ANTI-GRAVITY UAV FACE SHIELD DRONE EXTERIOR DC INDUCED CURRENT PROJECTILE BALLISTIC TASER PROTECTION FACE SHIELD SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE INVENTOR JERMAINE MORTON DESIGNGADOLINIUM JOINED WITH QUARTZ ENERGY CRYSTAL THERMAL REACTIVE INDUCED CURRENT MODULATED HARMONIC ULTRASONIC TRANSDUCTOR HORN FACE SHIELD ELECTROMOTIVE AC DC INDUCED CURRENT CARRYING OUTPUT ENERGY CAPACITANCE DC (EE) PHASE PIEZOELECTRIC EFFECTIVE FACE SHIELD PYROELECTRICITY EEG METALLOID BOND SEEBECK EFFECTIVE PELTIER EFFECTIVE COOLER RADIATION PRESSURES FORCES PARAMAGNETIC PARTICLES DISPLACEMENT ELECTRICAL ENERGY WINDING ELECTROSTATIC VORTEX ROTATING ELECTRON COLLISION QUANTUM MASS ACCUMULATION CIRCULAR CAGE VECTORING VELOCITY TYPE GYROSCOPIC GAUSS PRECESSION GENERATES NEWTONIAN ENERGY PHASE BY CIRCULAR MECHATRONICS AND OSCILLATIONS SUSPENDING CONTROLLED MATTER BETWEEN THE MEDIUM RISE PHASE LIQUID FILLED ENCLOSURE WITHIN VECTOR FIELD SOLENOID HOLD SENSORY PROXIMITY HOLD SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE INVENTOR JERMAINE MORTON DESIGN

ANTI-GRAVITY UAV FACE SHIELD DRONE EXTERIOR DC INDUCED CURRENT PROJECTILE BALLISTIC TASER PROTECTION FACE SHIELD SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE INVENTOR JERMAINE MORTON DESIGN

GADOLINIUM JOINED WITH QUARTZ ENERGY CRYSTAL THERMAL REACTIVE INDUCED CURRENT MODULATED HARMONIC ULTRASONIC TRANSDUCTOR HORN FACE SHIELD ELECTROMOTIVE AC DC INDUCED CURRENT CARRYING OUTPUT ENERGY CAPACITANCE DC (EE) PHASE PIEZOELECTRIC EFFECTIVE FACE SHIELD PYROELECTRICITY EEG METALLOID BOND SEEBECK EFFECTIVE PELTIER EFFECTIVE COOLER RADIATION PRESSURES FORCES PARAMAGNETIC PARTICLES DISPLACEMENT ELECTRICAL ENERGY WINDING ELECTROSTATIC VORTEX ROTATING ELECTRON  COLLISION QUANTUM MASS ACCUMULATION CIRCULAR CAGE VECTORING VELOCITY TYPE GYROSCOPIC GAUSS PRECESSION GENERATES NEWTONIAN ENERGY PHASE BY CIRCULAR MECHATRONICS AND OSCILLATIONS SUSPENDING CONTROLLED MATTER BETWEEN THE MEDIUM RISE PHASE LIQUID FILLED ENCLOSURE WITHIN VECTOR FIELD SOLENOID HOLD SENSORY PROXIMITY HOLD SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE INVENTOR JERMAINE MORTON DESIGN

 

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ANTI-GRAVITY UAV FACE SHIELD DRONE EXTERIOR DC INDUCED CURRENT PROJECTILE BALLISTIC TASER PROTECTION FACE SHIELD SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE INVENTOR JERMAINE MORTON DESIGN

GADOLINIUM JOINED WITH QUARTZ ENERGY CRYSTAL THERMAL REACTIVE INDUCED CURRENT MODULATED HARMONIC ULTRASONIC TRANSDUCTOR HORN FACE SHIELD ELECTROMOTIVE AC DC INDUCED CURRENT CARRYING OUTPUT ENERGY CAPACITANCE DC (EE) PHASE PIEZOELECTRIC EFFECTIVE FACE SHIELD PYROELECTRICITY EEG METALLOID BOND SEEBECK EFFECTIVE PELTIER EFFECTIVE COOLER RADIATION PRESSURES FORCES PARAMAGNETIC PARTICLES DISPLACEMENT ELECTRICAL ENERGY WINDING ELECTROSTATIC VORTEX ROTATING ELECTRON  COLLISION QUANTUM MASS ACCUMULATION CIRCULAR CAGE VECTORING VELOCITY TYPE GYROSCOPIC GAUSS PRECESSION GENERATES NEWTONIAN ENERGY PHASE BY CIRCULAR MECHATRONICS AND OSCILLATIONS SUSPENDING CONTROLLED MATTER BETWEEN THE MEDIUM RISE PHASE LIQUID FILLED ENCLOSURE WITHIN VECTOR FIELD SOLENOID HOLD SENSORY PROXIMITY HOLD SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE INVENTOR JERMAINE MORTON DESIGN

 

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FLYMORTON WEARABLE PERMANENT MAGNET FACE SHIELD vector field 22mm 2.6kg pull rate magnet series MODULATED electromotive Ultrasonic ELECTROMAGNET HALL EFFECTS SOLENOID HOLD SENSORY UAV TYPE ORNITHOPTER WING TYPE DIAMAGNETIC COPPER COIL EXHIBITING PERMANENT MAGNET CENTRAL HELIX CORE BARING 52N NEODYMIUM MAGNET GAUSS FORCE RATE 8.4KG AT 18.519 pounds FORCE RATE, WINGS ARE MECHATRONIC 40,000 OSCILLATIONS 1,120,000 times phase repulsive vector field 
 WING PAIR VECTOR FIELD COLLISION REPULSIVE COMMON FORCE RATE AWAY 28KG 66OZ INTRODUCED GAUSS KINETIC ENERGY FORCES AWAY OSCILLATION LIMITED TO 22MM VECTOR FIELD 1,120,000 OSCILLATION repulsive phase vector field times 40,000per minute RETURNING 53.464 pounds x40,000 =
2138.56
 REPULSIVE ENERGY phase COMMON VECTOR FIELD gauss between 22mm RANGE 1,120,000 TIMES PER MINUTE AGAINST PERMANENT MAGNET REPULSIVE RATE 2.6KG KINETIC ENERGY 5.732 pounds of GAUSS FACE SHIELD 40,000 oscillations 
2138.56 pound forces per minute
 2,138lbs and 56oz kinetic energy modified by five pairs of
Voltage booster power capacitor 1,000,000 volts phase wire output modulated hollow aluminum cylindrical block motorized ARMATURE rotating neodymium/ PYRO/ silicon/ Bismuth aluminum/copper/ conductive liquid energy cell power generator powered mesh power supply powered phase wire Magnetism atomic electrons precession increased newtron precession energy capacitance metallic BOND current carrying electromotive iron rod spark-gap between wing and face shield face rest cockpit core surfaces EXHIBITING
Spark-gap ARC fire newtron precession plasma vortex synchronous AC induced current carrying Capacitance actuator transductor hall effects solenoid pull push sensory






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FLYMORTON WEARABLE BIOMETRIC RANGE ELECTRONICS TRANSCEIVER METALLOID BIONIC MULTI CHANNEL RADIO ENERGY HARVESTING POWER ARMOR GENERATOR MODULATED 40,000khz 1sec SONIC NANO PIEZOELECTRIC PARALLEL PHASE INDUCTOR V~ BOOST METALLIC BOND {MFD} EMI ELECTRON INDUCTION MOTOR MODULATED SOFTWARE BASE PROCESSING CURRENT CARRYING INDUCTOR SONIC OUTPUT VOLTAGE {MB}EMI} (DC);ULTRA CAPACITOR {AC} ELECTROACOUSTIC CRYSTALLOID PYROELECTRIC PRISM PIEZO ELECTRIC EFFECT ELECTRICAL WIRE TYPE CU~Fe~AI WIRE Uc} {DC/AC DIAMAGNETIC IONIC DYNAMICS EMI AC/AC WPT FERRO-MAGNETIC DYNAMICS AC/AC/EDI {UC} AC/AC PARAMAGNETIC WIRE IONIC DYNAMICS EDT EDF EDS ESC ENGINE DESIGN TYPE LINEAR SOLENOID HALL EFFECT PULL PUSH SENSORY (EDI}INDUCTION MOTOR COIL ARRANGED STEP UP VOLTAGE CYCLING ELECTRON ACCELERATOR SOLID STATE CRYSTALLOID BATTERY POWER BODY ARMOR (WPT) POWERED ALUMINUM BLOCK SHEET ENCLOSURES ESC DESIGN ELECTROMAGNET COIL SONIC VIBRATOR TRANSDUCER WIRE HORN SONIC OSCILLATOR ACOUSTOPHORESIS ATMOSPHERIC OMNI-DIRECTIONAL GRAVITATIONAL GRAHAM'S LAW+FICKS LAW~ gas law (PV = nRT) 4.8~NEWTONS NANOPARTICLE LAW OF VELOCITY HENRY'S LAW~ COLLISIONAL FORCES Centrifugal forces nanoparticle DECAY VENTRIFUGAL DISPLACEMENT OF GRAVITY AWAY FROM THE BODY ARMOR ENCLOSURES SURFACES AREA OF FRACTION BETWEEN THE MEDIUM RISE POWER SUPPLY SOURCE OF EMISSION, BODY ARMOR DESIGN VOLTAGE TRANSFORMER STRUCTURE COUPLE TO A COMMON ELEMENT METALLIC DESIGN ELECTRICAL WIRE ENGINE CIRCUIT SECTIONAL VOLTAGE NEWTON'S LAWS 1+2+3 LAW OF MOMENTUM ELECTROMOTIVE FORCE HIGH VELOCITY ELECTRODYNAMICS REPEL FORCES AWAY FARADAY'S CAGE MICROWAVE BLOCKING ARIEL DYNAMIC ACROBATIC BIONICS BIOMECHATRONICS LINEAR TRANSDUCTIVE SOLENOID MANNED UAV ORTHOSIS FOREARM BIAXIAL ROM BRACE ACTUATOR SUBSYSTEM ENGINE DESIGN SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON Intuitive intelligence aeronautic engineering Characterize as in Wearable biomechatronic biometric range bionic manned UAV body armor flight suit machine subsystem structure electrical circuit consist of 450voltsUc×8Uc=3,600v lenz's law's 450voltsUc×4module units multiplyed phase=1,800volts Wire rated at 600v~1,000v maximum voltage awg#14 EMI power supply 600volts×41 12ft of lengthy wire measures at 472ft of lengthy Cu awg#14 =41teslas coil of wire turns {Ohm's law}of lengthy awg#14{amphere's law} ELECTRODYNAMICS ELECTROSTATIC IONIC COLLISION atmospheric environment FARADAY'S ELECTROCHEMICAL PROCESS OF {GAS LAW}BOYLE'S LAW~ CHARLES LAW~Avogadro's law~{GAUSS LAW}= 24,600v of energy÷767watts=32hp times of EDF of 1 hp 550lbs× 32hp=17,600LBS{ linear force) per ORTHOSIS arm brace and so air traveling plank time is uniquely inevitable subject not limiting to additional system or structure potentiometric range design inventor Jermaine Morton Portescap small DC motors can deliver a torque range from 0.36 mNm up to 160 mNm continuously and from 2.5 mNm up to 1,487 mNm in intermittent operation. A "linear force" is a force that acts directly along a straight line, meaning it only causes motion in one direction without any rotational component; essentially, it's a force that produces linear acceleration in an object, pushing or pulling it along a straight path motion along a single line, with no sideways or twisting components. Against its weight of gravity gravitational constant and mass of the earth The precise strength of Earth's gravity varies depending on location. The nominal "average" value at the Earth's surface, known as standard gravity is, by definition, 9.80665 m/s2 (about 32.1740 ft/s2). Subject not limiting to additional system or structure potentiometric range design inventor Jermaine Morton

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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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