS BETA WAVES CURRENT CARRYING ELECTROMOTIVE REPULSIVE FORCES LIFT, CLAIM; FLYMORTON WEARABLE FUNCTIONAL LIKENESSES AS AN ELECTROMAGNETICS, CLAIM: FLYMORTON WEARABLE BODY ARMOR DIAMAGNETIC SELF SUSPENSION SELF REPULSION AWAY IT'S LOCALIZED ALUMINUM EXTERIOR, BIOMETRIC RANGE FULL BODY ARMOR, ROBOTIC FLIGHT SUIT LEVITATION ACTUATOR. CLAIM; FLYMORTON CHARACTERIZED AS IN WEARABLE ENERGY BODY ARMOR SUBSYSTEM SUBSYSTEM USES TGAM BRAINWAVE EEG SENSOR BRAIN CONTROL ARDUINO MODULATED NEUROSKY SENSES, alpha waves: 8-13 Hz; beta waves, 18-25; theta waves: 3.5-7 Hz; delta waves: 0.5-3.5 Hz, and gamma waves: 30-70 Hz. CLAIM; FLYMORTON CHARACTERIZED AS IN WEARABLE ELECTRONIC ENGINE CONTROLS BY AN ELECTRONIC CIRCUIT AS AN EEG ELECTRICAL ENERGY GENERATOR PROGRAM. CLAIM THE FLYMORTON SUBSYSTEM BODY ARMOR MODULATION ENABLES THE SYNCHRONIZATION OF NEURAL ACTIVITY WITHIN AND ACROSS BRAIN REGIONS, CLAIM: THE USES OF THE FLYMORTON WEARABLE BIOMECHATRONIC FLIGHT SUIT SYSTEM SENSES THE HUMAN USERS BRAIN IS AROUSED AND ACTIVELY ENGAGED IN MENTAL ACTIVITIES CLAIM; THE BRAIN GENERATES BETA WAVES SENSED BY THE BODY ARMOR. CLAIM; FLYMORTON WEARABLE BODY ARMOR SENSES BETA WAVES THAT ARE of THE HUMAN USERS BRAIN RELATIVELY LOW AMPLITUDE, AND ARE THE FASTEST OF THE FOUR DIFFERENT BRAINWAVES. CLAIM; FLYMORTON WEARABLE BIOMECHATRONIC MANNED UAV ORTHOSIS BIOMETRIC RANGE MANACLE BODY ARMOR FLIGHT SUIT SENSES THE FREQUENCY OF BETA WAVES RANGES FROM 15 to 40 CYCLES A SECOND DEFINE AS 15 HERTZ to 40 HERTZ WITHIN ONE SECOND REFRESHING RATE 15 TO 40 TIMES PER SECOND, HERTZ IS A UNIT OF FREQUENCY (OF CHANGE IN STATE OR CYCLE IN A SOUND WAVE, CLAIM; FLYMORTON WEARABLE BIOMECHATRONIC SUBSYSTEM ELECTRICAL CIRCUIT PROVIDES ALTERNATING CURRENT, OR OTHER CYCLICAL WAVEFORMS) OF ONE CYCLE PER SECOND. IT REPLACES THE EARLIER TERM OF "CYCLE PER SECOND. CLAIM FLYMORTON WEARABLE HUMAN FACILITY SENSES BIOELECTRICAL WAVES THESE ELECTRICAL SIGNALS SYNCHRONOUSLY INDUCED CURRENT CARRYING MODULATION AMPLIFIED GENERATES HIGH VOLTAGE ELECTRICAL ENERGY AMPLIFIED THROUGHOUT DIRECT CURRENT CARRYING INDUCTION INDUCED CURRENTS INTO AN INDUCTOR CURRENT ARE MODULATED THROUGHOUT BYPASS CRYSTAL OSCILLATORS MODULE, CLAIM; FLYMORTON WEARABLE PIEZOELECTRIC EFFECT ACTIVE CRYSTAL OSCILLATORS ARE DIGITAL INTEGRATED CIRCUITS PROVIDING A STABLE SIGNALS AT high-frequency. CLAIM FLYMORTON WEARABLE BIOMECHATRONIC BIOMETRIC RANGE MANACLE BODY ARMOR FLIGHT SUIT MANNED UAV ORTHOSIS MACHINE SUBSYSTEM USES PASSIVE COMPONENTS WITHIN THE BODY ARMOR CHARACTERIZED AS CIRCUIT . THE CIRCUIT DON'T AFFECT THE BASIC CHARACTERISTICS OF THE INDUCED CURRENT SIGNAL, BUT ONLY PASS THE SIGNAL WITHOUT MODIFICATION AMPLIFICATION CONNECTIONS TO RESISTORS, OR CAPACITORS, INDUCTORS, OSCILLATORS, TRANSFORMERS VOLTAGE POWER UP CURRENT CARRYING RECORDED REPEATED RHYTHMIC GAMMA WAVES OSCILLATIONS. CLAIM FLYMORTON WEARABLE BIOMECHATRONIC MANNED UAV ORTHOSIS BIOMETRIC RANGE MANACLE BODY ARMOR FLIGHT SUIT MACHINE SYSTEM PROVIDES ENERGY TRANSFER, CLAIM; FLYMORTON WEARABLE BIOMECHATRONIC BODY ARMOR ENERGY TRANSFER IS BASE ON AMPLIFIED GAMMA ENERGY AMPLIFIED TO HIGHER ENERGY LEVELS WITHIN AN EXTERNAL BODY ARMOR MAGNETIC FIELD. CLAIM; FLYMORTON WEARABLE BIOMECHATRONIC BODY ARMOR ENERGY POWER TRANSFER OCCURS AT WAVELENGTH THAT COINCIDES WITH THE SAME BRAINWAVES FREQUENCY. CLAIM; FLYMORTON WEARABLE BIOMECHATRONIC TRANSDUCTOR BODY ARMOR EMITS ELECTROMAGNETIC FREQUENCY (EMF) ELECTROMOTIVE FORCE (EDS) ELECTRODYNAMICS SUSPENSION (EDS) CLAIM; FLYMORTON WEARABLE BIOMECHATRONIC SUBSYSTEM ELECTRONICS COMPONENTS, ARE ELECTRICAL CONDUCTIVE INDUCTIVE METALLIC ELEMENTS OF WIRE CIRCLES, COMPRISED FOR ENERGY WINDING WITHIN THE BODY ARMOR SUBSYSTEM STRUCTURE ELEMENTS ARE PIEZOELECTRIC EFFECTIVE, CONDUCTIVE DIAMAGNETIC ELEMENTS OPERATE ACTIVE OSCILLATING ELECTRICAL ENERGY WINDING FOR EXAMPLE 220V -240V GENERATES SIGNALS MODULATES THE INDUCED CURRENT CARRYING ELECTROMOTIVE OSCILLATIONS ENERGY POWER TRANSFER POWER UP GAMMA WAVES TRANSMITTED THROUGH TRANSDUCTOR ELECTRICAL WINDING ENERGY POWER TRANSFERS EMISSIONS ARE BETA WAVES ELECTRICAL ENERGY REPULSIVE FORCES ALUMINUM WITHIN VECTOR FIELD AWAY telekinesis is a hypothetical psychic ability allowing a person to influence a physical system without physical interaction. Human Neuro electrolytic bioelectric Alpha wave active electron oscillating rhythmic synchronous active magneto radiation pressures electrons active spin precession torque atomic energy vortex tightly accelerates electrons collisions generates neutrons kinetic force current to voltage bio-caloric rhythmic electrophoresis ion amplification vapor displacement particle collision radiation pressures forces paramagnetic synchronization of matter suspended between the medium vector field phase three dimensional area of fraction. The human body's voltage increases when the right foot rises, and its peak value is 13 V. The human body's voltage decreases and increases immediately to 7 V when the right foot is lowered. The largest human body voltage is 17 V. Brainwaves are electrical impulses in the brain. An individual's behavior, emotions, and thoughts are communicated between neurons within our brains. All brainwaves are produced by synchronised electrical pulses from masses of neurons communicating with each other. Gamma. Your brain produces the speediest of brain waves, the gamma waves, when you're actively involved in processing information and learning. You're concentrating and solving problems, and these brainwaves, which tend to measure upward of 35 Hz, 100hz OSCILLATION occurring radionuclides within our bodies. The major one that produces penetrating gamma radiation that can escape from the body is a radioactive isotope of potassium, called potassium-40. controlling their own alpha brain waves based on neurofeedback they receive as they perform a particular tasking phase-locked loop oscillating gamma wave The elements in our bodies, like sodium, potassium, calcium, and magnesium, have a specific electrical charge. Almost all of our cells operates by these charged The elements in our bodies, like sodium, potassium, calcium, and magnesium, have a specific electrical charge. Almost all of our cells can use these charged elements, called ions, to generate electricity. An electroscope initially has a net negative charge. The foils come together when the electroscope is touched by a human hand because a. humans have a net positive charge. The human Brain waves are, essentially, the evidence of electrical activity produced by your brain. When a group of neurons sends a burst of electrical pulses to another group of neurons, it creates a wave-like pattern. These waves are measured in speed cycles per second, which we describe as Hertz The elements in our bodies, like sodium, potassium, calcium, and magnesium, have a specific electrical charge. Almost all of our cells can use these charged elements, called ions, to generate electricity. The SLEIGHT magician theory CLAIM:19 FLYMORTON Bioelectric output modulation electromotive Brainwave gamma waves Power up amplification modulated by an electronic circuit Active Crystal oscillator amplifies gamma wave amphere booster bridge bus input gamma wave passive crystal oscillator output gamma wave emits ions energy produces penetrating gamma radiation induced from the human users body as alternative current radioactive rhythmic ion synchronous induce currents to an electrical conductivie element established a charge wearable electrical circuit element deformed silicone WIRE SPUN TIGHTLY HELIX SHAPED COIL structure body armor DESIGN AS AN WEARABLE ARIEL ROBOTICSType 1 https://youtu.be/Q_ocOblMrb4 https://youtu.be/0TZUyCQ2R6s Subject not limiting to additional system or structure potentiometric range inventor Jermaine Morton designArmor exhibits Induced current as voltage charge thermal reactive Piezoelectric effective copper 2 quartz powder roll conductive resin epoxy glued to the copper roll DC SINGLE PHASE RECTIFIER OUTPUT DC ACTIVE CRYSTAL OSCILLATOR OUTPUT INDUCED CURRENT CARRYING PIEZOELECTRIC EFFECTIVE TRANSDUCTOR within titanium sheet roll surfaces as an electrical circuit embedded within a ceramic stone Electrodynamics between copper sheet exhibit on one side aluminum roll several times zigzag fold individual segments of the armorHorizontal or vertical self Repulsive forces lift against the weight of gravity or inertial Mass concert to provide BIOELECTRICAL BETA WAVES ENERGY repulsive FORCES AWAY ALUMINUM WEARABLE BODY ARMOR EXTERIOR used FOR LEVITATION AS TO FLY MAGNETICALLY SAIL SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON https://youtube/6Zl07XrZbSQ

SCISSORING PIPELINE INCORPORATED MECHATRONICS ARE PIEZOELECTRIC RING SERIES ELECTROMOTIVE ULTRASONIC PYROELECTRIC EFFECT CRYSTAL ENERGY CELL (EEG) ALONGSIDE PELTIER EFFECT COOLER SHAFT MAGNETO HYDRO CALORIC DYNAMICS PLASMA BEAM JOULE UP CYLINDER SIZE STEP DOWN COMBUSTIBLE BOMB SAMPLER BLEEDER

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 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

powder/2 Raw Bismuth Metal powder/2 Yellow Citrine Quartz Inlay Sand Painting Craft Powder/2 Quartz Crystal Dust Powder/2 Smoky Quartz Crystal Dust Powder/2 Green Silicon Carbide Tumbler Powder/2 Pure Silicon Silicium Si High Purity 99.9% Metal Powder. BODY CAST OVER MODIFIED THERMOPLASTIC BIOMETRIC RANGE SUBJECT TO SOLENOID PUSH PULL COIL BARING PERMANENT MAGNETS MODULATED TRANSFORMER SEPARATE CIRCUIT ELECTROMOTIVE ULTRASONIC ACOUSTIC DRIVEN. MODIFIED BODY ARMOR TYPE TRANSDUCER HORN EXTERIOR AROUND ABOUT THE STATOR ENGINE. THE BODY CAST COMPOUND MODULATED OSCILLATOR REACTOR TYPE CURRENT CARRYING PYROELECTRICITY ELECTRICAL ENERGY GENERATOR BODY ARMOR HIGH VOLTAGE AC METALLOID BALLISTIC PROOF PROTECTION ARMOR,SEE LORENTZ PHYSICS LAW FORCE, RIGHT HAND RULE. BIOMETRIC RANGE SOLENOID TYPE BODY ARMOR PYROELECTRICITY CHARGE THERMOMAGNETIC THERMOELECTRIC EFFECT REFRIGERATION PELTIER EFFECTS COOLER METALLOID LIQUID MOISTURE ACCUMULATOR MAGNETO HYDRO CALORIC THERMAL DYNAMICS MODULATED thermal acoustic ACCELERATOR INTENSE RADIATION PRESSURE FORCES AGAINST MATTER exerts from the solid state body armor metalloid LIQUID FILLED ENCLOSURE in space WITHIN THE block SOLID STATE of armor NANO SIZE AIR POCKET oxygen environment reaction CYLINDRICAL Thermal dynamics COMBUSTIBLE ENVIRONMENT TEMPERATURE DIFFERENCES BEAMING COOLER VERSES HEATING PARTICLE COLLISIONS CAUSES MOISTURE BLEEDING THERMODYNAMICS FORCES BLEEDING OXIDATION cooler particle NEUTRON OXYGEN.EXPANSION SPEED mega Joules VELOCITY collision density accumulator micromass pellet FORCE WITHIN THE MEDIUM RISE AGAINST IT'S WEIGHT OF GRAVITY. Body armor modified HEAT RESISTANT SOLID MODULATED YELLOW PHOTOVOLTAIC DIODE IMPLANT H-BRIDGE magneto inductor bus bridge junction MODULATED light ELECTROMOTIVE wireless EEG synchronous human brainwaves RADAR distance sensory proximity switch electrical energy power generator GPS MAGNETIC BIOELECTRIC mapping microwave human bioelectric radar tractor beam wireless power transfer induction electromotive syntax variable recorded alpha frequencies script hertz communication POTASSIUM SENSORY TO BRAINWAVES SENSORY SWITCH INDUCTION SOLENOID PULL PUSH TYPE BODY ARMOR MODULATED HARMONIC DRIVE SONIC OSCILLATING PYROELECTRICITY ELECTRICAL ENERGY GENERATOR BUS BRIDGE SUPER- CAPACITOR BIOMETRIC RANGE FOIL FOLD THERMAL SOLID QUARTZ CRYSTAL RESISTANT INTERFACE AUDIO COIL BARING PERMANENT MAGNET SOLENOID PULL PUSH TYPE MODULATED ACOUSTIC SONIC DRIVEN CIRCUIT. HARMONIC SONIC SUPER CAPACITOR BIOMETRIC RANGE OSCILLATING HORN RESIDENCE SECTION REACTION TYPE AUTOMATIC RECHARGE SUPER CAPACITOR RESONATOR MODIFIED TRANSDUCER HORN OSCILLATING INTENSE DEFORMATION PYROELECTRICITY charge super capacitor ion particle energy charge metalloid magneto hydro caloric thermodynamic RADIATION PRESSURES FORCES MATTER WITHIN medium rise THRUST VECTORING levitation body armor.

https://www.flymorton.com/flymorton_super_sonic_pulse_detonantion_engine.html FLYMORTON WEARABLE MANNED UAV ANODE COMMUTATOR RESERVOIR CAGE EFB GEL CELL PHASE CHARGE COPPER SPHERE ROTARY DIAMAGNETIC REPULSION BIOMECHATRONIC AMG(STI)(EEG)(EFB) GEL CELL (EDF(EMS)ESC(EMT)EMF(EDS) MANNED UAV ORTHOSIS PALMA BIOMETRIC HAND SIDE PALMA RANGE METALLIC STACKED COMMUTATOR HORN ELECTROMAGNETIC POLARIZED CAGE ARMATURE OPERATE BIAXIAL ROM FIXATOR MOTORIZED POWER ARMOR IRON STACKED WEARABLE GAUNTLET METHOD FARADAY'S LAW MAGNETIC BLOCKING SCISSORING LINEAR SOLENOID BODY ARMOR ACTUATOR ESC MOTOR DIAMAGNETIC SELF REPULSION ENGINE ELECTRODYNAMICS SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON www.flymorton.com jhandy.simdif.com manneduav.simdif.com uavbiomechatronic.simdif.com manneduavengine.simdif.com mortonuav.simdif.com mortonsvision.simdif.com

UNIGRAVITY SUIT MACHINES

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

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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

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 refrigerated by MCE HFC liquid cooling 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 winding 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 air defined as orthosis calf shin ankle heel foot toe brace levitated push pull within vector field of the emissions source tractor pull or beam push suspended within proximity solenoid hold sensory

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