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| INVENTOR JERMAINE MORTON DESIGNED Xwing REMOTE CONTROLS BATTERY POWERED ELECTRONICS ELECTROMOTIVE FORCE PULSE PHASE 250TESLA'S COPPER COIL WIRE (MFD) TURNS. THE AIRPLANE UTILIZES ELECTRODYNAMICS REPEL FORCES THE AIRCRAFT INTO THE AIR. THE PLANE SUBSYSTEM CORE ELECTRICAL CIRCUITRY UTILIZES DIAMAGNETIC ELECTRICAL ENERGY WINDING PULSE PHASE AC ELECTROMOTIVE FORCE INDUCE A CURRENT WITHIN A NONE GALVANIZED FERRO-MAGNETIC ELEMENT VOLTAGE REACTIVE ELECTROMAGNETIC, MODULATED HYPERSONIC PULSE ELECTRODYNAMICS, ELECTROSTATIC GAUSS RADIATION PRESSURES PARTICLE COLLISIONS COMMON ION RADIATION PRESSURES FROM TWO SEPARATE SOURCES EMITTING POSITIVE CHARGE NANO-PARTICLES VECTOR FIELD MICROWAVE RADIATION PRESSURES FORCES AWAY COMMON POSITIVE ION GAUSS TRANSMITTED FROM A LOCALIZED COMMON ELEMENT AS AN COPPER TOP DESIGN AS ONE SIDE OF THE AIRPLANE TOP PART EXTERIOR ENCLOSURES, CONTRARY OF ITS ALUMINUM ELEMENT CONNECTIONS TO A SEPARATE SOURCE OF POWER. WHEN SO EVER THE CONDUCTIVE AIRPLANE LOWER SIDE BOTTOM ALUMINUM CURRENT CARRYING VOLTAGE TO ESTABLISH A SIGNAL AGAINST ITS COPPER COIL ELECTRICAL ENGINE CIRCUIT WIRE TURNS WEIGHS MORE THAN IT'S INERTIAL MASS OF THE AIRPLANE ELECTRODYNAMICS DENSIFIED STRENGTHS ARE MEASUREMENT 4 TO THE TENTH POWER OF ITS INITIAL FORCE, ESCAPING AWAY FROM THE ALUMINUM BOTTOM MICROWAVE VELOCITY WAVELENGTH STRENGTHS OF IONIC RADIATION VECTOR FIELD DRAG FORCES THE ALUMINUM BOTTOM THAT IS PERMANENTLY CONNECTED TO THE AIRPLANE ALUMINUM BOTTOM SIDE DRAG FORCED INTO THE AIR HAVING LESS WEIGHT THAN ITS CENTRAL CIRCUIT MASS AND ITS EMISSION FORCES AGAINST THE CIRCUIT'S WEIGHT OF GRAVITY ABOUT 40TIMES+THE CIRCUIT PHYSICAL MASS AND EMITTING GAUSS 40TIMES THE WEIGHT OF ITS GRAVITY OF THE AIRPLANE DC/AC EMI VOLTAGE CAPACITOR FILTER 10,000w~40,000w Max voltage HPF SQUARE WAVE 1/4TH OF HERTZ 20,000HZ~100,000HZ HFP PHASE BORON FERROMAGNETISM COMMUTATOR TRANSDUCTOR HORN EMI 10,000W~40,000w SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON |
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| INVENTOR JERMAINE MORTON DESIGNED Xwing REMOTE CONTROLS BATTERY POWERED ELECTRONICS ELECTROMOTIVE FORCE PULSE PHASE 250TESLA'S COPPER COIL WIRE (MFD) TURNS. THE AIRPLANE UTILIZES ELECTRODYNAMICS REPEL FORCES THE AIRCRAFT INTO THE AIR. THE PLANE SUBSYSTEM CORE ELECTRICAL CIRCUITRY UTILIZES DIAMAGNETIC ELECTRICAL ENERGY WINDING PULSE PHASE AC ELECTROMOTIVE FORCE INDUCE A CURRENT WITHIN A NONE GALVANIZED FERRO-MAGNETIC ELEMENT VOLTAGE REACTIVE ELECTROMAGNETIC, MODULATED HYPERSONIC PULSE ELECTRODYNAMICS, ELECTROSTATIC GAUSS RADIATION PRESSURES PARTICLE COLLISIONS COMMON ION RADIATION PRESSURES FROM TWO SEPARATE SOURCES EMITTING POSITIVE CHARGE NANO-PARTICLES VECTOR FIELD MICROWAVE RADIATION PRESSURES FORCES AWAY COMMON POSITIVE ION GAUSS TRANSMITTED FROM A LOCALIZED COMMON ELEMENT AS AN COPPER TOP DESIGN AS ONE SIDE OF THE AIRPLANE TOP PART EXTERIOR ENCLOSURES, CONTRARY OF ITS ALUMINUM ELEMENT CONNECTIONS TO A SEPARATE SOURCE OF POWER. WHEN SO EVER THE CONDUCTIVE AIRPLANE LOWER SIDE BOTTOM ALUMINUM CURRENT CARRYING VOLTAGE TO ESTABLISH A SIGNAL AGAINST ITS COPPER COIL ELECTRICAL ENGINE CIRCUIT WIRE TURNS WEIGHS MORE THAN IT'S INERTIAL MASS OF THE AIRPLANE ELECTRODYNAMICS DENSIFIED STRENGTHS ARE MEASUREMENT 4 TO THE TENTH POWER OF ITS INITIAL FORCE, ESCAPING AWAY FROM THE ALUMINUM BOTTOM MICROWAVE VELOCITY WAVELENGTH STRENGTHS OF IONIC RADIATION VECTOR FIELD DRAG FORCES THE ALUMINUM BOTTOM THAT IS PERMANENTLY CONNECTED TO THE AIRPLANE ALUMINUM BOTTOM SIDE DRAG FORCED INTO THE AIR HAVING LESS WEIGHT THAN ITS CENTRAL CIRCUIT MASS AND ITS EMISSION FORCES AGAINST THE CIRCUIT'S WEIGHT OF GRAVITY ABOUT 40TIMES+THE CIRCUIT PHYSICAL MASS AND EMITTING GAUSS 40TIMES THE WEIGHT OF ITS GRAVITY OF THE AIRPLANE DC/AC EMI VOLTAGE CAPACITOR FILTER 10,000w~40,000w Max voltage HPF SQUARE WAVE 1/4TH OF HERTZ 20,000HZ~100,000HZ HFP PHASE BORON FERROMAGNETISM COMMUTATOR TRANSDUCTOR HORN EMI 10,000W~40,000w SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON |
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| INVENTOR JERMAINE MORTON DESIGNED Xwing REMOTE CONTROLS BATTERY POWERED ELECTRONICS ELECTROMOTIVE FORCE PULSE PHASE 250TESLA'S COPPER COIL WIRE (MFD) TURNS. THE AIRPLANE UTILIZES ELECTRODYNAMICS REPEL FORCES THE AIRCRAFT INTO THE AIR. THE PLANE SUBSYSTEM CORE ELECTRICAL CIRCUITRY UTILIZES DIAMAGNETIC ELECTRICAL ENERGY WINDING PULSE PHASE AC ELECTROMOTIVE FORCE INDUCE A CURRENT WITHIN A NONE GALVANIZED FERRO-MAGNETIC ELEMENT VOLTAGE REACTIVE ELECTROMAGNETIC, MODULATED HYPERSONIC PULSE ELECTRODYNAMICS, ELECTROSTATIC GAUSS RADIATION PRESSURES PARTICLE COLLISIONS COMMON ION RADIATION PRESSURES FROM TWO SEPARATE SOURCES EMITTING POSITIVE CHARGE NANO-PARTICLES VECTOR FIELD MICROWAVE RADIATION PRESSURES FORCES AWAY COMMON POSITIVE ION GAUSS TRANSMITTED FROM A LOCALIZED COMMON ELEMENT AS AN COPPER TOP DESIGN AS ONE SIDE OF THE AIRPLANE TOP PART EXTERIOR ENCLOSURES, CONTRARY OF ITS ALUMINUM ELEMENT CONNECTIONS TO A SEPARATE SOURCE OF POWER. WHEN SO EVER THE CONDUCTIVE AIRPLANE LOWER SIDE BOTTOM ALUMINUM CURRENT CARRYING VOLTAGE TO ESTABLISH A SIGNAL AGAINST ITS COPPER COIL ELECTRICAL ENGINE CIRCUIT WIRE TURNS WEIGHS MORE THAN IT'S INERTIAL MASS OF THE AIRPLANE ELECTRODYNAMICS DENSIFIED STRENGTHS ARE MEASUREMENT 4 TO THE TENTH POWER OF ITS INITIAL FORCE, ESCAPING AWAY FROM THE ALUMINUM BOTTOM MICROWAVE VELOCITY WAVELENGTH STRENGTHS OF IONIC RADIATION VECTOR FIELD DRAG FORCES THE ALUMINUM BOTTOM THAT IS PERMANENTLY CONNECTED TO THE AIRPLANE ALUMINUM BOTTOM SIDE DRAG FORCED INTO THE AIR HAVING LESS WEIGHT THAN ITS CENTRAL CIRCUIT MASS AND ITS EMISSION FORCES AGAINST THE CIRCUIT'S WEIGHT OF GRAVITY ABOUT 40TIMES+THE CIRCUIT PHYSICAL MASS AND EMITTING GAUSS 40TIMES THE WEIGHT OF ITS GRAVITY OF THE AIRPLANE DC/AC EMI VOLTAGE CAPACITOR FILTER 10,000w~40,000w Max voltage HPF SQUARE WAVE 1/4TH OF HERTZ 20,000HZ~100,000HZ HFP PHASE BORON FERROMAGNETISM COMMUTATOR TRANSDUCTOR HORN EMI 10,000W~40,000w SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON |
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