FLYMORTON WEARABLE BIOMECHATRONIC MANNED UAV ORTHOSIS BOOT ENGINE ELEMENT DIAMAGNETIC SELF REPULSIVE ESC BOOTS LINEAR MOTOR SELF ACTUATOR SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON

FLYMORTON WEARABLE POWER ARMOR FLIGHT BOOTS SUBSYSTEM COMPONENTS ELECTRICAL POWERED (DC) 210V-240V (AC) SYNCHRONOUS OUTPUT POWER TRANSFER ELECTROMAGNETIC INDUCTION PHASE ONE VOLTAGE STEP-UP SYNCHRONOUS (AC)TRANSFORMER (AC) ELECTROMOTIVE WIRELESS POWER TRANSFER TRANSDUCTOR INDUCED CURRENT CARRYING LINEAR SELF REPULSION ACTUATOR DESIGN ELECTROMAGNETIC EDDY CURRENTS COPPER COIL EMITTER SOLENOID PUSH SENSORY POWERED BY MAGNETISM CURRENT CARRYING SILICON METALLIC WIRE COIL HORN ELECTRICAL ENERGY WINDING ELECTROSTATIC EMITTER SILICON ELEMENT TYPE SEMICONDUCTIVE JUNCTION DC ALONGSIDE BORON WIRE COIL ELECTRICAL ENERGY WINDING ONE-WAY SINGLE PHASE RECTIFIER DIODE THERMOELECTRIC EFFECT TRANSDUCTOR MAGNETICS LOW TEMPERATURE TRANSMISSION SEEBECK EFFECTS TYPE SUPERCONDUCTIVE PHASE WIRE BYPASS MODULATED BY AUDIO AMPLIFIER ELECTRON AMPHERE AS PRESSURE OR VELOCITY OF THE DIAMAGNETIC EMISSIONS AGAINST COMMON COMPONENT ELEMENT ALUMINUM SELF REPULSIVE FORCED AWAY BY HIGH AMPHERE PRESSURE ELECTROSTATIC VORTEX NEWTRON ACCELERATING PARAMAGNETIC ELECTROSTATIC ELECTROLYTIC MAGNETO OOBLECK GAUSS DISPLACEMENT NON-NEWTONIAN BUOYANT LIQUID FILLED ENCLOSURE BETWEEN THE MEDIUM RISE AT COLLISIONS AT HIGH VELOCITY HIGH VISCOSITY HIGH NEWTONIAN DENSITY SECTIONAL RADIATION SWITCHING BETWEEN 20HERTZ STEP-UP MAX 328 HERTZ ELECTRODYNAMICS ELECTRON MAGNETIZED GYRO PRECESSION QUANTUM VACUUM AMPHERE MAGNETO ACCELERATOR ELECTRON COLLISION MATTER TORQUE NEWTRON ENERGIES VELOCITY FORCE OF DENSITY PHASE COMMON ELEMENT AWAY FROM WAVELENGTH REPEL FORCED FROM WITHIN FIELD AS TO LEVITATION TRANSMITS SOLENOID PULL PUSH SENSORY SWITCH SELF ACTUATED DAMPERING VIBRATION SWITCH VECTOR FIELD GRAVITY SENSORY SWITCH PROXIMITY FIELD HOLD SENSORY SWITCH SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON. INTUITIVE INTELLIGENCE PROGRESSIVE DEVELOPMENT IDEA 

The wire turns in this footage are more than a typical AC powered motor rotor grinder having torque energy enough to lift a man by it's freedom ball BARING armature central of it commutator localized separate and spaced by one millimeter whereas armature maybe couplet to a lever mechanically lift a human adult on stand or platform surface its power COMMUTATOR having one pair two horn exhibits coil turns direct current phase wire round having been deformed round spun tightly helix shape turned 135 time circular per horn enumerates 270t turns. For comparison the boot exhibiting round wire deformed turned circular spun tightly into helix shape coil method current carrying likenesses as an solenoid type hall effect sensory actuator type linear self actuated aluminum boot frame ACTUATED by electromagnetics emissions Electrodynamics at high velocity superconducting electron ACCELERATING movements gyroscopic electron PRECESSION tightly quantum vacuum vortex TIGHTING electrons together repulsive collision ELECTROSTATIC vortex Electrodynamics reactive newtron kinetic torque energy generates repulsive paramagnetic particle collision moisture accumulator kinetic gauss energy velocity density generator transmitted by Diamagnetic superconducting repulsive forces away common element aluminum block boot frame join to this coil BARING boot overlapping it's exterior coil couple to coil operates underneath within it's central core if powered by a power generator repulsive torque force maybe more the 5 high torque force rotary grinder motor as of now however the motor is incomplete and shall inherit more audio wire turns that shall exceed pass 1100newton repulsive torque energies forces the aluminum frame constant upwards away from the fixed permanent position aluminum block coil cage within the Electrodynamic Eddy currents vector field proximity field wavelength between the medium rise push energy phases aluminum surfaces within the metric range or FRACTION phased area actuated or area within fraction surface actuated