Characterized as an MANNED UAV EDS HOVERCRAFT AIRPLANE OR SUBMARINE TRAVELING MACHINE CHASSIS FULL BODY structure electrical circuit architectural vertical stacked hollow open clearance metallic sheets and crystal sheets parallel frame structure ends are horizontally stacked hollow metallic sheets and crystal sheets position central enterceptive structure enterconnective hollow frame foundation bottom enclosures end and topped foundation enclosures functional likenesses as an electrical circuit EDT type ONE-WAY voltage SINGLE PHASE CURRENT CARRYING Rectifying electromagnet induction (PNPNPN) transistor (AC)(EDT)transductor(AC VOLTAGE transformer (AC/DC/ transducer OSCILLATING EDT horn PULSE EMI SONIC HFP DC/AC EMI EDT EDF EDS LINEAR SOLENOID MOTOR PULSE EMI SONIC PULSE ELECTRODYNAMICS SELF EMITTER PULSE PHASE REPEL SUSPENSION DRONE SUBJECT NOT LIMITING TO ADDITIONAL SYSTEMS OR STRUCTURES POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE

















Characterized as an MANNED UAV EDS HOVERCRAFT AIRPLANE OR SUBMARINE TRAVELING MACHINE CHASSIS FULL BODY structure electrical circuit architectural vertical stacked hollow open clearance metallic sheets and crystal sheets parallel frame structure ends are horizontally stacked hollow metallic sheets and crystal sheets position central enterceptive structure enterconnective hollow frame foundation bottom enclosures end and topped foundation enclosures functional likenesses as an electrical circuit EDT type ONE-WAY voltage SINGLE PHASE CURRENT CARRYING Rectifying electromagnet induction (PNPNPN) transistor (AC)(EDT)transductor(AC VOLTAGE transformer (AC/DC/ transducer OSCILLATING EDT horn PULSE EMI SONIC HFP DC/AC EMI EDT EDF EDS LINEAR SOLENOID MOTOR 
 PULSE EMI SONIC PULSE ELECTRODYNAMICS SELF EMITTER PULSE PHASE REPEL SUSPENSION DRONE SUBJECT NOT LIMITING TO ADDITIONAL SYSTEMS OR STRUCTURES POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON 

MANNED UAV DC/AC PARALLEL VOLTAGE RECTIFING C-FRAME STACK VT METALLOID COMMUTATOR PNP SC VT EEG EFB AIRCRAFT CHASSIS MOTOR TRANSDUCTOR AIRPLANE ENCLOSURES HORN COMMON SC POWERED DC/AC POSITIVE IONIC GAUSS EMITTER MANNED MOBILITY VEHICLE ENGINE EDT EDF ESC EDS LINEAR SOLENOID ARIEL TRAVELING DRONE


Characterized as an MANNED UAV EDS HOVERCRAFT AIRPLANE OR SUBMARINE TRAVELING MACHINE CHASSIS FULL BODY structure electrical circuit architectural vertical stacked hollow open clearance metallic sheets and crystal sheets parallel frame structure ends are horizontally stacked hollow metallic sheets and crystal sheets position central enterceptive structure enterconnective hollow frame foundation bottom enclosures end and topped foundation enclosures functional likenesses as an electrical circuit EDT type ONE-WAY voltage SINGLE PHASE CURRENT CARRYING Rectifying electromagnet induction (PNPNPN) transistor (AC)(EDT)transductor(AC VOLTAGE transformer (AC/DC/ transducer OSCILLATING EDT horn PULSE EMI SONIC HFP DC/AC EMI EDT EDF EDS LINEAR SOLENOID MOTOR 
 PULSE EMI SONIC PULSE ELECTRODYNAMICS SELF EMITTER PULSE PHASE REPEL SUSPENSION DRONE SUBJECT NOT LIMITING TO ADDITIONAL SYSTEMS OR STRUCTURES POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON









































WEARABLE EXOSKELETRONIC EMI VT SC EDT EDF ESC EDS POWER BODY ARMOR MANNED UAV ORTHOSIS BIOMETRIC RANGE BRACE POWERED EDL BODY ARMOR DRONE 
BIOMECHATRONIC BRAINWAVES SWITCH CONTROLS AIRPLANE ENCLOSURES ACTING EDT TRANSDUCER TRANSDUCTOR MAGNETO HUMAN RADAR DOPPLER EFFECTS INTERFACES HUMAN BODY BRAINWAVES NEURON LOOP FEEDBACK SWITCH CONTROLS SEPARATE PIOLET HUMAN NERVE OR NEURON OSCILLATIONS. THE AIRPLANE ENCLOSURES EMI EEG SC ACEP EXTERIOR SURFACES ACTIVE VOLTAGE ONE-WAY RECTIFIER- ONE WAY VOLTAGE MOSFIT ENCLOSURES ELECTRONS EMITTER HEAT DOPING SEEBECK EFFECTS FARADAY'S CAGE ENCLOSURES EMT EMI VT SC EDT EDF ESC EDS LINEAR SOLENOID MANNED UAV ROTORLESS AIRPLANE DRONE DESIGN subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

This may be similar to the scale of an alien spacecraft pill structure shaped
Somewhat fundamental concepts alien Ariel dynamic technology aeronautic engineering aircraft system Hardware signals software based processing multiple relay channels switch output EMI FILTER 20,000HZ~ 500,000hz+ LOW NOISE hypersonic vibrations atmospheric electrophoresis acoustophoresis atmospheric electrolysis atmospheric faradays electrochemical thermal magneto hydro caloric thermal dynamics boyle's law Charles's Law atmospheric vapor dynamics between the medium rise rapid suspension from the source of radiation vapor suspension cloaking aircraft from visibile light spectrums blocking use's atmospheric vapor oscillator fogger generator infrared light blocking aircraft's armor exterior surfaces without light bouncing off of aircraft armor makes the visible spectrum of its light or shape impossible to see structure or design for parallel voltage thermal emissions subsystem circuit 400amphere+ induce electrons wavelength 1/4th of 1hz,1second voltage modulated electromotive FORCE PHASE INDUCTOR electromagnetic force pulse phase one way voltage Step Up sets of Transformer consist of positive charge DC pulse phase diamagnetic elements synchronous voltage induced DC AC phase ferromagnetic elements galvanized seebeck effect silicon quartz pyroelectric effect energy cell reactive magnetic flux electromagnetics hyper pulse electrodynamics Force phase paramagnetic element aircraft enclosures self- repel esc away ionic radiation vector field electromagnetic source of emission strengths wavelength forces against its weight of gravity or inertial mass as to levitation as to fly

UFO 
https://youtu.be/n36KOqbwrMY?si=O2IMlVPxy52kVVDl













 









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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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