Atomic Electronic Weight Chips and Circuits, Inc. ELECTRIC PROPULSION; ENERGY; AND BIO RESEARCH
Atomic Electronic Weight Chips and Circuits, Inc.ELECTRIC PROPULSION; ENERGY; AND BIO RESEARCH

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PROPULSION TECHNOLOGY & RENEWABLE ENERGY GENERATION

USAGE OF RENEWABLE ENERGY GENERATION

ELECTRIC PROPULSION. HYPOTHETICALLY ANTIMATTER PROPULSION

This is an experimental output used to demonstrate the potential usage of the power source in Electric Propulsion Modules. Output from the power source may be in ranges of very high current; Therefore, this configuration is necessary. The overall current of the power source by usage of 4 sets of Propulsion Modules (I Fmt, I Fmb, I Fdt, I Fdb), or highest current generated by the power source, is approximately 4A p-p (±4A). See Figure 4.

 

The charging or power source ON-time, takes approximately 2.646 minutes. Once the charge time is met, the power source can be left running until usage is not necessary, and turned back ON, when usage is necessary.

GENERATED AC-DC OUTPUT

 

The power source is powered ON by usage of 2x1e-9V (2 Exotic Matter Batteries—In retrospect, the initial input voltage used by the batteries, is equivalent of charging the batteries by usage of free energy—) or equivalent to the usage of free energy, Electrons and Protons). Hypothetically that is DC turned AC.

The charging or power source ON-time, takes approximately 2.632 minutes. Once the charge time is met, the power source can be left running until usage is not necessary, and turned back ON, when usage is necessary.

This is an experimental output used to demonstrate the potential usage of the power source to generate low voltage, current and power, proportional to DC (~ +

2.1241V, -162.902mV) output positions. Output from the power source may be in ranges of very high current; Therefore, this configuration is necessary. The throughput current of the power source by usage of RL1 (1) at the main output point, or highest current generated by the power source, is ~ (± 7A).

AC TO SECOND POSITION AC/TRANSFORMER. "GENERATED AC-DC OUTPUT".

LOW CURRENT HIGH WATTAGE (BIT)

This is an experimental output used to demonstrate the potential usage of the power source to generate high wattage at low current—This wattage output is still minute. No higher wattage values will be displayed on this website—. Output from the power source may be in ranges of very high current; Therefore, this configuration is necessary. The overall current of the power source by usage of the approximated valued current of the Battery (I), is 6nA to -16nA p-p (±22nA), or highest current generated by the power source, (I) battery, and output array (54t—45T—, 54b—54B—), is approximately 300mA p-p (±300mA).

 

The power source is powered ON by usage of 1e-9V (1 Exotic Matter Positioning Battery—In retrospect, the initial input voltage used by the battery, is equivalent of charging the battery by usage of free energy—) or equivalent to the usage of free energy, Electrons and Protons). Hypothetically that is DC turned AC.

 

The charging or power source ON-time, takes approximately 3.499 minutes. Once the charge time is met, the power source can be left running until usage is not necessary, and turned back ON, when usage is necessary.

 

The capacitors’ (54t—45T—, 54b—54B—) current, are coupled to the negative polarity of the battery (I) with an RCL; (RL) Resistor—And the RL value controls the (I) battery’s current, as a lot of other components of the power source configuration allow—Capacitor, and inductor. “RCL”. These components were used in this experiment, to allow further control of the oscillating power source. Perfection in functionality hasn’t been achieved as yet. That may not be true. I fabricated some of these functioning devices before—Noting this powerful—. During those experiments, I noticed that real-life output from such devices, were smoother, and stable repetitions of the same functions occurred, than shown in this and many other computer simulations of such device variables. Those latter tests were performed with oscillating resistances (Reactance).

 

“The capacitors’ (54t—45T—, 54b—54B—) current, are coupled to the negative polarity of the battery (I) with an RCL…”. The rest of the power source connects to the positive polarity of I (battery), and coupled to ground by usage of resistors, and at some points, capacitors. The device ends up being absolutely grounded, with no open positions. The only open positions that are ever used in a series of experiments, is to gain output through capacitor to ground, or RC (Resistor Capacitor) to ground, or RCL (Resistor Capacitor Inductor) to ground.

 

Coupled to Ground are a usage of this power source to achieve usable power generation output. And that usage is equivalent to the usage of a battery in parallel with an electronic component. The output dose not fail in computer simulation, nor in real life; See wattages of capacitors (54t—45T—, 54b—54B—). See current of Battery (I). See current of capacitors (54t—45T—, 54b—54B—).

 

CURRENT & REACTANCE COMPARISON

Illustrated are resistive or reactance generated by currents (I Fmt, I Fmb, I Fdt, I Fdb). See Figure 5. In comparison, see resistive or reactance of Figure 3 devices, currents (I (MTR-A to MTR-D)). See Figure 6 below for more details.

USAGE OF RENEWABLE ENERGY GENERATION

MOTOR DRIVER & LOW CAPACITAVE VALUES POWER GENERATION

This is an experimental output used to demonstrate the potential usage of the power source with MOTOR DRIVERS. Output from the power source may be in ranges of very high current; Therefore, this configuration is necessary. The overall current of the power source by usage of the MOTOR DRIVER, or highest current generated by the power source, is approximately 3A p-p (±3A).

This image is from a power source used to gain power generation for usage on STAGE MOTORS. Four 1pF Capacitors are used to simulate motor stage positions.  There are 4 motor stages (MTR-A to MTR-D). The power source is powered ON by usage of 2x1e-9V (2 Exotic Matter Positioning Batteries—In retrospect, the initial input voltage used by the batteries, is equivalent of charging the batteries by usage of free energy—) or equivalent to the usage of free energy, Electrons and Protons). Hypothetically that is DC turned AC. The amplitudes of power from the power source can be adjusted to drive conventional motors that would have higher capacitance ratings that 1pf. This initial capacitance used, is much more useful for this power source and MOTOR DRIVER configuration to allow high power generation ratios, than with the usage of 1µF capacitance and higher value capacitances.

The amplitudes of the stage motor currents (I (MTR-A to MTR-D)) are equivalent to the usage of the 1pF Capacitors used to simulate the 4 motor stage positions. Had the 4 capacitors used been higher in values, let’s say 1µF and up, a different MOTOR DRIVER specification has to be used with the power source or this MOTOR DRIVER fails to operate the motor.

The charging or power source ON-time, takes approximately 3.053 minutes. Once the charge time is met, the power source can be left running until usage is not necessary, and turned back ON, when usage is necessary.

 

MOTOR DRIVER & HIGH CAPACITAVE VALUES POWER GENERATION

This is an experimental output used to demonstrate the potential usage of the power source with MOTOR DRIVERS. Output from the power source may be in ranges of very high current; Therefore, this configuration is necessary. The overall current of the power source by usage of the MOTOR DRIVER, or highest current generated by the power source, is approximately 7A p-p (±7A).

 

This image is from a power source used to gain power generation for usage on STAGE MOTORS. Four 10µF Capacitors are used to simulate motor stage positions.  There are also four 1µF (One of 4 Capacitors—DEV13—) Capacitors used in parallel of the four 10µF Capacitors for demonstrational purposes. DEV13 Capacitor is not very stable, as it does not remain completely carrying only 1 polarity. This MOTOR DRIVER configuration isn’t useful in that sense, in conjunction with the 10µF Capacitors. There are 4 motor stages (MTR-A to MTR-D) 10µF Capacitors.

The power source is powered ON by usage of 2x1e-9V (2 Exotic Matter Positioning Batteries—In retrospect, the initial input voltage used by the batteries, is equivalent of charging the batteries by usage of free energy—) or equivalent to the usage of free energy, Electrons and Protons). Hypothetically that is DC turned AC. The amplitudes of power from the power source can be adjusted to drive conventional motors that would have higher capacitance ratings than 1µF. The configurated range of the MOTOR DRIVER, is between 1µF and 10µF. These possible initial capacitances used, especially the 10µF Capacitors, are much more useful for this power source and MOTOR DRIVER configuration to allow high power generation ratios for higher value capacitors, than the 1pF capacitance MOTOR DRIVER described by usage of Figure 1. That only allows the functionality of lower value capacitances or motors.

 

The amplitudes of the stage motor currents (I (MTR-A to MTR-D)) are equivalent to the usage of the 10µF Capacitors used to simulate the 4 motor stage positions. Had the 4 capacitors used been higher in values, let’s say 22µF and up, the same MOTOR DRIVER specification could to be used with the power source. The power output of the power source (MOTOR DRIVER), would then by half of what it was.

The charging or power source ON-time, takes approximately 3.169 minutes. Once the charge time is met, the power source can be left running until usage is not necessary, and turned back ON, when usage is necessary.

 

MOTOR DRIVER & LOW CAPACITAVE VALUE POWER GENERATION

The power source is powered ON by usage of 2x1e-9V (2 Exotic Matter Batteries—In retrospect, the initial input voltage used by the batteries, is equivalent of charging the batteries by usage of free energy—) or equivalent to the usage of free energy, Electrons and Protons). Hypothetically that is DC turned AC.

The charging or power source ON-time, takes approximately 3.222 minutes. Once the charge time is met, the power source can be left running until usage is not necessary, and turned back ON, when usage is necessary.

This is an experimental output used to demonstrate the potential usage of the power source with MOTOR DRIVERS. Output from the power source may be in ranges of very high current; Therefore, this configuration is necessary. The overall current of the power source by usage of the MOTOR DRIVER, or highest current generated by the power source, is ~ (± 200mA).

AC TO SECOND POSITION AC/TRANSFORMER. GENERATED AC-DC OUTPUT, TO A REPEATER OUTPUT DEVICE WITH GROUND 2 (GX). "A REPEATER OUTPUT DEVICE" CAPABLE OF HANDLING MANY DEVICES AT ONCE. USAGE ON THE OUTPUT COMPONENT POSITION, 1µF CAPACITOR (MOT1), REPRESENTATIVE OF USING A MOTOR DRIVER TO POWER SUCH A MOTOR.

MOTOR DRIVER & HIGH CAPACITAVE VALUE POWER GENERATION

The power source is powered ON by usage of 2x1e-9V (2 Exotic Matter Batteries—In retrospect, the initial input voltage used by the batteries, is equivalent of charging the batteries by usage of free energy—) or equivalent to the usage of free energy, Electrons and Protons). Hypothetically that is DC turned AC.

The charging or power source ON-time, takes approximately 3.325 minutes. Once the charge time is met, the power source can be left running until usage is not necessary, and turned back ON, when usage is necessary.

This is an experimental output used to demonstrate the potential usage of the power source with MOTOR DRIVERS. Output from the power source may be in ranges of very high current; Therefore, this configuration is necessary. The overall current of the power source by usage of the MOTOR DRIVER, or highest current generated by the power source, is ~ (± 1.8A)

AC TO SECOND POSITION AC/TRANSFORMER. GENERATED AC-DC OUTPUT, TO A REPEATER OUTPUT DEVICE WITH GROUND 2 (GX). "A REPEATER OUTPUT DEVICE" CAPABLE OF HANDLING MANY DEVICES AT ONCE. USAGE ON THE OUTPUT COMPONENT POSITION, 10µF CAPACITOR (MOT1), REPRESENTATIVE OF USING A MOTOR DRIVER TO POWER SUCH A MOTOR.

TELECOMMUNICATIONS

LOW CURRENT HIGH VOLTAGE & HIGH POWER GNERATION

LOW VALUE INDUCTIVE COMPONENTS

This is an experimental output used to demonstrate the potential usage of the power source to transmit radio signals. Output from the power source may be in ranges of very high current; Therefore, this configuration is necessary. The overall current of the power source by usage of the values, 1 (10mH) + 10 of 4, the last inductor equaling approximately 39mH, or highest current generated by the power source and inductor array, is approximately 4A p-p (±4A).

 

The power source is powered ON by usage of 2x1e-9V (2 Exotic Matter Positioning Batteries—In retrospect, the initial input voltage used by the batteries, is equivalent of charging the batteries by usage of free energy—) or equivalent to the usage of free energy, Electrons and Protons). Hypothetically that is DC turned AC.

 

 

The charging or power source ON-time, takes approximately 2.9468 minutes. Once the charge time is met, the power source can be left running until usage is not necessary, and turned back ON, when usage is necessary.

 

The amplitudes of the inductors’ current (Open Circuit—Capacitive Ground (1µF/4)—; DEVL1 to DEVL4) are equivalent to the usage of approximately in values, 1 (10mH) + 10 of 4, the last inductor equaling approximately 39mH, used to simulate the 4-bit signals. Had the 4 inductors used been lower in values, let’s say 1000nH (DEVL1) to 4µH (DEVL4), the same signal specification may not to be as useful with the power source output signal array (DEVL1 to DEVL4) configuration. The power output of the power source signal specification, would be between 400W to 100W, with DEVL4 being close to 100W p-p, and DEVL1 being close to 400W p-p.

LOW CURRENT HIGH WATTAGE 4 COMPONENTS (INDUCTOR (HIGH, LOW VALUES); CAPACITORS (HIGH, LOW VALUES)) OUTPUT

This is an experimental output used to demonstrate the potential usage of the power source with 4 Components (INDUCTOR (HIGH (5H), LOW (10µH) VALUES); CAPACITOR (HIGH (10µ), LOW (1pF) VALUES)) at once. Output from the power source may be in ranges of very high current; Therefore, this configuration is necessary. The overall current of the power source by usage of the 4 COMPONENTS array, or highest (Throughput) current generated by the power source, is approximately 5.4A p-p (±5.4A).

INDUCTOR (HIGH (5H—L18—), LOW (10µH—L17—) VALUES); CAPACITOR (HIGH (10µ—C70—), LOW (1Pf—C74—) VALUES).

The power source is powered ON by usage of 1e-9V (2 Exotic Matter Positioning Batteries—In retrospect, the initial input voltage used by the battery, is equivalent of charging the battery by usage of free energy—) or equivalent to the usage of free energy, Electrons and Protons). Hypothetically that is DC turned AC.

The charging or power source ON-time, takes approximately 3.104 minutes. Once the charge time is met, the power source can be left running until usage is not necessary, and turned back ON, when usage is necessary.

 

BIOLOGICAL (BIO) RESEARCH

The overall current of the power source, or highest current generated by the power source, is approximately 11.67mA p-p (±11.67mA). The charging or power source ON-time, takes approximately 11.025 seconds. Once the charge time is met, the power source can be left running until usage is not necessary, and turned back ON, when usage is necessary.

V1 and V2 currents have been maximized, and can reach ranges from the default positions to as low as needed. Dev1 or DEV1 (Device 1) current is the main output point. The energy output can be used in organic experimentations, biological instrumentation research, manipulation and testing.

The test resistor value used in experimentation; 1 Ohm (DEV1).

 

The power source is powered ON by usage of 2x1e-9V (2 Matter Positioning Batteries—In retrospect, the initial input voltage used by the batteries, is equivalent of charging the batteries by usage of free energy—) or equivalent to the usage of free energy, Electrons and Protons). Hypothetically that is DC turned AC.

"The charging or power source ON-time, takes approximately 11.025 seconds.".

DATA & WORK PROCESSING 

POWER GENERATION

FIGURE 13 SHOWS, FOR EACT DATA AND/OR WORK INPUT ENTRY (L1 & L2)—IN THE ACTIVE—FIGURE 13—OR IF EVER, PASSIVE SYSTEM—THERE IS AN OUTPUT (L6 & L8).

 

The charging or power source ON-time, takes ~3.75 minutes. Once the charge time is met, the power source can be left running until usage is not necessary, and turned back ON, when usage is necessary.

FIGURE 14 SHOWS, FOR EACT DATA AND/OR WORK INPUT ENTRY (L5 & L7)—IN THE ACTIVE—FIGURE 13—OR IF EVER, PASSIVE SYSTEM—THERE IS AN OUTPUT (L10 & L11).

 

The charging or power source ON-time, takes ~17.9 Seconds. Once the charge time is met, the power source can be left running until usage is not necessary, and turned back ON, when usage is necessary.

PLATEAU WAVE FORMS & PARALLEL L6, R117 VIA CAT3

The power source is powered ON by usage of 2x1e-9V (2 Matter Positioning Batteries—In retrospect, the initial input voltage used by the batteries, is equivalent of charging the batteries by usage of free energy—) or equivalent to the usage of free energy, Electrons and Protons). Hypothetically that is DC turned AC.

The charging or power source ON-time, takes approximately 2.68 minutes. Once the charge time is met, the power source gradually generates stable Plateau Wave Forms. Also, when the charge time is met, the power source can be left running until usage is not necessary, and turned back ON, when usage is necessary.

The throughput current of the power source  is ~ (± 9A). 

THz Waves

Highest device generated voltage used, ~ -84.28K.

Highest device generated voltage used, ~ -84.28K.

Highest device generated voltage used, ~ -84.28K.

Highest device generated voltage used, ~ -84.28K.

NOT A SOLUTION NOR SUBSTITUTION

VIDEOS

License agreement—PRICELESS TECHNOLOGIES—

 

  • Limited Research License Agreement Fee: $300,000.

 

  • Limited Research Annual Stipulation Before Marketing and Royalties: $50,000.

 

  • Full Propulsion Technology Research: $3,991,900

 

  • Full Propulsion Technology Research Annual Stipulation Before Marketing and Royalties: $1,119,900

 

  • Limited Research Definition: Power Source Development as Chip Form or Circuit Board Form. For reasons, other than propulsion or any sort of flight technology; For usage towards the Development of tiny flying devices such as drones and road vehicles and wheel vehicles for marketing purposes, it is "Limited Research".

 

  • Full Propulsion Technology Research: For usage in Space and Geo-Propulsion Technology based upon Electromagnetism or as defined, the forces of Quantum Mechanics; Telecommunications and Remote Systems; Development of devices and equipment for medical purposes.
 
  • The Development of Limited and Full Technologies: Propulsion; Medical Technology and Equipment, are not limited to this License Agreement of technology definitions. Developments of Limited and Full Technologies may go beyond scopes, not included in the License Agreement of technology's specifications and definitions, at this time.

 

 

LAWS

5.14    Petition for license; corresponding U.S. application:

https://mpep.uspto.gov/RDMS/MPEP/current#/current/d0e337465.html

 

5.15    Scope of license: How licenses are granted and eligibility that the owner of the

intellectual property already has permission for license granted to whoever they may so choose:

https://mpep.uspto.gov/RDMS/MPEP/current#/current/d0e337491.html

 

5.12    Petition for license:

https://mpep.uspto.gov/RDMS/MPEP/current#/current/d0e337427.html

 

RESTRICTIONS

5.13    Petition for license; no corresponding application:

https://mpep.uspto.gov/RDMS/MPEP/current#/current/d0e337449.html

 

35 U.S.C. 184   Filing of application in foreign country:

https://mpep.uspto.gov/RDMS/MPEP/current#/current/d0e304599912.html

 

35 U.S.C. 181   Secrecy of certain inventions and withholding of patent:

https://mpep.uspto.gov/RDMS/MPEP/current#/current/d0e304551.html

 

140    Foreign Filing Licenses [R-07.2015]:

https://www.uspto.gov/web/offices/pac/mpep/s140.html

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