Uses of hydrocarbon nanorings
10072642 ยท 2018-09-11
Inventors
Cpc classification
Y10S977/932
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F03H3/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B82Y30/00
PERFORMING OPERATIONS; TRANSPORTING
B64G1/409
PERFORMING OPERATIONS; TRANSPORTING
H04B13/00
ELECTRICITY
H02N11/00
ELECTRICITY
Y10S977/771
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
F02C1/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03H99/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B64G1/40
PERFORMING OPERATIONS; TRANSPORTING
F03H3/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H02N11/00
ELECTRICITY
B82Y30/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
Hydro-carbon nanorings may be used, e.g., in power storage power transmission and transportation. Sufficiently cooled, an externally hydrogen doped carbon nanoring may be used to create a radial dipole containment field for electrons rotating in the nanoring. Such nanorings may transmit DC current with little or no loss. Similarly, an internally hydrogen doped carbon nanoring may be used to create a radial dipole containment field for positrons rotating in the nanoring. Virtually lossless transmission of AC current may be achieved by pairing such streams of electrons and positrons in their respective containment fields. Closed rotation of such streams may also be used to efficiently store large amounts of electrical energy. Finally, selectively accelerating and decelerating pairs of such paired electron and positron streams, which are moving at relativistic speeds, differential momentum may be created to cause physical movement.
Claims
1. A propulsion apparatus for moving a craft, including: at least one first pair of primary rings, each containing a stream of electrons circulating at relativistic speed, wherein the streams of electrons in the respective primary rings of the first pair of primary rings circulate in opposite directions to each other; and at least one second pair of primary rings, each containing a stream of positrons, each circulating at relativistic speed, wherein the streams of positrons in the respective primary rings of the second pair of primary rings circulate in opposite directions to each other; wherein each of said primary rings of said at least one first pair of primary rings and said at least one second pair of primary rings consists of two straight tubes, each coupled to first and second curved tubes at respective first and second ends of each of said straight tubes; and wherein said propulsion apparatus is configured to move by accelerating said streams of electrons and said streams of positrons through said first curved tubes and decelerating said streams of electrons and said streams of positrons through said second curved tubes.
2. The propulsion apparatus as in claim 1, wherein each of said at least one first pair of primary rings contains a first and a second ring of each respective pair of said at least one first pairs of primary rings, and wherein each said at least one second pair of primary rings contains a first and second ring of each respective pair of said at least one second pairs of primary rings, wherein the streams of electrons in said first rings of each of said at least one first pair of primary rings and the streams of positrons in said first rings of each of said at least one second pair of primary rings all circulate in a first direction, and the streams of electrons in said second rings of each of said at least one first pair of primary rings and the streams of positrons in said second rings of each of said at least one second pair of primary rings all circulate in a second direction, wherein said first direction is opposite said second direction, and wherein said straight tubes of said first rings of said at least one first pair of primary rings are electrically coupled to said straight tubes of said first rings of said at least one second pair of primary rings, said straight tubes of said second rings of said at least one first pair of primary rings are electrically coupled to said straight tubes of said second rings of said at least one second pair of primary rings, said curved tubes of said first rings of said at least one first pair of primary rings are magnetically coupled to said curved tubes of said second rings of said at least one second pair of primary rings, and said curved tubes of said second rings of said at least one first pair of primary rings are magnetically coupled to said curved tubes of said first rings of said at least one second pair of primary rings.
3. A propulsion apparatus as in claim 1, including at least one control loop, wherein said at least one control loop is configured to accelerate said streams of electrons in said first curved tubes of each of said at least one first primary ring, and to accelerate said streams of positrons in said first curved tubes of each of said at least one second primary ring and to decelerate said streams of electrons in said second curved tubes of each of said at least one first primary ring, and to decelerate said streams of positrons in said second curved tubes in each of said at least one second primary ring by electrically coupling said streams of electrons and said streams of positrons with streams of electrons in said at least one control loop.
4. A propulsion apparatus as in claim 3, wherein said streams of electrons in said at least one first pair of primary rings and said streams of positrons in said at least one second pair of primary rings are accelerated to relativistic speed by issuing sets of electrical pulses coupled into said stream of electrons within said at least one control loop in synchronization with the speed of said streams of electrons in said at least one first pair of primary rings and said streams of positrons in said at least one second pair of primary rings.
5. A propulsion apparatus as in claim 1, including at least two control loops; wherein a first of said at least two control loops is configured to accelerate said streams of electrons from a center of said first curved tube to the first end of a first of the two connecting straight tubes in at least one first pair of primary rings, to accelerate streams of positrons from the center of said first curved tube to the first end of a first of the two connecting straight tubes in at least one second pair of primary rings, to decelerate said streams of electrons from a center of said second curved tube to the second end of said first of the two connecting straight tubes in at least one first pair of primary rings, and to decelerate streams of positrons from the center of said second curved tube to the second end of said first of the two connecting straight tubes in said at least one second pair of primary rings, by electrically coupling to said stream of electrons in said first of said at least two control loops; and wherein a second of said at least two control loops configured to accelerate said streams of electrons from the center of said first curved tube to the first end of a second of the two connecting straight tubes in said at least one first pair of primary rings, to accelerate streams of positrons from the center of said first curved tube to the first end of a second of the two connecting straight tubes in said at least one second pair of primary rings, to decelerate said streams of electrons from the center of said second curved tube to the second end of said second of the two connecting straight tubes in said at least one first pair of primary rings, and to decelerate streams of positrons from the center of said second curved tube to the second end of said second of the two connecting straight tubes in said at least one second pair of primary rings, by electrical coupling to said stream of electrons in said second of said at least two control loops, thereby turning said craft when inducing a different currents respectively into each of said at least two control loops.
6. A propulsion apparatus as in claim 5, wherein said primary rings of said at least one first pair of primary rings and at least one second pair of primary rings and said at least two control loops are composed of hydrocarbon nanorings.
7. A propulsion apparatus as in claim 6, wherein said hydrocarbon nanorings form radial dipole fields sufficient to contain said streams of electrons within said at least one first pair of primary rings and to contain said streams of positrons within said at least one second pair of primary rings and said streams of electrons in said at least two control loops.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) In the accompanying drawings, reference characters refer to the same parts throughout the different views. The drawings are not necessarily to scale; emphasis has instead been placed upon illustrating the principles of the invention. Of the drawings:
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DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
(21) Reference is made to
(22) Reference is now made to
(23) Now let's look at the atomic structure of such a doped nanoring. Reference is now made to
(24) On the other hand, the hydrogen protons and electrons form many electrical dipoles evenly spaced just outside of the neutral shell of the nanoring, with each of the hydrogen's electron between its proton and the carbon in the shell of the nanoring. It should be understood, that other alkali metals such as lithium or sodium may be as good, or even better than Hydrogen, in this structure.
(25) Given this structure let's look at the forces on an electron in the middle of the circle. Reference is now made to
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(27) Clearly at point 43 the force is 0, because a=0 and ? sin(?)=0, but for all other locations the field pushes the charge toward the center. The protons 44 are outside of their electrons 43 in the dipole. The protons charges create a field of attraction that, to the first order, pulls a electron in the center of the ring toward the edge of the ring by F=?q.sup.2/(r+b).sup.2 where b is the distance between the dipole charges, but the Hydrogen's electron pushes the electron away with a force F=q.sup.2/r.sup.2 so the net field is E=q[1/r.sup.2?1/(r+d).sup.2], a dipole field that is the sum of the two fields.
(28) More specifically, the distance of a hydrogen-carbon bond is ?109 picometers. It is therefore reasonable to assume ?54 picometers between the proton and electron of the hydrogen atom on the inside wall of a 256 hexagonal carbon linked tube, which would be about 10 nanometers in radius. This nanotube's dipole electric field is sufficient to keep an electron moving within the nanotube as long as the tube is not bent too tightly. Furthermore as the electron's velocity approaches the speed of light, its effective mass and charge perpendicular to its direction of travel both grow as 1/(1?v.sup.2/c.sup.2).sup.1/2 where c is the speed of light. This effectively cancels the centripetal force up to the bonding energy of the nanotube.
(29) Inserting electrons into such a structure may be accomplished by charging the nanoring while surrounding it with a constant magnetic field. Charging the nanoring will drive excess electrons into the center of the ring. While the ring is under a magnetic field, the excess electrons will flow around the ring accelerating until the magnetic field is canceled. Clearly, each additional electron in the tube forces the rest of the electrons to redistribute such that they are equally spaced around the ring. As such, each electron reduces the distance between the electrons in the circulating stream, thereby requiring an increasing voltage (or electrical force) to insert subsequent electrons into the ring. The force to insert another electron into a ring of electrons equally spaced apart is q.sup.2(n+1).sup.2/d.sup.2, where q is the charge of the electrons, d is the length of the nanoring, and n is the number of electrons in the ring. Clearly, the voltage goes no by the square of the inserted charge. Given a low enough temperature, the stream of electrons, which is not bound by the individual atoms in the structure, should move around the ring without resistance. Furthermore, once the electrons are circulating in the ring they should stay in the ring unless external electrical fields are strong enough to dislodge them.
(30) As with other superconducting structures, the free electrons in the tube may form cooper pairs, which would collapse the spacing between the charges because the force of 2q/R.sup.2 is twice the force between cooper pairs which is 4q/(2R).sup.2=q/R.sup.2, where R is the distance between the electrons. In other words it is likely that when cooper pairs form, it will require less voltage to insert subsequent electrons into the ring, until the ring is filled with cooper pairs.
(31) Reference is now made to
(32) Clearly the repulsive forces between the two electron streams in the two nanotubes 51 and 52 may be controlled so they do not of the dipole field which keeps the electrons in the nanoring. Furthermore, as the currents increase the repulsive force between the nanotubes 51 and 52 increases by the relativistic factor 1/(1?4 v.sup.2/c.sup.2). In other words there is a maximum current carrying capacity for any given distance separating the two nanotubes 51 and 52. This limit may be increased by separating the nanotubes, or shielding their electrostatic charge with a correspondingly positively charged conductor 57 between the pair nanotubes.
(33) Similar to other superconducting structures, this nanoring should transmit a constant amount of power without any resistive losses characteristic of normal transmission lines. On the other hand, changes in the load 56 may result in changes of the current flowing down the pair of nanotubes 51 and 52, creating electromagnetic losses. Shortening the distance between the nanotubes 51 and 52 should help cancel the opposing differential waveforms on the pair of nanotubes, caused by the changes in the source 55 generation or load 56 demand, which would greatly reduce the electromagnetic losses, but it would also significantly reduce the power carrying capacity of the nanotubes.
(34) Alternatively, these electromagnetic losses may be eliminated by placing a similarly doped but physically different nanoring with opposite charges next to the existing nanoring 50, such that their currents cancel between the source and load.
(35) Reference is now made to
(36) Reference is now made to
(37) Positrons may be created for Positron Emission Tomography by bombarding hydrogen into Oxygen, with an atomic weight of 17, or Oxygen-17, producing a radioactive isotope Fluorine-18, which decays into a positron and Oxygen-18. Alternatively bombarding hydrogen into Oxygen-16 produces Nitrogen-13 and an alpha particle, Helium. The Nitrogen-13, has a ten minute half life, breaking down into Carbon-13 and a positron. By injecting protons into an interior doped nanoring with such embedded Nitrogen, while under a sufficiently strong enough magnetic field to move the subsequently created positrons, they will enter the interior of the nanoring and will continue to move down the nanoring while other non-reacting protons may attach to available sites on the newly created carbon-13 in the nanoring. To enhance this process, the nanoring may be initially charged. Once injected with positrons the radial dipole field should continue to contain the positrons.
(38) Alternatively, with the proper structure such as shown in
(39) It is further suspected, but not known, that the positrons may form pairs in a manner corresponding to electrons forming cooper pairs, increasing their density in a manner similar to and under similar but oppositely charged conditions as electrons.
(40) It is further contemplated that multiple nanorings of both types may be combined together to form a larger lossless electrical transmission cable. Reference is now made to
(41) Reference is now made to
(42) Reference is now made to
(43) It is further contemplated that the transmission structure shown in
(44) Such a structure has no apparent magnetic field except at the twisted ends of the structure, yet it can contain a large amount of energy in the form of relativistic mass of the electrons and positrons. In normal conductors the moving electrons appear stronger by a factor of (1?V.sup.2/C.sup.2).sup.1/2, due to the Lorentz contraction. This results in a corresponding magnetic force, but the force is cancelled in the transmission structure shown in
(45) This leads into another use of hydro-carbon nanorings, translation of relativistic rotational energy into translational movement, which may be used e.g., to propel it craft. A plurality of pairs of streams of positrons and electrons embedded in adjacent appropriately structured oval nanorings, organized in a manner similar to the transmission lines of
(46) These nanorings also have the characteristic of being superconducting when brought down to a sufficiently low temperature, which means when a superconducting nanoring is subjected to an external magnetic field, electrons will move forming a circular current about the ring to cancel the external magnetic field. Furthermore two sufficiently adjacent electron currents going in opposite directions may cancel their magnetic fields, which by this magnetic coupling may cancel their differential momentum. As a result superconducting nanorings may be used as superconducting transmission lines to transfer the energy from one end of the craft to the other.
(47) In one embodiment these transmission lines may be composed of nanorings carrying streams of electrons. For brevity we will call these transmission lines the control loop 111 as shown in
(48) To initiate movement in the apparatus of
(49) In an actual system there may be as many control loops as needed to transfer the energy into and out of the primary rings, and as many primary rings as needed to transfer an adequate amount of relativistic mass to cause motion of the apparatus. As was described above, the control loops are superconducting transmission lines transferring energy between the ends of the oval primary rings, where the ratio of the number of control loops to each primary ring acts like a superconducting DC transformer at each end of the craft. This ratio determines the force or voltage with which the energy is transferred into or out of the primary rings. The pairs of primary rings may be re-oriented or grouped to transfer the control loop's energy into or out of the primary rings.
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(51) By surrounding the primary nanorings with parts of control loops, and balancing the current in both directions in the control loops as well as the primary nanorings, the stray electromagnetic energy is minimized with respect to changes resulting in accelerations and decelerations of the overall craft.
(52) It should be noted here that the electrical and magnetic forces and aids between the primary rings differ significantly from normal currents, and may need to be separately analyzed for the straight and curved portions of the oval, because these charged particle streams are moving at relativistic speeds in electrically neutral nanotubes, as opposed to normal current, which consists of displaced electrons moving in an oppositely charged conductive medium.
(53) The initial operation of the disclosed system is as follows: Inducing a current in one direction one side of the control loop, and an equal current in the opposite direction of the other side of the control loop, may be accomplished by flowing current in opposite directions through the lines differentially coupled to the control lines in the center of the craft as shown in 114,
(54) In such an embodiment, the lateral forces in the primary and control rings cancel, because the particles in them are being equally accelerated and decelerated opposite to each other at the ends and middle of the respective rings. Rotational forces cancel because the particles in the primary rings and control rings are circulating in equal and opposite directions, which leaves the force of accelerating and decelerating the particles in the primary rings and the control rings. This produces motion in an apparatus of length L as follows: To transfer energy from one end of the craft to the other, the control rings have slower, higher density particle streams going from the positive coupled to the negative coupled end, and faster, lower density streams moving in the opposite direction. Since both skies of the control rings 111 in
(55) On the other hand, currents in the primary ring are moving at relativistic speeds, which means the mass of the particles significantly change with small changes in velocity. The mass of the accelerated particles Mx=M/[1?(V+dv).sup.2/C.sup.2].sup.1/2 is much greater than the mass of the decelerated particles My=M/[1?(V?dv).sup.2/C.sup.2].sup.1/2. Since the differential velocity dv is small, and the basic relativistic velocity V is large, the density of the particle streams changes far less than the mass of the particles change. As a result, over the length of straight portion of the oval there is a differential momentum approximately equal to (Mx?My)V. This differential momentum in one direction is offset by the apparatus or craft moving in the opposite direction.
(56) In other words, energy is being constantly transferred between the primary and control loops, but, as can be seen in
(57) The craft accelerates until the accelerated and decelerated streams of particles reach the other end of the craft, after which these initial forces balance, but the initial change also causes a continuous transfer of energy in the control loops from the decelerating end to the accelerating end of the craft. Since the energy taken from the decelerated stream equals the energy added to the accelerated stream of particles, there is no net energy lost in the primary rings, except what is distributed into a magnetic field induced by the control loop itself and the kinetic energy of the whole craft. The velocity of the craft and the control current continues to increase until the energy initially induced into the control loop is distributed between the magnetic field of the control loop and the motion of the craft. While a huge amount of energy is continually transferred through the control loops, very little of that energy is stored in the control loop's magnetic field because the cross sectional area of the control loop is extremely small, which limits the stored energy, so a large percentage of the induced energy is transferred into the kinetic energy of the craft. Some losses may occur in electromagnetic radiation due to the changing electromagnetic fields, but these will be small due to the limited distances between and characteristics of the primary rings.
(58) After the acceleration and deceleration of the particle streams in primary rings stabilize, the forces again cancel, with the craft moving at a constant velocity. At that point, there should be no electromagnetic radiation because, the currents varying currents completely cancel, so there are no changes to the electromagnetic fields. The control loop will continue to transfer energy from the decelerating end and supply it to the accelerating end, of the craft as it continues its relativistic momentum transfer, and in a frictionless environment, the corresponding velocity will continue with no energy lost because the rings are all superconducting. On the other hand, if there is any leakage due to transmission inefficiencies or if there is any resistance due to air or other friction, it will require a constant flow of energy equivalent to these losses to maintain the craft's velocity.
(59) This constant velocity can be determine by the net differential momentum moving opposite the velocity vector of the craft at any instant in time. If the craft is moving at a velocity, and the control current isn't changing, there is no acceleration, and the differential momentum is stable. The differential mass M.sub.d is moving at close to the speed of light so the differential momentum is ?M.sub.dC. Now if the mass of the craft is M.sub.t, to the first order the velocity of the craft is simply V.sub.t=?M.sub.dC/M.sub.t, because the resulting velocity is much less than the speed of light, and Newtonian calculations are a good approximation at non-relativistic velocities. The oval shown in
(60) As an additional current is induced throughout the whole control loop the streams or particles in the primary rings are accelerated to higher mass on one side of the ring and lower mass on the other side, the forces on the craft, which were initially balanced, become imbalanced, causing acceleration of the craft in the opposite direction to the transfer of differential momentum. Furthermore, this acceleration continues as energy is transferred by the control loop further decelerating the streams of particles at one end and accelerating them at the other until the energy originally induced into the control loop is either stored in the control loop's magnetic held or transferred into translational energy of the overall craft.
(61) Movement up through a gravitational field may also be determined by the energy required for such movement. Absent other forces, the craft should rise to the level determined by the energy transferred to the craft. Conversely, decreases in velocity, or down through a gravitational field, may be obtained by extracting energy out of the control rings. Reducing the control current to zero should bring the craft to its initial velocity, or will reduce the energy of the object the craft has come in contact with.
(62) The maximum velocity, or distance through a gravitational well may be determined by the amount of energy stored in the primary rings. The apparatus, e.g., craft's, velocity may be changed by increasing the acceleration and deceleration of the particle streams in the primary rings. At some point the velocity difference between the accelerated and decelerated rings becomes large enough to be offset by density changes in the particle streams, limiting further increases in velocity. In this manner the amount of relativistic mass contained in the primary rings prior to moving the craft determines the maximum velocity the craft can obtain.
(63) In another embodiment of the invention, the control loops may be used to accelerate the streams of particles in the primary rings thereby increasing the relativistic mass of their particle streams.
(64) In yet another embodiment of the present invention, by offsetting the coupling of two or more portions of the control loops at the curved ends of the primary rings, turning the craft is merely a matter of using only one of these two or more control loops or inducing more current in some than others. The net effect is to move the craft more to the right or left, depending on which side has accelerated or decelerated the streams in the primary rings. In
(65) It will be appreciated by persons skilled in the art that the present invention is not limited by what has been particularly shown and described hereinabove. Rather the scope of the present invention includes both combinations and sub-combinations of various features described hereinabove as well as modifications and variations which would occur to persons skilled in the art upon reading, the foregoing description and which are not in the prior art.