The technical field generally relates to plasma technologies and, more particularly, to plasma focus systems and methods.
Dense plasma focus systems (or simply plasma focus systems) are pinch-based plasma generation systems in which a high pulsed voltage is applied between two coaxial electrodes disposed inside a vacuum chamber filled with a process or working gas. The coaxial electrodes extend from a closed end to an open end, with an electrical insulator disposed between the electrodes at the closed end. The application of the voltage leads to the ionization and breakdown of the gas on the insulator, and the formation of a plasma shockwave-current-sheath layer, hereinafter referred to as a plasma current sheath for simplicity. Under the effect of the Lorentz force created by the radial current flowing in the plasma and the current-induced azimuthal magnetic field, the current sheath is driven axially along the electrodes toward the open end. Upon reaching the open end, the current sheath is radially compressed onto the axis to form a hot and dense pinch plasma column. During the pinch phase, plasma instabilities can lead to the emission of electron and ion beams, electromagnetic radiation pulses (e.g., X-rays), and, if the working gas contains neutronic fusion fuel, neutrons. In fusion power applications, the kinetic energy of the fusion neutrons is converted into thermal energy, which is subsequently converted into electricity. Problems and limitations associated with neutronic fusion include structural radiation damage, radioactive waste produced by neutron activation, indirect conversion of fusion energy into electricity, and the requirements for biological shielding. It is envisioned that aneutronic fusion could help mitigate these problems and limitations.
The present description generally relates to plasma focus systems and methods for producing aneutronic fusion.
In accordance with an aspect, there is provided a plasma focus system for aneutronic fusion, the plasma focus system including:
In some embodiments, the tapered tip tapers from a first radius, at a taper start point located between the discharge end and the focus end, to a second radius, at the focus end, wherein a ratio of the first radius to the second radius is greater than twenty. In some embodiments, the ratio of the first radius to the second radius ranges between from about twenty to about one hundred.
In some embodiments, the first radius ranges from about 2 cm to about 40 cm and the second radius ranges from about 1 mm to about 20 mm. In some embodiments, the tapered tip tapers from the first radius to the second radius at a tapering angle ranging from about 40° to about 85°, wherein the tapering angle is defined with respect to a direction parallel to the pinch axis. In some embodiments, the tapered tip tapers linearly from the first radius to the second radius. In other embodiments, the tapered tip tapers nonlinearly from the first radius to the second radius.
In some embodiments, the tapered tip has a longitudinal extent ranging from about 1 cm to about 10 cm. In some embodiments, a ratio of the longitudinal extent of the tapered tip to a longitudinal extent of the inner electrode ranges from about 0.05 to about 0.7.
In some embodiments, a ratio of a longitudinal extent of the inner electrode to a diameter of the inner electrode at the discharge end is greater than one. In other embodiments, a ratio of a longitudinal extent of the inner electrode to a diameter of the inner electrode at the discharge end is equal to or less than one.
In some embodiments, the tapered tip has a hollow interior configured to allow the plasma pinch to extend at least partially thereinside.
In some embodiments, the power supply unit includes a pulsed-DC power supply including a capacitor bank and a switch.
In some embodiments, the power supply unit is configured to apply the discharge driving signal as a voltage pulse having a peak magnitude ranging from about 12 kV to about 1 MV, a half-cycle pulse duration ranging from about 1 μs to about 50 μs, and a peak current amplitude ranging from about 100 kA to about 10 MA.
In some embodiments, the power supply unit is configured to apply the discharge driving signal once every one minute to sixty minutes, corresponding to a single-shot operation mode. In some embodiments, the power supply unit is configured to apply the discharge driving signal once every ten milliseconds to ten seconds, corresponding to a repetitive-shot operation mode.
In some embodiments, the power supply unit is configured to apply the discharge driving signal based on the configuration of the tapered tip to control the speed of the plasma current sheath to reach a maximum sheath speed value ranging from about 100 cm/μs to about 1,000 cm/μs as the plasma current sheath collapses toward the pinch axis to form the plasma pinch. Such maximum sheath speed values are higher than the maximum speed values of plasma current sheaths in the radial phase of non-tapered arrangements, which can range from about 14 cm/μs to about 30 cm/μs. In some embodiments, the plasma focus system is configured to increase a maximum speed of the plasma current sheath by a speed-enhancement factor ranging from about eight to about fifty compared to conventional plasma focus systems provided with non-tapered inner electrodes.
In some embodiments, the power supply unit is configured to apply the discharge driving signal based on the configuration of the tapered tip to form the plasma pinch with a pinch temperature ranging from about 30 keV to about 500 keV.
In some embodiments, the power supply unit is configured to apply the discharge driving signal to control the speed of the plasma current sheath prior to the tapered tip to remain below a threshold sheath speed value at which the plasma current sheath undergoes mass-field-force-field separation. In some embodiments, the threshold sheath speed value is about 10 cm/μs.
In some embodiments, the electrode assembly includes an electrical insulator interposed between the inner electrode and the outer electrode at the discharge end.
In some embodiments, the plasma focus system includes a vacuum chamber housing at least part of the electrode assembly and configured to contain the process gas therein. In some embodiments, the outer electrode forms part of the vacuum chamber.
In some embodiments, the plasma focus system includes a process gas supply unit configured to supply the process gas inside the plasma channel. In some embodiments, the vacuum chamber can include at least one gas inlet port configured for connection to the process gas supply unit to allow the process gas to be introduced inside the vacuum chamber, and thus inside the plasma channel.
In some embodiments, the aneutronic fusion fuel includes the aneutronic fusion fuel includes decaborane B10H14 (for the p-11B reaction), or deuterium-helium-3 (for the D-3He reaction), or helium-3 (for the 3He-3He reaction), or lithium hydride (for the p-6Li reaction or the p-7Li reaction), or lithium deuteride (for the D-6Li reaction), or any other practical aneutronic fusion fuel, or any combination thereof. In some embodiments, the process gas is filled or created with the help of a discharge or laser irradiation inside the vacuum chamber with a fill pressure equivalent which ranges from about 1 Torr to about 100 Torr. For example, decaborane, lithium hydride, and lithium deuteride are solid at room temperature and can be sublimated into gaseous form by an electric discharge or pulsed laser irradiation prior to the main discharge.
In some embodiments, the plasma focus system includes a direct energy conversion unit configured to extract energy from reaction products of the aneutronic fusion reactions and convert the extracted energy into electricity.
In some embodiments, a fill pressure of the process gas inside the plasma channel ranges from about 1 Torr to about 100 Torr.
In some embodiments, the inner electrode is configured as an anode and the outer electrode is configured as a cathode, in that the inner electrode is positively biased with respect to the outer electrode. In other embodiments, the polarity of the inner and outer electrodes is reversed.
In accordance with another aspect, there is provided a plasma focus method of aneutronic fusion, including:
In some embodiments, providing the plasma focus system includes configuring the tapered tip to taper from a first radius, at a taper start point located between the discharge end and the focus end, to a second radius, at the focus end, wherein a ratio of the first radius to the second radius ranges from about twenty to about one hundred. In some embodiments, the first radius ranges from about 2 cm to about 40 cm and the second radius ranges from about 1 mm to about 20 mm. In some embodiments, configuring the tapered tip includes providing the tapered tip with a tapering angle ranging from about 400 to about 85°, wherein the tapering angle is defined with respect to a direction parallel to the pinch axis.
In some embodiments, configuring the tapered tip includes providing the tapered tip with a longitudinal extent ranging from about 1 cm to about 10 cm.
In some embodiments, applying the discharge driving signal includes applying the discharge driving signal as a voltage pulse having a peak magnitude ranging from about 12 kV to about 1 MV, a half-cycle pulse duration ranging from about 1 μs to about 50 μs, and a peak current amplitude ranging from about 100 kA to about 10 MA.
In some embodiments, applying the discharge driving signal includes applying the discharge driving signal once every one minute to sixty minutes, corresponding to a single-shot operation mode. In some embodiments, applying the discharge driving signal includes applying the discharge driving signal once every ten milliseconds to ten seconds, corresponding to a repetitive-shot operation mode.
In some embodiments, applying the discharge driving signal includes controlling the discharge driving signal based on the configuration of the tapered tip to control the speed of the plasma current sheath to reach a maximum sheath speed value ranging from about 100 cm/μs to about 1,000 cm/μs as the plasma current sheath collapses toward the pinch axis to form the plasma pinch.
In some embodiments, applying the discharge driving signal includes controlling the discharge driving signal based on the configuration of the tapered tip to form the plasma pinch with a pinch temperature ranging from about 30 keV to about 500 keV.
In some embodiments, applying the discharge driving signal includes controlling the discharge driving signal to control the speed of the plasma current sheath prior to the tapered tip to remain below a threshold sheath speed value at which the plasma current sheath undergoes mass-field-force-field separation. In some embodiments, the threshold sheath speed value is about 10 cm/μs.
In some embodiments, providing the plasma focus system includes enclosing at least part of the electrode assembly in a vacuum chamber configured to contain the process gas therein.
In some embodiments, the aneutronic fusion fuel includes decaborane B10H14, for the p-11B reaction; or deuterium-helium-3, for the D-3He reaction; or helium-3, for the 3He-3He reaction; or lithium hydride, for the p-6Li reaction or the p-7Li reaction; or lithium deuteride for the D-6Li reaction; or any combination thereof.
In some embodiments, the method further includes extracting energy from reaction products of the aneutronic fusion reactions, and converting the extracted energy into electricity
In accordance with another aspect, there is provided a plasma focus system for aneutronic fusion, the plasma focus system including:
Other method and process steps may be performed prior, during, or after the steps described herein. The order of one or more steps may also differ, and some of the steps may be omitted, repeated, and/or combined, as the case may be.
Other objects, features, and advantages of the present description will become more apparent upon reading of the following non-restrictive description of specific embodiments thereof, given by way of example only with reference to the appended drawings. Although specific features described in the above summary and in the detailed description below may be described with respect to specific embodiments or aspects, it should be noted that these specific features may be combined with one another unless stated otherwise.
In the present description, similar features in the drawings have been given similar reference numerals. To avoid cluttering certain figures, some elements may not be indicated if they were already identified in a preceding figure. The elements of the drawings are not necessarily depicted to scale, since emphasis is placed on clearly illustrating the elements and structures of the present embodiments. Furthermore, positional descriptors indicating the location and/or orientation of one element with respect to another element are used herein for ease and clarity of description. Unless otherwise indicated, these positional descriptors should be taken in the context of the figures and should not be considered limiting. Such spatially relative terms are intended to encompass different orientations in the use or operation of the present embodiments, in addition to the orientations exemplified in the figures. Furthermore, when a first element is referred to as being “on”, “above”, “below”, “over”, or “under” a second element, the first element can be either directly or indirectly on, above, below, over, or under the second element, respectively, such that one or multiple intervening elements may be disposed between the first element and the second element.
The terms “a”, “an”, and “one” are defined herein to mean “at least one”, that is, these terms do not exclude a plural number of elements, unless stated otherwise.
The term “or” is defined herein to mean “and/or”, unless stated otherwise.
The expressions “at least one of X, Y, and Z” and “one or more of X, Y, and Z”, and variants thereof, are understood to include X alone, Y alone, Z alone, any combination of X and Y, any combination of X and Z, any combination of Y and Z, and any combination of X, Y, and Z.
Terms such as “substantially”, “generally”, and “about”, which modify a value, condition, or characteristic of a feature of an exemplary embodiment, should be understood to mean that the value, condition, or characteristic is defined within tolerances that are acceptable for the proper operation of this exemplary embodiment for its intended application or that fall within an acceptable range of experimental error. In particular, the term “about” generally refers to a range of numbers that one skilled in the art would consider equivalent to the stated value (e.g., having the same or an equivalent function or result). In some instances, the term “about” means a variation of 10% of the stated value. It is noted that all numeric values used herein are assumed to be modified by the term “about”, unless stated otherwise. The term “between” as used herein to refer to a range of numbers or values defined by endpoints is intended to include both endpoints, unless stated otherwise.
The term “based on” as used herein is intended to mean “based at least in part on”, whether directly or indirectly, and to encompass both “based solely on” and “based partly on”. In particular, the term “based on” may also be understood as meaning “depending on”, “representative of”, “indicative of”, “associated with”, “relating to”, and the like.
The terms “match”, “matching”, and “matched” refer herein to a condition in which two elements are either the same or within some predetermined tolerance of each other. That is, these terms are meant to encompass not only “exactly” or “identically” matching the two elements, but also “substantially”, “approximately”, or “subjectively” matching the two elements, as well as providing a higher or best match among a plurality of matching possibilities.
The terms “connected” and “coupled”, and derivatives and variants thereof, refer herein to any connection or coupling, either direct or indirect, between two or more elements, unless stated otherwise. For example, the connection or coupling between elements may be mechanical, optical, electrical, magnetic, thermal, chemical, fluidic, logical, operational, or any combination thereof.
The term “concurrently” refers herein to two or more processes that occur during coincident or overlapping time periods. The term “concurrently” does not necessarily imply complete synchronicity and encompasses various scenarios including time-coincident or simultaneous occurrence of two processes; occurrence of a first process that both begins and ends during the duration of a second process; and occurrence of a first process that begins during the duration of a second process, but ends after the completion of the second process.
The present description generally relates to plasma focus systems and methods for producing aneutronic fusion reactions. The techniques disclosed herein may be used in various fields and applications that use aneutronic energetic fusion reactions, including, to name a few, fusion power applications, direct conversion of charged particle energy to electricity, direct conversion of X-rays to electricity, and aneutronic fusion engine.
Nuclear fusion energy is energy produced by a nuclear fusion process in which at least two or more lighter atomic nuclei are joined to form a heavier nucleus whose mass is less than the sum of the masses of the lighter nuclei. The difference in mass is released as energy, which can be harnessed to produce electricity. Fusion reactions can be neutronic or aneutronic depending on whether the fusion reaction products include neutrons or not, in addition to charged nuclei. Non-limiting examples of neutronic fusion reactions include the deuterium-deuterium (D-D) reaction and the deuterium-tritium (D-T) reaction, which generates neutrons at 2.45 MeV and 14.1 MeV, respectively. Most fusion energy research is currently based on neutronic fusion, notably the D-T reaction due to its low ignition temperature and high reactivity compared to other fusion fuels. However, as noted above, neutronic fusion presents a number of challenges and issues, which include structural radiation damage, radioactive waste produced by neutron activation, indirect conversion of fusion energy into electricity, and the requirements for biological shielding. By contrast, in aneutronic fusion, no or negligible amounts of neutrons are produced, thus avoiding or mitigating the adverse effects associated with neutron radiation. Furthermore, because fusion energy is released mostly in the form of charged particles, aneutronic fusion could allow for the direct energy conversion to electricity. Non-limiting examples of aneutronic fusion reactions include the proton-boron-11 (p-11B) reaction, the deuterium-helium-3 (D-3He) reaction, the helium-3-helium-3 (3He-3He) reaction, the proton-lithium-6 (p-6Li) reaction, the proton-lithium-7 (p-7Li) reaction, and the deuterium-lithium-6 (D-6Li) reaction. The p-11B reaction is often considered as the most promising for aneutronic fusion. One challenge with aneutronic fusion is that it involves peak reactivities that are lower and that occur at higher temperatures compared to the D-T reaction, making it more difficult to reach ignition conditions.
It has been observed that a wide range of conventional neutron-optimized plasma focus systems operate with a speed factor (or drive parameter)
having a near-constant value of
where I is the peak drive current, a is the anode radius, and p is the fill gas pressure [1]. This near-constant value of S is consistent with a narrow range of peak axial speeds around 10 cm/μs and peak radial speeds around 20-30 cm/μs. These speed values lead to pinch temperatures ranging from about 0.1 keV to about 1 keV. At such pinch temperatures, the thermonuclear reactivities of several relevant aneutronic fusion reactions are very far below significant levels, which would be reached at pinch temperatures of the order of at least 30 keV. Such pinch temperatures represent an increase of about 100 times compared to pinch temperatures values observed in conventional plasma focus systems. As pinch temperature scales about quadratically with plasma speed, such an increase in pinch temperature could, in principle, be achieved by increasing the peak plasma speeds of conventional plasma focus systems by a factor of the order of 1001/2=10, that is, from about 10 cm/μs to about 100 cm/μs for the peak axial speed and from about 20-30 cm/μs to about 200-300 cm/μs for the peak radial speed. However, conventional plasma focus systems tend to not operate well above certain speeds. It was found that increasing the peak axial speed above 10 cm/μs can lead to a separation between the mass-field and the force-field in the magnetic field structure of the plasma. This separation causes the mass-field to reach the end of the axial acceleration phase and enter the radial collapse phase while the driving force-field is still in the axial phase. In this situation the force-field is pushing in the axial direction while the mass-field is already flowing in the radial direction. This angular disparity between the pushing force-field and the mass-field can result in a pinch characterized by poor compression and low fusion yield.
The present techniques aim to provide plasma focus systems and methods in which the pinch temperature can be increased sufficiently for aneutronic fusion conditions to be achievable within the pinch, but in which the angular disparity mentioned above, due to mass-field-force-field separation, can be avoided or at least mitigated. As described in greater detail below, this can be achieved at least in part by the provision of a tapered tip at the focus end of the inner electrode of the plasma focus system.
Referring to
The electrode assembly 102 includes an inner electrode 110 and an outer electrode 112 forming a plasma gun. In
Returning to
Returning to
Returning to
Referring still to
The electrode assembly 102 of
Referring still to
The vacuum chamber 106 is configured to house various components of the plasma focus system 100, including the plasma channel 114 defined in the annular gap formed between the inner electrode 110 and the outer electrode 112. The vacuum chamber 106 may be embodied by any suitable pressure vessel. In some embodiments, the vacuum chamber 106 may be provided as a cylindrical tank made of stainless steel and coaxially enclosing the electrode assembly 102. Various other configurations may be used in other embodiments. For example, in some embodiments, the outer electrode 112 may form part of the vacuum chamber 106, as depicted in the embodiment of
The process gas 116 can be any suitable gas or gas mixture containing aneutronic fusion fuel capable of undergoing aneutronic fusion reactions within the plasma focus system 100. Non-limiting examples of aneutronic fusion fuel that can be used as the process gas 116 includes decaborane B10H14 (for the p-11B reaction), deuterium-helium-3 (for the D-3He reaction), helium-3 (for the 3He-3He reaction), lithium hydride (for the p-6Li reaction or the p-7Li reaction), lithium deuteride (for the D-6Li reaction), and any other practical aneutronic fusion fuel or fuel mixtures.
The process gas supply unit 108 can include or be coupled to a gas source 138 configured to store the process gas 116. The gas source 138 can be embodied by a gas storage tank or any suitable pressurized dispensing container. The process gas supply unit 108 can also include a process gas supply line 140 connected between the gas source 138 and the gas inlet port 136 of the vacuum chamber 106 to allow the process gas 116 to enter and fill the interior of the vacuum chamber 106. The process gas supply unit 108 can also include various additional flow control devices (not shown), for example, valves, pumps, regulators, restrictors, pulsed electric discharge systems, and pulsed laser irradiation systems configured to control the introduction or the creation of the process gas 116 inside the vacuum chamber 106. It is appreciated that various configurations and arrangements are contemplated for the process gas supply unit 108, and that various gas injection techniques can be used.
The operation of embodiments of the plasma focus system disclosed herein will now be considered in greater detail, with reference to the flow diagram of
The method 200 can include a step 202 of providing a plasma focus system 100, such as the ones depicted in
The method 200 can also include a step 204 of supplying a process gas 116 containing aneutronic fusion fuel inside the plasma channel 114 formed between the inner electrode 110 and the outer electrode 112. This step 204 can be performed by using a suitable process gas supply unit 108 to supply the process gas 116 into a vacuum chamber 106 housing at least part of the electrode assembly 102. Non-limiting examples of aneutronic fusion fuels have been given above. In some embodiments, the step 204 of supplying the process gas 116 inside the plasma channel 114 can be performed over a time period ranging from about 1 second to about 100 seconds.
The method 200 can further include a step 206 of applying the discharge driving signal to the inner electrode 110 and the outer electrode 112. This step 206 can be performed by using a suitable power supply unit 104 that is part of or coupled to plasma focus system 100. For example, the power supply unit 104 can be embodied by a pulsed-DC power supply including a capacitor bank and a switch. The application of the discharge driving signal causes the process gas 116 to be ionized and to form a plasma current sheath 142 inside the plasma channel 114, at the discharge ends 120, 124 of the electrodes 110, 112. The Lorentz force drives the plasma current sheath 142 down the plasma channel 114. Upon reaching the focus end 122 of the inner electrode 110, the plasma current sheath 142 radially collapses toward the pinch axis 118 to form a hot and dense plasma pinch 144. In some embodiments, the tapered tip 128 has a hollow interior, which can allow the plasma pinch 144 to extend at least partly inside the tapered tip 128.
In some embodiments, the step 206 of applying the discharge driving signal (e.g., by discharging the capacitor bank of the power supply unit 104 into the electrode assembly 102) can be performed over a time period ranging from about 1 microsecond to about 1 millisecond. In some embodiments, the step 206 of applying the discharge driving signal can be initiated after a time delay ranging from about 1 millisecond to about 100 seconds after initiating the step 204 of supplying the process gas 116 inside the plasma channel 114. In some embodiments, the step 206 of applying the discharge driving signal can be repeated at longer intervals (e.g., the discharge driving signal is applied once every one minute to sixty minutes or longer, which can be referred to as a single-shot operation mode) or at shorter intervals (e.g., the discharge driving signal is applied once every ten milliseconds to tens seconds, which can be referred to as a repetitive-shot operation mode). In some embodiments, the processes going from the formation of the plasma current sheath to the generation of the fusion neutrons 146 can occur over a time period ranging from about 1 microsecond to about 10 microseconds.
In the plasma focus system 100 of
In addition to increasing the speed of the plasma current sheath 142 in the radial phase just before formation of the plasma pinch 144, the provision of the tapered tip 128 can allow for the angular disparity due to the mass-field-force-field separation effect mentioned above to be controlled (e.g., avoided or at least mitigated). When the plasma current sheath 142 flows along the tapered tip 128, its speed gradually increases until the plasma current sheath 142 reaches the end of the tapered tip 128, which corresponds to the focus end 122 of the inner electrode 110. Then, the radial phase begins, which leads to the formation of the plasma pinch 144. With the provision of the tapered tip 128, the plasma current sheath 142 can move at a significantly higher speed during the radial phase than in conventional plasma focus systems. This enhanced sheath speed in the radial phase can be understood from the fact that the speed factor of the plasma current sheath 142, at any radius r, is
This means that the ratio of the sheath speed at the exit of the tapered tip 128 to the sheath speed at the entrance of the tapered tip 128 is expected to scale as a1/a2. The step 206 of applying the discharge driving signal can include controlling the discharge driving signal to control a speed of the plasma current sheath 142 prior to the tapered tip to remain below a threshold sheath speed value at which the plasma current sheath 120 undergoes or is expected to undergo mass-field-force-field separation. For example, in some embodiments, the threshold sheath speed value can be about 10 cm/μs.
It is appreciated that by providing a sufficiently large tapering angle (e.g., larger than 40°), the tapered tip 128 can have both a sufficiently large radius ratio a1/a2 to achieve aneutronic fusion and a sufficiently short axial length to avoid or at least mitigate the angular disparity between the mass-field direction and the force-field direction due to the mass-field-force-field separation. It is also appreciated that in some embodiments, the plasma focus system 100 can be operated as would a conventional plasma focus system (e.g., operating with axial speeds of the order of 10 cm/μs), so that the increase in speed along the tapered tip 128 results from the provision of the tip 128 itself, without requiring additional changes in the operating parameters of the system 100 (e.g., in the operating parameters of the power supply unit 104 and/or the vacuum chamber 106).
In the plasma focus system 100 of
It is appreciated that by adjusting the radius ratio of the tapered tip 128, the pinch temperature can be increased in a controlled manner to suit a particular aneutronic fusion reaction, as different aneutronic fusion reactions involve different temperature conditions. For example, the following aneutronic fusion reactions are characterized by the following ignition temperatures: p-11B reaction: 123 keV; p-6Li reaction: 66 keV; and D-3He reaction: 58 keV. Thus, using Tpinch,no-taper=0.1 keV and Itaper/Ino-taper=0.9 as in the example above yields Tpinch,taper=123 keV for a1/a2≈39; Tpinch,taper=66 keV for a1/a2≈29; and Tpinch,taper=58 keV for a1/a2≈27.
The thermonuclear reactivity <σv> represents the fusion cross-section and relative velocity of two potential fusion reactants, averaged over the Maxwell-Boltzmann distribution. The thermonuclear reactivity <σv> characterizes the probability of a given thermonuclear fusion reaction as a function of the kinetic temperature of the reactants. The thermonuclear reactivities of many aneutronic fusion reactions, including the p-11B, p-6Li, and D-3He reactions, increase exponentially with increasing temperature in the range from 0.1 keV to 1,000 keV. For example, the thermonuclear reactivity of the p-11B reaction, <σv>p-11B, increases by about four to five orders of magnitude in the range from 20 keV (where <σV>p-11B/<σv>D-T≈10−5−10−4) to 400 keV (where <σv>p-11B≈<σv>D-T). This means that the capability of fulfilling the conditions for achieving a particular aneutronic fusion reaction can be quite sensitive to the value of the radius ratio. It has been recognized herein that because the thermonuclear reactivities <σv> of several aneutronic fusion reactions (including the p-11B, p-6Li, and D-3He reactions) increase exponentially with increasing temperatures in the range from 0.1 keV to 1000 keV, which overlaps and extends appreciably beyond the pinch temperature range observed in conventional plasma focus systems, a radius ratio a1/a2 of at least about one to two orders of magnitude (e.g., ranging from about 20 to about 100) is desirable or required in some embodiments for the tapered tip to achieve aneutronic fusion conditions.
Simulations were carried out using the Lee model code [3], a widely recognized and verified [2; pp. 510-513] code used for simulating the operation of plasma focus systems. The simulations were performed with several gases with higher atomic numbers Z than any of the possible aneutronic fusion fuel constituent mentioned above (e.g., Z=5 for boron) for the purpose of assessing the pinch temperatures that may be achieved when the plasma is subjected to the increased radiation emission due to the higher-Z effect. It is expected that the higher-Z effect would increase the radiation and lead to a certain reduction in the achievable pinch temperature. Using the Lee model code, the pinch temperature obtained for a radius ratio a1/a2=40 was 61 keV for neon (Z=10) and 105 keV with a D-T mixture. Both temperature values are lower than the pinch temperature of about 130 keV obtained from taper ratio scaling relationship introduced above (i.e., Tpinch,taper/Tpinch,no-taper˜(a1/a2)2(Itaper/Ino-taper)2). Since an aneutronic plasma would be expected to radiate more than a D-T plasma but less then a neon plasma, one may reasonably expect that the pinch temperature of the aneutronic plasma with a1/a2=40 would lie somewhere in the range from 61 keV to 105 keV if radiation emission is accounted for. In fact, considering in more detail the Z-dependence of radiation emission, it is expected that the pinch temperature of the aneutronic plasma would be much closer (i.e., 94 keV) to that of the simulated D-T plasma (i.e., 105 keV) than to that of the simulated neon plasma (i.e., 61 keV). This reduction in pinch temperature due to radiation emission may be accounted for in the taper ratio scaling relationship by introducing a correction factor, Cradiation, such that Tpinch,taper/Tpinch,no-taper˜Cradiation(a1/a2)2(Itaper/Ino-taper)2. Using Cradiation≈¾ (i.e., from 125 keV/94 keV≈¾), one finds that Tpinch,taper=123 keV for a1/a2≈45 instead of a1/a2≈39; Tpinch,taper=66 keV for a1/a2≈33 instead of a1/a2≈29; and Tpinch,taper=58 keV for a1/a2≈31 instead of a1/a2≈27. It is appreciated that the impact of radiation emission on reducing pinch temperature could be accounted for with only a modest increase (i.e., of the order of Cradiation1/2) in the value of the radius ratio a1/a2. It is also appreciated that different values of Cradiation can be used in other embodiments depending, for example, on the operation conditions and the type of aneutronic fusion fuel, and that different or more complex functions may be used for modeling Cradiation in certain cases.
Referring to
Referring still to
The processor 154 can implement operating systems, and may be able to execute computer programs, also known as commands, instructions, functions, processes, software codes, executables, applications, and the like. While the processor 154 is depicted in
The memory 156, which may also be referred to as a “computer readable storage medium” or a “computer readable memory” is configured to store computer programs and other data to be retrieved by the processor 154. The terms “computer readable storage medium” and “computer readable memory” refer herein to a non-transitory and tangible computer product that can store and communicate executable instructions for the implementation of various steps of the techniques disclosed herein. The memory 156 may be any computer data storage device or assembly of such devices, including a random-access memory (RAM); a dynamic RAM; a read-only memory (ROM); a magnetic storage device; an optical storage device; a flash drive memory; and/or any other non-transitory memory technologies. The memory 156 may be associated with, coupled to, or included in the processor 154, and the processor 154 may be configured to execute instructions contained in a computer program stored in the memory 156 and relating to various functions and operations associated with the processor 154. While the memory 156 is depicted in
The plasma focus system 100 may also include one or more user interface devices (not shown) operatively connected to the control and processing unit 152 to allow the input of commands and queries to the plasma focus system 100, as well as present the outcomes of the commands and queries. The user interface devices can include input devices (e.g., a touch screen, a keypad, a keyboard, a mouse, a switch, and the like) and output devices (e.g., a display screen, a printer, visual and audible indicators and alerts, and the like).
The following aspects are also disclosed herein.
Numerous modifications could be made to the embodiments described above without departing from the scope of the appended claims.
The following is a list of references, the entire contents of which are incorporated herein by reference.
The present application claims priority to U.S. Provisional Patent Application No. 63/323,697 filed on Mar. 25, 2022, the disclosure of which is incorporated herein by reference in its entirety.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/US2023/016273 | 3/24/2023 | WO |
| Number | Date | Country | |
|---|---|---|---|
| 63323697 | Mar 2022 | US |