EDS UAV XWING DRONE

INVENTOR JERMAINE MORTON DESIGNED 
Xwing
REMOTE CONTROLS BATTERY POWERED ELECTRONICS ELECTROMOTIVE FORCE PULSE PHASE 250TESLA'S COPPER COIL WIRE (MFD) TURNS. THE AIRPLANE UTILIZES ELECTRODYNAMICS REPEL FORCES THE AIRCRAFT INTO THE AIR. THE PLANE SUBSYSTEM CORE ELECTRICAL CIRCUITRY UTILIZES DIAMAGNETIC ELECTRICAL ENERGY WINDING PULSE PHASE AC ELECTROMOTIVE FORCE INDUCE A CURRENT WITHIN A NONE GALVANIZED FERRO-MAGNETIC ELEMENT VOLTAGE REACTIVE ELECTROMAGNETIC, MODULATED HYPERSONIC PULSE ELECTRODYNAMICS, ELECTROSTATIC GAUSS RADIATION PRESSURES PARTICLE COLLISIONS COMMON ION RADIATION PRESSURES FROM TWO SEPARATE SOURCES EMITTING POSITIVE CHARGE NANO-PARTICLES VECTOR FIELD MICROWAVE RADIATION PRESSURES FORCES AWAY COMMON POSITIVE ION GAUSS TRANSMITTED FROM A LOCALIZED COMMON ELEMENT AS AN COPPER TOP DESIGN AS ONE SIDE OF THE AIRPLANE TOP PART EXTERIOR ENCLOSURES, CONTRARY OF ITS ALUMINUM ELEMENT CONNECTIONS TO A SEPARATE SOURCE OF POWER. WHEN SO EVER THE CONDUCTIVE AIRPLANE LOWER SIDE BOTTOM ALUMINUM CURRENT CARRYING VOLTAGE TO ESTABLISH A SIGNAL AGAINST ITS COPPER COIL ELECTRICAL ENGINE CIRCUIT WIRE TURNS WEIGHS MORE THAN IT'S INERTIAL MASS OF THE AIRPLANE ELECTRODYNAMICS DENSIFIED STRENGTHS ARE MEASUREMENT 4 TO THE TENTH POWER OF ITS INITIAL FORCE, ESCAPING AWAY FROM THE ALUMINUM BOTTOM MICROWAVE VELOCITY WAVELENGTH STRENGTHS OF IONIC RADIATION VECTOR FIELD DRAG FORCES THE ALUMINUM BOTTOM THAT IS PERMANENTLY CONNECTED TO THE AIRPLANE ALUMINUM BOTTOM SIDE DRAG FORCED INTO THE AIR HAVING LESS WEIGHT THAN ITS CENTRAL CIRCUIT MASS AND ITS EMISSION FORCES AGAINST THE CIRCUIT'S WEIGHT OF GRAVITY ABOUT 40TIMES+THE CIRCUIT PHYSICAL MASS AND EMITTING GAUSS 40TIMES THE WEIGHT OF ITS GRAVITY OF THE AIRPLANE DC/AC EMI VOLTAGE CAPACITOR FILTER 10,000w~40,000w Max voltage HPF SQUARE WAVE 1/4TH OF HERTZ 20,000HZ~100,000HZ HFP PHASE BORON FERROMAGNETISM COMMUTATOR TRANSDUCTOR HORN EMI 10,000W~40,000w SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON 

INVENTOR JERMAINE MORTON DESIGNED 
Xwing
REMOTE CONTROLS BATTERY POWERED ELECTRONICS ELECTROMOTIVE FORCE PULSE PHASE 250TESLA'S COPPER COIL WIRE (MFD) TURNS. THE AIRPLANE UTILIZES ELECTRODYNAMICS REPEL FORCES THE AIRCRAFT INTO THE AIR. THE PLANE SUBSYSTEM CORE ELECTRICAL CIRCUITRY UTILIZES DIAMAGNETIC ELECTRICAL ENERGY WINDING PULSE PHASE AC ELECTROMOTIVE FORCE INDUCE A CURRENT WITHIN A NONE GALVANIZED FERRO-MAGNETIC ELEMENT VOLTAGE REACTIVE ELECTROMAGNETIC, MODULATED HYPERSONIC PULSE ELECTRODYNAMICS, ELECTROSTATIC GAUSS RADIATION PRESSURES PARTICLE COLLISIONS COMMON ION RADIATION PRESSURES FROM TWO SEPARATE SOURCES EMITTING POSITIVE CHARGE NANO-PARTICLES VECTOR FIELD MICROWAVE RADIATION PRESSURES FORCES AWAY COMMON POSITIVE ION GAUSS TRANSMITTED FROM A LOCALIZED COMMON ELEMENT AS AN COPPER TOP DESIGN AS ONE SIDE OF THE AIRPLANE TOP PART EXTERIOR ENCLOSURES, CONTRARY OF ITS ALUMINUM ELEMENT CONNECTIONS TO A SEPARATE SOURCE OF POWER. WHEN SO EVER THE CONDUCTIVE AIRPLANE LOWER SIDE BOTTOM ALUMINUM CURRENT CARRYING VOLTAGE TO ESTABLISH A SIGNAL AGAINST ITS COPPER COIL ELECTRICAL ENGINE CIRCUIT WIRE TURNS WEIGHS MORE THAN IT'S INERTIAL MASS OF THE AIRPLANE ELECTRODYNAMICS DENSIFIED STRENGTHS ARE MEASUREMENT 4 TO THE TENTH POWER OF ITS INITIAL FORCE, ESCAPING AWAY FROM THE ALUMINUM BOTTOM MICROWAVE VELOCITY WAVELENGTH STRENGTHS OF IONIC RADIATION VECTOR FIELD DRAG FORCES THE ALUMINUM BOTTOM THAT IS PERMANENTLY CONNECTED TO THE AIRPLANE ALUMINUM BOTTOM SIDE DRAG FORCED INTO THE AIR HAVING LESS WEIGHT THAN ITS CENTRAL CIRCUIT MASS AND ITS EMISSION FORCES AGAINST THE CIRCUIT'S WEIGHT OF GRAVITY ABOUT 40TIMES+THE CIRCUIT PHYSICAL MASS AND EMITTING GAUSS 40TIMES THE WEIGHT OF ITS GRAVITY OF THE AIRPLANE DC/AC EMI VOLTAGE CAPACITOR FILTER 10,000w~40,000w Max voltage HPF SQUARE WAVE 1/4TH OF HERTZ 20,000HZ~100,000HZ HFP PHASE BORON FERROMAGNETISM COMMUTATOR TRANSDUCTOR HORN EMI 10,000W~40,000w SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON 

INVENTOR JERMAINE MORTON DESIGNED 
Xwing
REMOTE CONTROLS BATTERY POWERED ELECTRONICS ELECTROMOTIVE FORCE PULSE PHASE 250TESLA'S COPPER COIL WIRE (MFD) TURNS. THE AIRPLANE UTILIZES ELECTRODYNAMICS REPEL FORCES THE AIRCRAFT INTO THE AIR. THE PLANE SUBSYSTEM CORE ELECTRICAL CIRCUITRY UTILIZES DIAMAGNETIC ELECTRICAL ENERGY WINDING PULSE PHASE AC ELECTROMOTIVE FORCE INDUCE A CURRENT WITHIN A NONE GALVANIZED FERRO-MAGNETIC ELEMENT VOLTAGE REACTIVE ELECTROMAGNETIC, MODULATED HYPERSONIC PULSE ELECTRODYNAMICS, ELECTROSTATIC GAUSS RADIATION PRESSURES PARTICLE COLLISIONS COMMON ION RADIATION PRESSURES FROM TWO SEPARATE SOURCES EMITTING POSITIVE CHARGE NANO-PARTICLES VECTOR FIELD MICROWAVE RADIATION PRESSURES FORCES AWAY COMMON POSITIVE ION GAUSS TRANSMITTED FROM A LOCALIZED COMMON ELEMENT AS AN COPPER TOP DESIGN AS ONE SIDE OF THE AIRPLANE TOP PART EXTERIOR ENCLOSURES, CONTRARY OF ITS ALUMINUM ELEMENT CONNECTIONS TO A SEPARATE SOURCE OF POWER. WHEN SO EVER THE CONDUCTIVE AIRPLANE LOWER SIDE BOTTOM ALUMINUM CURRENT CARRYING VOLTAGE TO ESTABLISH A SIGNAL AGAINST ITS COPPER COIL ELECTRICAL ENGINE CIRCUIT WIRE TURNS WEIGHS MORE THAN IT'S INERTIAL MASS OF THE AIRPLANE ELECTRODYNAMICS DENSIFIED STRENGTHS ARE MEASUREMENT 4 TO THE TENTH POWER OF ITS INITIAL FORCE, ESCAPING AWAY FROM THE ALUMINUM BOTTOM MICROWAVE VELOCITY WAVELENGTH STRENGTHS OF IONIC RADIATION VECTOR FIELD DRAG FORCES THE ALUMINUM BOTTOM THAT IS PERMANENTLY CONNECTED TO THE AIRPLANE ALUMINUM BOTTOM SIDE DRAG FORCED INTO THE AIR HAVING LESS WEIGHT THAN ITS CENTRAL CIRCUIT MASS AND ITS EMISSION FORCES AGAINST THE CIRCUIT'S WEIGHT OF GRAVITY ABOUT 40TIMES+THE CIRCUIT PHYSICAL MASS AND EMITTING GAUSS 40TIMES THE WEIGHT OF ITS GRAVITY OF THE AIRPLANE DC/AC EMI VOLTAGE CAPACITOR FILTER 10,000w~40,000w Max voltage HPF SQUARE WAVE 1/4TH OF HERTZ 20,000HZ~100,000HZ HFP PHASE BORON FERROMAGNETISM COMMUTATOR TRANSDUCTOR HORN EMI 10,000W~40,000w SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON 









 

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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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