FLYMORTON WEARABLE BIOMECHATRONIC UAV ORNITHOPTER WING FACE SHIELD DRONE

FLYMORTON WEARABLE ANTI-GRAVITY ORNITHOPTER UAV FACE SHIELD
SUBSYSTEM STRUCTURE OPERATES BY
ELECTROMAGNETIC ATTRACTION CENTRAL CORE permanent magnet COMMON PUSH RATE 4.6KG COUPLE TO FACE SHIELD INTRODUCE TO ELECTROMAGNETIC LIMITLESS PULL WING EXHIBITS A PERMANENT MAGNET COMMON SIDE 4.6KG REPULSIVE FORCES AWAY PERMANENT MAGNET FACE SHIELD FREEDOM OF MOVEMENT HIGH VOLTAGE BOOSTER CAPACITOR SPARK-GAP TASER DESIGN AC INDUCED CURRENT WIRELESSLY BETWEEN THE WING AND FACE SHIELD METALLIC CATHODE SURFACE
CORRESPONDING TOGETHER COORDINATED EVENTS OF SONIC OSCILLATING CONSTANT MOVEMENT AWAY BY ELECTROMAGNETICALLY INTRODUCING THE ELECTRODE WING LOCALLY TO THE FACE SHIELD POWER TRANSFER SURFACE CLOSING THE PLASMA SPARK GAP GENERATING ION (MFD) CHARGE INDUCTOR COIL INDUCED CURRENT TOWARDS THE ATTRACTIVE TO THE IRON SHEET SURFACE EXHIBITS A CENTRAL PERMANENT MAGNET WITHIN VECTOR FIELD OF THE PERMANENT MAGNET COMMON SIDE VECTOR FIELD REPULSIVE FORCES AWAY INTO THE AIR AS TO LEVITATION AS TO FLY MAGNETICALLY INDUCED KINETIC REPULSIVE ENERGY FORCES FREEDOM OF MOVEMENT FACE SHIELD ESC
Subject not limiting to additional system or structure potentiometric range inventor Jermaine Morton design
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FLYMORTON WEARABLE BIOMECHATRONIC MIXED METALLIC ELEMENTS ARE COPPER SHEETS ALUMINUM SHEET IRON SHEET INCORPORATES THE BIOMETRIC STRUCTURE FACE PROTECTION FUNCTIONAL LIKENESSES AS AN SHIELD MODIFIED UAV MODULATED ORNITHOPTER WING FACE SHIELD WEARABLE DRONE SUBSYSTEM
PERMANENT MAGNET POLAR REPULSIVE FORCES AWAY PERMANENT MAGNET WING BARING COPPER WIRE COIL SOLENOID PUSH SENSORY SURFACE BASE CONNECTIONS TO  High voltage TESLA emitter DC PHASE AC INDUCED CURRENT diamagnetic REPULSIVE FORCES PERMANENT MAGNET ESCAPE MODULATED ELECTROMOTIVE AUDIO ENCODER DRIVEN ULTRASONIC VERTICAL OSCILLATING RAPID RADIATION INTENSE REPULSIVE PERMANENT MAGNET GAUSS AGAINST PERMANENT MAGNET GAUSS PRESSURES PERMANENT  MAGNET AWAY CONSTANT FORCES AGAINST GRAVITATIONAL WEIGHT AND INERTIAL MASS AWAY LIFT FORCES PERMANENT MAGNET FACE SHIELD INTO THE AIR SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE INVENTOR JERMAINE MORTON DESIGN


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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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