FLYMORTON HELMET DIAGRAM NOT LIMITING TO ADDITIONAL SYSTEM OR STRUCTURE

Fig 1

FLYMORTON WEARABLE ULTRASONIC SOLENOID PNEUMATIC AIR ENGINE FACE FRAME BIOMECHATRONIC TRANSFORMER FACE GEAR FRAME PERMANENT MAGNET ELECTROMAGNETIC PROPELLER FRAME NEURON MOTOR CONTROLS FIBER-OPTIC IMAGE OR MOVING IMAGE PROJECTOR DISPLAY AUGMENTED REALITY UV PROTECTION MOTORIZED LENS HEADS UP DISPLAY 3 SETS OF FOCAL (AR) IMAGE DISPLAY HEAD-GEAR EXOSKELETRONIC ELECTROMOTIVE PIEZOELECTRIC EFFECT BIOMETRIC FACE FRAME FAN PROPELLER ACTUATOR ULTRASONIC PROPULSION RECIPROCATING FRAME BLADE 180°-45°ANGLER 4.5KG+ THRUST AIRSHIP UAV DRONE

Fig. 2

2021 UPDATE TITANIUM CORE PIEZOELECTRIC CERAMIC ULTRASONIC HELMET ALONGSIDE THE FACEPLATE ELEMENTS TITANIUM EXTERIOR PYRO- CRYSTAL CORE NEODYMIUM FRAME ALONGSIDE TITANIUM EDGES HOUSING THE BIOMECHATRONIC BIOMETRIC FACE FRAME ELEMENTS PIEZOELECTRIC ULTRASONIC FAN PROPELLER FACE-FRAME HARMONIC PROPELLER WINGS UAV DRONE REST

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Progressive development

Progressive development (DC) LITHIUM BATTERY POWER UAV ROCKET POWER LEVITATION FACE SHIELD, SUBSYSTEM MICRO FLUID FUEL ENERGY CELL POWER GENERATOR POWERED METALLIC BOND SUPER CAPACITOR QUARTZ CRYSTAL ENERGY CELL CORE LAYER BIOFRINGENT TRANSDUCER HORN MODIFIED EXHIBITS FACE BIOMETRIC RANGE. ACRYLIC MODULATED SYNCHRONOUS LIGHT BRAINWAVES PIR ACRYLIC MODIFIED DIODE LIGHT EMITTING FACE SHIELD PHOTVOLTAIC SYNCHRONOUS ALPHA RADIATION SYNCHRONOUS LIQUID ION ELECTROLYTIC QUANTUM COLLISION QUANTUM ENTANGLEMENT

Lithium powered BIOMECHANICAL BIOMECHATRONIC manned UAV HUMANOID RC ROCKET JET SUIT EXOSKELETRONIC C-FRAME STACKED IRON COMMUTATOR ORTHOSIS BIOMETRIC RANGE BIOFRINGENT BIAXIAL ROM CIRCULAR CAGE STATOR ROTOR AIR ENGINE GRIPPING REST BODY BRACE EXTREME HARD SUIT MACHINE

Faceplate progressive development FLYMORTON AR VISION SYSTEM UAV RC ROCKET FACEPLATE DRONE DESIGN CREATED WITH LIQUID SOLID METAL LAB PUTTY REPAIR MIXED TO YTTRIUM POWDER TO ENCLOSE PAIRS OF LEED SHAFT STEPPER MOTOR EMBEDDED WITHIN THE SOLID OPERATES MOVEMENT tubing SPOOL ENGINE ROCKET WITHIN thermal refrigeration open clearance METALLIC THRUST NOZZLE copper coil that shall be EMBEDDED alongside the rotary propeller housing. The RC engine spool tubing thrusts throughout the thermal protection copper tubing open clearance shaft, the thermal protection refrigeration copper tubing deformed spun into spiral shape exhibiting double shaft, the spiral coil exterior exhibits ultrasonic piezoelectric ceramic transducers ring series alongside the base, the ceramic piezoelectric ultrasonic buzzers are embedded within BISMUTH TO QUARTZ ENERGY CRYSTAL COUPLE TO NICKEL NEODYMIUM PERMANENT MAGNET MODULATED ELECTROMOTIVE ULTRASONIC peltier EFFECTS cooler ROCKET ENGINE SHAFT