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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 https://manneduav.simdif.com/Wireless_Electronic_indoor_outdoor_floor_tiles.html |
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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 https://manneduav.simdif.com/Wireless_Electronic_indoor_outdoor_floor_tiles.html |
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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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