Three part sectional segment caloric thermal dynamics compressor vapor cycling EDS THERMAL DYNAMICS PHASE TUBING OPERATES HEATING FLUID tubing process high temperatures vapor bleeder choke nozzle.cooling tubing heat dissipation tubing repeat microwave thermal dynamics compressor vapor bleeder head dissipation vapor phase by combustible vaporr VELOCITY low temperature PARTICLE pellet Peltier cooling fluid adapters converted action boiler

FACEPLATE UAV HAVING A MOTOR  STRUCTURE ALUMINUM DIAMAGNETIC ELEMENT FUNCTIONS AS AN COMMUTATOR EXHIBITING PERMANENT MAGNETS INTERFACE FIX FOR VERTICAL EMISSION COUPLE TO THE DIAMAGNETIC SURFACES BARING ELECTRIC ( DC) BATTERY POWERED 40,000RPM PANCAKE STEPPER MOTORIZED ARMATURE CONNECTIONS TO DIAMAGNETIC RECTANGULAR ELEMENT BARING INDUCTOR AUDIO WIRING SPUN TIGHTLY AROUND ALUMINUM SURFACE BASE FORMING A RECTANGULAR HELIX SHAPE INDUCTOR PROPELLER.  THE MOTORIZED PROPELLER ROTATING WITHIN VECTOR FIELD PERMANENT MAGNET COMMUTATOR BASE SURFACE SYNCHRONOUS AC CHARGE TRANSDUCTOR SHAPED PROPELLER WHICH THEN TRANSMITS THE SIGNAL BACK AGAINST SOURCE ACTING AS IT’S ACTUATOR.  So there’s no need for cooling source the speed of the rotation of the blades does not accumulate heat neither does the COMMUTATOR or its PERMANENT MAGNET OR SURFACE BASE.

Wearable biomechatronic UAV face shield Incorporated practical elements Aluminum, quartz, Bismuth, silicon, iron, copper, SUBSYSTEM structure electrical circuit modulated voltage transformer (EEG) electromotive AC (EE) charge transductor diamagnetic repulsive ESC) linear actuator AC synchronous (EE) charge diamagnetism high voltage energy capacitor (DC) ballistic taser face shield conductive HIGH VOLTAGE (EE) (DC)CHARGE PHASE projectile PROOF cathode titanium face shield Maxwell electrodynamics Lorentz force law, Newton's 3rd Law,quantum mechanical effect of Electromagnetic induction, teslas coil turns,Electric Charges, Electrostatic fields, Vector field, proximity field, Potential energy, energy Capacitance, Current carrying Electricity, Moving Charge particles, Electromagnetic Induction Alternating Current, Electrodynamics, magneticflux density,Synchronous capacitor C = Q V R = \frac{V}{I} R = resistance (Ohms, Ω) V = voltage difference which is between the two ends of a resistor (Volts, V) Electromagnetic Waves Diamagnetic Repulsive force escape, SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE INVENTOR JERMAINE MORTON DESIGN

DIAMAGNETIC REPULSIVE ESC UAV FACE SHIELD DRONE PROGRESSIVE DEVELOPMENT TRIAL AND ERROR Permanent magnet Synchronous ELECTRICAL ENERGY CHARGE inductor AWG#24 spun tightly helix shape pancake coil modulated two phase wire ends bypass single phase rectifier diode wire bypass one phase wire end bypass modulated capacitor phase wire inductor (right hand rule law of induction) capacitance coil current carrying electrical energy transductor electrostatic emissions repulsive forces diamagnetic aluminum base escape against the weight of gravity or inertial Mass mounted to diamagnetic face shield surface base are permanent magnets emissions charge the motorized Inductor coil action propeller rotary structure mounted separately connected to armature of a brushless motor connections to the diomagnetic surfaces base. the propeller structure exhibits copper protection coated wire, current carrying inductor spun tightly into Helix shape coil modulated triple action designed to function as an rotary wheel gyroscope or Transduction propeller current carrying electrical electron energy capacitor power generator that EMITS electromagnetic Eddy currents as a propellant against it's connections diamagnetic repulsive escape rotor UAV drone subject not limiting to additional system or structure potentiometric range inventor Jermaine Morton design I have intuitive intelligently Comprehended the electrical energy as in kilowatts Which may be translated into mechanical horsepower Force energies of Electrodynamics repulsive force two types of element to which is common in mass given atomic quantity energy equal to the same power Having the linkage connections between the two elements are greater than the strength of the two common elements however the source of one element may have connections to a voltage generator emissions which should increase the atomic quantity energy given to the 10th power against the second common element emissions having freedom without weight generating drag Forces the element phased within Vector field Atomic collisions Against common element weight of gravity and inertial mass I have a 750KW RC miniature motor for drone dame 1,000-watts of power, one kilowatt-hour, nevertheless 550lbs horsepower is equal to exactly 746 watts vice versa 746 watts is equal to one horsepower calculated 550 lb Force. So anyway It's useless to me because the power that charge the motor energies are more than enough the lift 10 full adult men weight at 200lb per human which only needs 1,100 Newton Force to lift a human adult man 1100 Newton is equal to 247.29 Pound-Force. Amphere pressures electrons velocity which should be employed mechatronic flight machines propellant field of emissions electrodynamics or diamagnetic repulsive behavior In science math converted Eddy currents radiation into the mechanical horsepower forces against the weight of gravity and inertial Mass. now I have a little knowledge on how to bypass coil overheating in the field Of electrodynamics levitation or diamagnetic repulsive ANTI-GRAVITY or unigravity machines behavior which may be used to create and design bigger and better aeronautic engineering vehicles

I use permanent magnets magnetic field communicate with the aluminum propeller baring an inductor coil. permanent magnets are mounted on an aluminum surface base. The base bearing induction coils spun tightly Helix shape around a reserved area of the surface base. the diamagnetic transduction propeller is rotated by the armature powered by a high speed flat pancake motor. the propeller blade is a wafer block wheel bearing inductor coil type solenoid pull push sensory. The reaction of the synchronous induction coil couple to the diamagnetic element repulsive reaction type ESC without the transduction coils phase end connections to a voltage generator

INDUCTOR PROPELLER BLADE CHARGE BY SEPARATE ROUNDED PERMANENT MOTOR MAGNETS EMBEDDED WITHIN THE DIAMAGNETIC ALUMINUM BLOCK COMMUTATOR INTERFACE, THE SEPARATE PART DESIGN. FUNCTIONAL LIKENESS AS AN COMMUTATOR SURFACE BASE. THE PERMANENT MAGNET COMMUTATOR OPERATES MAGNETIC EMISSIONS OR AS AN TRANSFORMER HAVING SEPARATE ELECTRICAL CIRCUIT ELECTROMOTIVE SYNCHRONOUS AC WIRELESS POWER TRANSFER CHARGES PROPELLER STRUCTURE DESIGN TRANSDUCTOR OPERATES EDS EMF DIAMAGNETIC REPULSIVE FORCES ESCAPE, INDUCTOR COIL PROPELLER GENERATES ENERGY WHENSOEVER THE INDUCTOR POWERED BY A MOTOR. INDUCTOR PROPELLER COIL METIC BLADE RANGE DESIGN ROTOR MOTION WITHIN THE MAGNETIC VECTOR FIELD SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE INVENTOR JERMAINE MORTON DESIGN

FLYMORTON WEARABLE BIOMECHATRONIC BIOMETRIC FACE RANGE UAV ORNITHOPTER WING TYPE PIEZOELECTRIC EFFECT TYPE ULTRASONIC DRIVEN DC)(AC SYNCHRONOUS ELECTROMOTIVE DIAMAGNETIC REPULSIVE AWAY PERMANENT MAGNET WING ACTUATOR SOLENOID HALL EFFECT SENSE VECTOR FIELD FORCES AWAY PERMANENT MAGNET GROUP MULTIPLE WING ACTUATOR STRUCTURE WING SERIES FACE SHIELD FANNER DESIGN EXHIBITS MULTIPLE BIOMETRIC FACE WING RANGE INCORPORATES PRACTICAL WING FUNCTIONS AS TO OSCILLATING AS AN FANNING AIR THRUST VECTORING VELOCITY ENERGY FORCES AGAINST THE EARTH AGAINST THE WEIGHT OF GRAVITY REDUCING INERTIAL WEIGHT OF GRAVITY AS TO LEVITATE AS TO FLY ORNITHOPTER FACE SHIELD DRONE SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE INVENTOR JERMAINE MORTON DESIGN

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Two part cooling segment and one part thermal dynamics vapor compressor vapor cycling hysteresis refrigeration subject not limiting to additional structure potential metric range inventor Jermaine Morton design Progressive development design

FLYMORTON WEARABLE BIOMECHATRONIC BIOMETRIC FACE RANGE UAV ORNITHOPTER WING TYPE PIEZOELECTRIC EFFECT TYPE ULTRASONIC DRIVEN DC)(AC SYNCHRONOUS ELECTROMOTIVE DIAMAGNETIC REPULSIVE AWAY PERMANENT MAGNET WING ACTUATOR SOLENOID HALL EFFECT SENSE VECTOR FIELD FORCES AWAY PERMANENT MAGNET GROUP MULTIPLE WING ACTUATOR STRUCTURE WING SERIES FACE SHIELD FANNER DESIGN EXHIBITS MULTIPLE BIOMETRIC FACE WING RANGE INCORPORATES PRACTICAL WING FUNCTIONS AS TO OSCILLATING AS AN FANNING AIR THRUST VECTORING VELOCITY ENERGY FORCES AGAINST THE EARTH AGAINST THE WEIGHT OF GRAVITY REDUCING INERTIAL WEIGHT OF GRAVITY AS TO LEVITATE AS TO FLY ORNITHOPTER FACE SHIELD DRONE SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE INVENTOR JERMAINE MORTON DESIGN

FACEPLATE UAV HAVING A MOTOR  STRUCTURE ALUMINUM DIAMAGNETIC ELEMENT FUNCTIONS AS AN COMMUTATOR EXHIBITING PERMANENT MAGNETS INTERFACE FIX FOR VERTICAL EMISSION COUPLE TO THE DIAMAGNETIC SURFACES BARING ELECTRIC ( DC) BATTERY POWERED 40,000RPM PANCAKE STEPPER MOTORIZED ARMATURE CONNECTIONS TO DIAMAGNETIC RECTANGULAR ELEMENT BARING INDUCTOR AUDIO WIRING SPUN TIGHTLY AROUND ALUMINUM SURFACE BASE FORMING A RECTANGULAR HELIX SHAPE INDUCTOR PROPELLER.  THE MOTORIZED PROPELLER ROTATING WITHIN VECTOR FIELD PERMANENT MAGNET COMMUTATOR BASE SURFACE SYNCHRONOUS AC CHARGE TRANSDUCTOR SHAPED PROPELLER WHICH THEN TRANSMITS THE SIGNAL BACK AGAINST SOURCE ACTING AS IT’S ACTUATOR.  So there’s no need for cooling source the speed of the rotation of the blades does not accumulate heat neither does the COMMUTATOR or its PERMANENT MAGNET OR SURFACE BASE. https://jhandy.simdif.com/ANTI-GRAVITY_EDS_EMF_DIAMAGNETIC_REPULSIVE_ESC_FACEPLATE.html

FLYMORTON WEARABLE BIOMECHATRONIC UAV ORNITHOPTER WING TYPE ULTRASONIC DRIVEN ELECTROMOTIVE PIEZOELECTRIC EFFECTS DIAMAGNETIC REPULSIVE WING VECTOR FIELD AWAY PERMANENT MAGNET MULTIPLE WING ACTUATOR SERIES FACE SHIELD DESIGN EXHIBITS MULTIPLE BIOMETRIC WING INCORPORATES THE STRUCTURE DESIGN UAV FACE SHIELD

WEARABLE MICROCOSM REFRIGERATION DIAMAGNETIC REPULSIVE ESC ENGINE UAV FACEPLATE SUBSYSTEM SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIAL METRIC RANGE INVENTOR JERMAINE MORTON DESIGN

SEMI-VOICE COIL STRUCTURE RECTANGULAR ALUMINUM SHEET ZIGZAG FOLD CUT TO MATCH IRONMAN MARK 42 FACEPLATE TEMPLATE SIZED BIOMETRIC FACE RANGE, ADDITIONAL RECTANGULAR CUTOUT FOR BARING AN ELECTRICAL CIRCUIT, THIS INCLUDES RECTANGULAR PLASTIC SHEET HIGH TEMPERATURE RESISTANCE, 2 set of circular curve shape permanent motor magnet nickel neodymium magnets permanently mounted onto the aluminum block surface circling a centered pancake flat (DC) STEPPER motor mount between the four voltage transformer coils spun around the rectangular curve base section. The motor rotary armature couple to and aluminum block round 9mm gauge wafer baring Inductor Audio wiring electromotive solenoid push pull sensory subject to synchronous permanent magnetic communicates by EE (MFD) AC CHARGE transduction coil (EDF)(EMF) ELECTROMOTIVE TRANSMITS (EDS)diamagnetic repulsive ESC TRANSDUCTOR WHEEL ROTARY EEG)(MFD)transduction TRANSMITTING (EDS) ALUMINUM SURFACE STRUCTURE diamagnetic BARING TRANSDUCTOR SOLENOID SENSORY repulsive DIAMAGNETIC wheel motorized SYNCHRONOUS ROTARY TRANSDUCTION EE DIAMAGNETIC REPULSIVE ESC actuator