Magnetic Direction of a Plasma Corona Provided Proximate to a Resonator

Information

  • Patent Application
  • 20190186456
  • Publication Number
    20190186456
  • Date Filed
    December 20, 2017
    7 years ago
  • Date Published
    June 20, 2019
    5 years ago
Abstract
Example implementations relate to magnetic direction of a plasma corona provided proximate to a resonator. An example implementation includes a system. The system includes a radio-frequency power source. The system also includes a resonator configured to electromagnetically couple to the radio-frequency power source. The resonator includes a dielectric between a first conductor and a second conductor. The resonator also includes an electrode configured to electromagnetically couple to the first conductor and including a concentrator. The resonator is configured to provide a plasma corona proximate to the concentrator when excited by the radio-frequency power source. Still further, the system includes a magnetic-field source configured to provide a magnetic field proximate to the concentrator so as to modify at least one feature of the plasma corona.
Description
BACKGROUND

Resonators are devices and/or systems that can produce a large response for a given input when excited at a resonance frequency. Resonators are used in various applications, including acoustics, optics, photonics, electromagnetics, chemistry, particle physics, etc. For example, electromagnetic resonators can be used as antennas or as energy transmission devices. Further, resonators can concentrate a large amount of energy in a relatively small location (for example, as in the electromagnetic waves radiated by a laser).


SUMMARY

In a first implementation, a system is provided. The system includes a radio-frequency power source. The system also includes a resonator configured to electromagnetically couple to the radio-frequency power source and having a resonant wavelength. The resonator includes a first conductor. The resonator also includes a second conductor. Further, the resonator includes a dielectric between the first conductor and the second conductor. In addition, the resonator includes an electrode configured to electromagnetically couple to the first conductor and including a concentrator. The resonator is configured to provide a plasma corona proximate to the concentrator when excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of the resonant wavelength. Additionally, the system includes a magnetic-field source configured to provide a magnetic field proximate to the concentrator so as to modify at least one feature of the plasma corona selected from the group consisting of a shape of the plasma corona, an angle of the plasma corona, and a position of the plasma corona with respect to the electrode.


In a second implementation, a method is provided. The method includes exciting, by a radio-frequency power source, a resonator electromagnetically coupled to the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of a resonant wavelength of the resonator. The resonator includes a first conductor. The resonator also includes a second conductor. Further, the resonator includes a dielectric between the first conductor and the second conductor. Additionally, the resonator includes an electrode electromagnetically coupled to the first conductor and including a concentrator. The method also includes concentrating an electric field at the concentrator. In addition, the method includes, in response to exciting the resonator, providing a plasma corona proximate to the concentrator. Still further, the method includes providing, by a magnetic-field source, a magnetic field proximate to the concentrator. Even further, the method includes modifying, by the magnetic field, at least one feature of the plasma corona selected from the group consisting of a shape of the plasma corona, an angle of the plasma corona, or a position of the plasma corona with respect to the electrode.


In a third implementation, a system is provided. The system includes a combustion chamber. The system also includes a radio-frequency power source. Further, the system includes a resonator configured to electromagnetically couple to the radio-frequency power source and having a resonant wavelength. The resonator includes a first conductor. The resonator also includes a second conductor. Further, the resonator includes a dielectric between the first conductor and the second conductor. In addition, the resonator includes an electrode configured to electromagnetically couple to the first conductor and including a concentrator. The resonator is configured to provide a plasma corona proximate to the concentrator when excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of the resonant wavelength. The plasma corona is usable to ignite a fuel/air mixture within the combustion chamber. In addition, the system includes a magnetic-field source configured to provide a magnetic field proximate to the concentrator so as to modify at least one feature of the plasma corona selected from the group consisting of a shape of the plasma corona, an angle of the plasma corona, and a position of the plasma corona with respect to the electrode.


Other implementations will become apparent to those of ordinary skill in the art by reading the following detailed description, with reference where appropriate to the accompanying drawings.





BRIEF DESCRIPTION OF THE FIGURES


FIG. 1A illustrates a cross-sectional view of an internal combustion engine.



FIG. 1B illustrates an isometric view of an example quarter-wave coaxial cavity resonator (QWCCR) structure, according to example implementations.



FIG. 1C illustrates a cutaway side view of a QWCCR structure, according to example implementations.



FIG. 1D illustrates a cross-sectional view of a QWCCR structure, according to example implementations.



FIG. 1E is a cross-sectional illustration of an electromagnetic mode in a QWCCR structure, according to example implementations.



FIG. 1F is a cross-sectional illustration of an electromagnetic mode in a QWCCR structure, according to example implementations.



FIG. 1G is a plot of a quarter-wave resonance condition of a QWCCR structure, according to example implementations.



FIG. 2 illustrates a system that includes a coaxial resonator, according to example implementations.



FIG. 3A illustrates a system that includes a coaxial resonator, according to example implementations.



FIG. 3B illustrates a system that includes a coaxial resonator, according to example implementations.



FIG. 4A illustrates a system that includes a coaxial resonator, according to example implementations.



FIG. 4B illustrates a controller, according to example implementations.



FIG. 5 illustrates a cutaway side view of a QWCCR structure connected to a fuel pump and a fuel tank, according to example implementations.



FIG. 6 illustrates a cross-sectional view of an example coaxial resonator connected to a direct-current (DC) power source through an additional resonator assembly acting as a radio-frequency (RF) attenuator, according to example implementations.



FIG. 7 illustrates a cross-sectional view of an example coaxial resonator connected to a DC power source through an additional resonator assembly acting as an RF attenuator, according to example implementations.



FIG. 8A illustrates a system that includes a resonator, according to example implementations.



FIG. 8B illustrates a system that includes a resonator, according to example implementations.



FIG. 8C illustrates a system that includes a resonator, according to example implementations.



FIG. 8D illustrates a system that includes a resonator, according to example implementations.



FIG. 8E illustrates a system that includes a resonator, according to example implementations.



FIG. 8F illustrates a system that includes a resonator, according to example implementations.



FIG. 8G illustrates a system that includes a resonator, according to example implementations.



FIG. 9A illustrates a system that includes a resonator, according to example implementations.



FIG. 9B illustrates a system that includes a resonator, according to example implementations.



FIG. 10 illustrates a method, according to example implementations.





DETAILED DESCRIPTION

Example methods, devices, and systems are presently disclosed. It should be understood that the word “example” is used in the present disclosure to mean “serving as an instance or illustration.” Any implementation or feature presently disclosed as being an “example” is not necessarily to be construed as preferred or advantageous over other implementations or features. Other implementations can be utilized, and other changes can be made, without departing from the scope of the subject matter presented in the present disclosure.


Thus, the example implementations presently disclosed are not meant to be limiting. Components presently disclosed and illustrated in the figures can be arranged, substituted, combined, separated, and designed in a wide variety of different configurations, all of which are contemplated in the present disclosure.


Further, unless context suggests otherwise, the features illustrated in each of the figures can be used in combination with one another. Thus, the figures should be generally viewed as components of one or more overall implementations, with the understanding that not all illustrated features are necessary for each implementation.


In the context of this disclosure, various terms can refer to locations where, as a result of a particular configuration, and under certain conditions of operation, a voltage component can be measured as close to non-existent. For example, “voltage short” can refer to any location where a voltage component can be close to non-existent under certain conditions. Similar terms can equally refer to this location of close-to-zero voltage (for example, “virtual short circuit,” “virtual short location,” or “voltage null”). In examples, “virtual short” can be used to indicate locations where the close-to-zero voltage is a result of a standing wave crossing zero. “Voltage null” can be used to refer to locations of close-to-zero voltage for a reason other than as result of a standing wave crossing zero (for example, voltage attenuation or cancellation). Moreover, in the context of this disclosure, each of these terms that can refer to locations of close-to-zero voltage are meant to be non-limiting.


In an effort to provide technical context for the present disclosure, the information in this section can broadly describe various components of the implementations presently disclosed. However, such information is provided solely for the benefit of the reader and, as such, does not expressly limit the claimed subject matter. Further, components shown in the figures are shown for illustrative purposes only. As such, the illustrations are not to be construed as limiting. As is understood, components can be added, removed, or rearranged without departing from the scope of this disclosure.


I. Overview

As described in the present disclosure, a resonator excited by a radio-frequency power source can provide a plasma corona. Such a plasma corona can be used for ignition of a fuel mixture within a combustion chamber, for example. In order to improve ignition and/or combustion, the plasma corona provided by the resonator can be manipulated using magnetic fields. For example, one or more electromagnetics and/or ferromagnets can provide a magnetic field near the resonator. The provided magnetic field can adjust a localized plasma density within the plasma corona, elongate the plasma corona, shorten the plasma corona, expand the plasma corona, contract the plasma corona, adjust orientation/location of the plasma corona, or extinguish the plasma corona.


As such, the magnetic field can be controlled so as to orient the plasma corona in a specific way in order to respond to changes in the combustion environment within the combustion chamber and/or for other reasons. For example, if a sensor detects that fuel within a specific region within the combustion chamber is not being completely combusted, the magnetic field can be modified such that the plasma corona extends toward the specific region, thereby improving combustion percentage in that region.


The magnetic field can be modified by a controller altering one or more qualities of one or more of the magnets used to provide the magnetic field. For example, the controller can increase the power supplied to one or more of the magnets, thereby increasing an intensity of the magnetic field. Alternatively, the controller can move one or more of the magnets, thereby adjusting the location of the source of the magnetic field. In some implementations, the one or more electromagnets can be individually energized. Hence, additionally or alternatively, the controller can selectively switch on or off one or more electromagnets in order to adjust the magnetic field strength, polarity, location, and/or one or more other attributes of the magnetic field.


Even further, in some implementations, the controller can energize the electromagnets sequentially according to a pre-determined sequence so that the plasma corona reorients with respect to the magnetic field based on the pre-determined sequence. For example, if one electromagnet supplies a magnetic field proximate to the resonator to control the plasma corona, the controller can switch the polarity of the electromagnet by reversing the direction of a current flowing through a wire of the electromagnet. By doing so, the magnetic field can change direction, thereby causing the plasma corona influenced by the magnetic field to be drawn nearer to or pushed farther from the electromagnet. By repeatedly switching the polarity of the electromagnet at a pre-determined frequency, the plasma corona can be caused to oscillate from side to side, for example.


II. Example Combustion

Igniters can be used to ignite a mixture of air and fuel (for example, within a combustion chamber of an internal combustion engine 101, such as that illustrated in cross-section in FIG. 1A). For example, igniters can be configured as gap spark igniters, similar to an automotive spark plug. However, gap spark igniters might not be desirable in some applications and/or under some conditions. For example, a gap spark igniter might not be capable of igniting and initiating combustion of fuel mixtures that have fuel-to-air ratios below a certain threshold. Further, lean mixtures of fuel and air might have significant environmental and economic benefits by making combustion (for example, within a combustor or an afterburner) more efficient, and thus, using a gap spark igniter might preclude achieving such benefits. In addition, higher thermal efficiencies can be achieved by operating at higher power densities and pressures. However, using more energetic or powerful gap spark igniters reduces overall ignition efficiency because the higher energy levels can be detrimental to the gap spark igniter's lifetime. Higher energy levels might also contribute to the formation of undesirable pollutants and can reduce overall engine efficiency.


While gap spark igniters are described above, other types of igniters can generally include glow plugs (for example, in diesel-fueled internal combustion engines), open flame sources (for example, cigarette lighters, friction spark devices, etc.), and other heat sources.


A variety of fuels (for example, hydrocarbon fuels) can be combusted to yield energy within an internal combustion engine, within a power-generation turbine, within a jet engine, or within various other applications. For example, kerosene (also known as paraffin or lamp oil), gasoline (also known as petrol), fractional distillates of petroleum fuel oil (for example, diesel fuel), crude oil, Fischer-Tropsch synthesized paraffinic kerosene, natural gas, and coal are all hydrocarbon fuels that, when combusted, liberate energy stored within chemical bonds of the fuel. Jet fuel, specifically, can be classified by its “jet propellant” (JP) number. The “jet propellant” (JP) number can correspond to a classification system utilized by the United States military. For example, JP-1 can be a pure kerosene fuel, JP-4 can be a 50% kerosene and 50% gasoline blend, JP-9 can be another kerosene-based fuel, JP-9 can be a gas turbine fuel (for example, including tetrahydrodimethylcyclopentadiene) specifically used in missile applications, and JP-10 can be a fuel similar to JP-9 that includes endo-tetrahydrodicyclopentadiene, exo-tetrahydrodicyclopentadiene, and adamantane. Other forms of jet fuel include zip fuel (for example, high-energy fuel that contains boron), SYNTROLEUM® FT-fuel, other kerosene-type fuels (for example, Jet A fuel and Jet A-1 fuel), and naphtha-type fuels (for example, Jet B fuel). It is understood that other fuels can be combusted as well. Further, the fuel type used can depend upon the application. For example, jet engines, internal combustion engines, and power-generation turbines may each burn different types of fuels.


When fuel (for example, hydrocarbon fuel) interacts with electromagnetic radiation, the fuel can change chemical composition. For example, when hydrocarbon fuel interacts with (for example, is irradiated by) microwaves, some of the hydrogen atoms can be ionized and/or one or more hydrogen atoms can be liberated from a hydrocarbon chain. The processes of liberating hydrogen within fuel, ionizing hydrogen within fuel, or otherwise changing the chemical composition of fuel are collectively referred to in the present disclosure as “reforming” the fuel. Reforming the fuel can include exciting the hydrocarbon fuel at one or more of its natural resonant frequencies (for example, acoustic and/or electromagnetic resonant frequencies) to break one or more of the carbon-hydrogen (or other) bonds within the hydrocarbon chain. When hydrogen within a hydrocarbon fuel becomes ionized and/or is liberated from the hydrocarbon chain, the resulting hydrocarbon fuel can require less energy to burn. Thus, a leaner fuel/air mixture that includes reformed fuel can achieve the same output power (for example, within a combustion chamber of a jet engine or a power-generation turbine) as compared to a more rich fuel/air mixture that includes non-reformed fuel, since the reformed fuel can combust more quickly and thoroughly. Analogously, when comparing equal fuel-to-air ratios, less input energy can be required to combust a mixture that includes reformed fuel when compared to a mixture that includes non-reformed fuel.


In addition to reforming fuels, electromagnetic radiation can alter an energy state of fuel and/or of a fuel mixture. In an example implementation, altering the energy state of fuel can include exciting electrons within the valence band of the hydrocarbon chain to higher energy levels. In such scenarios, raising the energy state can also include reorienting polar molecules (for example, water and/or polar hydrocarbon chains) within a fuel/air mixture due to electromagnetic fields applying a torque on polar molecules. Reorienting polar molecules can result in molecular motion, thereby increasing an effective temperature and/or kinetic energy of the molecule, which raises the energy state of fuel. By raising the energy state of fuel, the activation energy for combustion of the fuel can be reduced. When the activation energy for combustion is reduced, the energy supplied by the ignition source can also be decreased, thereby conserving energy during ignition.


Presently disclosed are ignition systems with resonators (for example, QWCCR structures) that use both RF power and DC power. The presently disclosed RF ignition systems provide an alternative to other types of igniters. For example, the QWCCR structure can be used as an igniter (for example, in place of an automotive gap spark plug) in the internal combustion engine 101. Such RF ignition systems can excite plasma (for example, within a corona). If an igniter is configured as one of the RF ignition systems presently disclosed, then more efficient, leaner, cleaner combustion can be achieved. Such increased combustion efficiency can be achieved at decreased air pressures and temperatures when compared with a gap spark igniter (for example, if the RF ignition system is used in a jet engine). Further, such increased combustion efficiency can be achieved at higher air pressures and temperatures when compared with a gap spark igniter. It is understood throughout this disclosure that where reference is made to “RF” or to microwaves, in alternate implementations, other wavelengths of electromagnetic waves outside of the RF range can be used alternatively or in addition to RF electromagnetic waves.


As described above, RF ignition systems can excite plasma. Plasma is one of the four fundamental states of matter (in addition to solid, liquid, and gas). Further, plasmas are mixtures of positively charged gas ions and negatively charged electrons. Because plasmas are mixtures of charged particles, plasmas have associated intrinsic electric fields. In addition, when the charged particles in the mixture move, plasmas also produce magnetic fields (for example, according to Ampere's law). Given the electromagnetic nature of plasmas, plasmas interact with, and can be manipulated by, external electric and magnetic fields. For example, placing a ferromagnetic material (for example, iron, cobalt, nickel, neodymium, samarium-cobalt, etc.) near a plasma can cause the plasma to be attracted to or repelled from the ferromagnetic material (for example, causing the plasma to move).


Plasmas can be formed in a variety of ways. One way of forming a plasma can include heating gases to a sufficiently high temperature (for example, depending on ambient pressure). Additionally or alternatively, forming a plasma can include exposing gases to a sufficiently strong electromagnetic field. Lightning is an environmental phenomenon involving plasma. One application of plasma can include neon signs. Further, because plasma is responsive to applied electromagnetic fields, plasma can be directed according to specific patterns. Hence, plasmas can also be used in technologies such as plasma televisions or plasma etching.


Plasmas can be characterized according to their temperature and electron density. For example, one type of plasma can be a “microwave-generated plasma” (for example, ranging from 5 eV to 15 eV in energy). Such a plasma can be generated by a QWCCR structure, for example.


III. Example Resonator

An example implementation of a QWCCR structure 100 is illustrated in FIGS. 1B-1D. As illustrated, the QWCCR structure 100 can include an outer conductor 102, an inner conductor 104 with an associated electrode 106, a base conductor 110, and a dielectric 108. Also as illustrated, the QWCCR structure 100 can be shaped as concentric circular cylinders. The inner conductor 104 can have radius ‘a’, the outer conductor 102 can have inner radius ‘b’, and the outer conductor 102 can have outer radius ‘c’, as illustrated in cross-section in FIG. 1D. In alternate implementations, the QWCCR structure 100 can have other shapes (for example, concentric ellipsoidal cylinders or concentric, enclosed, elongated volumes with square or rectangular cross-sections). The inner conductor 104, the outer conductor 102 (or just the inner surface of the outer conductor 102), the electrode 106, and the base conductor 110 can be made of various conductive materials (for example, steel, gold, silver, platinum, nickel, or alloys thereof). Further, in some implementations, the inner conductor 104, the outer conductor 102, and the base conductor 110 can be made of the same conductive materials, while in other implementations, the inner conductor 104, the outer conductor 102, and the base conductor 110 can be made of different conductive materials. Additionally, in some implementations, the inner conductor 104, the outer conductor 102, and/or the base conductor 110 can include a dielectric material coated in a conductor (for example, a metal-plated ceramic). In such implementations, the conductive coating can be thicker than a skin-depth of the conductor at a given excitation frequency of the QWCCR structure 100 such that electricity is conducted throughout the conductive coating.


As illustrated, an electrode 106 can be disposed at a distal end of the inner conductor 104. The electrode 106 can be made of a conductive material as described above (for example, the same conductive material as the inner conductor 104). For example, the electrode 106 can be machined with the inner conductor 104 as a single piece. In some implementations, as illustrated, the base conductor 110, the outer conductor 102, the inner conductor 104, and the electrode can be shorted together. For example, the base conductor 110 can short the outer conductor 102 to the inner conductor 104, in some implementations. When shorted together, these components can be directly electrically coupled to one another such that each of these components is at the same electric potential.


Further, in implementations where the base conductor 110, the outer conductor 102, and the inner conductor 104 (including the electrode 106) are shorted together, the base conductor 110, the outer conductor 102, and the inner conductor 104 (including the electrode 106) can be machined as a single piece. In addition, the electrode 106 can include a concentrator (for example, a tip, a point, or an edge), which can concentrate and enhance the electric field at one or more locations. Such an enhanced electric field can create conditions that promote the excitation of a plasma corona near the concentrator (for example, through a breakdown of a dielectric, such as air, that surrounds the concentrator). The concentrator can be a patterned or shaped portion of the electrode 106, for example. The electrode 106, including the concentrator, can be electromagnetically coupled to the inner conductor 104. In the present disclosure and claims, the electrode 106 and/or the concentrator can be described as being “configured to electromagnetically couple to” the inner conductor 104. This language is to be interpreted broadly as meaning that the electrode 106 and/or the concentrator: are presently electromagnetically coupled to the inner conductor 104, are always electromagnetically coupled to the inner conductor 104, can be selectively electromagnetically coupled to the inner conductor 104 (for example, using a switch), are only electromagnetically coupled to the inner conductor 104 when a power source is connected to the inner conductor 104, and/or are able to be electromagnetically coupled to the inner conductor 104 if one or more components are repositioned relative to one another. For example, the electrode 106 can be “configured to electromagnetically couple to” the inner conductor 104 if the electrode 106 is machined as a single piece with the inner conductor 104, if the electrode 106 is connected to the inner conductor 104 using a wire or other conducting mechanism, or if the electrode 106 is disposed sufficiently close to the inner conductor 104 such that the electrode 106 electromagnetically couples to one or more evanescent waves excited by the inner conductor 104 when the inner conductor 104 is connected to a power source.


As illustrated in FIG. 1C, the electrode 106 and/or a concentrator of the electrode 106 can extend beyond the distal end of the outer conductor 102 and/or the distal end of the dielectric 108. In alternate implementations, the electrode 106 and/or a concentrator of the electrode 106 can be flush with the distal end of the outer conductor 102 and/or the distal end of the dielectric 108. In alternate implementations, the electrode 106 and/or a concentrator of the electrode 106 can be shorter than the outer conductor 102, such that no portion of the electrode 106 and/or concentrator is flush with the distal end of the outer conductor 102 and no portion extends beyond the distal end of the outer conductor 102. The QWCCR structure 100 can be excited at resonance, in some implementations. The resonance can generate a standing voltage quarter-wave within the QWCCR structure 100. If the concentrator, the distal end of the outer conductor 102, and the distal end of the dielectric 108 are each flush with one another, the electromagnetic field can quickly collapse outside of the QWCCR structure 100, thereby concentrating the majority of the electromagnetic energy at the concentrator. In still other implementations, the distal end of the outer conductor 102 and/or the distal end of the dielectric 108 can extend beyond the electrode 106 and/or a concentrator of the electrode 106. The electrode 106 can effectively modify the physical length of the inner conductor 104, which can modify the resonance conditions of the QWCCR structure 100 (for example, can modify the electrical length of the QWCCR structure 100). Various resonance conditions can thus be achieved across a variety of QWCCR structures 100 by varying the geometry of the electrode 106 and/or a concentrator of the electrode 106.


Further, as illustrated in FIG. 1C, the base conductor 110 can be electrically coupled to the outer conductor 102 and the inner conductor 104. In alternate implementations, the inner conductor 104 can be electrically insulated from the outer conductor 102 (rather than shorted together through the base conductor 110).


Plasmas (for example, plasma coronas generated by the QWCCR structure 100) can be used to ignite mixtures of air and fuel (for example, hydrocarbon fuel for use in a combustion process). Plasma-assisted ignition (for example, using a QWCCR structure 100) is fundamentally different from ignition using a gap spark plug. For example, efficient electron-impact excitation, dissociation of molecules, and ionization of atoms, which might not occur in ignition using gap spark plugs, can occur in plasma-assisted ignition. Further, in plasmas, an external electric field can accelerate the electrons and/or ions. Thus, using electric fields, energy within the plasma (for example, thermal energy) can be directed to specific locations (for example, within a combustion chamber).


There are a variety of mechanisms by which plasma can impart the energy necessary to ignite mixtures of air and fuel. For example, electrons can impart energy to molecules during collisions. However, this singular energy exchange might be relatively minor (for example, because an electron's mass is orders of magnitude less than a molecule's mass). So long as the rate at which electrons are imparting energy to the molecules is higher than the rate at which molecules are undergoing relaxation, a population distribution of the molecules (for example, a population distribution that differs from an initial Boltzmann distribution of the molecules) can arise. The molecules having higher energy, along with the dissociation and ionization processes, can emit ultraviolet (UV) radiation (for example, when undergoing relaxation) that affects mixtures of fuel and air. Further, gas heating and an increase in system reactivity can increase the likelihood of ignition and flame propagation. In addition, when the average electron energy within a plasma (for example, within a combustion chamber) exceeds 10 eV, gas ionization can be the predominant mechanism by which plasma is formed (over electron-impact excitation and dissociation of molecules).


Plasma-assisted ignition can have a variety of benefits over ignition using a gap spark plug. For example, in plasma-assisted ignition, a plasma corona that is generated can be physically larger (for example, in length, width, radius, and/or overall volumetric extent) than a typical spark from a gap spark plug. This can allow a more lean fuel mixture (also known as lower fuel-to-air ratio) to be burned once combustion occurs as compared with alternative ignition, for example. Also, because a larger energy can be energized in plasma-assisted ignition, stoichiometric ratio fuels can be combusted more fully, thereby creating fewer regulated pollutants (for example, creating less NOx to be expelled as exhaust) and/or leaving less unspent fuel.


Dielectric breakdown of air or another dielectric material near the electrode 106 of the QWCCR structure 100 can be a mechanism by which a plasma corona is excited near the concentrator of the QWCCR structure 100. Factors that impact the breakdown of a dielectric, such as dielectric breakdown of air, include free-electron population, electron diffusion, electron drift, electron attachment, and electron recombination. Free electrons in the free-electron population can collide with neutral particles or ions during ionization events. Such collisions can create additional free electrons, thereby increasing the likelihood of dielectric breakdown. Oppositely, electron diffusion and attachment can each be mechanisms by which free electrons recombine and are lost, thereby reducing the likelihood of dielectric breakdown.


As presently described, a plasma corona can be provided “proximate to” a distal end of the QWCCR structure 100, the electrode 106, and/or a concentrator of the QWCCR structure 100. In other words, the plasma corona could be described as being provided “nearby” or “at” a distal end of the QWCCR structure 100, the electrode 106, and/or a concentrator of the QWCCR structure 100. Further, this terminology is not to be viewed as limiting. For example, while the plasma corona is provided “proximate to” the QWCCR structure 100, this does not limit the plasma corona from extending away from the QWCCR structure 100 and/or from being moved to other locations that are farther from the QWCCR structure 100 after being provided “proximate to” the QWCCR structure 100.


When used to describe a relationship between a plasma corona and a distal end of the QWCCR structure 100, a relationship between a plasma corona and the electrode 106, a relationship between a plasma corona and a concentrator of the electrode 106, or similar relationships, the term “proximate” can describe the physical separation between the plasma corona and the other component. In various implementations, the physical separation can include different ranges. For example, a plasma corona provided “proximate to” the concentrator can be separated from the concentrator (in other words, can “stand off from” the concentrator) by less than 1.0 nanometer, by 1.0 nanometer to 10.0 nanometers, by 10.0 nanometers to 100.0 nanometers, by 100.0 nanometers to 1.0 micrometer, by 1.0 micrometer to 10.0 micrometers, by 10.0 micrometers to 100.0 micrometers, or by 100.0 micrometers to 1.0 millimeter. Additionally or alternatively, a plasma corona provided “proximate to” the concentrator can be separated from the concentrator by 0.01 times a width of the plasma corona to 0.1 times a width of the plasma corona, by 0.1 times a width of the plasma corona to 1.0 times the width of the plasma corona, or by 1.0 times a width of the plasma corona to 10.0 times a width of the plasma corona. Even further, a plasma corona provided “proximate to” the concentrator can be separated from the concentrator by 0.01 times a radius of the concentrator to 0.1 times a radius of the concentrator, by 0.1 times a radius of the concentrator to 1.0 times a radius of the concentrator, or by 1.0 times a radius of the concentrator to 10.0 times a radius of the concentrator.


It is understood that in various implementations, the plasma corona can emit light entirely within the visible spectrum, partially within the visible spectrum and partially outside the visible spectrum, or completely outside the visible spectrum. In other words, even if the plasma corona is “invisible” to the human eye and/or to optics that only sense light within the visible spectrum, it is not necessarily the case that the plasma corona is not being provided.


IV. Mathematical Description of Example Resonator

In order for dielectric breakdown to occur, an electric field within the dielectric must be greater than or equal to an electric field breakdown threshold. An electric field generated by an alternating current (AC) source can be described by a root-mean-square (rms) value for electric field (Erms). The rms value for electric field (Erms) can be calculated according the following equation:







E
rms

=



1


T
2

-

T
1








T
1


T
2





E
2


dt








where T2−T1 represents the period over which the electric field is oscillating (for example, corresponding to the period of the AC source generating the electric field). As described mathematically above, the rms value for electric field (Erms) represents the quadratic mean of the electric field. Using the rms value for electric field, an effective electric field (Eeff) can be calculated that is approximately frequency independent (for example, by removing phase lag effects from the oscillating electric field):







E
eff
2

=


E
rms
2




v
c
2



ω
2

+

v
c
2








where ω represents the angular frequency of the electric field (for example,







ω
=


2

π



T
2

-

T
1




)




and vc represents the effective momentum collision frequency of the electrons and neutral particles. The angular frequency (ω) of the electric field can correspond to the frequency of an excitation source used to excite the electric field (for example, the QWCCR structure 100). Using this effective electric field (Eeff), DC breakdown voltages for various gases (and potentially other dielectrics) can be related to AC breakdown values for uniform electric fields. For air, vc≈5·109×p, where p represents the pressure (in torr). At atmospheric pressure (for example, around 760 torr) or above and excitation frequencies of below 1 THz, the effective momentum collision frequency of the electrons and neutral particles (vc) will dominate the denominator of the fractional coefficient of Erms2. Therefore, an approximation of the rms breakdown field (Eb) can be used. The rms breakdown field (Eb), in V/cm, of a uniform microwave field in the collision regime can be given by:







E
b

=


30
·
297



(

p
T

)






where T is the temperature in Kelvin.


An analytical description of the electromagnetics of the QWCCR structure 100 follows.


If fringing electromagnetic fields are assumed to be small, the lowest quarter-wave resonance in a coaxial cavity is a transverse electromagnetic mode (TEM mode) (as opposed to a transverse electric mode (TE mode) or a transverse magnetic mode (TM mode)). The TEM mode is the dominant mode in a coaxial cavity and has no cutoff frequency (ωc). In the TEM mode (as illustrated in FIG. 1E), because neither the electric field nor the magnetic field have any components in the z-direction (coordinate system illustrated in FIG. 1D), the electric and magnetic fields can be written, respectively, as:






H
=



H
ϕ




a
^

ϕ


=



I
0


2

π





r




cos


(

β





z

)





a
^

ϕ









E
=



E
r




a
^

r


=



V
0


2

π





r




sin


(

β





z

)





a
^

r







where H is a phasor representing the magnetic field vector, E is a phasor representing the electric field vector, ây represents a unit vector in the φ direction (labeled in FIG. 1D), âr represents a unit vector in the r direction (labeled in FIG. 1D), β represents the wave number (canonically defined as







β
=


2

π

λ


,




where λ is the wavelength), I0 represents the maximum current in the cavity, V0 represents the maximum voltage in the cavity, and z represents a distance along the QWCCR structure 100 in the z direction (labeled in FIG. 1D).


In various implementations, various electromagnetic modes of the QWCCR structure 100 can be excited in order to achieve various electromagnetic properties. In some implementations, for instance, a single electromagnetic mode can be excited, whereas in alternate implementations, a plurality of electromagnetic modes can be excited. For example, in some implementations, the TE01 mode (as illustrated in FIG. 1F) can be excited.


Quality factor (Q) can be defined as:






Q
=




ω
·
U


P
L



U

=



P
L

·
Q

ω






where ω is the angular frequency, U is the time-average energy, and PL is the time-average power loss. Quality factor (Q) can be used to measure goodness of a resonator cavity. Other formulations of goodness measurement can also be used (for example, based on full-width, half-max (FWHM) or a 3 decibel (dB) bandwidth of cavity resonance). In some implementations, the quality factor (Q) can be maximized when the ratio of the inner radius of the outer conductor ‘b’ to the radius of the inner conductor ‘a’ is approximately equal to 4. However, it will be understood that many other ways to adjust and/or maximize quality factor (Q) are possible and contemplated in the present disclosure.


At resonance, the stored energy of the QWCCR structure 100 oscillates between electrical energy (Ue) (within the electric field) and magnetic energy (Um) (within the magnetic field). Time-average stored energy in the QWCCR structure 100 can be calculated using the following:






U
=



U
m

+

U
e


=



1
4





vol



μ




H


2




+

ɛ




E


2








where μ is magnetic permeability and E is dielectric permittivity. By inserting the values for electric field and magnetic field from above, and integrating over the entire volume of the QWCCR structure 100, the following expression can be obtained:






U
=




ln


(

b
a

)


·
λ


64

π




(


μ
·

I
0
2


+

ɛ
·

V
0
2



)






where b represents the inner radius of the outer conductor 102 of the QWCCR structure 100 (as illustrated in FIG. 1D), a represents the radius of the inner conductor 104 of the QWCCR structure 100 (as illustrated in FIG. 1D), and represents the wavelength of the source (for example, AC source) used to excite the QWCCR structure 100. Because the magnetic energy at maximum is the same as the electric energy at maximum, μ·I02 can be replaced with ε·V02, thus resulting in:






U
=




ln


(

b
a

)


·
λ


32

π




(

ɛ
·

V
0
2


)






Now, by equating the two above expressions for U, the following relationship can be expressed:









P
L

·
Q

ω

=






ln


(

b
a

)


·
λ


32

π




(

ɛ
·

V
0
2


)




V
0


=



32


π
·
Q
·

P
L




ω
·
ɛ
·

ln


(

b
a

)


·
λ








Further, in recognizing that







ω
=


2


π

f


=


2


π

c


λ



,




where c is the speed of light;








c
=


1

μ
·
ɛ




;


and





η

=


μ
ɛ




,




where η is the impedance of the dielectric between the inner conductor 104 and the outer conductor 102 of the QWCCR structure 100, the following relationship for the peak potential (V0) can be identified:







V
0

=

4




η
·
Q
·

P
L



ln


(

b
a

)









Given that electric field decays as the distance from the peak potential (V0) increases, the largest value of electric field corresponding to the peak potential (V0) occurs exactly at the surface of the inner conductor (for example, at radius a, as illustrated in FIG. 1D). Using the above equation for phasor electric field (E), the peak value of electric field (Ea) can be expressed as:







E
a

=



V
0


2


π

a



=


2

π

a






η
·
Q
·

P
L



ln


(

b
a

)










If the above peak value of electric field (Ea) meets or exceeds the above-described rms breakdown field (Eb), a dielectric breakdown can occur. For example, a dielectric breakdown of the air surrounding the tip of the QWCCR structure 100 can result in a plasma corona being excited. As indicated in the above equation for peak electric field (Ea), the smaller the radius a of the inner conductor 104, the smaller the inner radius b of outer conductor 102, the higher the quality factor (Q) of the QWCCR structure 100, and the larger the time-average power loss (PL), the more likely it is that breakdown can occur (for example, because the peak value of electric field (Ea) is larger). A larger excitation power can correspond to a larger time-average power loss (PL) in the QWCCR structure 100, for example.


The power loss (PL) can include ohmic losses (Pa) on conductive surfaces (for example, the surface of the outer conductor 102, the surface of the inner conductor 104, and/or the surface of the base conductor 110, as illustrated in FIG. 1C), dielectric losses (Pσe) in the dielectric 108, and radiation losses (Prad) from a radiating end of the QWCCR structure 100 (for example, the distal end of the QWCCR structure 100). Each of the conductors can have a corresponding surface resistance (RS). The surface resistance (RS) can be the same for one or more of the conductors if the corresponding conductors are made of the same conductive materials. The corresponding surface resistance for each conductor can be expressed as








R
S

=



ω
·

μ
c



2
·

σ
c





,




where μc is the magnetic permeability of the respective conductor and σc is the conductivity of the respective conductor. The power lost by each conductor can be calculated according to the following:







P
σ

=


1
2





A




R
S






H
//



2








where H// is the magnetic field parallel to the surface of the conductor. Thus, the total power loss in all conductors can be represented by:







P
σ

=



P
inner

+

P
outer

+

P
base


=




R
S

·

I
0
2



4

π




[


λ

8
·
a


+

λ

8
·
b


+

ln


(

a
b

)



]







Further, if the dielectric 108 is an isotropic, low-loss dielectric, the dielectric 108 can be characterized by its dielectric constant (ε) and its loss tangent (tan(δe)), where the loss tangent (tan(δe)) represents conductivity and alternating molecular dipole losses. Using dielectric constant (ε) and loss tangent (tan(δe)), an effective dielectric conductivity (σe) can be approximately defined as:





σe≈(ω)·ε·tan(δe)


Based on the above, the power dissipated in the dielectric can be calculated according to the following:







P

σ
e


=



1
2





vol




σ
e





E


2




=




σ
e

·
η
·

I
0
2



4

π




(



ln


(

b
a

)


·
λ

8

)







In order to combine all quality factors of the QWCCR structure 100 into a total internal quality factor (Qint), the following relationship can be used:







Q
int

=

1

(


Q
inner

-
1


+

Q
outer

-
1


+

Q
base

-
1


+

Q

σ
e


-
1



)






where Qinner−1, Qouter−1, Qbase−1, and Qσe−1 are the quality factors of the inner conductor 104, the outer conductor 102, the base conductor 110, and the dielectric 108, respectively. Using the above expression for quality factor (Q) in terms of time-average power loss (PL), angular frequency (ω), and time-average energy (U), the following expression for internal quality factor (Qint) can be determined:







Q
int

=


(




R
S


2
·
π
·
η




[



(


b
a

+
1

)








b

a

·

ln


(

b
a

)




+
8

]


+

tan


(

δ
e

)



)


-
1






Based on the definitions of the individual quality factors above, the individual contribution of the outer conductor quality factor (Qouter) to the internal quality factor (Qint) can be greater than the individual contribution of the inner conductor quality factor (Qinner). Thus, to increase the internal quality factor (Qint), a material with higher conductivity can be used for the inner conductor 104 than is used for the outer conductor 102. Further, the base conductor 110 quality factor (Qbase) and the dielectric 108 quality factor (Qσe) can be unaffected by the geometry of the QWCCR structure 100 (both in terms of






b
a




and in terms of








b
λ

)

.




The QWCCR structure 100 can also radiate electromagnetic waves (for example, from a distal, non-closed end opposite the base conductor 110). For example, if the QWCCR structure 100 is being excited by an RF power source (for example, a signal generator oscillating at radio frequencies), the QWCCR structure 100 can radiate microwaves from a distal end (for example, from an aperture of the distal end) of the QWCCR structure 100. Such radiation can lead to power losses, which can be approximated using admittance. Assuming that the transverse dimensions of the QWCCR structure 100 are significantly smaller than the wavelength (λ) being used to excite the QWCCR structure 100 (in other words, a<<λ and b<<λ), the real part (Gr) and imaginary part (Br) of admittance can be represented by:







G
r




4
·

π
5

·


[



(


(

b
λ

)


(

b
a

)


)

2

-


(

b
λ

)

2


]

2



3
·
η
·


ln
2



(

b
2

)











B
r





16
·
π
·

(



(

b
λ

)


(

b
a

)


-

(

b
λ

)


)



η
·


ln
2



(

b
2

)




·

[


E
(


2



b
a




1
+

b
a



)

-
1

]






where E(x) is the complete elliptical integral of the second kind. Namely:







E


(
x
)


=



0

π
a







1
-


x
2

·


sin
2



(
θ
)





·
d






θ






Further, the line integral of the electric field from the inner conductor 104 to the outer conductor 102 can be used to determine the potential difference (Vab) across the shunt admittance corresponding to the electromagnetic waves radiated.







V


ab
|

β





z


=

π
4



=





a

b




E
r


=



V
0






ln






(

b
a

)



2





π







Using the potential difference (Vab) across the shunt admittance corresponding to the electromagnetic waves radiated, the power going to radiation (Prad) can be represented by:







P
rad

=



1
2



G
r



V
ab
2


=



V
0







π
3



(

b
λ

)


4



[



(

b
a

)

2

-
1

]


2



6







η


(

b
a

)


4








In addition, using the potential difference (Vab) across the shunt admittance corresponding to the electromagnetic waves radiated, the energy stored during radiation (Urad) can be represented by:







U
rad

=



1
4



(


B
r

ω

)



V
ab
2


=



ɛ






V
0
2




λ


(

b
λ

)




[



(

b
a

)


-
1


+
1

]




2






π
2



[


E
(


2



b
a




1
+

b
a



)

-
1

]






Based on the above, the overall quality factor of the QWCCR structure 100 (QQWCCR) can be described by the following:







Q
QWCCR

=


ω


(

U
+

U
rad


)




P
inner

+

P
outer

+

P
base

+

P

σ
e


+

P
rad







If the energy stored during radiation (Urad) is small compared with the energy stored in the interior of the QWCCR structure 100 (U), the radiation power (Prad) can be treated similarly to the other losses. Further, the energy stored during radiation (Urad) can be neglected in the above equation:






Q



ω


(
U
)




P
inner

+

P
outer

+

P
base

+

P

σ
e


+

P
rad







Still further, the quality factor of the radiation component (Qrad) can be described using the above relationship for quality factors:







Q
rad

=



ω





U


P
rad


=


3



(

b
λ

)

4


ln






(

b
a

)



8










π
3



(

b
λ

)


4



[



(

b
a

)

2

-
1

]


2








Even further, using the above-referenced quality factors, the total quality factor of the QWCCR structure 100 (QQWCCR) can be approximated by:







Q
QWCCR




(



8










π
3



(

b
λ

)


4



[



(

b
a

)

2

-
1

]


2



3



(

b
a

)

4


ln






(

b
a

)



+



R
S


2





πη




[



(


(

b
a

)

+
1

)








(

b
λ

)


ln






(

b
a

)




+
8

]


+

tan


(

δ
e

)



)


-
1






Based on the above relationships, it can be shown that one method of minimizing losses due to radiation of electromagnetic waves by the QWCCR structure 100 is to minimize the inner radius b of the outer conductor 102 with respect to the excitation wavelength (λ). Another way of minimizing losses due to radiation of electromagnetic waves is to select an inner radius b of the outer conductor 102 that is close in dimension to the radius a of the inner conductor 104.


Various physical quantities and dimensions of the QWCCR structure 100 can be adjusted to modify performance of the QWCCR structure 100. For example, physical quantities and dimensions can be modified to maximize and/or optimize the total quality factor of the QWCCR structure 100 (QQWCCR). In some implementations, different dielectrics can be inserted into the QWCCR structure 100. In one implementation, the dielectric 108 can include a composite of multiple dielectric materials. For example, a half of the dielectric 108 near a proximal end of the QWCCR structure 100 can include alumina ceramic while a half of the dielectric 108 near a distal end of the QWCCR structure 100 can include air. The resonant frequency can be based on the dimensions and the fabrication materials of the QWCCR structure 100. Hence, modification of the dielectric 108 can modify a resonant frequency of the QWCCR structure 100. In some implementations, the resonant frequency can be 2.45 GHz based on the dimensions of the QWCCR structure 100. In other implementations, the resonant frequency of the QWCCR structure 100 could be within an inclusive range between 1 GHz to 100 GHz. In still other implementations, the resonant frequency of the QWCCR structure 100 could be within an inclusive range of 100 MHz to 1 GHz or an inclusive range of 100 GHz to 300 GHz. However, other resonant frequencies are contemplated within the context of the present disclosure.


An RF power source exciting the QWCCR structure 100 can generate a standing electromagnetic wave within the QWCCR structure 100. In some implementations, the resonant frequency of the QWCCR structure 100 can be designed to match the frequency of an RF power source that is exciting the QWCCR structure 100 (for example, to maximize power transferred to the QWCCR structure 100). For example, if a desired excitation frequency corresponds to a wavelength of λ0, dimensions of the QWCCR structure 100 can be modified such that the electrical length of the QWCCR structure 100 is an odd-integer multiple of quarter wavelengths (for example, ¼λ0, ¾λ0, 5/4λ0, 7/4λ0, 9/4λ0, 11/4λ0, 13/4λ0, etc.). The electrical length is a measure of the length of a resonator in terms of the wavelength of an electromagnetic wave used to excite the resonator. The QWCCR structure 100 can be designed for a given resonant frequency based on the dimensions of the QWCCR structure 100 (for example, adjusting dimensions of the inner conductor 104, the outer conductor 102, or the dielectric 108) or the materials of the QWCCR structure 100 (for example, adjusting materials of the inner conductor 104, the outer conductor 102, or the dielectric 108).


In other implementations, the resonant frequency of the QWCCR structure 100 can be designed or adjusted such that its resonant frequency does not match the frequency of an RF power source that is exciting the QWCCR structure 100 (for example, to reduce power transferred to the QWCCR structure 100). Analogously, the frequency of an RF power source can be de-tuned relative to the resonant frequency of a QWCCR structure 100 that is being excited by the RF power source. Additionally or alternatively, the physical quantities and dimensions of the QWCCR structure 100 can be modified to enhance the amount of energy radiated (for example, from the distal end) in the form of electromagnetic waves (for example, microwaves) from the QWCCR structure 100. As an example, one or more elements of the QWCCR structure 100 could be movable or otherwise adjustable so as to modify the resonant properties of the QWCCR structure 100. Enhancing the amount of energy radiated might be done at the expense of maximizing the electric field at a concentrator of the electrode 106 at the distal end of the inner conductor 104. For example, some implementations can include slots or openings in the outer conductor 102 to increase the amount of radiated energy despite possibly reducing a quality factor of the QWCCR structure 100.


In still other implementations, the physical quantities and dimensions of the QWCCR structure 100 can be designed in such a way so as to enhance the intensity of an electric field at a concentrator of the electrode 106 of the QWCCR structure 100. Enhancing the electric field at a concentrator of the electrode 106 of the QWCCR structure 100 can result in an increase in plasma corona excitation (for example, an increase in dielectric breakdown near the concentrator), when the QWCCR structure 100 is excited with sufficiently high RF power/current. To increase electric field at a concentrator of the electrode 106 of the QWCCR structure 100, a radius of the concentrator can be minimized (for example, configured as a very sharp structure, such as a tip). Additionally or alternatively, to increase the electric field at a tip of the QWCCR structure 100 (for example, thereby increasing the intensity and/or size of an excited plasma corona), the intrinsic impedance (η) of the dielectric 108 can be increased, the power used to excite the QWCCR structure 100 can be increased, and the total quality factor of the QWCCR structure 100 (QQWCCR) can be increased (for example, by increasing the volume energy storage (U) of the cavity or by minimizing the surface and radiation losses).


Further, the shunt capacitance (C) of a circular coaxial cavity (for example, in farads/meter, and neglecting fringing fields) can be expressed as follows:






C
=


2






πɛ
0



ɛ
r



ln






(

b
a

)







where ε0 represents the permittivity of free space, εr represents the relative dielectric constant of the dielectric 108 between the inner conductor 104 and the outer conductor 102, b is the inner radius of the outer conductor 102, and a is the radius of the inner conductor 104 (as illustrated in FIG. 1D).


Similarly, the shunt inductance (L) of a circular coaxial cavity (for example, in henrys/meter) can be expressed as follows:






L
=




µ
0



µ
r



2





π



ln






(

b
a

)






where μ0 represents the permeability of free space, μr represents the relative permeability of the dielectric 108 between the inner conductor 104 and the outer conductor 102, b is the inner radius of the outer conductor 102, and a is the radius of the inner conductor 104 (as illustrated in FIG. 1D).


Based on the above, the complex impedance (Z) of a circular coaxial cavity (for example, in ohms, Ω) can be expressed as follows:






Z
=



R
+

j





ω





L



G
+

j





ω





C








where G represents the conductance per unit length of the dielectric between the inner conductor and the outer conductor, R represents the resistance per unit length of the QWCCR structure 100, j represents the imaginary unit (for example, √{square root over (−1)}), ω represents the frequency at which the QWCCR structure 100 is being excited, L represents the shunt inductance of the QWCCR structure 100, and C represents the shunt capacitance of the QWCCR structure 100.


At very high frequencies (for example, GHz frequencies) the complex impedance (Z) can be approximated by:







Z
0

=


L
C






where Z0 represents the characteristic impedance of the QWCCR structure 100 (in other words, the complex impedance (Z) of the QWCCR structure 100 at high frequencies).


As described above, the shunt inductance (L) and the shunt capacitance (C) of the QWCCR structure 100 depend on the relative permeability (μr) and the relative dielectric constant (εr), respectively, of the dielectric 108 between the inner conductor 104 and the outer conductor 102. Thus, any modification to either the relative permeability μr) or the relative dielectric constant (εr) of the dielectric 108 between the inner conductor 104 and the outer conductor 102 can result in a modification of the characteristic impedance (Z0) of the QWCCR structure 100. Such modifications to impedance can be measured using an impedance measurement device (for example, an oscilloscope, a spectrum analyzer, and/or an AC volt meter).


The above characteristic impedance (Z0) represents an impedance calculated by neglecting fringing fields. In some applications and implementations, the fringing fields can be non-negligible (for example, the fringing fields can significantly impact the impedance of the QWCCR structure 100). Further, in such implementations, the composition of the materials surrounding the QWCCR structure 100 can affect the characteristic impedance (Z0) of the QWCCR structure 100. Measurements of such changes to characteristic impedance (Z0) can provide information regarding the environment (for example, a combustion chamber) surrounding the QWCCR structure 100 (for example, the temperature, pressure, or atomic composition of the environment). A change in the characteristic impedance (Z0) can coincide with a change in the cutoff frequency, resonant frequency, short-circuit condition, open-circuit condition, lumped-circuit model, mode distribution, etc. of the QWCCR structure 100.



FIG. 1G illustrates a quarter-wave resonance condition of the QWCCR structure 100. The y-axis of the plot corresponds to a power of electromagnetic waves radiated from a distal end of the QWCCR structure 100 and the x-axis corresponds to an excitation frequency (ω) (for example, from a radio-frequency power source that is electromagnetically coupled to the QWCCR structure 100) used to excite the QWCCR structure 100. As illustrated, the shape of the curve can be a Lorentzian.


As illustrated in FIG. 1G the curve has a maximum power at a quarter-wave (λ/4) resonance. This resonance can correspond to excitation frequency (ω) that has an associated excitation wavelength that is four times the length of the QWCCR structure 100. In other words, at the resonant frequency (ω0) the QWCCR structure 100 is being excited by a standing wave, where one-quarter of the length of the standing wave is equal to the length of the QWCCR structure 100. Although not illustrated, it is understood that the QWCCR structure 100 could experience additional resonances (for example, at odd-integer multiples of the resonant wavelength: ¾λ0, 5/4λ0, 7/4λ0, 9/4λ0, 11/4λ0, 13/4λ0, etc.). Each of the additional resonances could look similar to the resonance illustrated in FIG. 1G (for example, could have a Lorentzian shape).


As illustrated, the power of the electromagnetic waves radiated from the distal end of the QWCCR structure 100 decreases exponentially the further the excitation frequency (ω) is from the resonant frequency (ω0). However, the power of the electromagnetic waves is not necessarily zero as soon as you move away from resonance. Hence, it is understood that even when excited near the quarter-wave resonance condition (in other words, proximate to the quarter-wave resonance condition), rather than exactly at the resonance condition, the QWCCR structure 100 can still radiate electromagnetic waves with non-zero power and/or provide a plasma corona, depending on arrangement.


When the QWCCR structure 100 is being excited such that it provides a plasma corona proximate to the distal end (for example, at the electrode 106), a plot with a shape similar to that of FIG. 1G could be provided. In such a scenario, a plot of voltage at the electrode 106 versus excitation frequency (ω) could include a Gaussian shape, rather than a Lorentzian shape. In other words, the voltage at the electrode 106 may reach a peak when excited by a resonant frequency. The voltage at the electrode 106 may fall off exponentially according to a Gaussian shape as the excitation frequency moves away from the resonant frequency. It will be understood that the Gaussian and Lorentzian shapes presently described may be based on one or more characteristics of the QWCCR structure 100, such as its shape, quality factor, bias conditions, or other factors.


It is understood that when the term “proximate” is used to describe a relationship between a wavelength of a signal (for example, a signal used to excite the QWCCR structure 100) and a resonant wavelength of a resonator (for example, the QWCCR structure 100), the term “proximate” can describe a difference in length. For example, if the wavelength of the signal is “proximate to an odd-integer multiple of one-quarter of the resonant wavelength,” the wavelength of the signal can be equal to, within 0.001% of, within 0.01% of, within 0.1% of, within 1.0% of, within 5.0% of, within 10.0% of, within 15.0% of, within 20.0% of, and/or within 25.0% of one-quarter of the resonant wavelength. Additionally or alternatively, if the wavelength of the signal is “proximate to an odd-integer multiple of one-quarter of the resonant wavelength,” the wavelength of the signal can be within 0.1 nm, within 1.0 nm, within 10.0 nm, within 0.1 micrometers, within 1.0 micrometers, within 10.0 micrometers, within 0.1 millimeters, within 1.0 millimeters, and/or within 1.0 centimeters of one-quarter of the resonant wavelength, depending on context (for example, depending on the resonant wavelength). Still further, if the wavelength of the signal is “proximate to an odd-integer multiple of one-quarter of the resonant wavelength,” the wavelength of the signal can be a multiple of one-quarter of the resonant wavelength that is an odd number plus or minus 0.5, an odd number plus or minus 0.1, an odd number plus or minus 0.01, an odd number plus or minus 0.001, and/or an odd number plus or minus 0.0001.


The quality factor of the QWCCR structure 100 (QQWCCR), described above, can be used to describe the width and/or the sharpness of the resonance (in other words, how quickly the power drops off as you excite the QWCCR structure 100 further and further from the resonance condition). For example, a square root of the quality factor can correspond to the voltage modification experienced at the electrode 106 of the QWCCR structure 100 when the QWCRR structure 100 is excited at the quarter-wave resonant condition. Additionally, the quality factor may be equal to the resonant frequency (ω0) divided by full width at half maximum (FWHM). The FWHM is equal to the width of the curve in terms of frequency between the two points on the curve where the power is equal to 50% of the maximum power, as illustrated). The 50% power maximum point can also be referred to as the −3 decibel (dB) point, because it is the point at which the maximum voltage at the distal end of the QWCCR structure 100 decreases by 3 dB (or 29.29% for voltage) and the maximum power radiated by the QWCCR structure 100 decreases by 3 dB (or 50% for power). In various implementations, the FWHM of the QWCCR structure 100 could have various values. For example, the FWHM could be between 5 MHz and 10 MHz, between 10 MHz and 20 MHz, between 20 MHz and 40 MHz, between 40 MHz and 60 MHz, between 60 MHz and 80 MHz, or between 80 MHz and 100 MHz. Other FWHM values are also possible.


Further, the quality factor of the QWCCR structure 100 (QQWCCR) can also take various values in various implementations. For example, the quality factor could be between 25 and 50, between 50 and 75, between 75 and 100, between 100 and 125, between 125 and 150, between 150 and 175, between 175 and 200, between 200 and 300, between 300 and 400, between 400 and 500, between 500 and 600, between 600 and 700, between 700 and 800, between 800 and 900, between 900 and 1000, or between 1000 and 1100. Other quality factor values are also possible.


It is understood that, in alternate implementations, alternate structures (for example, alternate quarter-wave structures) can be used to emit electromagnetic radiation and/or excite plasma coronas (for example, other structures that concentrate electric field at specific locations using points or tips with sufficiently small radii). For example, other quarter-wave resonant structures, such as a coaxial-cavity resonator (sometimes referred to as a “coaxial resonator”), a dielectric resonator, a crystal resonator, a ceramic resonator, a surface-acoustic-wave resonator, a yttrium-iron-garnet resonator, a rectangular-waveguide cavity resonator, a parallel-plate resonator, a gap-coupled microstrip resonator, etc. can be used to excite a plasma corona.


Further, it is understood that wherever in this disclosure the terms “resonator,” “QWCCR,” “QWCCR structure,” and “coaxial resonator,” are used, any of the structures enumerated in the preceding paragraph could be used, assuming appropriate modifications are made to a corresponding system. In addition, the terms “resonator,” “QWCCR,” “QWCCR structure,” and “coaxial resonator” are not to be construed as inclusive or all-encompassing, but rather as examples of a particular structure that could be included in a particular implementation. Still further, when a “QWCCR structure” is described, the QWCCR structure can correspond to a coaxial resonator, a coaxial resonator with an additional base conductor, a coaxial resonator excited by a signal with a wavelength that corresponds to an odd-integer multiple of one-quarter (¼) of a length of the coaxial resonator, and other structures, in various implementations.


Additionally, whenever any “QWCCR,” “QWCCR structure,” “coaxial resonator,” “resonator,” or any of the specific resonators in this disclosure or in the claims are described as being “configured such that, when the resonator is excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of the resonant wavelength, the resonator provides at least one of a plasma corona or electromagnetic waves,” some or all of the following are contemplated, depending on context. First, the corresponding resonator could be configured to provide a plasma corona when excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of a resonant wavelength of the resonator. Second, the corresponding resonator could be configured to provide electromagnetic waves when excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of a resonant wavelength of the resonator. Third, the corresponding resonator could be configured to provide, when excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of a resonant wavelength of the resonator, both a plasma corona and electromagnetic waves.


V. Example Resonator Systems

In some implementations, the coaxial resonator 201 can be used as an antenna (for example, instead of or in addition to generating a plasma corona). As an antenna, the coaxial resonator 201 can radiate electromagnetic waves. The electromagnetic waves can consequently influence charged particles. As illustrated in the system 200 of FIG. 2, such electromagnetic waves can be radiated when the coaxial resonator 201 is excited by a signal generator 202. For example, the signal generator 202 can be coupled to the coaxial resonator 201 in order to excite the coaxial resonator 201 (for example, to excite a plasma corona and to produce electromagnetic waves). Such a coupling can include inductive coupling (for example, using an induction feed loop), parallel capacitive coupling (for example, using a parallel plate capacitor), or non-parallel capacitive coupling (for example, using an electric field applied opposite a non-zero voltage conductor end). Further, the electrical distance between the signal generator 202 and the coaxial resonator 201 can be optimized (for example, minimized or adjusted based on wavelength of an RF signal) in order to minimize the amount of energy lost to heating and/or to maximize a quality factor. Further, in some implementations, the coaxial resonator 201 can radiate acoustic waves when excited (for example, at resonance). The acoustic waves produced can induce motion in nearby particles, for example.


The signal generator 202 can be a device that produces periodic waveforms (for example, using an oscillator circuit). In various implementations, the signal generator 202 can produce a sinusoidal waveform, a square waveform, a triangular waveform, a pulsed waveform, or a sawtooth waveform. Further, the signal generator 202 can produce waveforms with various frequencies (for example, frequencies between 1 Hz and 1 THz). The electromagnetic waves radiated from the coaxial resonator 201 can be based on the waveform produced by the signal generator 202. For example, if the waveforms produced by the signal generator 202 are sinusoidal waves having frequencies between 300 MHz and 300 GHz (for example, between 1 GHz and 100 GHz), the electromagnetic waves radiated by coaxial resonator 201 can be microwaves. In various implementations, the signal generator 202 can, itself, be powered by an AC power source or a DC power source.


Depending on the signal used by the signal generator 202 to excite the coaxial resonator 201, the coaxial resonator 201 can additionally excite one or more plasma coronas. For example, if a large enough voltage is used to excite the coaxial resonator 201, a plasma corona can be excited at the distal end of the electrode 106 (for example, at a concentrator of the electrode 106). In some implementations, a voltage step-up device can be electrically coupled between the signal generator 202 and the coaxial resonator 201. In such scenarios, the voltage step-up device can be operable to increase an amplitude of the AC voltage used to excite the coaxial resonator 201.


In some implementations, the signal generator 202 can include one or more of the following: an internal power supply; an oscillator (for example, an RF oscillator, a surface acoustic wave resonator, or a yttrium-iron-garnet resonator); and an amplifier. The oscillator can generate a time-varying current and/or voltage (for example, using an oscillator circuit). The internal power supply can provide power to the oscillator. In some implementations, the internal power supply can include, for example, a DC battery (for example, a marine battery, an automotive battery, an aircraft battery, etc.), an alternator, a generator, a solar cell, and/or a fuel cell. In other implementations, the internal power supply can include a rectified AC power supply (for example, an electrical connection to a wall socket passed through a rectifier). The amplifier can magnify the power that is output by the oscillator (for example, to provide sufficient power to the coaxial resonator 201 to excite plasma coronas). For example, the amplifier can multiply the current and/or the voltage output by the oscillator. Additionally, in some implementations, the signal generator 202 can include a dedicated controller that executes instructions to control the signal generator 202.


Additionally or alternatively, as illustrated in the system 300 of FIG. 3A, the coaxial resonator 201 can be electrically coupled (for example, using a wired connection or wirelessly) to a DC power source 302. Further, in some implementations, an RF cancellation resonator (not shown) can prevent RF power (for example, from the signal generator 202) from reaching, and potentially interfering with, the DC power source 302. The RF cancellation resonator can include resistive elements, lumped-element inductors, and/or a frequency cancellation circuit.


In some implementations, the DC power source 302 can include a dedicated controller that executes instructions to control the DC power source 302. The DC power source 302 can provide a bias signal (for example, corresponding to a DC bias condition) for the coaxial resonator 201. For example, a DC voltage difference between the inner conductor 104 and the outer conductor 102 of the coaxial resonator 201 in FIG. 3A can be established by the DC power source 302 by increasing the DC voltage of the inner conductor 104 and/or decreasing the DC voltage of the outer conductor 102 (given the orientation of the positive terminal and negative terminal of the DC power source 302). In other implementations, a DC voltage difference between the inner conductor 104 and the outer conductor 102 can be established by the DC power source 302 by decreasing the DC voltage of the inner conductor 104 and/or increasing the DC voltage of the outer conductor 102 (if the orientation of the positive terminal and negative terminal of the DC power source 302 in FIG. 3A were reversed). The bias signal (for example, the voltage of the bias signal and/or the current of the bias signal) output by the DC power source 302 can be adjustable.


By providing the coaxial resonator 201 with a bias signal, an increased voltage can be presented at a concentrator of the electrode 106, thereby yielding an increased electric field at the concentrator of the electrode 106. The total electric field at the concentrator can thus be a sum of the electric field from the bias signal of the DC power source 302 and the electric field from the signal generator 202 exciting the coaxial resonator 201 at a resonance condition (for example, exciting the coaxial resonator 201 at a quarter-wave resonance condition so the electric field of the signal from the signal generator 202 reaches a maximum at the distal end of the coaxial resonator 201). Because of this increased total electric field, an excitation of a plasma corona near the concentrator can be more probable.


As an alternative, rather than using a bias signal, the signal generator 202 can simply excite the coaxial resonator 201 using a higher voltage. However, this might use considerably more power than providing a bias signal and augmenting that bias signal with an AC voltage oscillation.


In some implementations, the DC power source 302 can be switchable (for example, can generate the bias signal when switched on and not generate the bias signal when switched off). As such, the DC power source 302 can be switched on when a plasma corona output is desired from coaxial resonator 201 and can be switched off when a plasma corona output is not desired from coaxial resonator 201. For example, the DC power source 302 can be switched on during an ignition sequence (for example, a sequence where fuel is being ignited within a combustion chamber to begin combustion), but switched off during a reforming sequence (for example, a sequence in which electromagnetic radiation is being used to chemically modify fuel). Further, in some implementations, the electric field at the concentrator of the electrode 106 used to initiate the plasma corona can be larger than the electric field at the concentrator used to sustain the plasma corona. Hence, in some implementations, the DC power source 302 can be switched on in order to excite the plasma corona, but switched off while the plasma corona is maintained by the signal from the signal generator 202.


In alternate implementations, the system 200 of FIG. 2 and/or the system 300 of FIG. 3A can include a plurality of coaxial resonators 201. If the system 200 of FIG. 2 includes a plurality of coaxial resonators 201, the plurality of coaxial resonators 201 can each be electrically coupled to the same signal generator (for example, such that each of the plurality of coaxial resonators 201 is excited by the same signal), can each be electrically coupled to a respective signal generator (for example, such that each of the plurality of coaxial resonators 201 is independently excited, thereby allowing for unique excitation frequency, power, etc. for each of the plurality of coaxial resonators 201), or one set of the plurality of coaxial resonators 201 can be connected to a common signal generator and another set of the plurality of coaxial resonators 201 can be connected to one or more other signal generators, which could be similar or different from signal generator 202. In implementations of the system 300 that include a plurality of coaxial resonators 201, each of the coaxial resonators 201 can be attached to a respective DC power source (for example, multiple instances of DC power source 302) and a common signal generator (for example, such that a bias signal can be independently switchable and/or adjustable for each coaxial resonator 201, while maintaining a common excitation waveform across all coaxial resonators 201 in the system 300), different signal generators and a common DC power source (for example, such that a bias signal can be jointly switchable across all coaxial resonators 201 in the system 300, while maintaining an independent excitation waveform for each coaxial resonator 201), or different DC power sources and different signal generators (for example, such that the bias signal is independently switchable for each coaxial resonator 201, while maintaining an independent excitation waveform for each coaxial resonator 201).



FIG. 3B illustrates a circuit diagram of the system 300 of FIG. 3A, which includes the signal generator 202, the DC power source 302, and the coaxial resonator 201 (illustrated in vertical cross-section). As illustrated, similar to the QWCCR structure 100, the coaxial resonator 201 includes an outer conductor 322, an inner conductor 324 (including an electrode 326), and a dielectric 328. In addition, when the DC power source 302 is switched off, the circuit illustrated in FIG. 3B may not be an open-circuit. Instead, the signal generator 202 can simply be shorted to the inner conductor 324 when the DC power source 302 is switched off. As illustrated, the outer conductor 322 can be electrically coupled to ground. Further, the signal generator 202 and the DC power source 302 can be connected in series, with their negative terminals connected to ground. The positive terminals of the signal generator 202 and the DC power source 302 can be electrically coupled to the inner conductor 324. Consequently, the electrode 326 can also be electrically coupled to the positive terminals through an electrical coupling between the inner conductor 324 and the electrode 326.


In alternate implementations, the negative terminals of the signal generator 202 and the DC power source 302 can instead be connected to the inner conductor 324 and the positive terminals can be connected to the outer conductor 322. In this way, the signal generator 202 and the DC power source 302 can instead apply a negative voltage (relative to ground) to the electrode 326 and/or inner conductor 324, rather than a positive voltage (relative to ground). Further, in some implementations, the negative terminals of the DC power source 302 and the signal generator 202 and/or the inner conductor 324 might not be grounded.


As stated above, the DC power source 302 can be switchable. In this way a positive bias signal or a negative bias signal can be selectively applied to the inner conductor 324 and/or the electrode 326 relative to the outer conductor 322. When the DC power source 302 is switched on, a bias condition can be present, and when the DC power source 302 is switched off, a bias condition might not be present. A bias signal provided by the DC power source 302 can increase the electric potential, and thus the electric field, at the electrode 326 (for example, at a concentrator of the electrode 106, such as a tip, edge, or blade). By increasing the electric field at the electrode 326, dielectric breakdown and potentially plasma excitation can be more prevalent. Thus, by switching on the DC power source 302, the amount of plasma excited at a plasma corona can be enhanced.


In some implementations, the voltage of the DC power source 302 can range from +1 kV to +100 kV. Alternatively, the voltage of the DC power source 302 can range from −1 kV to −100 kV. Even further, the voltage of the DC power source 302 can be adjustable in some implementations. Furthermore, the voltage of the DC power source 302 can be pulsed, ramped, etc. For example, the voltage can be adjusted by a controller connected to the DC power source 302. In such implementations, the voltage of the DC power source 302 can be adjusted by the controller according to sensor data (for example, sensor data corresponding to temperature, pressure, fuel composition, etc.).


As illustrated in FIG. 4A, an example system 400 can include a controller 402. In various implementations, the controller 402 can include a variety of components. For example, the controller 402 can include a desktop computing device, a laptop computing device, a server computing device (for example, a cloud server), a mobile computing device, a microcontroller (for example, embedded within a control system of a power-generation turbine, an automobile, or an aircraft), and/or a microprocessor. As illustrated, the controller 402 can be communicatively coupled to the signal generator 202, the DC power source 302, an impedance sensor 404, and one or more other sensors 406. Through the communicative couplings, the controller 402 can receive signals/data from various components of the system 400 and control/provide data to various components of the system 400. For example, the controller 402 can switch the DC power source 302 in order to provide a time-modulated bias signal to the coaxial resonator 201 (for example, during an ignition sequence within a combustion chamber adjacent to, coupled to, or surrounding the coaxial resonator 201).


Further, a “communicative coupling,” as presently disclosed, is understood to cover a broad variety of connections between components, based on context. “Communicative couplings” can include direct and/or indirect couplings between components in various implementations. In some implementations, for example, a “communicative coupling” can include an electrical coupling between two (or more) components (for example, a physical connection between the two (or more) components that allows for electrical interaction, such as a direct wired connection used to read a sensor value from a sensor). Additionally or alternatively, a “communicative coupling” can include an electromagnetic coupling between two (or more) components (for example, a connection between the two (or more) components that allows for electromagnetic interaction, such as a wireless interaction based on optical coupling, inductive coupling, capacitive coupling, or coupling though evanescent electric and/or magnetic fields). In addition, a “communicative coupling” can include a connection (for example, over the public internet) in which one or more of the coupled components can transmit signals/data to and/or receive signals/data from one or more of the other coupled components. In various implementations, the “communicative coupling” can be unidirectional (in other words, one component sends signals and another component receives the signals) or bidirectional (in other words, both components send and receive signals). Other directionality combinations are also possible for communicative couplings involving more than two components. One example of a communicative coupling could be the controller 402 communicatively coupled to the coaxial resonator 201, where the controller 402 reads a voltage and/or current value from the resonator directly. Another example of a communicative coupling could be the controller 402 communicating with a remote server over the public Internet to access a look-up table. Additional communicative couplings are also contemplated in the present disclosure.


In some implementations, the controller 402 can control one or more settings of the signal generator 202 (for example, waveform shape, output frequency, output power amplitude, output current amplitude, or output voltage amplitude) or the DC power source 302 (for example, switching on or off or adjusting the level of the bias signal). For example, the controller 402 can control the bias signal of the DC power source 302 (for example, a voltage of the bias signal) based on a calculated voltage used to excite a plasma corona (for example, based on conditions within a combustion chamber). The calculated voltage can account for the voltage amplitude being output by the signal generator 202, in some implementations. The calculated voltage can ensure, for example, that the bias signal has a small effect on any standing electromagnetic wave formed within the coaxial resonator 201 based on an output of the signal generator 202.


The controller 402 can be located nearby the signal generator 202, the DC power source 302, the impedance sensor 404, and/or the one or more other sensors 406. For example, the controller 402 may be connected by a wire connection to the signal generator 202, the DC power source 302, the impedance sensor 404, and/or the one or more other sensors 406. Alternatively, the controller 402 can be remotely located relative to the signal generator 202, the DC power source 302, the impedance sensor 404, and/or the one or more other sensors 406. For example, the controller 402 can communicate with the signal generator 202, the DC power source 302, the impedance sensor 404, and/or the one or more other sensors 406 over BLUETOOTH®, over BLUETOOTH LOW ENERGY (BLE)®, over the public Internet, over WIFI® (IEEE 802.11 standards), over a wireless wide area network (WWAN), etc.


In some implementations, the controller 402 can be communicatively coupled to fewer components within the system 400 (for example, only communicatively coupled to the DC power source 302). Further, in implementations that include fewer components than illustrated in the system 400 (for example, in implementations, having only the coaxial resonator 201, the signal generator 202, and the controller 402), the controller 402 can interact with fewer components of the system 400. For instance, the controller can interact only with the signal generator 202.


The impedance sensor 404 can be connected to the coaxial resonator 201 (for example, one lead to the inner conductor 324 of the coaxial resonator 201 and one lead to the outer conductor 322 of the coaxial resonator 201) to measure an impedance of the coaxial resonator 201. In some implementations, the impedance sensor 404 can include an oscilloscope, a spectrum analyzer, and/or an AC volt meter. The impedance measured by the impedance sensor 404 can be transmitted to the controller 402 (for example, as a digital signal or an analog signal). In some implementations, the impedance sensor 404 can be integrated with the controller 402 or connected to the controller 402 through a printed circuit board (PCB) or other mechanism. The impedance data can be used by the controller 402 to perform calculations and to adjust control of the signal generator 202 and/or the DC power source 302.


Similarly, the other sensors 406 can also transmit data to the controller 402. Analogous to the impedance sensor 404, in some implementations, the other sensors 406 can be integrated with the controller 402 or connected to the controller 402 through a PCB or other mechanism. The other sensors 406 can include a variety of sensors, such as one or more of: a fuel gauge, a tachometer (for example, to measure revolutions per minute (RPM)), an altimeter, a barometer, a thermometer, a sensor that measures fuel composition, a gas chromatograph, a sensor measuring fuel-to-air ratio in a given fuel/air mixture, an anemometer, a torque sensor, a vibrometer, an accelerometer, or a load cell.


In some implementations, the controller 402 can be powered by the DC power source 302. In other implementations, the controller 402 can be independently powered by a separate DC power source or an AC power source (for example, rectified within the controller 402).


As an example, a possible implementation of the controller 402 is illustrated in FIG. 4B. As illustrated, the controller 402 can include a processor 452, a memory 454, and a network interface 456. The processor 452, the memory 454, and the network interface 456 can be communicatively coupled over a system bus 450. The system bus 450, in some implementations, can be defined within a PCB.


The processor 452 can include one or more central processing units (CPUs), such as one or more general purpose processors and/or one or more dedicated processors (for example, application-specific integrated circuits (ASICs), digital signal processors (DSPs), or network processors). The processor 452 can be configured to execute instructions (for example, instructions stored within the memory 454) to perform various actions. Rather than a processor 452, some implementations can include hardware logic (for example, one or more resistor-inductor-capacitor (RLC) circuits, flip-flops, latches, etc.) that performs actions (for example, based on the inputs from the impedance sensor 404 or the other sensors 406).


The memory 454 can store instructions that are executable by the processor 452 to carry out the various methods, processes, or operations presently disclosed. Alternatively, the method, processes, or operations can be defined by hardware, firmware, or any combination of hardware, firmware, or software. Further, the memory 454 can store data related to the signal generator 202 (for example, control signals), the DC power source 302 (for example, switching signals), the impedance sensor 404 (for example, look-up tables related to changes in impedance and/or a characteristic impedance of the coaxial resonator 201 based on certain environmental factors), and/or the other sensors 406 (for example, a look-up table of typical wind speeds based on elevation).


The memory 454 can include non-volatile memory. For example, the memory 454 can include a read-only memory (ROM), electrically erasable programmable read-only memory (EEPROM), a hard drive (for example, hard disk), and/or a solid-state drive (SSD). Additionally or alternatively, the memory 454 can include volatile memory. For example, the memory 454 can include a random-access memory (RAM), flash memory, dynamic random-access memory (DRAM), and/or static random-access memory (SRAM). In some implementations, the memory 454 can be partially or wholly integrated with the processor 452.


The network interface 456 can enable the controller 402 to communicate with the other components of the system 400 and/or with outside computing device(s). The network interface 456 can include one or more ports (for example, serial ports) and/or an independent network interface controller (for example, an Ethernet controller). In some implementations, the network interface 456 can be communicatively coupled to the impedance sensor 404 or one or more of the other sensors 406. Additionally or alternatively, the network interface 456 can be communicatively coupled to the signal generator 202, the DC power source 302, or an outside computing device (for example, a user device). Communicative couplings between the network interface 456 and other components can be wireless (for example, over WIFI®, BLUETOOTH®, BLUETOOTH LOW ENERGY (BLE)®, or a WWAN) or wireline (for example, over token ring, t-carrier connection, Ethernet, a trace in a PCB, or a wire connection).


In some implementations, the controller 402 can also include a user-input device (not shown). For example, the user-input device can include a keyboard, a mouse, a touch screen, etc. Further, in some implementations, the controller 402 can include a display or other user-feedback device (for example, one or more status lights, a speaker, a printer, etc.) (not shown). That status of the controller 402 can alternatively be provided to a user device through the network interface 456. For example, a user device such as a personal computer or a mobile computing device can communicate with the controller 402 through the network interface 456 to retrieve the values of one or more of the other sensors 406 (for example, to be displayed on a display of the user device).


VI. Resonators with Fuel Injection


As illustrated in FIG. 5, in some implementations, the QWCCR structure 100 (or the coaxial resonator 201) can be attached to a fuel tank 502. The fuel tank 502 can provide a fuel source for a combustion chamber or other environment, for example. The fuel tank 502 can contain or be connected to a fuel pump 504 through a fuel-supply line (for example, a hose or a pipe). The fuel pump 504 can transfer fuel from the fuel tank 502 into the fuel-supply line and propel the fuel through a fuel conduit 506 defined by or disposed within the inner conductor 104 of the QWCCR structure 100. For example, the fuel pump 504 can include a mechanical pump (for example, gear pump, rotary vane pump, diaphragm pump, screw pump, peristaltic pump) or an electrical pump. In some implementations, the fuel tank 502 can include various sensors (for example, a pressure sensor, a temperature sensor, or a fuel-level sensor). Such sensors can be electrically connected to the controller 402 in order to provide data regarding the status of the fuel tank 502 to the controller 402, for example. Additionally or alternatively, the fuel pump 504 can be connected to the controller 402. Through such a connection, the controller 402 could control the fuel pump 504 (for example, to switch the fuel pump on and off, set a fuel injection rate, etc.).


In some implementations, the fuel conduit 506 can inject fuel (for example, into a combustion chamber) at one or more outlets 508 defined within the electrode 106 (for example, within a concentrator of the electrode 106). By conveying fuel through the fuel conduit 506 and out one or more outlets 508, fuel can be introduced proximate to a source of ignition energy (for example, proximate to a plasma corona generated near a concentrator of the electrode 106), which can allow for efficient combustion and ignition. In alternate implementations, one or more outlets can be defined with other locations of the fuel conduit 506 (for example, so as not to interfere with the electric field at the concentrator of the electrode 106).


In some implementations, the fuel conduit 506 can act, at least in part, as a Faraday cage (for example, by encapsulating the fuel within a conductor that makes up the fuel conduit 506) to prevent electromagnetic radiation in the QWCCR structure 100 from interacting with the fuel while the fuel is transiting the fuel conduit 506. In other structures, the fuel conduit 506 can allow electromagnetic radiation to interact with (for example, reform) the fuel within the fuel conduit 506.


In some implementations, the QWCCR structure 100 can include multiple fuel conduits 506 (for example, multiple fuel conduits running from the proximal end of the QWCCR structure 100 to the distal end of the QWCCR structure 100). Additionally or alternatively, one or more fuel conduits 506 can be positioned within the dielectric 108 or within the outer conductor 102. As described above, the outlet(s) 508 of the fuel conduit(s) 506 can be oriented in such as a way as to expel fuel toward concentrators (for example, tips, edges, or points) of one or more electrodes 106 (for example, toward regions where plasma coronas are likely to be excited).


VII. Additional Resonator Implementations


FIG. 6 illustrates a cross-sectional view of an example alternative coaxial resonator 600 connected to a DC power source through an additional resonator assembly acting as an RF attenuator, in accordance with example implementations. The coaxial resonator 600 is an assembly of two quarter-wave coaxial cavity resonators that are coupled together. More specifically, the coaxial resonator 600 includes a first resonator 602 and a second resonator 604 electrically coupled in a series arrangement along a longitudinal axis 606. In some implementations, the coaxial resonator 600 includes a DC bias condition established at a node of the voltage standing wave (for example, between quarter-wave segments). In such implementations, there may be no impedance mismatch. Because there is no impedance mismatch, the diameters of the inner conductor and the outer conductor of the first resonator 602 can be different than the diameters of the inner conductor and the outer conductor of the second resonator 604, respectively, without impacting the quality factor (Q). In such a way, the DC bias condition might not affect or interact with the AC signal coming from a signal generator.


The first resonator 602 and the second resonator 604 are defined by a common outer conductor wall structure 608. The outer conductor wall structure 608 includes a first cylindrical wall 610 and a second cylindrical wall 612 centered on the longitudinal axis 606. The first cylindrical wall 610 is constructed of a conducting material and surrounds a first cylindrical cavity 614 centered on the longitudinal axis 606. The first cylindrical cavity 614 is filled with a dielectric 616 having a relative dielectric constant approximately equal to four (εr≈4), for example.


In the example implementation of FIG. 6, the first resonator 602 and the second resonator 604 adjoin one another in a connection plane 618 that is perpendicular to the longitudinal axis 606. In other examples, the connection plane 618 might not be perpendicular to the longitudinal axis 606, and can instead be designed with a different configuration that maintains constant impedance between the first resonator 602 and the second resonator 604.


The second cylindrical wall 612 is constructed of a conducting material and surrounds a second cylindrical cavity 620 that is also centered on the longitudinal axis 606. The second cylindrical cavity 620 is coaxial with the first cylindrical cavity 614, but can have a greater physical length. The second cylindrical wall 612 provides the second cylindrical cavity 620 with a distal end 622 spaced along the longitudinal axis 606 from a proximal end 624 of the second cylindrical cavity 620.


A center conductor structure 626 is supported within the conductor wall structure 608 of the coaxial resonator 600 by the dielectric 616. The center conductor structure 626 includes a first center conductor 628, a second center conductor 630, and a radial conductor 632.


The first center conductor 628 reaches within the first cylindrical cavity 614 along the longitudinal axis 606. In the example implementation shown in FIG. 6, the first center conductor 628 has a proximal end 634 adjacent a proximal end 636 of the first cylindrical cavity 614, and has a distal end 638 adjacent the distal end 624 of the first cylindrical cavity 614. The radial conductor 632 projects radially from a location adjacent the distal end 638 of the first center conductor 628, across the first cylindrical cavity 614, and outward through an aperture 640.


The second center conductor 630 has a proximal end 642 at the distal end 638 of the first center conductor 628. The second center conductor 630 projects along the longitudinal axis 606 to a distal end 644 configured as an electrode tip located at or in close proximity to the distal end 622 of the second cylindrical cavity 620.


To reduce any mismatch in impedances between the first resonator 602 and the second resonator 604, the relative radial thicknesses between both the cylindrical walls 610, 612 and the respective center conductors 628, 630 are defined in relation to the relative dielectric constant of the dielectric 616 and the dielectric constant of the air or gas that fills the second cylindrical cavity 620. In the example implementation of FIG. 6, the physical length of the second center conductor 630 along the longitudinal axis 606 is approximately twice the physical length of the first center conductor 628 along the longitudinal axis 606. However, based at least in part on the dielectric 616 having a relative dielectric constant approximately equal to four, the electrical lengths of the two center conductors 628 and 630 are approximately equal.


In example implementations, any gaps between any of the center conductors 628, 630 and any outer conductor could be filled with a dielectric and/or the gap (for example, the second cylindrical cavity 620) could be large enough to reduce arcing (in other words, large enough such that the electric field is not of sufficient intensity to result in a dielectric breakdown of air or the intervening dielectric). As further shown in FIG. 6, the dielectric 616 fills the first cylindrical cavity 614 around the first center conductor 628 and the radial conductor 632.


In the illustrated example, a DC power source 646 is connected to the center conductor structure 626 through the radial conductor 632 connected adjacent to a virtual short-circuit point of the DC power source 646.


An RF control component, specifically, an RF frequency cancellation resonator assembly 648 is disposed between the radial conductor 632 and the DC power source 646 to restrict RF power from reaching the DC power source 646. The RF frequency cancellation resonator assembly 648 is an additional resonator assembly having a center conductor 650. The center conductor 650 has a first portion 652 and a second portion 654, each of which has the same electrical length “X” illustrated in FIG. 6 (and the same electrical length as the first center conductor 628 and the second center conductor 630).


In an example implementation, the electrical length “X” depicted in FIG. 6 can be sized such that the center conductor 650 is an odd-integer multiple of half wavelengths (for example, ½λ0, 3/2λ0, 5/2λ0, 7/2λ0, 9/2λ0, 11/2λ0, 13/2λ0, etc.) out of phase (in other words, 180° out of phase) with the outer conducting wall 656 and the outer conducting wall 658, simultaneously, where λ0 is the resonant wavelength, and where the resonant wavelength λ0 is inversely related to the frequency of the RF power. In alternative implementations, a similar “folded” structure to the electrical length “X” could be located within the cylindrical cavity 614 to achieve a similar phase shift between the inner conductor and the outer conductor.


The RF frequency cancellation resonator assembly 648 also has a short outer conducting wall 656 and a long outer conducting wall 658. The short outer conducting wall 656 has first and second ends on opposite ends of the RF frequency cancellation resonator assembly 648. The long outer conducting wall 658 also has first and second ends on opposite ends of the RF frequency cancellation resonator assembly 648. The first and second ends of the short outer conducting wall 656 are each on the opposite side of the RF frequency cancellation resonator assembly 648 from the corresponding first and second ends of the long outer conducting wall 658.


In an example implementation, the difference in electrical length between the short outer conducting wall 656 and the long outer conducting wall 658 is substantially equal to the combined electrical length of the first portion 652 and the second portion 654. In this example, the combined electrical length of the first portion 652 and the second portion 654 is substantially equal to twice the electrical length of the first center conductor 628.


In an example implementation, the short outer conducting wall 656 and the long outer conducting wall 658 surround a cavity 660 filled with a dielectric. In operation, with this example implementation, electric current running along the outer conductor of the RF frequency cancellation resonator assembly 648 primarily follows the shortest path and run along the short outer conducting wall 656. Accordingly, electric current on the outer conductor of the RF frequency cancellation resonator assembly 648 travels two fewer quarter-wavelengths than current running along the center conductor 650 of the RF frequency cancellation resonator assembly 648.


In examples, the RF frequency cancellation resonator assembly 648 can also have an internal conducting ground plane 662 disposed within the cavity 660 and between the first portion 652 and the second portion 654 of the center conductor 650. Based on the geometry of the cancellation resonator assembly 648, this configuration provides a frequency cancellation circuit connected between the DC power source 646 and the radial conductor 632.


Further, in examples, the RF frequency cancellation resonator assembly 648 is configured to shift a voltage supply of RF energy 180 degrees out of phase relative to the ground plane 662 of the coaxial resonator 600 due to the difference in electrical length between the short outer conducting wall 656 and the center conductor 650 of the RF frequency cancellation resonator assembly 648.



FIG. 7 illustrates a cross-sectional view of another example alternative coaxial resonator 700 connected to a DC power source through an additional resonator assembly acting as an RF attenuator, in accordance with an example implementation. The coaxial resonator 700 includes a first resonator portion 702 and a second resonator portion 704 electrically coupled in a series arrangement along a longitudinal axis 706.


As depicted in FIG. 7, the first resonator portion 702 and the second resonator portion 704 are defined by a common outer conductor wall structure 708. The wall structure 708 includes a first cylindrical wall portion 710 and a second cylindrical wall portion 712 centered on the longitudinal axis 706. The first cylindrical wall portion 710 is constructed of a conducting material and surrounds a first cylindrical cavity 714 centered on the longitudinal axis 706. In this example implementation, the first cylindrical cavity 714 is filled with a dielectric 716.


An annular edge 718 of the first cylindrical wall portion 710 defines a proximal end 720 of the first cylindrical cavity 714. A proximal end of the second cylindrical wall portion 712 adjoins a distal end 722 of the first cylindrical cavity 714.


The coaxial resonator 700 further includes a first center conductor portion 724 and a second center conductor portion 726 (the center conductor portions 724, 726 represented by the densest cross-hatching in FIG. 7). For illustration, the first center conductor portion 724 and the second center conductor portion 726 are separated by the vertical dashed line in FIG. 7. In some implementations, both the first center conductor portion 724 and the second center conductor portion 726 can correspond to an odd-integer multiple of quarter wavelengths based on the frequency of an RF power source used to excite the coaxial resonator 700. The second center conductor portion 726 has a proximal end 728 adjoining a distal end 730 of the first center conductor portion 724. The second center conductor portion 726 projects along the longitudinal axis 706 to a distal end configured as a concentrator 732 (for example, a tip) of an electrode located at or in close proximity to a distal end 734 of a second cylindrical cavity 736.


The coaxial resonator 700 has an aperture 738 that reaches radially outward through the first cylindrical wall portion 710. A radial conductor 740 extends out through the aperture 738 from the longitudinal axis 706 to be connected to an RF power source (for example, the signal generator 202) by an RF power input line. The end of the radial conductor 740 that is closer to the longitudinal axis 706 connects to a parallel plate capacitor 742 that is in a coupling arrangement to a center conductor structure 744. The parallel plate capacitor 742 is also in a coupling arrangement to an inline folded RF attenuator 746. The spacing between the parallel plate capacitor 742 and the center conductor structure 744 can depend on the materials used for fabrication (for example, the materials used to fabricate the parallel plate capacitor 742, the center conductor structure 744, and/or the dielectric 716).


In an example, the DC power source 646 described above is connected to the center conductor structure 744 at a proximal end 748 of the center conductor structure 744 with a DC power input line. The inline folded RF attenuator 746 is disposed between the second resonator portion 704 and the DC power source 646 to restrict RF power from reaching the DC power source 646.


The inline folded RF attenuator 746 includes an interior center conductor portion 750 having a proximal end 752 and a distal end 754. The inline folded RF attenuator 746 also includes an exterior center conductor portion 756 and a transition center conductor portion 758 that connects or couples the interior center conductor portion 750 and the exterior center conductor portion 756.


The exterior center conductor portion 756 has a proximal end largely in the same plane as the proximal end 752, and a distal end largely in the same plane as the distal end 754. For example, in the cross-sectional illustration of FIG. 7, the plane of the proximal end 752 and the plane of the proximal end of the exterior center conductor portion 756 can be the plane of the cross-section that is illustrated. In this example implementation, the transition center conductor portion 758 is located proximal to the distal end 754. The exterior center conductor portion 756 surrounds the interior center conductor portion 750.


In this example, the exterior center conductor portion 756 resembles a cylindrical portion of conducting material surrounding the rest of the interior center conductor portion 750. The longitudinal lengths of the interior center conductor portion 750 and the exterior center conductor portion 756 are substantially equal to the longitudinal length of the parallel plate capacitor 742 with which they are in a coupling arrangement. The electrical length between the proximal end 752 to the distal end 754, for both the interior center conductor portion 750 and the exterior center conductor portion 756, is substantially equal to one quarter-wavelength. The second center conductor portion 726 and the second cylindrical wall portion 712 are both configured to have an electrical length of one quarter-wavelength.


The wall structure 708 includes a short outer conducting portion 760 which has a proximal end largely in the same plane as the proximal end 752, and a distal end largely in the same plane as the distal end 754. An outer conducting path runs from the distal end of the wall structure 708 (that is substantially coplanar with the distal end 734 of the second cylindrical cavity 736), along the short outer conducting portion 760, and stops at the proximal end 720 of the first cylindrical wall portion 710. In this example, the outer conducting path has an electrical length of two quarter-wavelengths.


An inner conducting path runs from the concentrator 732 to the proximal end 728 of the second center conductor portion 726, along the outside of the transition center conductor portion 758, then along the outside from the distal end to the proximal end of the exterior center conductor portion 756, then along an interior wall 762 of the exterior center conductor portion 756 from its proximal end to its distal end, then along the interior center conductor portion 750 from its distal end to its proximal end. In this example, the electrical length of this inner conducting path is four quarter-wavelengths, or two half wavelengths. The difference in electrical lengths between the inner conducting path and the outer conducting path is one half wavelength.


With this configuration, the inline folded RF attenuator 746 operates as a radio-frequency control component connected between the DC power source 646 and the voltage supply of RF energy. The inline folded RF attenuator 746 is configured to shift a voltage supply of RF energy 180 degrees out of phase relative to the ground plane of the coaxial resonator 700.


The particular arrangement depicted in FIG. 7 is not limiting with respect to the orientation of the inline folded RF attenuator 746. In other examples, the entire arrangement depicted in FIG. 7 can be “stretched,” with the inline folded RF attenuator 746 being disposed further away from the concentrator 732 and not directly coupled to the parallel plate capacitor 742. For example, the inline folded RF attenuator 746 could be separated by one quarter-wavelength from the portion of the center conductor that would remain in direct coupling arrangement with the parallel plate capacitor 742. The coaxial resonator 700 can achieve a maximize efficiency when (i) the inline folded RF attenuator 746 is an odd-integer multiple of quarter wavelengths from the concentrator 732; and (ii) the inline folded RF attenuator 746 is an odd-integer multiple of quarter wavelengths in electrical length.


In another example, the arrangement depicted in FIG. 7 could be more compressed, with the exterior center conductor portions 756 of the inline folded RF attenuator 746 extending longitudinally as far as the parallel plate capacitor 742 and also surrounding the portion of center conductor exposed for plasma creation. This can be implemented by arranging the center conductor structure 744 in the middle so that the exterior center conductor portions 756 extends in either direction longitudinally. Any particular geometry of this arrangement can involve adjusting the various parameters of dielectrics to ensure impedance matching and full 180 degree phase cancellation.


In one example, the arrangements described with respect to FIGS. 6 and 7 and the particular combination of components that provide the RF signal to the coaxial resonators are contained in a body dimensioned approximately the size of a gap spark igniter and adapted to mate with a combustor (for example, of an internal combustion engine). As an example for illustration, a microwave amplifier could be disposed at the resonator, and the resonator could be used as the frequency determining element in an oscillator amplifier arrangement. The amplifier/oscillator could be attached at the top or back of an igniter, and could have the high voltage supply also integrated in the module with diagnostics. This example permits the use of a single, low-voltage DC power supply for feeding the module along with a timing signal.


VIII. Magnetic Direction of Plasma Corona


FIG. 8A illustrates a system 800 that includes a resonator, according to example implementations. The resonator can be a coaxial-cavity resonator, similar to the coaxial resonator 201 illustrated in FIG. 2, for example. Alternatively, the resonator can be a dielectric resonator, a crystal resonator, a ceramic resonator, a surface-acoustic-wave resonator, a yttrium-iron-garnet resonator, a rectangular-waveguide cavity resonator, a parallel-plate resonator, or a gap-coupled microstrip resonator. While reference is made to “QWCCR,” “QWCCR structure,” and “coaxial resonator” elsewhere in the description, it will be understood that other types of resonators are possible and contemplated.


As illustrated, the system 800 can also include a signal generator. For example, the system 800 can include the signal generator 202 illustrated in FIG. 2. As in FIG. 2, the signal generator 202 can be used to excite the coaxial resonator 201 in order to produce a plasma corona (identified by reference numeral 802 in FIG. 8). For example, when the signal generator 202 excites the coaxial resonator 201 using a signal that has a wavelength proximate to an odd-integer multiple of one-quarter (¼) of a resonant wavelength of the coaxial resonator 201 and is of a sufficient power, the coaxial resonator 201 can provide the plasma corona 802 proximate to the electrode 326.


In alternate implementations, the system 800 can additionally include a DC power source configured to provide a bias signal between the inner conductor 324 and the outer conductor 322. For example, the system 800 can include the DC power source 302 of FIG. 3A. In some implementations, the bias signal can reduce the power output from the signal generator 202 used to provide the plasma corona 802.


As described above, given the electromagnetic nature of plasma, the plasma corona 802 can interact with, and be manipulated by, external magnetic fields. For example, placing a ferromagnetic material (for example, iron, cobalt, nickel, neodymium, samarium-cobalt, etc.) near the plasma corona 802 can cause the plasma corona 802 to be attracted to or repelled from the ferromagnetic material (for example, causing the plasma corona 802 to move). Similarly, the plasma corona 802 can be attracted to or repelled from an electromagnet that is energized to produce a magnetic field. As such, in some implementations, the system 800 can include one or more ferromagnets (stationary or in motion), one or more electromagnets (stationary or in motion), and/or a combination of electromagnet(s) and ferromagnet(s) to generate magnetic fields that interact with the plasma corona 802. Additionally or alternatively, other sources of magnetic fields now known or later developed can be used in place of or in addition to the ferromagnets and electromagnets referenced throughout the present disclosure. Further, in addition to manipulating the plasma corona 802, ferromagnetics (stationary or in motion) and electromagnets (stationary or in motion) can modify non-visible ionized gases or other charged particles, whether or not such charged particles are in a plasma state.


For example, FIG. 8B illustrates a system 810 that includes the components of the system 800 illustrated in FIG. 8A, with the addition of a ferromagnet 804. The dashed lines illustrated in FIG. 8B show the magnetic field produced by the ferromagnet 804. As illustrated, in some implementations, the ferromagnet 804 can include a bar magnet. In other implementations, the ferromagnet 804 can instead include a horseshoe magnet, a circular magnet, a u-shaped magnet, a cylindrical magnet, a ring magnet, a disk magnet, a kidney-shaped magnet, a trapezoidal magnet, a marble magnet, a cow magnet, or a spherical magnet. Such a ferromagnet 804 can include paramagnetic materials such as iron, cobalt, and nickel. Additionally or alternatively, the ferromagnet 804 can include rare-earth materials such as gadolinium, neodymium, and samarium.


Further, in some implementations, the ferromagnet 804 can be mounted on or integrated with a structure within a combustion chamber. For example, in an internal combustion engine, the ferromagnet 804 could be mounted on or integrated with a head of a piston. Hence, when the piston reaches top dead center within a cylinder during operation, the ferromagnet 804 can be nearest to the coaxial resonator 201 (for example, if the coaxial resonator 201 is mounted in a similar location within the cylinder as the spark plug in FIG. 1A). Further, the coaxial resonator 201 can be performing plasma ignition of fuel within the cylinder. Thus, the plasma corona 802 of the coaxial resonator 201 can be modified by the ferromagnet 804 during ignition.


Also as illustrated, the ferromagnet 804 can be oriented such that the north pole of the ferromagnet 804 is directed toward the plasma corona 802, the electrode 826, and the coaxial resonator 201. Alternatively, in some implementations, the ferromagnet 804 can be oriented such that the south pole of the ferromagnet 804 is directed toward the plasma corona 802, the electrode 326, and the coaxial resonator 201. In still other implementations, the ferromagnet can be oriented such that neither pole is directed toward the plasma corona 802, the electrode 826, and the coaxial resonator 201. For example, the plane of a bar magnet can be oriented such that it is perpendicular to an axis of the inner conductor 324.


As illustrated in FIG. 8B, the plasma corona 802 can be shortened with respect to the electrode 326 based on the magnetic field applied by the ferromagnet 804. In some implementations, having the south pole of the ferromagnet 804 directed to toward the plasma corona 802, the electrode 326, and the coaxial resonator 201, rather than the north pole, can shorten the plasma corona 802. Whether the north pole of the ferromagnet 804 directed toward the plasma corona 802 or the south pole of the ferromagnet 804 directed toward the plasma corona 802 causes the plasma corona 802 to shorten can depend on the polarity of the signal generator 202 and/or an associated DC power source, in some implementations. Further, the degree to which the plasma corona 802 is shortened can depend on the proximity of the ferromagnet 804 to the electrode 326 and/or a strength of the magnetic field produced by the ferromagnet 804.


Shortening the plasma corona 802 is just one example of many plasma corona features that can be modified by a magnetic field. Other example features of a plasma corona that can be modified by a magnetic field include a shape of the plasma corona, an angle of the plasma corona, and a position of the plasma corona with respect to the electrode 326.


In still other implementations, rather than a ferromagnet 804, an electromagnet could be used to generate the magnetic field. Such an electromagnet can include one or more loops of wire or other conductor. In order to increase the strength of the electromagnet, the one or more loops of wire can be wrapped around a core. The core can include a material having non-unity relative magnetic permeability (μr). For example, the core can include one or more of the following: neodymium (μr=1.05), nickel (μr=100), ferrite (MnZn)(μr=640), or iron (μr=5000). Based on the relative magnetic permeability (μr), the number of loops of wire, and the current flowing through the one or more loops or wire, a corresponding magnetic field can be produced. In some implementations, one end of the core material of the electromagnetic can be oriented proximate to the inner conductor 324, the electrode 326, and/or the plasma corona 802.


The polarity of the electromagnet can be determined based on the direction of current flowing within the electromagnet for example. Thus, if the south pole directed toward the plasma corona 802 and the electrode 326 causes the plasma corona 802 to shorten, instead of rotating the electromagnet to cause the plasma corona 802 to elongate, the current within the electromagnet could instead be reversed. Upon reversing the current, a north pole of the electromagnet can then be directed toward the plasma corona 802 and the electrode 326.


In addition to controlling the direction of the current, the magnitude of the current can be adjusted. Adjusting the magnitude of the current can modify the strength of the corresponding magnetic field generated. For example, in order to further shorten the plasma corona 802, an intensity of the magnetic field can be increased by increasing the magnitude of the current flowing within the electromagnet.


The direction of the current within the electromagnet and the magnitude of the electric current within the electromagnet can be controlled by a controller, in some implementations. Such a controller could receive sensor data and make determinations based on that data. Additionally or alternatively, such a controller could receive a control signal. For example, a user could indicate settings for a shape of the plasma corona 802. The settings can be communicated to the controller based on a control signal. Then, based on the control signal, the controller can energize the one or more electromagnets with a specific current direction and magnitude.



FIG. 8C illustrates the system 810 of FIG. 8B. However, in FIG. 8C, the ferromagnet 804 has been rotated 180 degrees with respect to the plasma corona 802, the electrode 326, and the coaxial resonator 201. In other words, the polarity of the ferromagnet 804 relative to the plasma corona 802, the electrode 326, and the coaxial resonator 201, has been reversed from FIG. 8B. As such, rather than the plasma corona 802 being shortened, the plasma corona 802 is instead elongated. Analogous with what is described above, elongating the plasma corona 802 can, in some implementations, be done be orienting the north pole of the ferromagnet 804 toward the plasma corona 802, rather than the south pole of the ferromagnet 804, as illustrated. Further, the degree to which the plasma corona 802 is elongated can depend on the proximity of the ferromagnet 804 to the electrode 326 and/or a strength of the magnetic field produced by the ferromagnet 804. As with FIG. 8B, the ferromagnet 804 could be replaced by multiple ferromagnets, in some implementations. In other implementations, as with FIG. 8B, the ferromagnet 804 could be replaced with or augmented by one or more electromagnets.



FIG. 8D illustrates the system 810 of FIGS. 8B and 8C. However, in FIG. 8D, the ferromagnet 804 has been oriented perpendicularly with respect to an axis of the inner conductor 324 (rather than parallel as illustrated in FIGS. 8B and 8C). Alternatively, in some implementations, the ferromagnet 804 could be oriented such that an axis of the ferromagnet 804 is neither parallel nor perpendicular with respect to an axis of the inner conductor 324. For example, the ferromagnet 804 could be angled at 45 degrees with respect to an axis of the inner conductor 324 and with respect to the electrode 326. As illustrated in FIG. 8D, a magnetic field produced by the ferromagnet 804 can angle the plasma corona 802 with respect to the electrode 326 and the coaxial resonator 201. Analogous with what is described above, angling the plasma corona 802 to the right can, in some implementations, be done be orienting the south pole of the ferromagnet 804 toward the plasma corona 802, rather than the north pole of the ferromagnet 804, as illustrated in FIG. 8D.


Further, the degree to which the plasma corona 802 is angled can depend on the proximity of the ferromagnet 804 to the electrode 326, the angle of the ferromagnet 804 with respect to the electrode 326, and/or the strength of the magnetic field produced by the ferromagnet 804.



FIG. 8E illustrates the system 810 of FIGS. 8B, 8C, and 8D. Similar to FIG. 8D, in FIG. 8E, the ferromagnet 804 has been oriented perpendicularly with respect to an axis of the inner conductor 324 (rather than parallel as illustrated in FIGS. 8B and 8C). However, the polarity of the ferromagnet 804 is reversed in FIG. 8E when compared with FIG. 8D. This could be done by rotating the ferromagnet 804, for example. As illustrated in FIG. 8E, a magnetic field produced by the ferromagnet 804 can angle the plasma corona 802 with respect to the electrode 326 and the coaxial resonator 201. Analogous with what is described above, angling the plasma corona 802 to the left can, in some implementations, be done by orienting the north pole of the ferromagnet 804 toward the plasma corona 802, rather than the south pole of the ferromagnet 804, as illustrated in FIG. 8D.


Further, the degree to which the plasma corona 802 is angled can depend on the proximity of the ferromagnet 804 to the electrode 326, the angle of the ferromagnet 804 with respect to the electrode 326, and/or the strength of the magnetic field produced by the ferromagnet 804.



FIGS. 8F and 8G illustrate the system 810 of FIGS. 8B-8E. FIG. 8F is a top-view of the system 810 and FIG. 8G is a side-view of the system 810. However, in the system 810 as illustrated in FIGS. 8F and 8Q the ferromagnet 804 is instead a torus that wraps around the coaxial resonator 201. Depending on the polarity and orientation of the ferromagnet 804, the plasma corona 802 can be elongated or shortened by the ferromagnet 804. In alternate implementations, the toroidal ferromagnet 804 could instead cause the plasma corona 802 to stand off from the electrode 326 by an increased distance. Further, if the inner conductor 324 and or the outer conductor 322 include ferromagnetic materials, the coaxial resonator 201, itself, can act as a core material having non-unity magnetic permeability to strengthen an effect of the ferromagnet 804 on the plasma corona 802.


The ferromagnet 804 as illustrated in FIGS. 8F and 8G could be adhered to outer conductor 322, in some implementations. In other implementations, the ferromagnet 804 as illustrated in FIGS. 8F and 8G could be machined as a single piece with the outer conductor 322. Additionally or alternatively, in some implementations, the ferromagnet 804 in FIGS. 8F and 8G could be electrically insulated from the outer conductor 322 such that the ferromagnet 804 does not alter a resonant wavelength of the coaxial resonator 201. Further, in some implementations, the outer conductor 322 can include a ferromagnetic plating, which could produce a similar effect on the plasma corona 802 to the toroidal ferromagnet 804 illustrated in FIGS. 8F and 8G.


In some implementations, other than modifying the angle or elongation of the plasma corona (as in FIGS. 8B-8G), the ferromagnet 804 (or an electromagnet performing an analogous function) can change a stand-off distance between the electrode 326 and the plasma corona 802. For example, a magnetic field generated by the ferromagnet 804 and/or an electromagnet could produce magnetic conditions amenable to the generation of the plasma corona 802. Based on the location of the ferromagnet 804 and/or the electromagnet, the magnetic field can be positioned a given distance from the electrode 326. In such implementations, the plasma corona 802 can be generated at the given distance from the electrode 326.


In still other implementations, a magnetic field generated by the ferromagnet 804 and/or an electromagnet, could transit the plasma corona 802, once generated, away from the electrode 326. For example, an electromagnet configured to source high-intensity magnetic field lines and disposed near the coaxial resonator 201 could be energized after a plasma corona is generated near the electrode 326. The electromagnet can be energized continuously or in a pulsed fashion, in various implementations. Upon energizing the electromagnet, the high-intensity magnetic field lines can be generated and used to transit the plasma corona 802 along those magnetic field lines. In an implementation where the coaxial resonator 201 is disposed within a combustion chamber, for instance, the transiting of the plasma corona 802 along magnetic field lines can be used to move the plasma corona 802 to different regions of the combustion chamber. In other words, the plasma corona 802 can be “shot” from one region to another within the combustion chamber. For example, the plasma corona 802 can be transported to regions of the combustion chamber housing unburned fuel so as to more efficiently combust fuel within the combustion chamber.


Even further, in an implementation where the coaxial resonator 201 is disposed within a combustion chamber, the plasma corona 802 can be shaped by a magnetic field such that it conforms to a shape of the combustion chamber. For example, if the combustion chamber is shaped circularly, the plasma corona 802 can be shaped as an arc using a magnetic field such that the plasma corona 802 traces out a perimeter of an interior wall of the combustion chamber. Additionally or alternatively, the plasma corona 802 could be elongated such that the plasma corona 802 spans a diameter of the combustion chamber. Shaping the plasma corona 802 to mirror a shape of a combustion chamber can improve the ignition conditions within the combustion chamber, in some implementations. Further, such a shaping can be done in addition to or instead of transporting the plasma corona 802 along magnetic field lines.


In some implementations, a magnetic field can be generated by a plurality of ferromagnets and/or electromagnets (as opposed to a single ferromagnet or electromagnet). FIG. 9A is a top-view illustration of a system 900 that includes a resonator, according to example implementations. The resonator can be the coaxial resonator 201 illustrated in other figures, for example. The system 900 can also include a plurality of electromagnets. For example, the system 900 can include a first electromagnet 910, a second electromagnet 920, a third electromagnet 930, a fourth electromagnet 940, a fifth electromagnet 950, a sixth electromagnet 960, a seventh electromagnet 970, and an eighth electromagnet 980. Further, as illustrated, each of the electromagnets can have an associated power supply. For example, the system 900 can include a first power source 912, a second power source 922, a third power source 932, a fourth power source 942, a fifth power source 952, a sixth power source 962, a seventh power source 972, and an eighth power source 982. In alternate implementations, one or more of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 can share a single power supply. For example, all of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 could be powered by a common power supply, in some implementations.


The electromagnets 910, 920, 930, 940, 950, 960, 970, 980 illustrated in FIG. 9A can replace and/or augment one or more ferromagnets. In an example implementation, for instance, ferromagnets and electromagnets can be alternated (electromagnet, ferromagnet, electromagnet, ferromagnet, etc.) around the circumference of the coaxial resonator 201. Additionally, in various implementations, the system 900 can include greater or fewer than eight electromagnets. It is understood that eight electromagnets are illustrated merely by way of example.


Each of the electromagnets 910, 920, 930, 940, 950, 906, 970, 980 can include a length of wire (or other conductor) configured to guide current flow sourced by a respective power source. The length of wire can be wrapped a number of times around a core material. The number of wraps of the length of wire around the core material can correspond to the strength of the magnetic field generated by the corresponding electromagnet. Different electromagnets 910, 920, 930, 940, 950, 960, 970, 980 within the system 900 can have different numbers of wraps, in some implementations. Further, the core material can include one or more materials having non-unity relative magnetic permeability. For example, the core can include one or more of the following: neodymium (μr=1.05), nickel (μr=100), ferrite (MnZn) (μr=640), or iron (μr=5000). In addition, different electromagnets 910, 920, 930, 940, 950, 960, 970, 980 within the system 900 can include different core materials, in some implementations.


As illustrated, each of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 can be oriented such that an axis of the respective electromagnet is perpendicular with respect to an axis of the inner conductor 324. In alternate implementations, one or more of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 could be oriented such that an axis of the respective electromagnet is parallel with respect to an axis of the inner conductor 324.


Additionally or alternatively, in some implementations, one or more of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 could be oriented such that an axis of the respective electromagnet is neither parallel nor perpendicular with respect to an axis of the inner conductor 324. For example, the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 could each be angled at 45 degrees with respect to an axis of the inner conductor 324 and oriented such that a distal end of each of the corresponding core materials is directed toward a location that is in-line with an axis of the inner conductor 324 but disposed beyond the electrode 326. Based on such an orientation, the magnetic field can be concentrated at a point that is separated from the electrode 326 by a stand-off distance. Such an implementation is illustrated in FIG. 9B in cross section. Only two of the electromagnets 930, 970 are illustrated to prevent clutter of the figure. The stand-off distance is illustrated by reference numeral 992.


In still other implementations, one or more of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 could be oriented such that a distal end of the corresponding core material is directed away from the inner conductor 324 so as to disperse the magnetic field and/or affect the magnetic conditions in additional regions surrounding the coaxial resonator 201.


Further, in some implementations, one or more of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 can be disposed along the axis of the inner conductor 324 of the coaxial resonator 201 at the same location as the electrode 326. In other words, the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 can be located at the distal end of the coaxial resonator 201. In other implementations, one or more of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 can be located longitudinally beyond the distal end of the coaxial resonator 201, between the distal end and the proximal end of the coaxial resonator 201, and/or longitudinally beyond the proximal end of the coaxial resonator 201.


In various implementations, distances between the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 and the coaxial resonator 201 can vary. Further, in some implementations, the polarity of one or more of the electromagnetics 910, 920, 930, 940, 950, 960, 970, 980 with respect to the coaxial resonator 201 can be varied. For example, a first half of the electromagnets 910, 920, 930, 940 can have one magnetic pole oriented toward the coaxial resonator 201 (for example, a north pole) and a second half of the electromagnets 950, 960, 970, 980 can have an opposite magnetic pole oriented toward the coaxial resonator 201 (for example, the south pole). In this way, one of the two halves of electromagnets could be attracting a plasma corona, while the other half of the electromagnets could be opposing the plasma corona, thereby resulting in an increased force applied to the corona.


In some implementations, the respective power sources 912, 922, 932, 942, 952, 962, 972, 982 can be individually switchable in order to individually energize the corresponding electromagnet 910, 920, 930, 940, 950, 960, 970, 980. Further, the individual power sources 912, 922, 932, 942, 952, 962, 972, 982 can be communicatively coupled to one or more controllers. For example, a single controller can be communicatively coupled to each of the respective power sources 912, 922, 932, 942, 952, 962, 972, 982. Such a controller can independently and selectively switch or adjust each of the respective power sources 912, 922, 932, 942, 952, 962, 972, 982, in some implementations.


By independently switching each of the individual power sources 912, 922, 932, 942, 952, 962, 972, 982, the magnetic field near the coaxial resonator 201 and the electrode 326 can be controlled. For example, the individual power sources 912, 922, 932, 942, 952, 962, 972, 982 could be sequentially switched on/off according to a predetermined sequence. The predetermined sequence can include common durations and intensities across all of the individual power sources 912, 922, 932, 942, 952, 962, 972, 982, in some implementations. In alternate implementations, the predetermined sequence can include variable durations and/or intensities across the individual power sources 912, 922, 932, 942, 952, 962, 972, 982. Based on the predetermined sequence, the shape, angle, and/or position of the plasma corona 802 can be modified according to a predetermined sequence (for example, the plasma corona 802 could trace a predetermined pattern over time). In one implementation, the predetermined sequence can include the first power source 912 being switched on for a predetermined time, followed by the first power source 912 being switched off and the second power source 922 being switched on for a predetermined time, followed by the second power source 922 being switched off and the third power source 932 being switched on for a predetermined time, etc. Using such a predetermined sequence, the plasma corona 802 can precess through a range of angles about its axis.


In another implementation, the first four power sources 912, 922, 932, 942 can first be switched on for a predetermined time, followed by the first four power sources 912, 922, 932, 942 being switched off and the second four power sources 952, 962, 972, 982 being switched on for a predetermined time. This sequence could repeat periodically, causing the plasma corona 802 (based on the associated magnetic fields of the electromagnets) to oscillate (for example, from a first angle to a second angle and back again). In some implementations, for example, the sequence can be repeated periodically with varying magnitudes of the generated magnetic fields and/or varying polarities of the magnetic fields.


In yet another implementation, the first power source 912, the third power source 932, the fifth power source 952, and the seventh power source 972 can first be switched on for a predetermined time, followed by the first power source 912, the third power source 932, the fifth power source 952, and the seventh power source 972 being switched off and the second power source 922, the fourth power source 942, the sixth power source 962, and the eighth power source 982 being switched on for a predetermined time. This sequence could repeat periodically, causing the plasma corona 802 (based on the associated magnetic fields of the electromagnets) to oscillate (for example, from elongated to shortened and back again).


A myriad of other combinations of predetermined energizing sequences are contemplated within the present disclosure. The predetermined sequence can be based on a set of detectors feeding data to the controller, based on a user-input, or based on a sequence stored within a non-transitory, computer-readable medium (for example, the memory 454 illustrated in FIG. 4B), in various implementations. For example, for some implementations where the coaxial resonator 201 is disposed within or adjacent to a combustion chamber, the controller can receive data regarding combustion within the combustion chamber (for example, temperature readings, pressure readings, and/or fuel mixture composition readings from different regions of the combustion chamber). Based on the received data, the controller can determine a location of unburned fuel within the combustion chamber. For example, based on regions of low temperature within the combustion chamber (indicated by received data), the controller can infer that complete combustion has not taken place in those locations. Then, based on the location of unburned fuel, the controller can determine a predetermined sequence by which to energize the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 in order to promote combustion in the location of unburned fuel (for example, by angling or elongating the plasma corona 802 toward the location of unburned fuel).


Alternatively, in some implementations, multiple electromagnets 910, 920, 930, 940, 950, 960, 970, 980 could be connected to a single, switchable power source. Even further, in some implementations, all of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 could be connected to a single, switchable power source. In this way, the single, switchable power source could be switched on to energize all of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 and could be switched off to de-energize all of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980. By switching the single, switchable power source on or off, the magnetic field near the electrode 326, and consequently the plasma corona 802, could change conformation and/or intensity. Such a switching could be controlled by a controller communicatively coupled to the single, switchable power source.


In addition or alternative to a controller selectively energizing one or more of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980, a controller (for example, the controller 402 illustrated in FIGS. 4A and 4B) can be configured (for example, by executing instructions stored within the memory 454) move/reorient the electromagnets 910, 920, 930, 940, 950, 960, 970, 980. For example, each of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 can be mounted on a respective stage, each respective stage being capable of rotating and translating in six degrees (or fewer) of freedom. Moving/reorienting one of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 can allow the magnetic field produced by the respective electromagnet 910, 920, 930, 940, 950, 960, 970, 980 to change polarity, be directed in a different direction, change intensity, or be disposed/sourced from a different location. In implementations including one or more ferromagnets, the controller can also be capable of moving/reorienting the ferromagnets. For example, each of the one or more ferromagenets can be mounted on a respective stage having six degrees (or fewer) of freedom that is controlled by the controller. One or more servos can also be engaged by the controller to move/reorient ferromagnets and/or electromagnets.


Additionally or alternatively, a controller (for example, the controller 402 illustrated in FIGS. 4A and 4B) can be configured to move/reorient the coaxial resonator 201 with respect to the electromagnets 910, 920, 930, 940, 950, 960, 970, 980. For example, the coaxial resonator 201 can be mounted on a stage, where the stage is capable of rotating and translating in six degrees (or fewer) of freedom. Moving/reorienting the coaxial resonator 201 with respect to the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 can allow the magnetic fields incident on the coaxial resonator 201 to change polarity, be directed in a different direction, change intensity, or be disposed/sourced from a different relative location.


Even further, a controller (for example, the controller 402 illustrated in FIGS. 4A and 4B) can be configured to interpose one or more materials with non-unity relative magnetic permeabilities between (i) one or more of the electromagnets 910, 920, 930, 940, 950, 960, 970, 980 and (ii) the coaxial resonator 201/the plasma corona 802 so as to modify the magnetic field near the plasma corona 802. In implementations including one or more ferromagnets, a controller can be configured to interpose one or more materials with non-unity relative magnetic permeabilities between (i) one or more of the ferromagnets and (ii) the coaxial resonator 201/the plasma corona 802 so as to modify the magnetic field near the plasma corona 802.


IX. Example Methods


FIG. 10 illustrates a method 1000, according to example implementations. The method 1000 can be performed by a system. For example, the method 1000 can be performed by the system 900 illustrated in FIG. 9A. Various features described above can be applied in the context of the method 1000. Such features can be applied in addition to or instead of the features of the method 1000 described below.


At block 1002, the method 1000 can include exciting, by a radio-frequency power source, a resonator electromagnetically coupled to the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of a resonant wavelength of the resonator. The resonator can include a first conductor. The resonator can also include a second conductor. Further, the resonator can include a dielectric between the first conductor and the second conductor. Even further, the resonator can include an electrode electromagnetically coupled to the first conductor and including a concentrator.


At block 1004, the method 1000 can include concentrating an electric field at the concentrator.


At block 1006, the method 1000 can include, in response to exciting the resonator, providing a plasma corona proximate to the concentrator.


At block 1008, the method 1000 can include providing, by a magnetic-field source, a magnetic field proximate to the concentrator.


At block 1010, the method 1000 can include modifying, by the magnetic field, at least one feature of the plasma corona selected from the group consisting of a shape of the plasma corona, an angle of the plasma corona, and a position of the plasma corona with respect to the electrode.


In some implementations, the method 1000 can also include providing a bias signal between the first conductor and the second conductor.


In some implementations, the method 1000 can also include receiving, by a controller, sensor data. Further, the method 1000 can include determining, by the controller based on the sensor data, a location of unburned fuel within a combustion chamber (for example, based on temperature data from one or more sensors within the combustion chamber). In addition, the method 1000 can include adjusting, by the controller based on the location of unburned fuel within the combustion chamber, the magnetic field provided by the magnetic-field source. Adjusting the magnetic field can include moving the magnetic-field source with respect to the plasma corona. Additionally or alternatively, adjusting the magnetic field can include interposing a material with non-unity relative permeability between the magnetic-field source and the plasma corona. Even further, the method 1000 can include directing, by the magnetic field, the plasma corona toward the location of unburned fuel.


In some implementations, the method 1000 can include selectively energizing, by a controller, the magnetic-field source and at least one additional individually energizable magnetic-field source according to a pre-determined sequence. Further, the method 1000 can include sequentially modifying the feature of the plasma corona from block 1010.


The particular arrangements shown in the figures should not be viewed as limiting. It should be understood that other implementations can include more or less of each element shown in a given figure. Further, some of the illustrated elements can be combined or omitted. Yet further, an illustrative implementation can include elements that are not illustrated in the figures.


A step or block that represents a processing of information can correspond to circuitry that can be configured to perform the specific logical functions of a method or technique as presently disclosed. Alternatively or additionally, a step or block that represents a processing of information can correspond to a module, a segment, or a portion of program code (including related data). The program code can include one or more instructions executable by a processor for implementing specific logical functions or actions in the method or technique. The program code and/or related data can be stored on any type of computer-readable medium such as a storage device including a disk, hard drive, or other storage medium.


The computer-readable medium can also include non-transitory computer-readable media such as computer-readable media that store data for short periods of time like register memory, processor cache, and random access memory (RAM). The computer-readable media can also include non-transitory computer-readable media that store program code and/or data for longer periods of time. Thus, the computer-readable media can include secondary or persistent long term storage, like read only memory (ROM), optical or magnetic disks, compact-disc read only memory (CD-ROM), for example. The computer-readable media can also be any other volatile or non-volatile storage systems. A computer-readable medium can be considered a computer-readable storage medium, for example, or a tangible storage device.


While various examples and implementations have been disclosed, other examples and implementations will be apparent to those skilled in the art. The various disclosed examples and implementations are for purposes of illustration and are not intended to be limiting, with the true scope being indicated by the claims.

Claims
  • 1. A system comprising: a radio-frequency power source;a resonator configured to electromagnetically couple to the radio-frequency power source and having a resonant wavelength, the resonator including: a first conductor,a second conductor,a dielectric between the first conductor and the second conductor, andan electrode configured to electromagnetically couple to the first conductor and including a concentrator, wherein the resonator is configured to provide a plasma corona proximate to the concentrator when excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of the resonant wavelength; anda magnetic-field source configured to provide a magnetic field proximate to the concentrator so as to modify at least one feature of the plasma corona selected from the group consisting of a shape of the plasma corona, an angle of the plasma corona, and a position of the plasma corona with respect to the electrode.
  • 2. The system of claim 1, further comprising a switchable direct-current power source configured to provide a bias signal between the first conductor and the second conductor.
  • 3. The system of claim 1, wherein the magnetic-field source includes a ferromagnet.
  • 4. The system of claim 1, wherein the magnetic-field source includes a switchable electromagnet.
  • 5. The system of claim 4, wherein the switchable electromagnet includes a length of wire wrapped around a core material including at least one end of the core material directed toward the concentrator,wherein, when a current flows through the length of wire, the switchable electromagnet generates a magnetic field in the core material and near the at least one end, andwherein the current that flows through the length of wire is controllable so as to modify an extent or direction of the magnetic field proximate to the concentrator.
  • 6. The system of claim 5, wherein the core material includes a material having a relative magnetic permeability above about 1.01.
  • 7. The system of claim 1, further comprising a plurality of additional magnetic-field sources, each configured to provide a magnetic field proximate to the concentrator so as to modify the at least one feature of the plasma corona.
  • 8. The system of claim 7, wherein each of the plurality of additional magnetic-field sources is individually energizable so as to independently modify the at least one feature of the plasma corona.
  • 9. The system of claim 8, further comprising a controller configured to carry out operations, the operations including: selectively energizing the magnetic-field source and plurality of additional magnetic-field sources according to a pre-determined sequence so as to sequentially modify the at least one feature of the plasma corona.
  • 10. The system of claim 1, wherein modifying the at least one feature of the plasma corona includes modifying the at least one feature of the plasma corona according to a predetermined pattern based on a location of unburned fuel within a combustion chamber so as to direct the plasma corona toward the location of unburned fuel.
  • 11. The system of claim 10, further comprising a controller configured to carry out operations, the operations including: determining, based on sensor data received by the controller, the location of unburned fuel within the combustion chamber, andadjusting, based on the location of unburned fuel within the combustion chamber, the magnetic field provided by the magnetic-field source so as to direct the plasma corona toward the location of unburned fuel.
  • 12. The system of claim 11, wherein the operation of adjusting the magnetic field includes: moving the magnetic-field source with respect to the plasma corona, orinterposing a material with non-unity relative magnetic permeability between the magnetic-field source and the plasma corona.
  • 13. The system of claim 1, wherein modifying the shape of the plasma corona includes: adjusting a localized plasma density within the plasma corona,elongating the plasma corona,shortening the plasma corona,expanding the plasma corona,contracting the plasma corona,adjusting an orientation of the plasma corona, orextinguishing the plasma corona.
  • 14. The system of claim 1, further comprising a combustion chamber configured to house combustion of an air/fuel mixture when the air/fuel mixture is ignited by the plasma corona, wherein modifying the feature of the plasma corona includes matching the plasma corona to a shape of the combustion chamber.
  • 15. The system of claim 1, wherein the resonator includes at least one resonator selected from the group consisting of a coaxial-cavity resonator, a dielectric resonator, a rectangular-waveguide cavity resonator, a parallel-plate resonator, and a gap-coupled microstrip resonator.
  • 16. A method comprising: exciting, by a radio-frequency power source, a resonator electromagnetically coupled to the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of a resonant wavelength of the resonator, wherein the resonator includes: a first conductor,a second conductor,a dielectric between the first conductor and the second conductor, andan electrode electromagnetically coupled to the first conductor and including a concentrator;concentrating an electric field at the concentrator;in response to exciting the resonator, providing a plasma corona proximate to the concentrator;providing, by a magnetic-field source, a magnetic field proximate to the concentrator; andmodifying, by the magnetic field, at least one feature of the plasma corona selected from the group consisting of a shape of the plasma corona, an angle of the plasma corona, and a position of the plasma corona with respect to the electrode.
  • 17. The method of claim 16, further comprising providing a bias signal between the first conductor and the second conductor.
  • 18. The method of claim 16, further comprising: receiving, by a controller, sensor data;determining, by the controller based on the sensor data, a location of unburned fuel within a combustion chamber;adjusting, by the controller based on the location of unburned fuel within the combustion chamber, the magnetic field provided by the magnetic-field source; anddirecting, by the magnetic field, the plasma corona toward the location of unburned fuel.
  • 19. The method of claim 18, wherein adjusting the magnetic field includes moving the magnetic-field source with respect to the plasma corona.
  • 20. The method of claim 18, wherein adjusting the magnetic field includes interposing a material with non-unity relative permeability between the magnetic-field source and the plasma corona.
  • 21. The method of claim 16, further comprising: selectively energizing, by a controller, the magnetic-field source and at least one additional individually energizable magnetic-field source according to a pre-determined sequence; andsequentially modifying the at least one feature of the plasma corona.
  • 22. A system comprising: a combustion chamber;a radio-frequency power source;a resonator configured to electromagnetically couple to the radio-frequency power source and having a resonant wavelength, the resonator including: a first conductor,a second conductor,a dielectric between the first conductor and the second conductor, andan electrode configured to electromagnetically couple to the first conductor and including a concentrator, wherein the resonator is configured to provide a plasma corona proximate to the concentrator when excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of the resonant wavelength, and wherein the plasma corona is usable to ignite a fuel/air mixture within the combustion chamber; anda magnetic-field source configured to provide a magnetic field proximate to the concentrator so as to modify at least one feature of the plasma corona selected from the group consisting of a shape of the plasma corona, an angle of the plasma corona, and a position of the plasma corona with respect to the electrode.
CROSS-REFERENCE TO RELATED APPLICATIONS

The present application hereby incorporates by reference U.S. Pat. Nos. 5,361,737; 7,721,697; 8,783,220; 8,887,683; 9,551,315; 9,624,898; and 9,638,157. The present application also hereby incorporates by reference U.S. Patent Application Pub. Nos. 2009/0194051; 2011/0146607; 2011/0175691; 2014/0283780; 2014/0283781; 2014/0327357; 2015/0287574; 2017/0082083; 2017/0085060; 2017/0175697; and 2017/0175698. In addition, the present application hereby incorporates by reference International Patent Application Pub. Nos. WO 2011/112786; WO 2011/127298; WO 2015/157294; and WO 2015/176073. Further, the present application hereby incorporates by reference the following U.S. patent applications, each filed on the same date as the present application: “Plasma-Distributing Structure in a Resonator System” (identified by attorney docket number 17-1501); “Fuel Injection Using a Dielectric of a Resonator” (identified by attorney docket number 17-1505); “Jet Engine Including Resonator-based Diagnostics” (identified by attorney docket number 17-1506); “Power-generation Turbine Including Resonator-based Diagnostics” (identified by attorney docket number 17-1507); “Electromagnetic Wave Modification of Fuel in a Jet Engine” (identified by attorney docket number 17-1508); “Electromagnetic Wave Modification of Fuel in a Power-generation Turbine” (identified by attorney docket number 17-1509); “Jet Engine with Plasma-assisted Combustion” (identified by attorney docket number 17-1510); “Jet Engine with Fuel Injection Using a Conductor of a Resonator” (identified by attorney docket number 17-1511); “Jet Engine with Fuel Injection Using a Dielectric of a Resonator” (identified by attorney docket number 17-1512); “Jet Engine with Fuel Injection Using a Conductor of At Least One of Multiple Resonators” (identified by attorney docket number 17-1513); “Jet Engine with Fuel Injection Using a Dielectric of At Least One of Multiple Resonators” (identified by attorney docket number 17-1514); “Plasma-Distributing Structure in a Jet Engine” (identified by attorney docket number 17-1515); “Power-generation Gas Turbine with Plasma-assisted Combustion” (identified by attorney docket number 17-1516); “Power-generation Gas Turbine with Fuel Injection Using a Conductor of a Resonator” (identified by attorney docket number 17-1517); “Power-generation Gas Turbine with Fuel Injection Using a Dielectric of a Resonator” (identified by attorney docket number 17-1518); “Power-generation Gas Turbine with Plasma-assisted Combustion Using Multiple Resonators” (identified by attorney docket number 17-1519); “Power-generation Gas Turbine with Fuel Injection Using a Conductor of At Least One of Multiple Resonators” (identified by attorney docket number 17-1520); “Power-generation Gas Turbine with Fuel Injection Using a Dielectric of At Least One of Multiple Resonators” (identified by attorney docket number 17-1521); “Plasma-Distributing Structure in a Power Generation Turbine” (identified by attorney docket number 17-1522); “Jet Engine with Plasma-assisted Combustion and Directed Flame Path” (identified by attorney docket number 17-1523); “Jet Engine with Plasma-assisted Combustion Using Multiple Resonators and a Directed Flame Path” (identified by attorney docket number 17-1524); “Plasma-Distributing Structure and Directed Flame Path in a Jet Engine” (identified by attorney docket number 17-1525); “Power-generation Gas Turbine with Plasma-assisted Combustion and Directed Flame Path” (identified by attorney docket number 17-1526); “Power-generation Gas Turbine with Plasma-assisted Combustion Using Multiple Resonators and a Directed Flame Path” (identified by attorney docket number 17-1527); “Plasma-Distributing Structure and Directed Flame Path in a Power Generation Turbine” (identified by attorney docket number 17-1528); “Jet engine with plasma-assisted afterburner” (identified by attorney docket number 17-1529); “Jet engine with plasma-assisted afterburner having Resonator with Fuel Conduit” (identified by attorney docket number 17-1530); “Jet engine with plasma-assisted afterburner having Resonator with Fuel Conduit in Dielectric” (identified by attorney docket number 17-1531); “Jet engine with plasma-assisted afterburner having Ring of Resonators” (identified by attorney docket number 17-1532); “Jet engine with plasma-assisted afterburner having Ring of Resonators and Resonator with Fuel Conduit” (identified by attorney docket number 17-1533); “Jet engine with plasma-assisted afterburner having Ring of Resonators and Resonator with Fuel Conduit in Dielectric” (identified by attorney docket number 17-1534); and “Plasma-Distributing Structure in an Afterburner of a Jet Engine” (identified by attorney docket number 17-1535).