Sunday, November 7, 2021

Untypical progressive development iron Man Mark 42 design RC BIOFRINGENT TITANIUM DEFORMED SHAPED BIOMETRIC RANGE MULTIPLE SOLENOID TELESCOPIC MICROFLUID ALUMINUM BLOCK ACTUATOR FOREARM DEVICE MAGNETO RUBBER PALMA ELECTROMAGNETIC GADOLINIUM COMMUTATOR CAGE ARMATURE CYLINDRICAL ATMOSPHERIC WATER GENERATOR RESERVOIR MAGNETO CALORIC EFFECTS MICROCOSM HHO HYDRO ENGINE BLOWER WHEEL PULSE ROCKET MANNED UAV FLIGHT STABILIZER DEVICE SUBJECT NOT LIMITING TO ADDITIONAL SUBSYSTEM STRUCTURE POTENTIOMETRIC DESIGN INVENTOR JERMAINE MORTON DESIGN

FLYMORTON CHARACTERIZED AS AN WEARABLE BIOMECHANICAL XYLOPHONE ELECTROMAGNET MODIFIED VIBERPHONIC MANNED C-FRAME PIEZOELECTRIC EFFECTS METALLOID STACKED SHAPED BIOMETRIC RANGE COMMUTATOR CAGE ARMATURE BIAXIAL ROTOR ROM BIOFRINGENT ORTHOSIS HUMAN FACILITY MOBILE CARRIER POWER SUIT MACHINE BODY ARMOR MODIFIED PYROELECTRIC EFFECTS  ELECTRON ENERGY CAPACITOR POWER BODY ARMOR POWERED EXOSKELETRONIC SOFTWARE BASE COGNITIVE MACHINE COMPUTING UBIQUITOUS AIR BREATHING MECHATRONIC ROTARY VACUUM ROCKET 
ATMOSPHERIC LIQUID SOLID FUEL CELL ENERGY GENERATOR SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIAL METRIC RANGE INVENTOR JERMAINE MORTON DESIGN
My invention is FLYMORTON WEARABLE BIOMECHANICS ORTHOSIS BIOMETRIC RANGE ROBOT MANNED UAV BODY ARMOR FLIGHT SUIT MACHINES SUBSYSTEM CONSISTS OF AN Energy rocket fuel engine generator
METHOD ACOUSTOPHORESIS collision BEAM
Atmospheric sodium hydroxide MAGNETO CALORIC ACOUSTOPHORESIS LIQUID SOLID generator
 THREE MODULATED TRANSDUCED SOLID ELEMENTS RADIATION PRESSURES FORCES  PARAMAGNETIC ELEMENTS ENTANGLEMENT BETWEEN A MEDIUM RISE PHASES PARTICLE FORCES COLLISIONS DEVELOPS LIQUID SOLID MASS OF
TRANSDUCED NEODYMIUM RADIATION EMISSIONS
TRANSDUCED GADOLINIUM RADIATION EMISSIONS
TRANSDUCED QUARTZ ENERGY CRYSTAL RADIATION EMISSIONS BEAM PRESSURES FORCES MATTER COLLISIONS SODIUM MATTER IRON GAS GENERATES SOLID MASS
SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIAL METRIC RANGE INVENTOR JERMAINE MORTON DESIGN

















FLYMORTON WEARABLE Biofringent  biomechanical guide rail gauntlet additional structure exoskeleton orthosis hand Palma finger also membrane biaxial ROM mechanical MANNED UAV brace SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIAL METRIC RANGE INVENTOR JERMAINE MORTON DESIGN

















Some of the solenoids was broken but now fixed and as far as the stainless steel rods baring 52N neodymium magnets rod pellets 3mm 3/32 Inch/ 0.11811 Inches

Progressive development UPDATE SOON NEW redesign biomechanical BIOMECHANICS software base orthosis ringer hand side Palma biofringent biaxial ROM rest manned uav rocket handheld brace machine system contains iron biometric range exhibiting permanent magnet design for armature baring with an aluminum functions as an latches additional structure piezoelectric effects stacked type hollow center flat bar frame exhibiting coil interface functional likenesses as an bore however flat parallel movement freedom within piezoelectric effects housing shaft resembles a stacked rectangular bar cage exhibiting hollow shaft functional likenesses as an commutator cage modulated ultrasonic armature dual action electromagnetic pulse PHASE 2 rectified AC/DC CHARGED solenoid pull push sense related to my diagram HAND image FINGERING drawing SUBJECT NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE POTENTIOMETRIC RANGE INVENTOR JERMAINE MORTON DESIGN









































ELECTRIC POWERED INDUCTOR COIL SOLENOID TYPE SENSORY ELECTROMAGNETIC HALL EFFECTS VECTOR PERMANENT MAGNET NEODYMIUM ELEMENT ALONGSIDE BISMUTH CRYSTAL ELECTRODYNAMICS PETTIER EFFECTS COOLER CALORIC ELECTROSTATIC GAS TRANSDUCER HORN MODULATED electromotive rapid oscillating ultrasonic amplification driven AUDIO ENCODER 


























Flymorton suit manned uav aircraft gyroscope drone submarine suit software base machines
 microcontroller contains one or more CPUs (processor cores) along with memory and programmable input/output peripherals
• microcontrollers is roughly at or above 8 MHz to 50 MHz, Instrumentation and Process Control: Oscilloscopes, Multi-meter, Leakage Current Tester, Data Acquisition and Control etc.
              Pulse-width modulation, reducing. The average value of voltage current 
              controlled by turning the switch between supply and load on and off

Stainless steel full body armor electromagnetic solenoid hold biomechanical EXO frame body armor biofringent
Biometric range
Titanium flat bar bracket mount
pan tilt pitch latches motorized powered flexi socket driven
BioMetric range shaped design
 wearable exoskeleton
 chest cockpit 2 door mount drum fan bracket 
Left side chest 1 cockpit door mount drum fan bracket 
Right side chest 1 cockpit door mount drum fan bracket 
Left side back rest 1 cockpit door mount drum fan bracket 
Right side back rest 1 cockpit door mount 8 drum fan bracket 
Arms motor 1 cockpit door mount drum fan bracket 
Left arm 1 cockpit door mount 8 drum fan bracket 
Right Hand side Palma thruster nozzle
Left Hand side Palma thruster nozzle
Right arm 1 cockpit door mount 8 drum fan bracket 
Left leg 1 cockpit door mount 8 drum fan bracket 
Right leg 1 cockpit door mount 8 drum fan bracket 
Left Foot thruster nozzle
Right foot thruster nozzle
Power supply
Right side Chest door baring 3v coin button batteries 220mah
53 coin button batteries 4x=159 coin button batteries x 4=636v 220mah 53x=1,1660mah
Left side Chest door baring 3v coin button batteries 220mah
53 coin button batteries 4x=159 coin button batteries x 4=636v 220mah 53x=1,1660mah
Back side Right rest door baring 3v coin button batteries 220mah
53 coin button batteries 4x=159 coin button batteries x 4=636v 220mah 53x=1,1660mah
Back side left rest door baring 3v coin button batteries 220mah
53 coin button batteries 4x=159 coin button batteries x 4=636v 220mah 53x=1,1660mah
Left Arm door baring 3v coin button batteries 70 coin button batteries=210v 220mah ×210v 46,200mah
Right arm door baring 3v coin button batteries 70 coin button batteries=210v 220mah ×210v 46,200mah
Left leg door baring 3v coin button batteries 220mah
120x 3v coin button batteries=360v 3v 220mah ×360v=79,200mah
Right leg door baring 3v coin button batteries 220mah
120x 3v coin button batteries=360v 3v 220mah ×360v=79,200mah
milli-Amp-hour - milli being 1/1000 of an amp. It is a measure of "capacity" of the battery, amp-hour or Ah) is a current of one ampere flowing for one hour. The amount of charge transferred in that hour is 3,600 coulombs
The body armor consist of materials that are
electromagnetic induction or inductive power transfer, IPT), power is transferred between coils of wire by a magnetic field. Inductive coupling

Body armor right side chest 60kg Servo motor
60kg to lbs
60 kilograms =Mass
132.277 pounds force
Servo motorized 
Chest plate: 16 servo 
60kgx16=960 kilograms =Mass 
2116.438 pounds force

Body armor left side chest 60kg Servo motor
60kg to lbs
60 kilograms =Mass
132.277 pounds force
Servo motorized 
Chest plate: 16 servo 
60kgx16=960 kilograms =Mass 
2116.438 pounds force

Body armor left arm Servo motor 
Per body armor arms 
200kgx16=
3200 kilograms
7054.792 pounds
Enumerates 6400lbs both arm

Tilt Trim Motor 4-STROKE HI-THRUST 40HP 50HP 

One horsepower force 550lbs
 550lbs torque force 50hpx=27,500lbs torque force 
27500lbs torque force 42x =1,155,000lbs torque Force
Maximum output power on the driving shaft for 4-blades propellers is up to 160 hp.
Four inch propeller blade diameter, 30 pitch,  number of blades 
‎15.3 x 14.3 x 7 inches
Drum fan bracket

 The propeller in turn transfers this rotational energy into forward thrust through the acceleration of a mass of air approximately equal to the diameter of the propeller through a momentum transfer to the air by the rotation of the propeller. It is the reaction force to this momentum transfer that produces the thrust that propels the aircraft through the air.

It is intuitive that energy must be expended in order for the engine to spin the propeller, and so the available power with which to generate thrust is equal to the total power produced by the engine less that power required to spin the propeller.














electrical force of induction coil producing high-frequency alternating currents.
Solenoid pull push telescopic body armor the body armor 
Magnetic refrigeration cooling body armor technology based on the magnetocaloric effect repeatedly exposing a magnetocaloric material as in magnetic field. As the piston oscillates its gadolinium alloy heats up, then cools as it passes through a gap in the field. In turn, cooling the water that surrounds it as it makes its trip 
causing the refrigerant cooling tubing, the tubes are modulated by a set series of ceramic piezo buzzers rings arranged within a chain linkage alongside the Cylindrical copper coil exterior. The piezo electric buzzers are driven by a circuit software based audio encoder signals hardware piezo electric ultrasonic deformation radiation pressures forces particles to a medium rise within the cylindrical tubing chamber as an acoustophoresis method for atmospheric gas to liquid. This process, called condensation, cools the surrounding area and produces the desired ice effect When you release the contents into the lower pressure open space, it turns from ice to liquid
Functional likenesses as an atmospheric water generator the body armor is a device that extracts water from humid ambient air. Water vapor in the air that are extracted by rotary vacuuming displacement of particles vectoring particles liquid field enclosures in space by suction thrusting particles against matter being rapidly displaced mechatronically by the liquid tubing modulated radiation pressures forces particles between the medium rise vectoring particle collision air below its dew point develops ice within a chamber modulated by an electrode cool exchanger melting the solid liquid ice. Subject not limited to additional system or structure

24:AWG alongside the telescopic gauntlet is designed to render the water portable Storage
Operates under the functional likenesses as in
 HFSSTC Tesla electronic candle plasma
Subject not limited to additional system or structure,
 Telescopic commutative linear motor rotor solenoid electrodynamics magneto caloric combustible thermodynamics HFSST(R) ion engine Rc rocket subject not limited to additional system or structure
Magnet Wire 24 AWG Enameled Copper Magnet Wire 24 HML 220C ONE Reel of 10 LBS, +/- 2 LBS 7000FT +/-

AWG 24
Diameter [inches] 0.0201
Max Frequency for 100% skin depth 68 kHz

AWG gauge 24
Conductor Diameter Inches 0.0201
Maximum amps chassis wiring 3.5

24AWG has a maximum current of 7A.
AWG gauge 24
Conductor Diameter Inches 0.0201
 Ohms per 1000 ft. =25.67

0.5106mm
Wire Gauge Conversion
Wire Number (Gauge) 24
A.W.G. or B&S (Inches 0.0201"
A.W.G. Metric (MM) 0.5106mm

24 ga can only handle 577 ma at any voltage. 

amps can 24 AWG handle?
From Current Carrying Capacity of Copper Conductors, has a maximum temperature of 90°C. At an ambient temperature of 30°C, 
1 mega amps to watt/volt = 1000000 watt/volt

2 mega amps to watt/volt = 2000000 watt/volt

3 mega amps to watt/volt = 3000000 watt/volt

4 mega amps to watt/volt = 4000000 watt/volt

5 mega amps to watt/volt = 5000000 watt/volt

6 mega amps to watt/volt = 6000000 watt/volt

7 mega amps to watt/volt = 7000000 watt/volt

8 mega amps to watt/volt = 8000000 watt/volt

9 mega amps to watt/volt = 9000000 watt/volt

10 mega amps to watt/volt = 10000000 watt/volt











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