FLYMORTON HYPERSONIC DETONANTION ENGINE
FLYMORTON CHARACTERIZED AS IN WEARABLE BIOMETRIC BIOMECHANICAL ACOUSTIC PERCUSSION BALLISTIC COMMULATOR BIOFRINGENT SOLENOID HYPERSONIC ORTHOPEDIC FULL BODY BRACE HALL EFFECT SOLENOID HOLD SENSORY POWERED REST BODY ARMOR BIAXIAL STEPPER ARMATURE EXOSKELETRONIC COMMULATOR MANNED HUMANOID BIOMEDIC AUTO RESIZER SELF CONFIGURATING ADDITIONAL STRUCTURE TRANSFORMER SELF BALANCING SELF RECHARGED HUMAN BODY ARMOR ENCLOSURES HUMAN RESIDENT MODIFIER COCKPIT CORE MANNED UAV COGNITIVE SUIT MACHINE
Hand-held Electromagnetics hypersonic solenoid (HSDE) thrusters
The FLYMORTON CHARACTERIZED AS IN WEARABLE: biomechanical biometric biofringent exsoskeletronic motorized biaxial robotic orthopedic hand orthotic palma also-membraine metalliod commulator silicon pyro-graphene mixed metalliod palma Peltier effect electromagnet hall effect rotary commulator armature operates pneumatic cylinder gas laser autoignition hypersonic combustion detonation bomb compressor chamber thermal protection shaft thermoelectric effect photovoltaic coil modified Peltier effect exerts throughout the thermelectric effect refrigeration engine coil pipeline towards within gauntlet exerts throughout the second solenoid combustion chamber with increased thermo energy forces throughout the commulator palma motorized pneumatic rotary mechanism detonation forces torques and exerts thrust throughout metalliod percussion wheel blower blades from the hypersonic modified modulated open clearance metalliod harmonic antimatter thermal protection chamber thruster baring a center diode cylinder laser gas ignition bomb bleeder core.
122milliliters 4.125 Fluid Ounces÷5=hydrogen liquid 0.825ml) aluminum powder 0.825mg)2coal powder 0.825mg) 2sodium alloy powder 0.825mg) 2potassium powder alloy (0.825mg) 2coal powder 0.825mg
Fuel thermal energy
Liquid Hydrogen energy fuel spontaneous autoignition is 500 °C (932 °F). 2/coal 0.825mg autoignition temperature above 450–650°C)2/aluminum themite powder oxide 0.825mg autoignition lower than 655 ° C (1215 ° F); 2425 ° C (4400 ° F)2Melting Point: 1,132° C (2,070° F) burns at temperatures above 2,200C), 2Sodium Oxide Powder autoignition 1,950° C (3,542°F) Potassium 63ºC
Split Ultrasonic mechanical oscillation solenoid piston autoignition detonation compressor combustable bomb bleeder engine method
Reciprocating 78.23400 times per second range within 0.106mm cylinder shaft length distance 4inch sonic modulated solenoid push solid mixed fuel energy compressor,
Compound solid metalliod chamber structure;
Silicon metalliod, 2sodium tungsten, 2(325)iron, 2(100)iron, 2cobolt magnet, 2yellow phosphorus, 2graphene,2 quartz crystalliod,
Thermal energy compound metalliod modulation engine structure operates;
Thermal energy-voltage booster-modulated-thermoelectric effect-voltage booster-electromagnetic hall effect shaft (EE) metalliod bond (MFD) voltage booster modulated shaft radiation energy method Magneto caloric effect-modulated-voltage booster-harmonic sonic solenoid compressor-modulated metalliod piston high voltage emitter head modulated ultrasonic transducer horn piston metalliod baring electron beam welding functional likenesses as in metalliod plunger having been thermoelectric effect cylinder piston head bleeder within the metalliod Pneumatic liquid energy fuel cell autoignition metalliod chamber fire detonation compressor combustible bomb cylinder chamber thermal energy thermoelectric effect refrigeration metalliod Peltier effect modulated impeller vacuum cylinder shaft cool exchanger liquid heating chamber parallel liquid tube vacuum rotary pump cylinder combustible bomb liquid energy fuel bleeder wearable hand-held thruster
Wearable (HSDE) Boot thrusters
Hydrogen2 2Aluminum 2,coal 2sodium, 2potassium
7000gr In one pound 42gr individual mach1 compressor velocity (4665 (ft / s) * (1422 (m / s)) =2 021 930.42 m2 / s2 *(mph) =
903 883.777 m3 / s3 *(joule)=2 021 930.42 m4 kg / s4 *(mm)=2 021.93042 m3 / s2* (mach 1) =693 522 135 m3 / s3hp) =1.50775326 × 109 m4 kg / s5 (Speeds velocity density constant discharge vertical however the electromagnetic solenoid engine hypersonic speeds are 10 to 25 Mach, 7,673 -19,183 mph, 12,348-30,870 km/h and 3,430-8,575 m/s Vertical dispatching thrusts. The body armor functional likenesses as an tractor beam transducer air horn body armor electromagnetic hypersonic vibrating body armor. 3d fraction of an area or area of fraction body armor enclosures are Electromagnetic cryonic metalliod Phosphores yellow crystalline enclosures Produces intense radiation full body armor cloaking mode.
FLYMORTON WEARABLE HYPERSONIC DETONATION ENGINE
The Gauntlet and Boot Hypersonic Detonation Engine (HSDE) is an propulsive device that uses supersonic detonation waves as a combustion mechanism.Thrust exerts the wheel blower above 2,500 feet per second (above 1,700 mph) after hydrogen exerts autoignition with a temperature of around 1800 K (1500 °C electron beam piston compressor chamber with spontaneous Sonic's (speeds of sound) ignition in air, is 500 °C (932 °F). Air and hydrogen exerts speeds of sound at (1270 mph) of the elastic properties of hydrogen, contrary of the density that is less than that of air. While hydrogen exerts coil heat exchanger cool flame having maximal temperature below about 400 °C (752 °F). It is produced in a chemical reaction of the environment Peltier effect cooler thermoelectric refrigeration modulation combustion shaft Sound travels (about 4 times as faster in air. sonic velocity of sound speeds in that hydrogen fluid (a gas/vapor). maximum forces can be achieved by the hydrogen fluid charcoal powder substrate mixed Salt powder substrate combustion boiling temperature of sodium is 881 °C ; monoxide starts evaporation at 1350 °C, a value equal to the measured flame temperature. along with Aluminum powder substrate all of which is entrusted as it's fuel source fuel source within this propulsion machine. The aluminum temperatures reaches of 1000–1800 K. The Aluminum powders in air or Coal dust suspended in air is just explosive as area per unit weight of coal, coal can produce combustion gases as hot as 2,500 °C (4,500 °F) spontaneous combustion. As a result for,PDE SONIC SPEEDS DETONATION PULSE propulsion method. The design offers numerous advantages over traditional gas turbine engines
gauge cylinder silicon metaloid mixed sodium tungsten graphite metaloid thermoprotection copper 3mm gauge 1in 1/2 open clearence magnet Piston plunger magneto caloric cooler wafer modulated Peltier effect liquid cooler magnetic coil modulated actuator linear wafer modulated ultrasonic magnetic reciprocation compressor within the liquid inductor coil cooler shaft.
0.106mm shaft length reciprocating compressor returner speeds of sound 767mm per 1 second)electron beam welding 1,000,000v sparkgap arc fire plasma 78.23400 times within 0.106mm times the speeds of sound autoignition fires1 per second within 0.106mm shaft limited distance. piston plunger magnet wafer oscillating 78.23400mm returner 1mm /per second, fire flame flashpoint detonation hydrogen vapor/gas/coal/sodium/aluminum/temperature 48,441,4190°F combustion exerts heat exchanger coil thermoelectric effect refrigeration vacuum shaft compressor cylinder harmonic sonic modulated transducer air horn resonator detonation bleeder 3mm open clearence shaft vacuum parallel wheel blower harmonic ultrasonic rotary tube modulated cool exchanger dispatching thrusts.
FLYMORTON CONCERT TO PROVIDE AUTO REFUELING SYSTEM
The Vacuum system tube wheel blower structure operates as an liquid generator. The tube wheel blower center core blades functional likenesses as in propane torches the maximum temperature of 3,623 degrees F, or 1,995 degrees C, while thermal suctioning vapor compression particles within a medium vacuum vapor drip chamber vapor compressor liquid accumulator chamber vacuum within a localized thermoelectric effect refrigeration Peltier effect liquid cooler modulation electrolysis chamber. The wheel blower having functional likenesses as an xlyophone acoustic percussion blades are individual heating element action vacuum blade's that incorporates the wheel blower structure the wheel blower Metalliod heating elements capable of temperatures up to 1425°C (2600°F) Individually having a diverse acoustics drum gauges for manpowered drum percussion sounding. The wheel blower having individual blade gauges C, D, E, F, G, A, B, C scales and sequence of the wheel blower blade's MODULATED harmonic sonic piezoelectric effect buzzer core transducer horn enclosures heating element modulation ultrasonic ultrasound above C-major scale's, or above 20,000 hertz is the start of the ultrasound. The wheel blower Ultrasound rotary operates with frequencies from 20 kHz up to several gigahertz. the tube wheel blower transducer horn wheel blower percussion blade's metallic thermoprotection structure modulation Intense radiation pressure compression by ultrasound waves against particles within a medium three dimensional area fraction of liquid-filled enclosures in space thermal compression improved efficiency and reduced mechanical complexity, subject not limiting to additional system or structure
UNIGRAVITY SUIT MACHINES
FLYMORTON CHARACTERIZED AS IN WEARABLE LINEAR MOTOR MANNED UAV ROTOR COMMUTATOR CAGE ORTHOSIS BIOMETRIC RANGE SHAPE MODULATED HARD SUIT SIGNALS SOFTWARE BASE PROCESSOR ELECTROMOTIVE BRAINWAVES SENSORY HUMAN MAGNETO ELECTROPHYSICAL RADAR BIOMETRIC RANGE NAVIGATION LANDING SWITCH CONTROLS GRIPPING VERTICAL WALL CLIMBING CROSS CRAWLING UNIGRAVITY ANTIGRAVITY ELECTRODYNAMICS ION PROPELLANT ENGINE ROCKET ELECTROMAGNETIC SELF- SUSPENSION SELF LEVITATION BIOMECHATRONIC POWERED FLIGHT SUIT MACHINE BODY ARMOR SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIAL METRIC RANGE INVENTOR JERMAINE MORTON DESIGN