The present invention concerns a process and a installation. The process is to be used in conjunction with the process and installation described in
European Patent No. 2,692,701. We shall call the installation described in the
EP 2,692,701, Radiant, as it is an energy production concept that combines a Power Plant (PP) with a Waste Water Treatment Plant (WWTP). The present invention refers to a transport concept and we shall call it Conexant and it applies to a six train FWSG as described in
EP 2,692,701, or a population equivalent between 280-2,236.
The most important feature of the concept it derives from the existence of a seasonal energy surplus and a seasonal energy deficit for Radiant plants as well as for photovoltaic energy production of an agglomeration, Connexant being used for the transport of both energies. In conclusion, Conexant keeps the principle of the Radiant plant which is to use the energy produced in summer during the winter, but applies it to pairs of plants located at antipodes and therefore with seasons in opposition.
Conexant may also transport other energy sources like nuclear, hydro and wind power, but the the subsequent development strategy however will be for only two main sources of energy: biomass (Radiant) and photovoltaic energy (at consumer level). Those sources of energy are complementary in respect to availability: one is available all the time, and the other only in the daytime. The energy compensation has two main tipes: seasonal and diurnal. We shall present them both.
The seasonal compensation for the warm season in northen hemisphere is presented inFigure 1. During the warm season (between the spring and autum equinox) there will be an energy transfer from parallel 46.9991 (EPSG 4326) to parallel -26.2185 (EPSG 4326). The same energy transfer will be made during the cold season (in the northern hemisphere), only this time from the parallel - 26.2185 (EPSG 4326) to the parallel 46.9991 (EPSG 4326). In this situation, presented inFigure 2, the energy transfer is made from the tropical zone to the temperate zone. The difference in latitude will be felt by a higher energy intensity per square meter for the southern hemisphere. However, more photovoltaic installations will be needed in the southern hemisphere to compensate for the much higher energy consumption imbalance in the northern hemisphere (proportional to the asymmetry in population distribution).
The six points are retransmission centers. The energy in that area is received and passed on under the seasonal compensation schemes. The positioning of each of the 6 retransmission centers was established by an algorithm. Positioning accuracy is in the tens of thousands of degrees (approximately 10 meters). The algorithm will be presented below. The presentation of the 6 points and the geographical equator is made inFigure 3.
The numbering of the points is from 1 to 6 starting from the top left, ending in the bottom right in the up-down, left-right directions. We will start by presenting the algorithm for establishing the points on the main meridian or meridian 3-4. This is the one that crosses Europe and Africa. The algorithm for establishing points 3-4 has three stages. The first of these was the one in which the meridian was determined, with the property that the intersections with the land areas have, in sum, the longest length. Also in the first stage, the maximum of the meridian + antimeridian intersections with the land was calculated. The result was identical to the first calculated maximum, namely the merdian 22.5565 (EPSG 4326). The second stage was to establish the parallel whose intersections with the land areas have, in sum, the longest length. The result was in North Africa, 30.4382 (EPSG 4326) and is called the main parallel. The first two steps are shown inFigure 4.
In the third stage, the parallel with the maximum land at the north of the main parallel (global maximum) was determined as well as the parallel with the maximum land south of the main parallel (local maximum but global for Australia). These are, as already mentioned, 46.9991 (EPSG 4326) and -26.2185 (EPSG 4326). The parallels will be called the northern parallel and the southern parallel. The two previously determined parallels will determine the existence of a "false equator" in the middle of the distance between them. This is important because it separates the Radiant power plants that will transmit to a retransmission center or another diametrically opposite. The false equator will be present in all the images that follow from now on. The parallels and the false equator are inFigure 5
. The algorithm for determining the western meridian or meridian 1-2 consisted of the following steps: establishingpoint 1, establishingpoint 2.
Point 1 resulted from the intersection of a meridian with a parallel. The merdian was the one that intersects the maximum land between the false equator and the North Pole, on the North American continent. The parallel was the northern parallel. The resulting point is: -98.0063; 46.9991 (EPSG 4326). The same procedure was applied withpoint 2. The difference was that the meridian intersected the maximum land between the equator and the South Pole, on the South American continent, and the parallel was the southern one. The resulting point is: -69.4974; -26.2185. The determination of meridian 1-2 is shown inFigure 6. The algorithm for establishing the eastern meridian or meridian 5-6 consisted of the following steps: establishing point 5, establishing point 6. Point 5 resulted from the intersection of a meridian with a parallel. The merdian was the one that intersects the maximum land between the false equator and the North Pole, on the Asian continent. The parallel was the northern parallel. The resulting point is: 103.7923; 46.9991 (EPSG 4326). The same procedure was applied with point 6. The difference was that the meridian intersected the maximum land between the equator and the South Pole, on the Australian continent, and the parallel was the southern one. The resulting point is: 142.1776; -26.2185 (EPSG 4326). The determination of the meridian 5-6 is presented inFigure 7.
The daytime compensation scheme equals the differences between the photovoltaic energy produced during the day and that produced during the night. For daytime compensation, in addition to the meridians, the diagonals were taken into account. Distances between points. including the diagonals are listed below. Seasonal are the distances 1-2, 3-4, 5-6, the rest beeing composite.
| Link | Distance (m) | Link | Distance (m) | Link | Distance (m) | Link | Distance (m) |
| 1-2 | 8,600,095 | 3-5 | 5,879,029 | 2-6 | 13,287,425 | 2-3 | 12,240,351 |
| 3-4 | 8,108,189 | 4-6 | 11,326,092 | 6-3 | 14,308,444 | 1-6 | 14,323,267 |
| 5-6 | 8,978,985 | 2-4 | 8,958,424 | 4-5 | 11,470,642 | 2-5 | 17,624,493 |
| 1-3 | 8,100,491 | 1-5 | 9,376,473 | 4-1 | 14,380,011 | | |
The largest diagonal is 2-5. Its distance is the maximum distance for which the 6 retransmission centers are dimensioned. Alternatively a pair of new retransmission centers (with retransmission from other centers only) may be positioned in the Pacific Ocean.
Figure 8 is the daytime compensation scheme for 12/21/2017 11:28 PM UTC. The (civil) night areas are the areas marked with transparent gray.
Figure 9 is the daily compensation scheme for 21.06.2018 23:06 UTC. Here the retransmission center, which is in the hot season and which releases energy during the night (3), is powered by the hydrogen reserve of the Radiant plant. Conexant has 3 levels of power supply:
- base load - when Conexant delivers from the hydrogen supply,
- peaking mode 1 - when within 5,000 km (for 0-3.5 hours) the energy is delivered directly in peer to peer mode (without retransmission), direct daytime offset.
- peaking mode 2 (peaking 2) - when it can no longer be supplied in peaking 1 it is delivered at a fixed point (retransmission center).
Figure 10 is the daytime compensation scheme for 21.03.2018 22:30 UTC (after the spring equinox). All six retransmission centers may be positioned within a 70 kilometers radius away from the points mentioned above. The coordinates precision is 10 meters for theoretical purposes only. The same observation goes for the starting/ending time of the warm seaseon which may be with an additional 0-40 days delay, depending on global wheather forcasts, according to an separate alghoritm that will be established. Also theoretical is the assumption of intersecting the maximum land surface. This assumtion is made with respect to a population that will be distributed evenly in villages that have an an average of 2.236 population equivalent, that is the maximum capacity of a Radiant FWSG.
This Patent purpose is not to be a design manual. The processes described in
US Patents No 593,198 (filled on 27/03/1897),
645,576 (filled on 02/09/1897),
649,621 (filled on 19/02/1900),
787,412 (filled on 16/05/1900),
1,119,732 (filled on 18/01/1902) are linked with a phenomenon that Tesla envisioned and shall be called Wireless in Tesla's Sense (WTS). WTS is to be applied following the Patents and all his lectures and articles. The prior art mentioned is cronologically ordered so will shall mention the features that remain from older Patents. Besides WTS which is coherent in all priror art mentioned, there are two distinct stages in the Patents: one of a smaller potential and scale experiments and the other, after the return from Colorado Springs in January 1900, of a greater potential and scale, the ready to build stage. And as we already mantained there are three levels of Conexant link-up (in both senses):
- level 1 from the household to the Radiant FSWG or from FWSG's reserve;
- level 2 from the FWSG to the retransmission centers or between 2 FWSG's;
- level 3 between retransmission centers.
Tesla builtlevel 1, experimental transmitters, then the prototype he tried to put in operation was alevel 2 for which he secured a reserve by making bigger the storage capacity of the condenser. So, having in view that in the present patent we deal with the whole system we shall mention only the differences and as already stated the features that remain from older patents.The first feature, presented in
US 593,138 is the conical spiral coil. Tesla used for the prototype an undeground structure that used the deep aquifers with very deep shafts. For
level 1 which is used at a range of 0-5 km and with transmitters at every house hold, we intend to use close-to-surface waterflows, namely wastewater. For this the grounding will be something like a cross formed by two semi-elipses intersected and conected to a central conductor, like an inversed lightning-protector from
Figure 5US 1,266,175 (filled by Tesla in 06/05/1916). And between excitation coil at the household and the grounding cross, the wastewater pipe will be positioned. Besides using the close to surface waterflows, this design is electrical shock hazard free. In respect with the conical spiral coil we have a new winding geometry for the single layer coil, named Io, based on the following equations:
and
Where the general equation of the winding, Io, is the reunion of G1 and G2 parametric curves witht (real number) beeing the parameter,r (real number) beeing the scale factor andk (natural number) beeing the closeness factor. The general equation curves forr=1, k=1 andt ∈ [-2,2] are inFigure 11 andFigure 12.
The two curves describing the winding have all points in the surface of two Gabriel's horns or they are enveloping the surface of two rectangular hyperbolas rotated around their asymptotes. The bigger is the closeness factork, the greater is the number of spins of the windings that are on the same Gabriel's horn. The biggest number of spins of each winding is around the vertex of the hyperbola. The bigger is the scale factorr the greater the diameter corresponding to the vertex, in other words the scale factor can be used for dimensioning a winding by transformingx(t), y(t) andz(t) in axis for measuring real lenghts.
Io can be used in the case of a homopolar generator (HPG) or a homopolar motor (HM), the space between the windings being the transfer surface which can also use new methods for transfer from a stationary to a rotating system. The rotor will also have a corresponding stator. The original idea for this HPG is mentioned in Nikola Tesla's article from "The Electrical Engineer", N.Y, Sept. 2, 1891.
Regarding the use in Conexant concept, the use of G1 and G2 will be restricted to only one of them, G2 will be used only in the northen hemisphere,Figure 11 rotated clockwise untilx = -∞ is at the top of the page and G1 will be used in the southern hemisphere,Figure 11 rotated counterclockwise untilx = -∞ is at the bottom of the page.
In conclusion, the secondary conical coil presented in
Figure 1 and
Figure 2 of the patent
US 593,138 will be replaced by G1 or G2, depending of the Earth's hemisphere. The curve of the secondary winding will be equally distanced from the hyperbola's vertex. The primary winding will be at the base of the secondary on a slightly bigger diameter corresponding to the vertex, and it will be calculated using a bigger scale factor. The second secondary coil presented in
US Patent 1,119,732 will remain as it is. The frequncies will be: level 1- greater or equal to 7.83 Hz, level 2-greater than 7 kHz, level 3-greater than 2 Mhz and flywheels may be used at all levels for momentary storing the energy. For opening comunication channels phase-shifting will be used.
Furthermore from the "state of the art" which is presented in Tesla's Patents lectures and articles there are no other observations. Nevertheless WTS implies a great importance given to:
- total length of the secondary circuit which is approximately one-quarter of the wave length of the electrical disturbance in the circuit which can be achevied at low frequencies by using thin graphene-infused copper wires;
- very large self-inductance and a comparatively small capacity;
- if necessary, for predimensioning the secondary coil, the calculus of hyprebola lenght by means of ellipic integrals, in order be divided to an wire diameter and also the total lenght of G1 or G2 coil wire;
- inductance calculations formulae for variable-pitch multi-section helical coils by means of elliptic integrals;
- capacitance to ground calculation formulae for sphere or toroid also by means of elliptic integrals.