Tuesday, March 19, 2024

WEARABLE ANTIMATTER GRAVITATIONAL SUPPRESSOR FREEDOM ARIEL DYNAMIC FLIGHT TRAVELING SHOES MANNED UAV BIOMECHATRONIC BRAINWAVES SWITCH CONTROLLED ELECTRICAL CIRCUIT ENERGY WINDING CAPTIVE HOUSING FLUIDIC FLOW VALVE TUBING DIAMAGNETIC COPPER EXHIBITS HOLLOW OPEN CLEARANCE BARING AN ELECTRICAL CIRCUIT CONTACT FLUID FLOW HOUSING ALONGSIDE THE AFOREMENTIONED SEGMENT FERROMAGÑETIC STAINLESS STEEL ELEMENT EXHIBITS AN HOLLOW OPEN CLEARANCE BARING AN ELECTRICAL CIRCUIT CONTACT FLUID FLOW HOUSING COUPLE TO PARAMAGNETIC HOLLOW ALUMINIUM TUBING OPEN CLEARANCE BARING AN ELECTRICAL CIRCUIT CONTACT FLUID FLOW HOUSING ELECTROLYSIS ELECTROPHORESIS MAGNETOHYDROCHLORIC THERMALDYNAMICS FLUID ACCELERATOR (134A HFC) FLUID FLOW THERMAL HYPER HYSTERESIS VAPOR CYCLING ELECTRICAL CIRCUIT REFIGERATION LOW TEMPERATURES TUBILOID DESIGN WEARABLE EDS ORTHOSIS SHOE ELECTROMAGNETIC HYPER REPEL FLIGHT SHOES MANNED MACHINE BRACE SUBJECT NOT LIMITING TO ADDITIONAL SYSTEMS OR STRUCTURES POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON

WEARABLE ANTIMATTER GRAVITATIONAL SUPPRESSOR FREEDOM ARIEL DYNAMIC FLIGHT TRAVELING SHOES MANNED UAV BIOMECHATRONIC BRAINWAVES SWITCH CONTROLLED ELECTRICAL CIRCUIT ENERGY WINDING CAPTIVE HOUSING FLUIDIC FLOW VALVE TUBING DIAMAGNETIC COPPER EXHIBITS HOLLOW OPEN CLEARANCE BARING AN ELECTRICAL CIRCUIT CONTACT FLUID FLOW HOUSING ALONGSIDE THE AFOREMENTIONED SEGMENT FERROMAGÑETIC STAINLESS STEEL ELEMENT EXHIBITS AN HOLLOW OPEN CLEARANCE BARING AN ELECTRICAL CIRCUIT CONTACT FLUID FLOW  HOUSING COUPLE TO  PARAMAGNETIC HOLLOW ALUMINIUM TUBING OPEN CLEARANCE BARING AN ELECTRICAL CIRCUIT CONTACT FLUID FLOW HOUSING ELECTROLYSIS ELECTROPHORESIS  MAGNETOHYDROCHLORIC THERMALDYNAMICS  FLUID ACCELERATOR  (134A HFC) FLUID FLOW THERMAL HYPER HYSTERESIS VAPOR CYCLING ELECTRICAL CIRCUIT REFIGERATION LOW TEMPERATURES TUBILOID DESIGN WEARABLE EDS ORTHOSIS SHOE ELECTROMAGNETIC HYPER  REPEL FLIGHT SHOES MANNED MACHINE BRACE SUBJECT NOT LIMITING TO ADDITIONAL SYSTEMS OR STRUCTURES POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON
The invention of female shoes with a revolutionary structure incorporating tubing for liquid cooling and refrigeration at the foot bottom, along with high heel integration, represents a groundbreaking leap in footwear technology. This innovative design seamlessly merges fashion with functionality, offering a unique blend of style and practicality. By integrating advanced cooling systems within the shoe structure, this invention not only enhances comfort but also introduces a new realm of possibilities for footwear engineering.

At the core of this invention lies the incorporation of 134A (HFC) thermal liquid for cooling purposes. This environmentally friendly refrigerant serves as the primary medium for transferring heat away from the foot, ensuring a constant and comfortable temperature within the shoe. The utilization of thermal liquid within the tubing system creates a closed-loop refrigeration cycle that effectively dissipates heat and regulates the internal climate of the shoe.

The inclusion of hysteresis hyper-vapor cycling fluid tubing in the foot bottom chamber further enhances the cooling efficiency of the shoe. This advanced fluid dynamics system enables rapid heat transfer and ensures optimal thermal management, effectively reducing perspiration and discomfort during extended wear. By harnessing the principles of fluid dynamics, this invention sets a new standard for cooling technology in footwear.

Moreover, the integration of electrical bulk wire functions within the shoe design introduces a sophisticated layer of control and automation. By leveraging electromagnetic forces and electrophoresis of cooler liquid, this invention enables precise temperature regulation and customization. The electrical linear wire circuit embedded within the shoe structure acts as a solenoid, facilitating the emission of ionic electrostatic and electrodynamic forces to maintain optimal cooling conditions.

In addition, the utilization of paramagnetic aluminum and copper sheet foot mounts enhances the functionality of the shoe by enabling levitation against gravity drag forces. By coupling paramagnetic materials with electromagnetic forces, this invention achieves levitation and reduces the impact of inertial mass on the wearer. This innovative feature not only enhances comfort but also adds a futuristic and dynamic element to the design.

Overall, the integration of advanced cooling systems, electrical functions, and paramagnetic materials in the design of female shoes represents a significant technological advancement in footwear engineering. This invention not only redefines the boundaries of fashion and functionality but also paves the way for a new era of smart and adaptive footwear. With its innovative features and cutting-edge design, this invention sets a new standard for comfort, style, and performance in the world of footwear.

WEARABLE ANTIMATTER GRAVITATIONAL SUPPRESSOR FREEDOM ARIEL DYNAMIC FLIGHT TRAVELING SHOES MANNED UAV BIOMECHATRONIC BRAINWAVES SWITCH CONTROLLED ELECTRICAL CIRCUIT ENERGY WINDING CAPTIVE HOUSING FLUIDIC FLOW VALVE TUBING DIAMAGNETIC COPPER EXHIBITS HOLLOW OPEN CLEARANCE BARING AN ELECTRICAL CIRCUIT CONTACT FLUID FLOW HOUSING ALONGSIDE THE AFOREMENTIONED SEGMENT FERROMAGÑETIC STAINLESS STEEL ELEMENT EXHIBITS AN HOLLOW OPEN CLEARANCE BARING AN ELECTRICAL CIRCUIT CONTACT FLUID FLOW HOUSING COUPLE TO PARAMAGNETIC HOLLOW ALUMINIUM TUBING OPEN CLEARANCE BARING AN ELECTRICAL CIRCUIT CONTACT FLUID FLOW HOUSING ELECTROLYSIS ELECTROPHORESIS MAGNETOHYDROCHLORIC THERMALDYNAMICS FLUID ACCELERATOR (134A HFC) FLUID FLOW THERMAL HYPER HYSTERESIS VAPOR CYCLING ELECTRICAL CIRCUIT REFIGERATION LOW TEMPERATURES TUBILOID DESIGN WEARABLE EDS ORTHOSIS SHOE ELECTROMAGNETIC HYPER REPEL FLIGHT SHOES MANNED MACHINE BRACE SUBJECT NOT LIMITING TO ADDITIONAL SYSTEMS OR STRUCTURES POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON


WEARABLE ANTIMATTER GRAVITATIONAL SUPPRESSOR FREEDOM ARIEL DYNAMIC FLIGHT TRAVELING SHOES MANNED UAV BIOMECHATRONIC BRAINWAVES SWITCH CONTROLLED ELECTRICAL CIRCUIT ENERGY WINDING CAPTIVE HOUSING FLUIDIC FLOW VALVE TUBING DIAMAGNETIC COPPER EXHIBITS HOLLOW OPEN CLEARANCE BARING AN ELECTRICAL CIRCUIT CONTACT FLUID FLOW HOUSING ALONGSIDE THE AFOREMENTIONED SEGMENT FERROMAGÑETIC STAINLESS STEEL ELEMENT EXHIBITS AN HOLLOW OPEN CLEARANCE BARING AN ELECTRICAL CIRCUIT CONTACT FLUID FLOW HOUSING COUPLE TO PARAMAGNETIC HOLLOW ALUMINIUM TUBING OPEN CLEARANCE BARING AN ELECTRICAL CIRCUIT CONTACT FLUID FLOW HOUSING ELECTROLYSIS ELECTROPHORESIS MAGNETOHYDROCHLORIC THERMALDYNAMICS FLUID ACCELERATOR (134A HFC) FLUID FLOW THERMAL HYPER HYSTERESIS VAPOR CYCLING ELECTRICAL CIRCUIT REFIGERATION LOW TEMPERATURES TUBILOID DESIGN WEARABLE EDS ORTHOSIS SHOE ELECTROMAGNETIC HYPER REPEL FLIGHT SHOES MANNED MACHINE BRACE SUBJECT NOT LIMITING TO ADDITIONAL SYSTEMS OR STRUCTURES POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON

 


Tuesday, March 5, 2024

INVENTOR JERMAINE MORTON TWIN ARMATURE STRUCTURE DC/AC PULSE PHASE STACKED COPPER SHEET COUPLE TO STAINLESS STEEL COUPLE TO ALUMINUM SHEET EXHIBITS A VOLTAGE CAPACITOR EMBEDDED WITHIN THE INTERFACE LOCALLY NEAREST TO THE CENTRAL HOLLOW OPEN CLEARANCE OF THE STATOR ACTIVE ARMATURE SHAFT BALL BARING BRACKET FREEDOM OF ROTATION BRUSH CHANNEL ROTOR STATOR EDT INRUNNER CIRCULAR ROUND SPHERICAL TRANSDUCTOR STATOR BARING DIAMAGNETIC #15 AWG COPPER WIRE COUPLE TO STAINLESS STEEL WIRE ALONG WITH ALUMINUM WIRE TOGETHER SPUN TIGHTLY INTO A HELIX SHAPE WIRE 3,000TURNS COIL MODIFIED CURRENT CARRYING MODULATED ELECTRIC FLOW EMI PULSE 1/4TH OF ONE HERTZ WATTAGE PHASE WIRE INPUT ONE-WAY SINGLE PHASE VOLTAGE RECTIFING MOS- PELTIER EFFECT ULTRA CAPACITANCE ( FET) OUTPUT INDUCE VOLTAGE CHARGE TO THE ELECTRICAL ENERGY WINDING LINEAR SOLENOID CIRCUIT ACTUATOR IT'S STATOR EXHIBITS 60 HORNS ENUMERATING 180,000TURNS PER WHEEL TWIN WHEEL ENUMERATES 360,000TESLA'S FERROMAGNETIC VOLTAGE TRANSFORMER MODULATED CIRCUIT EMI HIGH FREQUENCY PULSE DC/AC OUTPUT INRUNNER STATOR HORN EXHIBITS NEODYMIUM PERMANENT MAGNET CENTRAL CORE OF QUARTZ ENERGY CELL CRYSTAL EDT 1tesla=11lbs 360,000tesla= 3,960,000lbs OF FORCE+MFD~ 10/4POWER DENSIFIED radiation 3,600,000,000gauss+ THE SPHERE IS DIVIDED INTO FOUR SEPARATE PARTS ALUMINUM BOTTOM AND COPPER TOP. 1-4TH OF A SPHERICAL BALL DIVIDED PARTS ARE DC/AC EMI HFP PHASE CURRENT CARRYING SHEET METALLIC TRANSDUCTOR SEPARATELY DIVIDED ROUND BALL INTO FOUR PARTS GOUND FOUNDATION OF THE SPHERE SUBJECT TO MANNED UAV AIRCRAFT DESIGN EXHIBITS A CORE BARING COUPLE TO THE BOTTOM SURFACES BASE ALUMINUM CURVE ONE HALF A DOME THE SECOND HALF IS SEPARATED OPPOSITE SIDES OF THE COCKPIT CONTRARY OF THE UPPER ELEMENT COPPER SHEET METAL SHAPE SPLIT DOME EXTERIOR EXHIBITS COPPER WIRE COUPLE TO STAINLESS STEEL WIRE , ALUMINUM WIRE ALL TOGETHER COUPLE TO THE SURFACES ALONGSIDE THE COCKPIT BARING COPPER 2,000COILS 3,000TURNS per COIL 3,000,000turns.12ft of awg wire =1tesla=11lbsx3,000,000teslas=33,000,000lbs DENSIFIED 30,000,000,000GAUSS Forces ARRANGED TO OVERLAY ONE HALF OF A CIRCULAR COIL WITHIN LINEAR LINKAGE WITHIN A CHAIN SOLENOID TYPE ACTUATOR THE STATOR EMITS IONS SYNCHRONOUS EDT SIGNALS A CHARGE INDUCTION CIRCUIT BETWEEN TWIN COMMON ELEMENTS COPPER SHEET ENCLOSURE EMITTER TOP AND ALUMINUM SHEET FOUNDATION EMITTER SURFACE BASE EMITS AGAINST THE STATOR HORN EMISSIONS AGAINST ITS COMMON ELEMENT EMISSIONS ARE POSITIVE CHARGE IONS VECTOR STRENGTHS FORCES AWAY ENCLOSURES FIXED BARING TRANSDUCTOR CENTRAL WITHIN BETWEEN ENCLOSURES ELECTRODYNAMICS PULSE PHASE EDT EDS FARADAY'S CAGE ENCLOSURES PULSE TRANSMISSION HARMONIC ESC AWAY FROM OPPOSING TRANSMISSION SOURCE FORCES AWAY BY THE PULSE DENSIFIED RADIATION REPEL FORCES OF AGAINST ENCLOSURES ENTIRELY LIFTING THE MANNED VEHICLE WEIGHT OF GRAVITY INTO THE AIR OR INERTIAL MASS SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON FOR EXAMPLE:144inches of AWG WIRE =12feet=1tesla=11lbs= 10,000gauss per 12ft of awg wire as for144inches of lengthy wire math 144inches×300,100=43,214,400lbs of DENSIFIED GAUSS force https://metalsphere.com/category/large-steel-balls/ 3500 mm = 11 feet and 5.8 inches Brass hollow ball Brass hollow ball https://youtu.be/THXY1hUEdnA?si=ARFzuasTconXYfe7

https://www.facebook.com/share/p/DDtSCLAyqCReDQNT/?mibextid=qi2Omg

MANNED UAV ROBOTIC LEGGED WALKING AIRCRAFT SS SUBMARINE
USES ACOUSTOPHORESIS ELECTROLYSIS ATMOSPHERIC PARTICLE COLLISION FRICTIONAL GRAVITATIONAL RADIATION PRESSURES ELECTROPHORESIS ANTIMATTER FALL AWAY TRAVELING WITHOUT FRICTIONAL RADIATION PRESSURES FORCES OF GRAVITY 

SOME AIRCRAFT USERS ARE TO BUSY GASSING IT UP
ME CONTRARY ON THE OTHER HAND

INTUITIVE INTELLIGENCE PROGRESSIVE DEVELOPMENT AERONAUTIC ENGINEERING AERODYNAMIC ARIEL TRAVELING MANNED AI ROBOTICS FLIGHTS MACHINE MANNED UAV SS DEEP-SEA TRAVELING DIVING UNDERWATER SUBMARINE MANNED ROAD TRAVELING ROBOTIC LEGGED WALKING MOBILITY MACHINE MANNED SPHERE CENTRAL COCKPIT CORE CONTROLS NLP UAV SS SUBMARINE MOBILITY ROAD TRAVELING MACHINE DESIGN ELECTRICAL SYSTEM ENCLOSURES FUNCTIONS AS AN TRANSDUCTOR VOLTAGE RECTIFING TRANSISTOR ELECTROMAGNETIC SEMI- CONDUCTIVE VOLTAGE TRANSFORMER AC EDT EMI MOS- FERROMAGNETIZED (FET) TRANSDUCER TRANSONIC OSCILLATING TRANSMITTER ELECTRODYNAMICS RADIATION PRESSURES ATMOSPHERIC MATTER ELECTROLYSIS LONGITUDINAL GAUSS 1,000,000,000ALPHA PARTICLE DECAY GAUSS 1,000,000,000BETA PARTICLE DECAY GAUSS 1,000,000,000GAMMA PARTICLE DECAY LONGITUDINAL RADIATION PRESSURES FORCES COLLISION ATMOSPHERIC PARTICLE DECAY SUSPENSION AWAY FROM THE SOURCE OF TRANSMISSION ATMOSPHERIC PARTICLE BETWEEN THE MEDIUM RISE ATMOSPHERIC MATTER WITHIN NEWTON LAWS ATMOSPHERIC MATTER WITHIN FARADAY'S ELECTROCHEMISTRY ATMOSPHERIC PARTICLE WITHIN BOYLE'S LAW ATMOSPHERIC MATTER WITHIN CHARLES LAW ATMOSPHERIC PARTICLE ATOMIC RADIATION COLLISION SUPPRESSOR AGAINST ATMOSPHERIC GRAVITATIONAL PRESSURES ARE FRICTIONAL PARTICLE RADIATION FORCES OF GRAVITY ARE REPELLED BY ACTIVE ENCLOSURES PHASES AGAINST ATMOSPHERIC MATTER SUPPRESSOR ELECTROPHORESIS SPHERICAL METALLOID ENCLOSURES ACTING TRANSMITTER ENCLOSURES ELECTRICAL MULTIPLE FUNCTIONAL CIRCUITRY 
ACOUSTOPHORESIS ELECTROLYSIS ATMOSPHERIC PARTICLE COLLISION AGAINST FRICTIONAL GRAVITATIONAL RADIATION SUPPRESSION REDUCTION BY ATMOSPHERIC MATTER ELECTROPHORESIS A VEHICLE ENCLOSURES EMITS MICROWAVE RADIATION COLLISIONS AGAINST POSITIVE COMMON NEWTRON NUCLEI NUCLEUS ESC AWAY FROM COMMON POSITIVE IONIC RADIATION PRESSURES SPHERE VEHICLE ENCLOSURES ACTIVE EMITTER ACTIVE ANTIMATTER ENCLOSURES FREEDOM FALL INTO THE AIR AWAY FROM THE EARTHS SURFACES WHILE THE PLANET EARTH FALLS WITHIN SPACE LAWS OF ASTROPHYSICS DYNAMICS SCIENTIFICALLY EJECTS THE AIRCRAFT OUTER SPACE AIRCRAFT ANTIMATTER FREEDOM ARIEL DYNAMIC TRAVELING COMMON POSITIVE PARAMAGNETIC EMISSIONS REPELS COMMON ATMOSPHERIC SODIUM CALORIC NEWTRON NUCLEI NUCLEUS LIQUID FILLED ENCLOSURES WITHIN ATMOSPHERIC ENVIRONMENT COMMON POSITIVE PARTICLE ESC FROM AIRCRAFT ENCLOSURES SURFACES REPELS MATTER AWAY FROM VECTOR FIELD OR PROXIMITY FIELD FRACTION OF AREA AIRCRAFT ENCLOSURES ANTIMATTER FREEDOM FROM ATMOSPHERIC SODIUM CHLORIDE NEWTRON NUCLEI NUCLEUS LIQUID FILLED PARTICLE WITHIN SPACE ESC VECTOR OR PROXIMITY FIELD OF SOURCE OF TRANSMISSION RADIATION SUPPRESSION OF MAGNETO GRAVITATIONAL PARTICLE RADIATION VECTOR BEAM PROXIMITY BEAM NEWTRON NUCLEI NUCLEUS PARTICLE FRICTIONAL GRAVITATIONAL HOLD SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON

INTUITIVE INTELLIGENCE PROGRESSIVE DEVELOPMENT AERONAUTIC ENGINEERING AERODYNAMIC ARIEL TRAVELING MANNED AI ROBOTICS FLIGHTS MACHINE MANNED UAV SS DEEP-SEA TRAVELING DIVING UNDERWATER SUBMARINE MANNED ROAD TRAVELING ROBOTIC LEGGED WALKING MOBILITY MACHINE MANNED SPHERE CENTRAL COCKPIT CORE CONTROLS NLP UAV SS SUBMARINE MOBILITY ROAD TRAVELING MACHINE DESIGN ELECTRICAL SYSTEM ENCLOSURES FUNCTIONS AS AN TRANSDUCTOR VOLTAGE RECTIFING TRANSISTOR ELECTROMAGNETIC SEMI- CONDUCTIVE VOLTAGE TRANSFORMER AC EDT EMI MOS- FERROMAGNETIZED (FET) TRANSDUCER TRANSONIC OSCILLATING TRANSMITTER ELECTRODYNAMICS RADIATION PRESSURES ATMOSPHERIC MATTER ELECTROLYSIS LONGITUDINAL GAUSS 1,000,000,000ALPHA PARTICLE DECAY GAUSS 1,000,000,000BETA PARTICLE DECAY GAUSS 1,000,000,000GAMMA PARTICLE DECAY LONGITUDINAL RADIATION PRESSURES FORCES COLLISION ATMOSPHERIC PARTICLE DECAY SUSPENSION AWAY FROM THE SOURCE OF TRANSMISSION ATMOSPHERIC PARTICLE BETWEEN THE MEDIUM RISE ATMOSPHERIC MATTER WITHIN NEWTON LAWS ATMOSPHERIC MATTER WITHIN FARADAY'S ELECTROCHEMISTRY ATMOSPHERIC PARTICLE WITHIN BOYLE'S LAW ATMOSPHERIC MATTER WITHIN CHARLES LAW ATMOSPHERIC PARTICLE ATOMIC RADIATION COLLISION SUPPRESSOR AGAINST ATMOSPHERIC GRAVITATIONAL PRESSURES ARE FRICTIONAL PARTICLE RADIATION FORCES OF GRAVITY ARE REPELLED BY ACTIVE ENCLOSURES PHASES AGAINST ATMOSPHERIC MATTER SUPPRESSOR ELECTROPHORESIS SPHERICAL METALLOID ENCLOSURES ACTING TRANSMITTER ENCLOSURES ELECTRICAL MULTIPLE FUNCTIONAL CIRCUITRY 
ACOUSTOPHORESIS ELECTROLYSIS ATMOSPHERIC PARTICLE COLLISION AGAINST FRICTIONAL GRAVITATIONAL RADIATION SUPPRESSION REDUCTION BY ATMOSPHERIC MATTER ELECTROPHORESIS A VEHICLE ENCLOSURES EMITS MICROWAVE RADIATION COLLISIONS AGAINST POSITIVE COMMON NEWTRON NUCLEI NUCLEUS ESC AWAY FROM SPHERE VEHICLE ENCLOSURES ACTIVE ANTIMATTER FREEDOM FALL INTO THE AIR AWAY FROM THE EARTHS SURFACES WHILE THE PLANET EARTH FALLS WITHIN SPACE EJECTS THE AIRCRAFT OUTER SPACE ANTIMATTER ARIEL DYNAMIC TRAVELING WITHOUT ATMOSPHERIC MATTER COLLISION CAUSES FRICTIONAL RADIATION GRAVITATIONAL PRESSURES FORCES OF GRAVITY SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON




SOME AIRCRAFT USERS ARE TO BUSY GASSING IT UP
ME CONTRARY ON THE OTHER HAND

INTUITIVE INTELLIGENCE PROGRESSIVE DEVELOPMENT AERONAUTIC ENGINEERING AERODYNAMIC ARIEL TRAVELING MANNED AI ROBOTICS FLIGHTS MACHINE MANNED UAV SS DEEP-SEA TRAVELING DIVING UNDERWATER SUBMARINE MANNED ROAD TRAVELING ROBOTIC LEGGED WALKING MOBILITY MACHINE MANNED SPHERE CENTRAL COCKPIT CORE CONTROLS NLP UAV SS SUBMARINE MOBILITY ROAD TRAVELING MACHINE DESIGN ELECTRICAL SYSTEM ENCLOSURES FUNCTIONS AS AN TRANSDUCTOR VOLTAGE RECTIFING TRANSISTOR ELECTROMAGNETIC SEMI- CONDUCTIVE VOLTAGE TRANSFORMER AC EDT EMI MOS- FERROMAGNETIZED (FET) TRANSDUCER TRANSONIC OSCILLATING TRANSMITTER ELECTRODYNAMICS RADIATION PRESSURES ATMOSPHERIC MATTER ELECTROLYSIS LONGITUDINAL GAUSS 1,000,000,000ALPHA PARTICLE DECAY GAUSS 1,000,000,000BETA PARTICLE DECAY GAUSS 1,000,000,000GAMMA PARTICLE DECAY LONGITUDINAL RADIATION PRESSURES FORCES COLLISION ATMOSPHERIC PARTICLE DECAY SUSPENSION AWAY FROM THE SOURCE OF TRANSMISSION ATMOSPHERIC PARTICLE BETWEEN THE MEDIUM RISE ATMOSPHERIC MATTER WITHIN NEWTON LAWS ATMOSPHERIC MATTER WITHIN FARADAY'S ELECTROCHEMISTRY ATMOSPHERIC PARTICLE WITHIN BOYLE'S LAW ATMOSPHERIC MATTER WITHIN CHARLES LAW ATMOSPHERIC PARTICLE ATOMIC RADIATION COLLISION SUPPRESSOR AGAINST ATMOSPHERIC GRAVITATIONAL PRESSURES ARE FRICTIONAL PARTICLE RADIATION FORCES OF GRAVITY ARE REPELLED BY ACTIVE ENCLOSURES PHASES AGAINST ATMOSPHERIC MATTER SUPPRESSOR ELECTROPHORESIS SPHERICAL METALLOID ENCLOSURES ACTING TRANSMITTER ENCLOSURES ELECTRICAL MULTIPLE FUNCTIONAL CIRCUITRY 
ACOUSTOPHORESIS ELECTROLYSIS ATMOSPHERIC PARTICLE COLLISION AGAINST FRICTIONAL GRAVITATIONAL RADIATION SUPPRESSION REDUCTION BY ATMOSPHERIC MATTER ELECTROPHORESIS A VEHICLE ENCLOSURES EMITS MICROWAVE RADIATION COLLISIONS AGAINST POSITIVE COMMON NEWTRON NUCLEI NUCLEUS ESC AWAY FROM COMMON POSITIVE IONIC RADIATION PRESSURES SPHERE VEHICLE ENCLOSURES ACTIVE EMITTER ACTIVE ANTIMATTER ENCLOSURES FREEDOM FALL INTO THE AIR AWAY FROM THE EARTHS SURFACES WHILE THE PLANET EARTH FALLS WITHIN SPACE LAWS OF ASTROPHYSICS DYNAMICS SCIENTIFICALLY EJECTS THE AIRCRAFT OUTER SPACE AIRCRAFT ANTIMATTER FREEDOM ARIEL DYNAMIC TRAVELING COMMON POSITIVE PARAMAGNETIC EMISSIONS REPELS COMMON ATMOSPHERIC SODIUM CALORIC NEWTRON NUCLEI NUCLEUS LIQUID FILLED ENCLOSURES WITHIN ATMOSPHERIC ENVIRONMENT COMMON POSITIVE PARTICLE ESC FROM AIRCRAFT ENCLOSURES SURFACES REPELS MATTER AWAY FROM VECTOR FIELD OR PROXIMITY FIELD FRACTION OF AREA AIRCRAFT ENCLOSURES ANTIMATTER FREEDOM FROM ATMOSPHERIC SODIUM CHLORIDE NEWTRON NUCLEI NUCLEUS LIQUID FILLED PARTICLE WITHIN SPACE ESC VECTOR OR PROXIMITY FIELD OF SOURCE OF TRANSMISSION RADIATION SUPPRESSION OF MAGNETO GRAVITATIONAL PARTICLE RADIATION VECTOR BEAM PROXIMITY BEAM NEWTRON NUCLEI NUCLEUS PARTICLE FRICTIONAL GRAVITATIONAL HOLD SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON

SOME AIRCRAFT USERS ARE TO BUSY GASSING IT UP
ME CONTRARY ON THE OTHER HAND

INTUITIVE INTELLIGENCE PROGRESSIVE DEVELOPMENT AERONAUTIC ENGINEERING AERODYNAMIC ARIEL TRAVELING MANNED AI ROBOTICS FLIGHTS MACHINE MANNED UAV SS DEEP-SEA TRAVELING DIVING UNDERWATER SUBMARINE MANNED ROAD TRAVELING ROBOTIC LEGGED WALKING MOBILITY MACHINE MANNED SPHERE CENTRAL COCKPIT CORE CONTROLS NLP UAV SS SUBMARINE MOBILITY ROAD TRAVELING MACHINE DESIGN ELECTRICAL SYSTEM ENCLOSURES FUNCTIONS AS AN TRANSDUCTOR VOLTAGE RECTIFING TRANSISTOR ELECTROMAGNETIC SEMI- CONDUCTIVE VOLTAGE TRANSFORMER AC EDT EMI MOS- FERROMAGNETIZED (FET) TRANSDUCER TRANSONIC OSCILLATING TRANSMITTER ELECTRODYNAMICS RADIATION PRESSURES ATMOSPHERIC MATTER ELECTROLYSIS LONGITUDINAL GAUSS 1,000,000,000ALPHA PARTICLE DECAY GAUSS 1,000,000,000BETA PARTICLE DECAY GAUSS 1,000,000,000GAMMA PARTICLE DECAY LONGITUDINAL RADIATION PRESSURES FORCES COLLISION ATMOSPHERIC PARTICLE DECAY SUSPENSION AWAY FROM THE SOURCE OF TRANSMISSION ATMOSPHERIC PARTICLE BETWEEN THE MEDIUM RISE ATMOSPHERIC MATTER WITHIN NEWTON LAWS ATMOSPHERIC MATTER WITHIN FARADAY'S ELECTROCHEMISTRY ATMOSPHERIC PARTICLE WITHIN BOYLE'S LAW ATMOSPHERIC MATTER WITHIN CHARLES LAW ATMOSPHERIC PARTICLE ATOMIC RADIATION COLLISION SUPPRESSOR AGAINST ATMOSPHERIC GRAVITATIONAL PRESSURES ARE FRICTIONAL PARTICLE RADIATION FORCES OF GRAVITY ARE REPELLED BY ACTIVE ENCLOSURES PHASES AGAINST ATMOSPHERIC MATTER SUPPRESSOR ELECTROPHORESIS SPHERICAL METALLOID ENCLOSURES ACTING TRANSMITTER ENCLOSURES ELECTRICAL MULTIPLE FUNCTIONAL CIRCUITRY 
ACOUSTOPHORESIS ELECTROLYSIS ATMOSPHERIC PARTICLE COLLISION AGAINST FRICTIONAL GRAVITATIONAL RADIATION SUPPRESSION REDUCTION BY ATMOSPHERIC MATTER ELECTROPHORESIS A VEHICLE ENCLOSURES EMITS MICROWAVE RADIATION COLLISIONS AGAINST POSITIVE COMMON NEWTRON NUCLEI NUCLEUS ESC AWAY FROM COMMON POSITIVE IONIC RADIATION PRESSURES SPHERE VEHICLE ENCLOSURES ACTIVE EMITTER ACTIVE ANTIMATTER ENCLOSURES FREEDOM FALL INTO THE AIR AWAY FROM THE EARTHS SURFACES WHILE THE PLANET EARTH FALLS WITHIN SPACE LAWS OF ASTROPHYSICS DYNAMICS SCIENTIFICALLY EJECTS THE AIRCRAFT OUTER SPACE AIRCRAFT ANTIMATTER FREEDOM ARIEL DYNAMIC TRAVELING COMMON POSITIVE PARAMAGNETIC EMISSIONS REPELS COMMON ATMOSPHERIC SODIUM CALORIC NEWTRON NUCLEI NUCLEUS LIQUID FILLED ENCLOSURES WITHIN ATMOSPHERIC ENVIRONMENT COMMON POSITIVE PARTICLE ESC FROM AIRCRAFT ENCLOSURES SURFACES REPELS MATTER AWAY FROM VECTOR FIELD OR PROXIMITY FIELD FRACTION OF AREA AIRCRAFT ENCLOSURES ANTIMATTER FREEDOM FROM ATMOSPHERIC SODIUM CHLORIDE NEWTRON NUCLEI NUCLEUS LIQUID FILLED PARTICLE WITHIN SPACE ESC VECTOR OR PROXIMITY FIELD OF SOURCE OF TRANSMISSION RADIATION SUPPRESSION OF MAGNETO GRAVITATIONAL PARTICLE RADIATION VECTOR BEAM PROXIMITY BEAM NEWTRON NUCLEI NUCLEUS PARTICLE FRICTIONAL GRAVITATIONAL HOLD SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON

SOME AIRCRAFT USERS ARE TO BUSY GASSING IT UP
ME CONTRARY ON THE OTHER HAND

INTUITIVE INTELLIGENCE PROGRESSIVE DEVELOPMENT AERONAUTIC ENGINEERING AERODYNAMIC ARIEL TRAVELING MANNED AI ROBOTICS FLIGHTS MACHINE MANNED UAV SS DEEP-SEA TRAVELING DIVING UNDERWATER SUBMARINE MANNED ROAD TRAVELING ROBOTIC LEGGED WALKING MOBILITY MACHINE MANNED SPHERE CENTRAL COCKPIT CORE CONTROLS NLP UAV SS SUBMARINE MOBILITY ROAD TRAVELING MACHINE DESIGN ELECTRICAL SYSTEM ENCLOSURES FUNCTIONS AS AN TRANSDUCTOR VOLTAGE RECTIFING TRANSISTOR ELECTROMAGNETIC SEMI- CONDUCTIVE VOLTAGE TRANSFORMER AC EDT EMI MOS- FERROMAGNETIZED (FET) TRANSDUCER TRANSONIC OSCILLATING TRANSMITTER ELECTRODYNAMICS RADIATION PRESSURES ATMOSPHERIC MATTER ELECTROLYSIS LONGITUDINAL GAUSS 1,000,000,000ALPHA PARTICLE DECAY GAUSS 1,000,000,000BETA PARTICLE DECAY GAUSS 1,000,000,000GAMMA PARTICLE DECAY LONGITUDINAL RADIATION PRESSURES FORCES COLLISION ATMOSPHERIC PARTICLE DECAY SUSPENSION AWAY FROM THE SOURCE OF TRANSMISSION ATMOSPHERIC PARTICLE BETWEEN THE MEDIUM RISE ATMOSPHERIC MATTER WITHIN NEWTON LAWS ATMOSPHERIC MATTER WITHIN FARADAY'S ELECTROCHEMISTRY ATMOSPHERIC PARTICLE WITHIN BOYLE'S LAW ATMOSPHERIC MATTER WITHIN CHARLES LAW ATMOSPHERIC PARTICLE ATOMIC RADIATION COLLISION SUPPRESSOR AGAINST ATMOSPHERIC GRAVITATIONAL PRESSURES ARE FRICTIONAL PARTICLE RADIATION FORCES OF GRAVITY ARE REPELLED BY ACTIVE ENCLOSURES PHASES AGAINST ATMOSPHERIC MATTER SUPPRESSOR ELECTROPHORESIS SPHERICAL METALLOID ENCLOSURES ACTING TRANSMITTER ENCLOSURES ELECTRICAL MULTIPLE FUNCTIONAL CIRCUITRY 
ACOUSTOPHORESIS ELECTROLYSIS ATMOSPHERIC PARTICLE COLLISION AGAINST FRICTIONAL GRAVITATIONAL RADIATION SUPPRESSION REDUCTION BY ATMOSPHERIC MATTER ELECTROPHORESIS A VEHICLE ENCLOSURES EMITS MICROWAVE RADIATION COLLISIONS AGAINST POSITIVE COMMON NEWTRON NUCLEI NUCLEUS ESC AWAY FROM COMMON POSITIVE IONIC RADIATION PRESSURES SPHERE VEHICLE ENCLOSURES ACTIVE EMITTER ACTIVE ANTIMATTER ENCLOSURES FREEDOM FALL INTO THE AIR AWAY FROM THE EARTHS SURFACES WHILE THE PLANET EARTH FALLS WITHIN SPACE LAWS OF ASTROPHYSICS DYNAMICS SCIENTIFICALLY EJECTS THE AIRCRAFT OUTER SPACE AIRCRAFT ANTIMATTER FREEDOM ARIEL DYNAMIC TRAVELING COMMON POSITIVE PARAMAGNETIC EMISSIONS REPELS COMMON ATMOSPHERIC SODIUM CALORIC NEWTRON NUCLEI NUCLEUS LIQUID FILLED ENCLOSURES WITHIN ATMOSPHERIC ENVIRONMENT COMMON POSITIVE PARTICLE ESC FROM AIRCRAFT ENCLOSURES SURFACES REPELS MATTER AWAY FROM VECTOR FIELD OR PROXIMITY FIELD FRACTION OF AREA AIRCRAFT ENCLOSURES ANTIMATTER FREEDOM FROM ATMOSPHERIC SODIUM CHLORIDE NEWTRON NUCLEI NUCLEUS LIQUID FILLED PARTICLE WITHIN SPACE ESC VECTOR OR PROXIMITY FIELD OF SOURCE OF TRANSMISSION RADIATION SUPPRESSION OF MAGNETO GRAVITATIONAL PARTICLE RADIATION VECTOR BEAM PROXIMITY BEAM NEWTRON NUCLEI NUCLEUS PARTICLE FRICTIONAL GRAVITATIONAL HOLD SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON









No









INTUITIVE INTELLIGENCE PROGRESSIVE DEVELOPMENT AERONAUTIC ENGINEERING AERODYNAMIC ARIEL TRAVELING MANNED AI ROBOTICS FLIGHTS MACHINE MANNED UAV SS DEEP-SEA TRAVELING DIVING UNDERWATER SUBMARINE MANNED ROAD TRAVELING ROBOTIC LEGGED WALKING MOBILITY MACHINE MANNED SPHERE CENTRAL COCKPIT CORE CONTROLS NLP UAV SS SUBMARINE MOBILITY ROAD TRAVELING MACHINE DESIGN ELECTRICAL SYSTEM ENCLOSURES FUNCTIONS AS AN TRANSDUCTOR VOLTAGE RECTIFING TRANSISTOR ELECTROMAGNETIC SEMI- CONDUCTIVE VOLTAGE TRANSFORMER AC EDT EMI MOS- FERROMAGNETIZED (FET) TRANSDUCER TRANSONIC OSCILLATING TRANSMITTER ELECTRODYNAMICS RADIATION PRESSURES ATMOSPHERIC MATTER ELECTROLYSIS LONGITUDINAL GAUSS 1,000,000,000ALPHA PARTICLE DECAY GAUSS 1,000,000,000BETA PARTICLE DECAY GAUSS 1,000,000,000GAMMA PARTICLE DECAY LONGITUDINAL RADIATION PRESSURES FORCES COLLISION ATMOSPHERIC PARTICLE DECAY SUSPENSION AWAY FROM THE SOURCE OF TRANSMISSION ATMOSPHERIC PARTICLE BETWEEN THE MEDIUM RISE ATMOSPHERIC MATTER WITHIN NEWTON LAWS ATMOSPHERIC MATTER WITHIN FARADAY'S ELECTROCHEMISTRY ATMOSPHERIC PARTICLE WITHIN BOYLE'S LAW ATMOSPHERIC MATTER WITHIN CHARLES LAW ATMOSPHERIC PARTICLE ATOMIC RADIATION COLLISION SUPPRESSOR AGAINST ATMOSPHERIC GRAVITATIONAL PRESSURES ARE FRICTIONAL PARTICLE RADIATION FORCES OF GRAVITY ARE REPELLED BY ACTIVE ENCLOSURES PHASES AGAINST ATMOSPHERIC MATTER SUPPRESSOR ELECTROPHORESIS SPHERICAL METALLOID ENCLOSURES ACTING TRANSMITTER ENCLOSURES ELECTRICAL MULTIPLE FUNCTIONAL CIRCUITRY 
ACOUSTOPHORESIS ELECTROLYSIS ATMOSPHERIC PARTICLE COLLISION AGAINST FRICTIONAL GRAVITATIONAL RADIATION SUPPRESSION REDUCTION BY ATMOSPHERIC MATTER ELECTROPHORESIS A VEHICLE ENCLOSURES EMITS MICROWAVE RADIATION COLLISIONS AGAINST POSITIVE COMMON NEWTRON NUCLEI NUCLEUS ESC AWAY FROM SPHERE VEHICLE ENCLOSURES ACTIVE ANTIMATTER FREEDOM FALL INTO THE AIR AWAY FROM THE EARTHS SURFACES WHILE THE PLANET EARTH FALLS WITHIN SPACE EJECTS THE AIRCRAFT OUTER SPACE ANTIMATTER ARIEL DYNAMIC TRAVELING WITHOUT ATMOSPHERIC MATTER COLLISION CAUSES FRICTIONAL RADIATION GRAVITATIONAL PRESSURES FORCES OF GRAVITY SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON



INTUITIVE INTELLIGENCE PROGRESSIVE DEVELOPMENT AERONAUTIC ENGINEERING AERODYNAMIC ARIEL TRAVELING MANNED AI ROBOTICS FLIGHTS MACHINE MANNED UAV SS DEEP-SEA TRAVELING DIVING UNDERWATER SUBMARINE MANNED ROAD TRAVELING ROBOTIC LEGGED WALKING MOBILITY MACHINE MANNED SPHERE CENTRAL COCKPIT CORE CONTROLS NLP UAV SS SUBMARINE MOBILITY ROAD TRAVELING MACHINE DESIGN ELECTRICAL SYSTEM ENCLOSURES FUNCTIONS AS AN TRANSDUCTOR VOLTAGE RECTIFING TRANSISTOR ELECTROMAGNETIC SEMI- CONDUCTIVE VOLTAGE TRANSFORMER AC EDT EMI MOS- FERROMAGNETIZED (FET) TRANSDUCER TRANSONIC OSCILLATING TRANSMITTER ELECTRODYNAMICS RADIATION PRESSURES ATMOSPHERIC MATTER ELECTROLYSIS LONGITUDINAL GAUSS 1,000,000,000ALPHA PARTICLE DECAY GAUSS 1,000,000,000BETA PARTICLE DECAY GAUSS 1,000,000,000GAMMA PARTICLE DECAY LONGITUDINAL RADIATION PRESSURES FORCES COLLISION ATMOSPHERIC PARTICLE DECAY SUSPENSION AWAY FROM THE SOURCE OF TRANSMISSION ATMOSPHERIC PARTICLE BETWEEN THE MEDIUM RISE ATMOSPHERIC MATTER WITHIN NEWTON LAWS ATMOSPHERIC MATTER WITHIN FARADAY'S ELECTROCHEMISTRY ATMOSPHERIC PARTICLE WITHIN BOYLE'S LAW ATMOSPHERIC MATTER WITHIN CHARLES LAW ATMOSPHERIC PARTICLE ATOMIC RADIATION COLLISION SUPPRESSOR AGAINST ATMOSPHERIC GRAVITATIONAL PRESSURES ARE FRICTIONAL PARTICLE RADIATION FORCES OF GRAVITY ARE REPELLED BY ACTIVE ENCLOSURES PHASES AGAINST ATMOSPHERIC MATTER SUPPRESSOR ELECTROPHORESIS SPHERICAL METALLOID ENCLOSURES ACTING TRANSMITTER ENCLOSURES ELECTRICAL MULTIPLE FUNCTIONAL CIRCUITRY 
ACOUSTOPHORESIS ELECTROLYSIS ATMOSPHERIC PARTICLE COLLISION AGAINST FRICTIONAL GRAVITATIONAL RADIATION SUPPRESSION REDUCTION BY ATMOSPHERIC MATTER ELECTROPHORESIS A VEHICLE ENCLOSURES EMITS MICROWAVE RADIATION COLLISIONS AGAINST POSITIVE COMMON NEWTRON NUCLEI NUCLEUS ESC AWAY FROM SPHERE VEHICLE ENCLOSURES ACTIVE ANTIMATTER FREEDOM FALL INTO THE AIR AWAY FROM THE EARTHS SURFACES WHILE THE PLANET EARTH FALLS WITHIN SPACE EJECTS THE AIRCRAFT OUTER SPACE ANTIMATTER ARIEL DYNAMIC TRAVELING WITHOUT ATMOSPHERIC MATTER COLLISION CAUSES FRICTIONAL RADIATION GRAVITATIONAL PRESSURES FORCES OF GRAVITY SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON

 

SOME AIRCRAFT USERS ARE TO BUSY GASSING IT UP
ME CONTRARY ON THE OTHER HAND

INTUITIVE INTELLIGENCE PROGRESSIVE DEVELOPMENT AERONAUTIC ENGINEERING AERODYNAMIC ARIEL TRAVELING MANNED AI ROBOTICS FLIGHTS MACHINE MANNED UAV SS DEEP-SEA TRAVELING DIVING UNDERWATER SUBMARINE MANNED ROAD TRAVELING ROBOTIC LEGGED WALKING MOBILITY MACHINE MANNED SPHERE CENTRAL COCKPIT CORE CONTROLS NLP UAV SS SUBMARINE MOBILITY ROAD TRAVELING MACHINE DESIGN ELECTRICAL SYSTEM ENCLOSURES FUNCTIONS AS AN TRANSDUCTOR VOLTAGE RECTIFING TRANSISTOR ELECTROMAGNETIC SEMI- CONDUCTIVE VOLTAGE TRANSFORMER AC EDT EMI MOS- FERROMAGNETIZED (FET) TRANSDUCER TRANSONIC OSCILLATING TRANSMITTER ELECTRODYNAMICS RADIATION PRESSURES ATMOSPHERIC MATTER ELECTROLYSIS LONGITUDINAL GAUSS 1,000,000,000ALPHA PARTICLE DECAY GAUSS 1,000,000,000BETA PARTICLE DECAY GAUSS 1,000,000,000GAMMA PARTICLE DECAY LONGITUDINAL RADIATION PRESSURES FORCES COLLISION ATMOSPHERIC PARTICLE DECAY SUSPENSION AWAY FROM THE SOURCE OF TRANSMISSION ATMOSPHERIC PARTICLE BETWEEN THE MEDIUM RISE ATMOSPHERIC MATTER WITHIN NEWTON LAWS ATMOSPHERIC MATTER WITHIN FARADAY'S ELECTROCHEMISTRY ATMOSPHERIC PARTICLE WITHIN BOYLE'S LAW ATMOSPHERIC MATTER WITHIN CHARLES LAW ATMOSPHERIC PARTICLE ATOMIC RADIATION COLLISION SUPPRESSOR AGAINST ATMOSPHERIC GRAVITATIONAL PRESSURES ARE FRICTIONAL PARTICLE RADIATION FORCES OF GRAVITY ARE REPELLED BY ACTIVE ENCLOSURES PHASES AGAINST ATMOSPHERIC MATTER SUPPRESSOR ELECTROPHORESIS SPHERICAL METALLOID ENCLOSURES ACTING TRANSMITTER ENCLOSURES ELECTRICAL MULTIPLE FUNCTIONAL CIRCUITRY 
ACOUSTOPHORESIS ELECTROLYSIS ATMOSPHERIC PARTICLE COLLISION AGAINST FRICTIONAL GRAVITATIONAL RADIATION SUPPRESSION REDUCTION BY ATMOSPHERIC MATTER ELECTROPHORESIS A VEHICLE ENCLOSURES EMITS MICROWAVE RADIATION COLLISIONS AGAINST POSITIVE COMMON NEWTRON NUCLEI NUCLEUS ESC AWAY FROM COMMON POSITIVE IONIC RADIATION PRESSURES SPHERE VEHICLE ENCLOSURES ACTIVE EMITTER ACTIVE ANTIMATTER ENCLOSURES FREEDOM FALL INTO THE AIR AWAY FROM THE EARTHS SURFACES WHILE THE PLANET EARTH FALLS WITHIN SPACE LAWS OF ASTROPHYSICS DYNAMICS SCIENTIFICALLY EJECTS THE AIRCRAFT OUTER SPACE AIRCRAFT ANTIMATTER FREEDOM ARIEL DYNAMIC TRAVELING COMMON POSITIVE PARAMAGNETIC EMISSIONS REPELS COMMON ATMOSPHERIC SODIUM CALORIC NEWTRON NUCLEI NUCLEUS LIQUID FILLED ENCLOSURES WITHIN ATMOSPHERIC ENVIRONMENT COMMON POSITIVE PARTICLE ESC FROM AIRCRAFT ENCLOSURES SURFACES REPELS MATTER AWAY FROM VECTOR FIELD OR PROXIMITY FIELD FRACTION OF AREA AIRCRAFT ENCLOSURES ANTIMATTER FREEDOM FROM ATMOSPHERIC SODIUM CHLORIDE NEWTRON NUCLEI NUCLEUS LIQUID FILLED PARTICLE WITHIN SPACE ESC VECTOR OR PROXIMITY FIELD OF SOURCE OF TRANSMISSION RADIATION SUPPRESSION OF MAGNETO GRAVITATIONAL PARTICLE RADIATION VECTOR BEAM PROXIMITY BEAM NEWTRON NUCLEI NUCLEUS PARTICLE FRICTIONAL GRAVITATIONAL HOLD SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON


SOME AIRCRAFT USERS ARE TO BUSY GASSING IT UP
ME CONTRARY ON THE OTHER HAND

INTUITIVE INTELLIGENCE PROGRESSIVE DEVELOPMENT AERONAUTIC ENGINEERING AERODYNAMIC ARIEL TRAVELING MANNED AI ROBOTICS FLIGHTS MACHINE MANNED UAV SS DEEP-SEA TRAVELING DIVING UNDERWATER SUBMARINE MANNED ROAD TRAVELING ROBOTIC LEGGED WALKING MOBILITY MACHINE MANNED SPHERE CENTRAL COCKPIT CORE CONTROLS NLP UAV SS SUBMARINE MOBILITY ROAD TRAVELING MACHINE DESIGN ELECTRICAL SYSTEM ENCLOSURES FUNCTIONS AS AN TRANSDUCTOR VOLTAGE RECTIFING TRANSISTOR ELECTROMAGNETIC SEMI- CONDUCTIVE VOLTAGE TRANSFORMER AC EDT EMI MOS- FERROMAGNETIZED (FET) TRANSDUCER TRANSONIC OSCILLATING TRANSMITTER ELECTRODYNAMICS RADIATION PRESSURES ATMOSPHERIC MATTER ELECTROLYSIS LONGITUDINAL GAUSS 1,000,000,000ALPHA PARTICLE DECAY GAUSS 1,000,000,000BETA PARTICLE DECAY GAUSS 1,000,000,000GAMMA PARTICLE DECAY LONGITUDINAL RADIATION PRESSURES FORCES COLLISION ATMOSPHERIC PARTICLE DECAY SUSPENSION AWAY FROM THE SOURCE OF TRANSMISSION ATMOSPHERIC PARTICLE BETWEEN THE MEDIUM RISE ATMOSPHERIC MATTER WITHIN NEWTON LAWS ATMOSPHERIC MATTER WITHIN FARADAY'S ELECTROCHEMISTRY ATMOSPHERIC PARTICLE WITHIN BOYLE'S LAW ATMOSPHERIC MATTER WITHIN CHARLES LAW ATMOSPHERIC PARTICLE ATOMIC RADIATION COLLISION SUPPRESSOR AGAINST ATMOSPHERIC GRAVITATIONAL PRESSURES ARE FRICTIONAL PARTICLE RADIATION FORCES OF GRAVITY ARE REPELLED BY ACTIVE ENCLOSURES PHASES AGAINST ATMOSPHERIC MATTER SUPPRESSOR ELECTROPHORESIS SPHERICAL METALLOID ENCLOSURES ACTING TRANSMITTER ENCLOSURES ELECTRICAL MULTIPLE FUNCTIONAL CIRCUITRY 
ACOUSTOPHORESIS ELECTROLYSIS ATMOSPHERIC PARTICLE COLLISION AGAINST FRICTIONAL GRAVITATIONAL RADIATION SUPPRESSION REDUCTION BY ATMOSPHERIC MATTER ELECTROPHORESIS A VEHICLE ENCLOSURES EMITS MICROWAVE RADIATION COLLISIONS AGAINST POSITIVE COMMON NEWTRON NUCLEI NUCLEUS ESC AWAY FROM COMMON POSITIVE IONIC RADIATION PRESSURES SPHERE VEHICLE ENCLOSURES ACTIVE EMITTER ACTIVE ANTIMATTER ENCLOSURES FREEDOM FALL INTO THE AIR AWAY FROM THE EARTHS SURFACES WHILE THE PLANET EARTH FALLS WITHIN SPACE LAWS OF ASTROPHYSICS DYNAMICS SCIENTIFICALLY EJECTS THE AIRCRAFT OUTER SPACE AIRCRAFT ANTIMATTER FREEDOM ARIEL DYNAMIC TRAVELING COMMON POSITIVE PARAMAGNETIC EMISSIONS REPELS COMMON ATMOSPHERIC SODIUM CALORIC NEWTRON NUCLEI NUCLEUS LIQUID FILLED ENCLOSURES WITHIN ATMOSPHERIC ENVIRONMENT COMMON POSITIVE PARTICLE ESC FROM AIRCRAFT ENCLOSURES SURFACES REPELS MATTER AWAY FROM VECTOR FIELD OR PROXIMITY FIELD FRACTION OF AREA AIRCRAFT ENCLOSURES ANTIMATTER FREEDOM FROM ATMOSPHERIC SODIUM CHLORIDE NEWTRON NUCLEI NUCLEUS LIQUID FILLED PARTICLE WITHIN SPACE ESC VECTOR OR PROXIMITY FIELD OF SOURCE OF TRANSMISSION RADIATION SUPPRESSION OF MAGNETO GRAVITATIONAL PARTICLE RADIATION VECTOR BEAM PROXIMITY BEAM NEWTRON NUCLEI NUCLEUS PARTICLE FRICTIONAL GRAVITATIONAL HOLD SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON

Friday, March 1, 2024

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft Aluminum powder oxide+silver powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a low 1mm gauge titanium sheet wafer position at the bottom of mold step process and having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge between the wafers are Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON
INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION 
Engineering Sub system architecture
Structural design
bipolar ROTOR magnetic levitation disc craft 
Aluminum powder oxide+silver powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a low 1mm gauge titanium sheet wafer position at the bottom of mold step process and having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge between the wafers are 
Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are
TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla 
Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON
INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION 
Engineering Sub system architecture
Structural design
bipolar ROTOR magnetic levitation disc craft 
Aluminum powder oxide+silver powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a low 1mm gauge titanium sheet wafer position at the bottom of mold step process and having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge between the wafers are 
Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are
TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla 
Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON
INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION 
Engineering Sub system architecture
Structural design
bipolar ROTOR magnetic levitation disc craft 
Aluminum powder oxide+silver powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a low 1mm gauge titanium sheet wafer position at the bottom of mold step process and having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge between the wafers are 
Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are
TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla 
Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

INTUITIVE INTELLIGENCE AERONAUTIC ENGINEERING AERODYNAMIC ARCHITECTURE FLIGHT SYSTEM PROGRESSIVE DEVELOPMENT INVENTION  Engineering Sub system architecture Structural design bipolar ROTOR magnetic levitation disc craft  Aluminum powder oxide+silver  powder oxide+bismuth powder oxide+silicon powder oxide+quartz crystalline powder oxide+boron powder oxide+GERMANIUM POWDER OXIDE added within a 11mm depth round plaster mold add stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces of a  low 1mm gauge titanium sheet wafer position at the bottom of mold step process and  having 1mm gauge aluminum round wafer BARING stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the surfaces against aluminum sheet surfaces turned upside down used for the top BARING below step process Compound powder combine measured at 3mm+7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism solid hardener wafer 11mm gauge for two different sized wafers. Copper powder oxide,+stainless steel powder oxide+Neodymium powder oxide+boron powder oxide+GRAPHENE powder oxide+quartz crystalline powder oxide+ added within 11mm depth round plaster mold with a 1mm gauge copper sheet rounded wafer bottom topped stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed above the copper wafer surfaces position at the bottom of the mold step process and than stainless steel sheet 1mm gauge round wafer top BARING exhibits stainless steel wire together with copper wire spun tightly donut coil telescope method within series compressed against its bottom surfaces turned into the step process compound powder combine measured at 3mm-7mm gauge than add liquid sodium acetate 3M thermal crystal liquid solid tetrahedron crystal prism hardener solid wafer for two different sized wafers 11 mm gauge  between the wafers are  Stainless steel lengthy wire couple to Copper wire turned circular into a helix shape coils of electrical energy wire winding are TESLAS are 11lbs per 12ft of copper wire spun tightly into helix shape coil emits 10,000gauss per Tesla  Subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON