UAV ORTHOSIS BIOMETRIC RANGE CORRECTING NEURON ELECTROPHYSICS FEEDBACK BRACE DRONE
SYNCHRONOUS LIGHT BRAINWAVES CONTROLS OR ELECTROPHYSICS FEEDBACK.
Wearable UAV orthosis biometric range brace DRONE exterior human magneto induction electrophysic radar biomechatronic biometric range shape diode GPS synchronous human electrophysic brainwaves alpha frequencies, HUMAN MAGNETICS FLUX density radiation wave forces FEEDBACK, ELECTROPHYSICAL rhythmic waves emissions collisions corresponding paramagnetic liquid filled particles in space vectoring pulse magnetic longitude recorded electrophysic amphere molecule radiation beaming vector field proximity field (MFD) sensory subject not limiting to additional system or structure potentiometric range inventor Jermaine Morton design
IT'S-A-GO-COLD
FLYMORTON WEARABLE UAV ORTHOSIS BIOMETRIC RANGE CORRECTION MANACLE DRONE NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE INVENTOR JERMAINE MORTON DESIGN
THAT'S MY WORD... IT'S-A-GO-COLD UAV ORTHOSIS BACK CORRECTION DRONE BRACE. SWEET intuitive intelligence aeronautic engineering Technical Data Inner shroud diameter: 120mm Fan swept area: 82cm² Weight incl. motor, wires, connectors and Secure Fan Fix: 1240g Thrust range: 7.24kg to 9.27kg (71-91N) Exhaust speed range: 87-98m/s RPM range: 24.000-28.500rpm Input power: 4,2-6,2kW Allowed battery: 12-14S 9000mAh Overall efficiency: 71-72% 4x= Thrust range 37.08kg However Specification: Diameter: around 152mm Dynamic Brushless Motor 2815-3300KV 100A+ ESC BEC RC Airplanes EDF Planes or Marine ship Distance Between Mount Holes(centre hole to centre hole): around 115mm 2x 6in Diameter 152mm 5-blade Pitch: Width: Fan swept area: Oxygen newtron : Type (B) gas as an air weight: Blade Width pitch: area of matter quantity: Oxygen Per inch round vector: Velocity oxygen newtron collision: Fusion to liquid weight Translation: Type(B) To (A) liquid H2O velocity: Static Rotation strike force: Energy Toque: Thrust range: Exhaust speed range: RPM range: Input power: Allowed battery: Overall efficiency Reconstruction EDF ROTARY ELECTRODYNAMIC REPULSIVE SUSPENSION PERMANENT MAGNET SYNCHRONOUS AC EDDY CURRENTS INPUT SINGLE PHASE RECTIFIER DIODE PHASE WIRE CONNECTIONS TO CAPACITOR PHASE OUTPUT BYPASS INDUCTOR SINGLE PHASE WIRE END CHARGE COIL STRUCTURE ACTUATOR ORTHOSIS BACK BRACE DRONE Titanium sheet metal Titanium interface baring Baring 52N nickel neodymium 400lbs pull rate surfaces hollow open clearance Baring Deductive fan 152mm 5-blade 2x 6in blade : 6inch iron:hollow cylindrical housing Motor bracket hollow cylindrical exterior Wax sheet Protection paper Baring inductor audio wire gauge #24 Spun tightly helix shape coil alongside the hollow cylindrical deduct fan hollow cylindrical exterior Blade material:Neodymium protection: carbon fiber epoxy resin Coated One thing I've left out the human magneto radar Doppler module current carrying electromotive output phase point connections to an audio encoder current carrying aforementioned electromotive electrical radiation inductor input phase before the single phase rectifier wire modulated ultrasonic driven amplified human magneto radar transduction electromotive output phase wire electromotive synchronous charging inductor current carrying capacitance bypass phase wire modulated input capacitor output phase bypass wire inductor audio encoder power supply input phase wire connections to human magneto radar Doppler input power supply phase point metallic bond current carrying recycling Power generated by the Permanent magnet BLADE rotary action synchronous AC charge inductor voltage transformer EDDY CURRENTS Tesla MATH INDUCTOR WIRE COIL METRIC TURNS AMPHERE POWER UP VOLTAGE GENERATOR Electromagnetic Hall effects repulsive forces permanent magnet titanium surfaces escape as to levitation as to fly against the back brace gravitational Mass and inertial mass suspended in the air within repulsive Eddy currents pulling vector field and Eddy currents pushing proximity field sensory type solenoid hold sensory subject not limiting to additional system or structure potentiometric range inventor Jermaine Morton design
IRONMAN MARK 42 TYPE (EDF)MOTOR POWERED ORTHOSIS BIOMETRIC RANGE UAV ESC GYROSCOPE SUIT MACHINE AERIAL DRONE FLYMORTON PROTOTYPE VERSION INTUITIVE INTELLIGENCE PROGRESSIVE DEVELOPMENT DESIGN ATTRIBUTE AERONAUTIC ENGINEERING SUBJECT TO STRUCTURE MATERIALS CHANGE ELEMENT TYPE PYROELECTRIC EFFECTS CAPACITIVE SURFACES THERMOCOUPLE STACKED TITANIUM XYLOPHONIC GAUGE C# PERCUSSION MODIFIED PIEZOELECTRIC EFFECT TITANIUM'S MODIFIED PELTIER EFFECTS METALLOID SURFACES INTERFACE EXHIBITING NEODYMIUM COOLER SURFACES TYPE VIBER PHONIC C# FREQUENCY ABOVE 20,000HERTZ FUNCTIONS AS AN ELECTRONIC( DC) VIBRANIUM PHASE INPUT MODULATED BY AN ULTRASONIC ENCODER OUTPUT ELECTROMOTIVE SOLENOID SENSORY INTENSE COOLER RADIATION EDDY CURRENTS PRESSURES FORCES ESCAPE DIAMAGNETIC REPULSIVE BEHAVIOR (EMF) (EDS) ION ENGINE PROPELLANT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIAL METRIC RANGE INVENTOR JERMAINE MORTON DESIGN
SYNCHRONOUS PERMANENT MAGNET PELTIER EFFECTS COOLER BRUSH ROTOR MOTOR
SYNCHRONOUS PERMANENT MAGNET PELTIER EFFECTS COOLER BRUSH ROTOR MOTOR subject not limiting to additional system or structure potentiometric range inventor Jermaine Morton design
SYNCHRONOUS PERMANENT MAGNET PELTIER EFFECTS COOLER STACKED MAGNET BISMUTH CURRENT CARRYING CAPACITIVE COMMUTATOR CAGE BALL BARING BRACKET STATOR FREEDOM OF ROTATION ARMATURE NEODYMIUM FILAMENT SILICON STATOR CAPACITIVE AC VOLTAGE TRANSFORMER ELECTROMOTIVE ELECTRODYNAMICS CURRENT CARRYING ELECTRICAL REPULSIVE ENERGY WINDING BUSH ROTOR NEODYMIUM BISMUTH BRUSH JUNCTION ROTOR PANEL (DC) REPULSIVE COMMON NEODYMIUM FILAMENT SILICON ELECTRICAL ENERGY TRANSFER STATOR ROTOR MOTOR
