US20170276346A1 - Apparatus and method for electrically stabilized combustion - Google Patents

Apparatus and method for electrically stabilized combustion Download PDF

Info

Publication number
US20170276346A1
US20170276346A1 US15/617,836 US201715617836A US2017276346A1 US 20170276346 A1 US20170276346 A1 US 20170276346A1 US 201715617836 A US201715617836 A US 201715617836A US 2017276346 A1 US2017276346 A1 US 2017276346A1
Authority
US
United States
Prior art keywords
fuel
oxidant
flame holder
combustion reaction
flue gas
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US15/617,836
Inventor
Joseph Colannino
Robert E. Breidenthal
Igor A. Krichtafovitch
Christopher A. Wiklof
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Clearsign Technologies Corp
Original Assignee
Clearsign Combustion Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Clearsign Combustion Corp filed Critical Clearsign Combustion Corp
Priority to US15/617,836 priority Critical patent/US20170276346A1/en
Assigned to CLEARSIGN COMBUSTION CORPORATION reassignment CLEARSIGN COMBUSTION CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: COLANNINO, JOSEPH, KRICHTAFOVITCH, IGOR A., BREIDENTHAL, ROBERT E., WIKLOF, CHRISTOPHER A.
Publication of US20170276346A1 publication Critical patent/US20170276346A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/68Treating the combustion air or gas, e.g. by filtering, or moistening
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C9/00Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C99/00Subject-matter not provided for in other groups of this subclass
    • F23C99/001Applying electric means or magnetism to combustion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/20Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • F23D14/24Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other at least one of the fluids being submitted to a swirling motion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/62Mixing devices; Mixing tubes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/70Baffles or like flow-disturbing devices

Definitions

  • an electrically stabilized burner includes a conductive flame holder configured for mounting proximate a fuel jet and a charger disposed to cooperate with the conductive flame holder to cause a combustion reaction to be stabilized adjacent to the flame holder.
  • a mixer is configured to mix fuel and oxidant, air, and/or flue gas above the conductive flame holder.
  • the mixer is configured to mix the fuel and oxidant, air, and/or flue gas at a rate selected to maximize a rate of combustion reaction while avoiding quenching the combustion reaction.
  • the charger can be a corona electrode or another ion source disposed to output electrical charges to the fuel, to an entrainment volume adjacent to the fuel stream and below the conductive flame holder, or to the oxidant, air, and/or flue gas subsequently mixed with the fuel or diluted fuel. Additionally or alternatively, the charger can be a charge electrode in electrical continuity with a conductive portion of the combustion reaction (e.g., in electrical continuity with a flame sheath).
  • a method for operating an electrically stabilized burner includes supporting a conductive flame holder proximate to a fuel jet at a distance along the fuel jet corresponding to a selected fuel dilution, applying a voltage or charge to a combustion reaction supported by the fuel jet, and stabilizing the combustion reaction proximate to the conductive flame holder responsive to at least an intermittent voltage difference between the combustion reaction and the conductive flame holder.
  • the fuel is further mixed with oxidant, air, and/or flue gas above the conductive flame holder.
  • FIG. 1 is a side-sectional diagram of an electrically stabilized burner, according to an embodiment.
  • FIG. 2A is a plan view of a portion of the electrically stabilized burner of FIG. 1 with a block diagram of a mixer controller, according to an embodiment.
  • FIG. 2B is a side view of a portion of the electrically stabilized burner corresponding to FIG. 2A , according to an embodiment.
  • FIG. 3 is a perspective view of at least a portion of an electrically stabilized burner, according to an embodiment.
  • FIG. 4 is a simplified perspective view of an electrically stabilized burner, according to another embodiment.
  • FIG. 5 is a simplified perspective view of an electrically stabilized burner, according to another embodiment.
  • FIG. 6 is a simplified perspective view of an electrically stabilized burner, according to another embodiment.
  • FIG. 7 is a flowchart showing a method for operating an electrically stabilized burner, according to an embodiment.
  • FIG. 1 is a side-sectional diagram of an electrically stabilized burner 101 , according to an embodiment.
  • a conductive flame holder 102 is configured for mounting proximate a fuel jet 112 .
  • a charger 106 e.g., an electrode that is configured to apply an electrical charge
  • a mixer 110 is configured to mix fuel from the fuel jet 112 with oxidant, air, and/or flue gas above the conductive flame holder 102 .
  • the mixer 110 can include of one or more fluid passages 103 .
  • the mixer 110 is configured to cause a high mixing rate (or minimize a mixing time) of the fuel with oxidant, air, and/or flue gas without quenching the combustion reaction 108 .
  • the fuel jet 112 diverges at a substantially constant angle ⁇ from a fuel nozzle 116 .
  • the angle of divergence ⁇ of the fuel jet 112 is estimated to be a 7.5-degree angle of divergence from an axis of fuel transport. Alternatively, the angle of divergence can be referred to as a 15-degree solid angle (2 ⁇ ).
  • the fuel diverges from a point upstream from an aperture forming the fuel nozzle outlet such that the aperture coincides with the edges of the fuel jet at the point where the fuel stream exits the fuel nozzle 116 .
  • the expansion in fuel jet area corresponds to dilution of the fuel by entrainment of a surrounding fluid 114 .
  • the surrounding fluid 114 can include air and/or recycled flue gas. If the surrounding fluid 114 is air; for example, the entrained fluid can include about 21% A oxygen, about 78% nitrogen and small amounts of other gases. If the surrounding fluid 114 includes a flue gas recycle; for example, the entrained fluid can include about 2% to about 5% oxygen, about 78% nitrogen, and various combustion products such as carbon dioxide, water vapor and other species found in the recycled flue gas. Recycling flue gas 114 for entrainment with the fuel jet 112 therefore can result in a lower concentration of oxygen mixed with the fuel.
  • the fuel jet 112 exiting the fuel nozzle 116 can itself include oxidant, air, flue gas, and/or another diluent.
  • the fuel jet, as it exits the fuel nozzle 116 is either pure fuel or a fuel and oxidant mixture that is above the rich flammability limit of the fuel, such that a spark introduced at the fuel nozzle exit will not cause flashback into the fuel nozzle 116 .
  • Reduced oxides of nitrogen (NOx) are output from a combustion reaction 108 supported by the electrically stabilized burner 101 compared to a combustion reaction that is not partially premixed by entrainment in a region 120 between the fuel nozzle 116 and the conductive flame holder 102 .
  • the electrical stabilization provided by the burner 101 allows a more stable and reliable combustion reaction, less prone to blow-out at lean operating conditions than a burner 101 that is not electrically stabilized.
  • a combustion reaction 108 burned near a lean flammability limit has a lower temperature than a combustion reaction 108 burned richer, and outputs less NOx than a combustion reaction 108 burned richer. Moreover, a well-mixed combustion reaction 108 tends to output less NOx than a poorly-mixed combustion reaction 108 .
  • the burner 101 provides both enhanced mixing (for reduced “prompt NOx”) and leaner combustion (for reduced Zeldovich-mechanism (aka “thermal”) NOx). Moreover, a high mixing rate provided by the mixer 110 minimizes high temperature residence time, which reduces NOx output.
  • a support structure 118 supports the conductive flame holder 102 at a selected distance 120 along the fuel jet 112 .
  • the distance 120 along the fuel jet 112 at which the conductive flame holder 102 is supported can be selected to correspond to be at a desired fuel dilution.
  • the distance 120 can be selected to provide the fuel jet 112 to the conductive flame holder 102 at or slightly richer than a lean flammability limit of the fuel under the operating conditions.
  • the mixer 110 introduces additional dilution (for example, in embodiments corresponding to FIGS.
  • the distance 120 can be selected such that dilution by entrained air or flue gas 114 plus dilution by the mixer 110 provides a fuel mixture at or slightly richer than a lean flammability limit of the fuel under the operating conditions.
  • the mixer 110 is configured to mix the fuel with oxidant, air, or flue gas at a mixing rate corresponding to a selected DamkOhler number.
  • DamkOhler number (Da) is a dimensionless ratio of a mixing time to a chemical ignition delay time.
  • Da less than 1
  • the mixing time is shorter than chemical ignition delay time, and the combustion reaction is quenched by the cool reactants. This is because mixing occurs faster than the combustion reaction can release heat.
  • mixing time is greater than chemical ignition delay time.
  • the combustion reaction releases heat faster than (relatively cool) reactants are combined. Large Da combustion reactions are subject to detonation.
  • mixing at large Da is relatively inefficient, which causes combustion over a relatively large range of fuel dilutions and a relatively large range of fuel to oxidant ratios.
  • a large range of fuel to oxidant ratios generally causes the combustion reaction to also exhibit a large range of combustion temperatures (with a correspondingly wide Boltzmann distribution).
  • a large range of combustion temperatures is associated with high carbon monoxide and high NOx output, both of which are undesirable.
  • Da can alternatively be expressed as a ratio of the reaction rate to the convective mass transport rate, and is expressed in the equation
  • k c is a reaction rate constant
  • C 0 is an initial concentration
  • n is the reaction order
  • r is a mean residence time
  • the selected DamkOhler number can be equal to or greater than 1 without causing the combustion reaction 108 to be quenched.
  • the mixer 110 is operable to cause the selected DamkOhler number to be between 1.1 and 1.7.
  • the mixer 110 is operable to cause the selected DamkOhler number to be about 1.3. Running the mixer 110 at a Da greater than 1 can provide operating margin with respect to transient effects that could cause quenching of the combustion reaction 108 .
  • the conductive flame holder 102 is shaped to define an aperture 104 configured to be supported peripherally and adjacent to the fuel jet 112 .
  • the mixer 110 can be operated to produce a DamkOhler number selected to form a compact combustion reaction 108 disposed near the aperture 104 .
  • the DamkOhler number can be selected to form a compact combustion reaction disposed within the aperture 104 .
  • the charger 106 and the conductive flame holder 102 are configured to cooperate to maintain a current flow channel therebetween in the combustion reaction 108 .
  • the current flow channel stabilizes and holds the combustion reaction 108 adjacent to the conductive flame holder 102 .
  • a power supply 122 is operatively coupled to the charger 106 and configured to cause the charger 106 to apply current to the combustion reaction 108 .
  • the power supply 122 can be configured to cause the charger 106 to apply a time-varying current to the combustion reaction 108 .
  • a time-varying current corresponds to a time-varying charge concentration in the combustion reaction 108 , which may be measured as a corresponding electrical potential.
  • the time-varying charge can include a sign-varying charge.
  • the time-varying charge can include a periodic charge waveform having a frequency from about 50 to about 10,000 Hertz. In another embodiment, the time-varying charge can include a periodic charge waveform having a frequency from about 200 to about 800 Hertz.
  • the time-varying charge can include, for example, a square waveform, sine waveform, triangular waveform, truncated triangular waveform, sawtooth waveform, logarithmic waveform, exponential waveform or other arbitrary shape.
  • waveforms with sharp edges e.g., square, triangular, or sawtooth waveforms
  • the charger 106 includes a charge electrode 106 configured to be disposed proximate to the combustion reaction 108 .
  • the power supply 122 is configured to apply a voltage to the charge electrode 106 .
  • the power supply 122 can be configured to apply a substantially constant voltage or a time-varying voltage, to the charge electrode 106 .
  • the time-varying voltage can include a sign-varying voltage.
  • the time-varying voltage can include a periodic voltage waveform having a frequency of about 50 to about 10,000 Hertz.
  • the periodic voltage waveform can have a frequency of about 200 to about 800 Hertz.
  • the time-varying voltage can include a square waveform, sine waveform, triangular waveform, truncated triangular waveform, sawtooth waveform, logarithmic waveform, or exponential waveform.
  • the time-varying voltage applied to the charge electrode 106 includes a waveform having an amplitude of about ⁇ 1,000 volts to about ⁇ 115,000 volts.
  • the time-varying voltage includes a waveform having an amplitude of about ⁇ 8,000 volts to about ⁇ 40,000 volts.
  • the power supply 122 also is operatively coupled to the conductive flame holder 102 .
  • the power supply 122 is configured to apply a different voltage to the conductive flame holder 102 than to a charger (e.g., charge electrode 106 ).
  • the conductive flame holder 102 can be held at ground potential.
  • the conductive flame holder 102 can be galvanically isolated from voltages other than voltages corresponding to charges received from the combustion reaction 108 .
  • the power supply 122 can be additionally or alternatively operatively coupled to the fuel nozzle 116 .
  • the fuel nozzle 116 is generally held at ground potential.
  • the fuel nozzle 116 can be galvanically isolated from voltages other than voltages corresponding to charges received from the charger 106 through the combustion reaction 108 .
  • the fuel nozzle 116 is held in electrical continuity with the conductive flame holder 102 .
  • the power supply 122 is configured to apply to the conductive flame holder 102 and/or the fuel nozzle 116 one or more voltages opposite in polarity from charges applied to the combustion reaction 108 by the charger 106 .
  • Driving the conductive flame holder 102 to a voltage opposite in polarity to the charges applied to the combustion reaction 108 can provide greater flame attraction to the conductive flame holder 102 , and hence greater flame stability compared to holding the conductive flame holder 102 at ground potential.
  • Voltages applied by the power supply 122 can be selected dynamically, for example with larger voltages (and in particular, a larger voltage difference between the charger 106 and the conductive flame holder 102 ) being applied at higher fuel flow rates.
  • the power supply 122 is configured to drive the charger 106 to maintain a capacitance-coupled voltage relationship between the charger 106 and the conductive flame holder 102 .
  • the electrically stabilized burner 101 can include an electrical insulator 124 disposed between the conductive flame holder 102 and the charger 106 .
  • the mixer 110 can be formed integrally with the electrical insulator 124 .
  • FIG. 2A is a plan view 201 of a portion of the electrically stabilized burner 101 of FIG. 1 , according to an embodiment.
  • FIG. 2B is a side view of a portion of the electrically stabilized burner corresponding to FIG. 2A , according to an embodiment.
  • the mixer 110 further includes one or more fluid passages 103 entering aperture 104 tangentially so as to be configured to impart rotational velocity to impart a stream-wise vortex 202 onto the combustion reaction 108 .
  • the one or more fluid passages 103 can be arranged to drive the combustion reaction 108 in the stream-wise vortex 202 .
  • a fluid manifold 204 is configured to supply the mixing fluid to the one or more fluid passages 103 .
  • the rate of mixing is controlled according to a fluid flow rate through the fluid manifold 204 responsive to a flow control valve 206 .
  • a mixer controller 210 is configured to operate the control valve 206 to control the flow of fluid and the rate of mixing.
  • the fluid includes oxidant (e.g., included in any or all of oxygen, air, and flue gas), and/or fuel.
  • Fluid jets projected by the one or more fluid passages 103 can optionally be configured to act as a pilot flame if the main fuel jet 112 is reduced or stopped.
  • FIG. 3 is a perspective view of a portion of an electrically stabilized burner 301 , according to an embodiment.
  • the electrically stabilized burner 301 includes a support structure 118 configured to hold the conductive flame holder 102 at a selected distance from a fuel nozzle 116 . As described, the distance can be selected to correspond to a desired fuel and oxidant, air, and/or flue gas mixture.
  • An electrical insulator 124 can be disposed between the conductive flame holder 102 and a charger 106 .
  • the mixer 110 includes one or more fluid passages 103 formed into or through the electrical insulator 124 so as to output a mixing fluid substantially tangentially to the periphery of the aperture 104 defined by the electrical insulator 124 .
  • the conductive flame holder 102 , the fuel nozzle 116 , and the support structure 118 are configured as an integrated unit.
  • Fittings 306 are formed to accept coupling to a fluid manifold ( 204 shown schematically in FIG. 2 ).
  • An electrical lug 304 in electrical continuity with the charger 106 is configured for operative coupling to a lead (not shown) from a power supply 122 .
  • Some or all of the fuel nozzle 116 , support structure 118 , conductive flame holder 102 , electrical insulator 124 , fluid passages 103 , charger 106 , and electrical lug 304 can be formed as an integrated unit.
  • FIGS. 1, 2A, 2B, and 3 show mixers formed as vortex-generating jet nozzles.
  • oxidant, air, flue gas, or fuel alone or in combination, can be passed through the one or more fluid passages 103 .
  • the mixer 110 can include a plurality of electrodes configured to impart rotational force on charged particles carried by the combustion reaction 108 . The resulting movement of the charged particles can, in turn, convey momentum to uncharged particles in the combustion reaction 108 .
  • FIG. 4 is a simplified perspective view of an electrically stabilized burner 401 , according to another embodiment.
  • a mixer 410 includes a plurality of field electrodes 402 operatively coupled to one or more power supplies 122 and disposed between the charger 106 and the conductive flame holder 102 .
  • the plurality of field electrodes 402 can be carried by an electrical insulator 124 or can alternatively be supported within an air gap between the charger 106 and the conductive flame holder 102 .
  • the actual number of field electrodes used can be fewer or greater than three.
  • a mixer controller (not shown) is operatively coupled to the one or more power supplies 122 .
  • the mixer controller is configured to cause the one or more power supplies 122 to sequentially apply driving voltages to the field electrodes 402 .
  • the mixer controller is configured to drive the field electrodes 402 in a manner selected to cause the field electrodes 402 to mix fuel with oxidant, air, and/or flue gas at a selected rate of mixing.
  • the mixer controller can be configured to drive the field electrodes 402 in a sequence selected to cause the field electrodes 402 to sequentially attract and repel charged particles corresponding to a majority polarity of charged particles carried by combustion reaction 108 (the majority polarity of charged particles being supplied by the charger 106 ).
  • the sequential driving of the charged particles causes circulation of the charged particles and a corresponding stream-wise vortex in the aperture defined by the conductive flame holder 102 , field electrodes 402 , electrical insulator 124 , and/or the charger 106 .
  • the resultant circulation of the combustion reaction 108 causes mixing of the fuel with oxidant, air, and/or flue gas at the selected rate.
  • the voltage applied to the charger 106 by the power supply 122 can be substantially constant.
  • the voltage applied to the charger 106 by the power supply 122 can be time varying.
  • the time varying voltage can include a periodically varying sign voltage, such as an AC voltage.
  • the sequential voltages applied to the field electrodes 402 are also be modified or be made intermittent such that the rotational direction of majority charges in the combustion reaction 108 (not shown) is maintained when the polarity of the majority charge inverts.
  • the electrical insulator 124 and the field electrodes 402 can form an integrated unit or a portion of an integrated unit 401 . Some or all of the fuel nozzle 116 , support structure 118 , conductive flame holder 102 , electrical insulator 124 ), field electrodes 402 , charger 106 , and/or electrical lug(s) (not shown) can be formed as an integrated unit 401 .
  • FIG. 5 is a simplified perspective view of an electrically stabilized burner 501 , according to another embodiment. Compared to the embodiment 401 of FIG. 4 , in the embodiment 501 , the relative locations of the field electrodes 402 and the charger 106 are reversed.
  • a mixer 510 includes a plurality of field electrodes 402 operatively coupled to at least one power supply 122 .
  • the charger 106 is disposed between the field electrodes 402 and the conductive flame holder 102 . For purposes of illustration, only three field electrodes 402 are shown but more or fewer field electrodes 402 are possible.
  • the mixer controller (not shown) is operatively coupled to at least one power supply 122 and configured to cause the power supply(ies) 122 to apply driving voltages to the field electrodes 402 .
  • the mixer controller 210 is configured to cause the power supply(ies) to drive the field electrodes 402 in a manner selected to cause the field electrodes 402 to mix fuel with oxidant, air, and/or flue gas at a selected rate of mixing.
  • the power supply(ies) 122 can drive the field electrodes 402 in a sequence selected to cause the field electrodes 402 to sequentially attract and repel charged particles corresponding to a majority polarity of charged particles carried by combustion reaction 108 .
  • the sequential driving of the charged particles can cause circulation of the charged particles and a corresponding stream-wise vortex in an aperture defined by the conductive flame holder 102 , field electrodes 402 , electrical insulator 124 , and/or the charger 106 .
  • the resultant circulation of the combustion reaction 108 causes mixing of the fuel with oxidant, air, and/or flue gas at the selected rate.
  • the voltage applied to the charger 106 by the first power supply 122 can be substantially constant.
  • the voltage applied to the charger 106 by the power supply 122 can be time varying.
  • the time varying voltage can include a periodically varying sign voltage, such as an AC voltage.
  • the sequential voltages applied to the field electrodes 402 are also be modified or be made intermittent such that the rotational direction of the combustion reaction 108 is maintained when the majority charge polarity is inverted.
  • the field electrodes 402 can be at least partially carried by a second electrical insulator (not shown).
  • the second electrical insulator and the field electrodes 402 can form an integrated unit or a portion of an integrated unit 401 .
  • Some or all of the fuel nozzle 116 , support structure 118 , conductive flame holder 102 , first and second electrical insulator(s), field electrodes 402 , and/or charger 106 can be formed as an integrated unit 501 .
  • FIG. 6 is a simplified perspective view of an electrically stabilized burner 601 , according to another embodiment. Compared to the embodiments 401 and 501 shown in FIG. 4 and FIG. 5 respectively, in the embodiment illustrated by 601 , a separate charger 106 is omitted. The function of the charger 106 is performed by an integrated field and charge electrodes 602 .
  • the mixer 610 includes a plurality of field and charge electrodes 602 operatively coupled to a power supply 122 . For purposes of illustration, three field and charge electrodes 602 are shown but the actual number of field and charge electrodes 602 can be different.
  • a mixer controller (not shown) is operatively coupled to one or more power supplies 122 configured to apply driving voltages to the field and charge electrodes 602 .
  • the mixer controller 210 is configured to cause the power supply(ies) 122 to apply a bias voltage to the field and charge electrodes 602 superimposed over electrode sequence voltages similar to those described in embodiments illustrated in FIGS. 4 and 5 .
  • the electrode sequence voltages sequentially attract and repel charged particles corresponding to a majority polarity of charged particles carried by combustion reaction 108 .
  • the bias voltage causes the combustion reaction to carry the majority polarity.
  • the concentration of charges carried by the combustion reaction (which may be measured as a voltage) is proportional to the bias voltage.
  • the bias voltage can be substantially constant.
  • the bias voltage can be time varying.
  • the time varying voltage can include a periodically varying sign voltage, such as an AC voltage.
  • the sequential voltages (superimposed over the bias voltage) applied to the field and charge electrodes 602 can also be modified or be made intermittent such that the rotational direction of the combustion reaction is maintained.
  • the mixer controller is configured to cause the power supply(ies) 122 to drive the field and charge electrodes 602 in a manner selected to cause the field and charge electrodes 602 to mix the fuel with the oxidant, air, and/or flue gas at a selected rate of mixing.
  • the sequential driving of the charged particles can cause circulation of the charged particles and a corresponding stream-wise vortex 202 in an aperture 104 defined by the conductive flame holder 102 , field and charge electrodes 602 and/or electrical insulator (not shown).
  • the resultant circulation of combustion reaction causes mixing of the fuel with oxidant, air, and/or flue gas at the selected rate.
  • the field and charge electrodes 602 can be at least partially carried by an electrical insulator (not shown).
  • the electrical insulator and the field and charge electrodes 602 can form an integrated unit or a portion of an integrated unit 601 .
  • Some or all of a fuel nozzle 116 , support structure 118 , conductive flame holder 102 , one or more electrical insulator(s) (not shown), and field and charge electrodes 602 can be formed as an integrated unit 601 .
  • any of electrically stabilized burner embodiments 101 , 201 , 301 , 401 , 501 , and 601 can additionally include a second mixer (not shown) configured to mix fuel with oxidant, air, and/or flue gas below the conductive flame holder 102 .
  • a second mixer (not shown) configured to mix fuel with oxidant, air, and/or flue gas below the conductive flame holder 102 .
  • FIG. 7 is a flowchart showing a method 701 for operating an electrically stabilized burner, according to an embodiment.
  • a fuel jet is projected in step 702 .
  • a fuel jet typically diverges from a nozzle at about a 7.5° half angle (15° solid angle).
  • the divergence corresponds to the entrainment of gas or gases adjacent to the fuel jet.
  • oxidant, air, and/or flue gas can be entrained in the fuel jet.
  • the entrainment reduces the concentration of the fuel within the gas stream.
  • the resultant ratio of fuel to oxidant can be a determinate function of distance along the fuel jet.
  • Step 702 includes entraining oxidant, air, and/or flue gas, in the fuel jet.
  • Step 704 includes supporting a conductive flame holder proximate to a fuel jet at a distance along the fuel jet from the fuel nozzle corresponding to a selected fuel dilution.
  • the selected fuel dilution can correspond substantially to a lean flammability limit of the fuel.
  • supporting a conductive flame holder proximate to a fuel jet at a distance along the fuel jet corresponding to a selected fuel dilution can include supporting the conductive flame holder at a distance such that the dilution in the fuel caused by entrainment (and corresponding to fuel jet expansion) between the fuel nozzle and the conductive flame holder plus the dilution of the fuel caused by subsequent mixing results in a selected fuel dilution near the lean flammability limit of the fuel.
  • the method 701 can include the step (not shown) of selecting a fuel dilution.
  • a furnace or boiler using the burner can be operated at a relatively rich fuel mixture.
  • a richer fuel mixture is generally more stable when a combustion chamber is cool.
  • the fuel dilution can be increased such that the fuel is burned near its lean flammability limit.
  • operating a burner near the lean flammability limit of the fuel is generally associated with a cooler combustion reaction, and a cooler combustion reaction is generally associated with reduced NOx output.
  • the method 701 can further include (not shown) adjusting the distance along the fuel jet at which the conductive flame holder is supported, wherein the distance corresponds to the selected fuel dilution.
  • the burner described herein can be operated primarily when the furnace or boiler is cool. Later, after the combustion chamber is warmed-up, the combustion reaction can lift from the conductive flame holder to be held at a larger distance from the fuel nozzle by an aerodynamic flame holder (e.g., a bluff body). The combustion reaction can be lifted by removing application of the voltage or charge applied in step 706 , or responsive to higher temperatures that cause the conductive flame holder to be less effective at holding the combustion reaction (at a given applied voltage).
  • an aerodynamic flame holder e.g., a bluff body
  • a voltage or charge is applied to a combustion reaction supported by the fuel jet.
  • a charger can be disposed near the combustion reaction and raised to a potential to inject a charge into the combustion reaction.
  • applying a voltage or charge to the combustion reaction includes applying a voltage to the charger.
  • Applying a voltage or charge to the combustion reaction can include the application of a constant voltage to the charger, and hence a substantially constant current to the combustion reaction.
  • a high voltage high voltage is defined as equal to or greater than ⁇ 1000 volts
  • positive voltage was found to be somewhat more effective at holding the flame compared to an equal magnitude negative voltage.
  • +15,000 volts was applied to a charger formed as a charge electrode in electrical contact with a conductive flame, and the conductive flame holder (described in step 708 below) was held at ground potential.
  • the conductive flame holder can be held at a voltage opposite in polarity to the applied charge polarity.
  • the inventors contemplate a wide range of effective voltages. For example, voltages of ⁇ 1000 volts to about ⁇ 115,000 volts can be applied to the charger. More particularly, ⁇ 8000 volts to about ⁇ 40,000 volts can be applied to the charger. At +15,000 volts, current is typically in the range of hundreds of microamps up to hundreds of milliamps. A power supply capable of delivering a maximum power of about 15 Watts to 1500 Watts is generally appropriate, depending on operating conditions. Lower power is required at cooler furnace temperatures and at fuel flow rates corresponding to about 150,000 BTU/hour output.
  • applying a voltage or charge to the combustion reaction in step 706 can include applying a time-varying voltage or charge to the combustion reaction.
  • a time-varying voltage can be applied to a charger.
  • the time-varying voltage can include a periodic voltage waveform having a frequency of about 50 to about 10,000 Hertz.
  • the time-varying voltage can include a periodic voltage waveform having a frequency of about 200 to about 800 Hertz.
  • Applying the time-varying voltage can include applying a square waveform, sine waveform, triangular waveform, truncated triangular waveform, sawtooth waveform, logarithmic waveform, and/or exponential waveform to the charger.
  • the waveform can also have an amplitude of about ⁇ 1000 volts to about ⁇ 115,000 volts.
  • the waveform can have an amplitude of about ⁇ 8000 volts to about ⁇ 40,000 volts.
  • Step 706 includes holding the conductive flame holder at a voltage different than the voltage or charge applied to the combustion reaction.
  • Applying a voltage or charge to the combustion reaction can includes applying a time-varying voltage or charge to the combustion reaction and applying a second time-varying voltage to the conductive flame holder, the second time-varying voltage being instantaneously opposite in polarity from the time-varying voltage or charge applied to the combustion reaction.
  • the conductive flame holder can be held substantially at a ground potential, or can be galvanically isolated from ground and from voltages other than the voltage applied to the charger.
  • Step 708 includes stabilizing a combustion reaction supported by the fuel jet proximate to the conductive flame holder.
  • the stabilization can be responsive to at least an intermittent voltage difference between the combustion reaction and the conductive flame holder.
  • step 708 can include exciting at least an intermittent plasma state in the fuel jet responsive to the at least intermittent voltage difference between the combustion reaction and the conductive flame holder.
  • the plasma state can maintain fuel ignition in some embodiments.
  • Step 710 includes mixing the fuel with oxidant (e.g. oxygen), air, and/or flue gas above the conductive flame holder.
  • oxidant e.g. oxygen
  • the fuel and oxidant, air, and/or flue gas can be mixed to maintain a selected DamkOhler number at a location corresponding to the combustion reaction.
  • the selected DamkOhler number can be greater than or equal to 1.
  • the selected DamkOhler number can be in the range from about 1.1 to about 1.7.
  • mixing the oxidant, air, and/or flue gas and the fuel includes imparting rotational inertia on the combustion reaction.
  • the rotational inertia can be imparted by injecting one or more jets of gas that include oxidant, air, and/or flue gas into the fuel jet and entrained gas proceeding from the fuel nozzle and into the mixer aperture.
  • mixing the fuel with oxidant, air, and/or flue gas can include applying a rotating electric field to the combustion reaction or the fuel jet above the conductive flame holder. Applying the rotating electric field can include applying a sequential waveform to a plurality of field electrodes.
  • Step 710 further includes mixing the fuel with oxidant, air, and/or flue gas above the conductive flame holder and below a location where the voltage or charge is applied to the combustion reaction (e.g., see FIG. 4 ).
  • mixing the fuel with oxidant, air, and/or flue gas above the conductive flame holder can include mixing the fuel with oxidant, air, and/or flue gas above a location where the voltage or charge is applied to the combustion reaction or can include mixing the fuel with oxidant, air, and/or flue gas at a location substantially coincident with a location where the voltage or charge is applied to the combustion reaction (e.g., see FIGS. 5, 6 ).
  • the fuel can also be mixed with oxidant, air, and/or flue gas below the conductive flame holder.
  • Steps 706 and 710 can be combined, optionally, such as with an embodiment 601 (see FIG. 6 ). Applying the voltage or charge to the combustion reaction and mixing the combustion reaction can be performed by at least an overlapping set of field electrodes.
  • the mixing of fuel with oxidant of step 710 can include applying an electric field to the combustion reaction or to the fuel stream above the conductive flame holder. The electric field can be applied with a charger.
  • heat from the combustion reaction is output.
  • the heat can be output to heat a process material, to heat process equipment, to heat air and/or water, to generate electricity, to generate rotational energy, and/or to generate thrust.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)

Abstract

An electrically stabilized burner is configured to support a combustion reaction such as a combustion reaction substantially at a selected fuel dilution and with a mixing rate selected to maximize the reaction rate without quenching the combustion reaction.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • The present application is a U.S. Divisional application of co-pending U.S. patent application Ser. No. 13/950,249, entitled “ELECTRICALLY STABILIZED BURNER,” filed Jul. 24, 2013 (docket number 2651-070-03); which application claims priority benefit from U.S. Provisional Patent Application No. 61/675,079, entitled “ELECTRICALLY STABILIZED BURNER AND MIXER,” filed Jul. 24, 2012 (docket number 2651-070-02); each of which, to the extent not inconsistent with the disclosure herein, is incorporated herein by reference.
  • SUMMARY
  • According to an embodiment, an electrically stabilized burner includes a conductive flame holder configured for mounting proximate a fuel jet and a charger disposed to cooperate with the conductive flame holder to cause a combustion reaction to be stabilized adjacent to the flame holder. A mixer is configured to mix fuel and oxidant, air, and/or flue gas above the conductive flame holder. The mixer is configured to mix the fuel and oxidant, air, and/or flue gas at a rate selected to maximize a rate of combustion reaction while avoiding quenching the combustion reaction. The charger can be a corona electrode or another ion source disposed to output electrical charges to the fuel, to an entrainment volume adjacent to the fuel stream and below the conductive flame holder, or to the oxidant, air, and/or flue gas subsequently mixed with the fuel or diluted fuel. Additionally or alternatively, the charger can be a charge electrode in electrical continuity with a conductive portion of the combustion reaction (e.g., in electrical continuity with a flame sheath).
  • According to an embodiment, a method for operating an electrically stabilized burner includes supporting a conductive flame holder proximate to a fuel jet at a distance along the fuel jet corresponding to a selected fuel dilution, applying a voltage or charge to a combustion reaction supported by the fuel jet, and stabilizing the combustion reaction proximate to the conductive flame holder responsive to at least an intermittent voltage difference between the combustion reaction and the conductive flame holder. The fuel is further mixed with oxidant, air, and/or flue gas above the conductive flame holder.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a side-sectional diagram of an electrically stabilized burner, according to an embodiment.
  • FIG. 2A is a plan view of a portion of the electrically stabilized burner of FIG. 1 with a block diagram of a mixer controller, according to an embodiment.
  • FIG. 2B is a side view of a portion of the electrically stabilized burner corresponding to FIG. 2A, according to an embodiment.
  • FIG. 3 is a perspective view of at least a portion of an electrically stabilized burner, according to an embodiment.
  • FIG. 4 is a simplified perspective view of an electrically stabilized burner, according to another embodiment.
  • FIG. 5 is a simplified perspective view of an electrically stabilized burner, according to another embodiment.
  • FIG. 6 is a simplified perspective view of an electrically stabilized burner, according to another embodiment.
  • FIG. 7 is a flowchart showing a method for operating an electrically stabilized burner, according to an embodiment.
  • DETAILED DESCRIPTION
  • In the following detailed description, reference is made to the accompanying drawings, which form a part hereof. In the drawings, similar symbols typically identify similar components, unless context dictates otherwise. Other embodiments may be used and/or other changes may be made without departing from the spirit or scope of the disclosure.
  • FIG. 1 is a side-sectional diagram of an electrically stabilized burner 101, according to an embodiment. A conductive flame holder 102 is configured for mounting proximate a fuel jet 112. A charger 106 (e.g., an electrode that is configured to apply an electrical charge) is disposed to cooperate with the conductive flame holder 102 to cause a combustion reaction 108 to be stabilized adjacent to the conductive flame holder 102. A mixer 110 is configured to mix fuel from the fuel jet 112 with oxidant, air, and/or flue gas above the conductive flame holder 102. For example, the mixer 110 can include of one or more fluid passages 103. The mixer 110 is configured to cause a high mixing rate (or minimize a mixing time) of the fuel with oxidant, air, and/or flue gas without quenching the combustion reaction 108.
  • The fuel jet 112 diverges at a substantially constant angle θ from a fuel nozzle 116. The angle of divergence θ of the fuel jet 112 is estimated to be a 7.5-degree angle of divergence from an axis of fuel transport. Alternatively, the angle of divergence can be referred to as a 15-degree solid angle (2θ). The fuel diverges from a point upstream from an aperture forming the fuel nozzle outlet such that the aperture coincides with the edges of the fuel jet at the point where the fuel stream exits the fuel nozzle 116.
  • The expansion in fuel jet area corresponds to dilution of the fuel by entrainment of a surrounding fluid 114. For example, the surrounding fluid 114 can include air and/or recycled flue gas. If the surrounding fluid 114 is air; for example, the entrained fluid can include about 21% A oxygen, about 78% nitrogen and small amounts of other gases. If the surrounding fluid 114 includes a flue gas recycle; for example, the entrained fluid can include about 2% to about 5% oxygen, about 78% nitrogen, and various combustion products such as carbon dioxide, water vapor and other species found in the recycled flue gas. Recycling flue gas 114 for entrainment with the fuel jet 112 therefore can result in a lower concentration of oxygen mixed with the fuel.
  • It will be understood that the fuel jet 112 exiting the fuel nozzle 116 can itself include oxidant, air, flue gas, and/or another diluent. In embodiments, the fuel jet, as it exits the fuel nozzle 116, is either pure fuel or a fuel and oxidant mixture that is above the rich flammability limit of the fuel, such that a spark introduced at the fuel nozzle exit will not cause flashback into the fuel nozzle 116.
  • Reduced oxides of nitrogen (NOx) are output from a combustion reaction 108 supported by the electrically stabilized burner 101 compared to a combustion reaction that is not partially premixed by entrainment in a region 120 between the fuel nozzle 116 and the conductive flame holder 102. The electrical stabilization provided by the burner 101 allows a more stable and reliable combustion reaction, less prone to blow-out at lean operating conditions than a burner 101 that is not electrically stabilized.
  • A combustion reaction 108 burned near a lean flammability limit has a lower temperature than a combustion reaction 108 burned richer, and outputs less NOx than a combustion reaction 108 burned richer. Moreover, a well-mixed combustion reaction 108 tends to output less NOx than a poorly-mixed combustion reaction 108. The burner 101 provides both enhanced mixing (for reduced “prompt NOx”) and leaner combustion (for reduced Zeldovich-mechanism (aka “thermal”) NOx). Moreover, a high mixing rate provided by the mixer 110 minimizes high temperature residence time, which reduces NOx output.
  • A support structure 118 supports the conductive flame holder 102 at a selected distance 120 along the fuel jet 112. The distance 120 along the fuel jet 112 at which the conductive flame holder 102 is supported can be selected to correspond to be at a desired fuel dilution. For example, for a mixer 110 that does not introduce additional air or flue gas (for example, in embodiments corresponding to FIGS. 4-6), the distance 120 can be selected to provide the fuel jet 112 to the conductive flame holder 102 at or slightly richer than a lean flammability limit of the fuel under the operating conditions. Alternatively, for embodiments where the mixer 110 introduces additional dilution (for example, in embodiments corresponding to FIGS. 1, 2A, 2B, and/or 3), the distance 120 can be selected such that dilution by entrained air or flue gas 114 plus dilution by the mixer 110 provides a fuel mixture at or slightly richer than a lean flammability limit of the fuel under the operating conditions.
  • In an embodiment, the mixer 110 is configured to mix the fuel with oxidant, air, or flue gas at a mixing rate corresponding to a selected DamkOhler number. DamkOhler number (Da) is a dimensionless ratio of a mixing time to a chemical ignition delay time. At small Da (less than 1), the mixing time is shorter than chemical ignition delay time, and the combustion reaction is quenched by the cool reactants. This is because mixing occurs faster than the combustion reaction can release heat. At large Da (>>1) mixing time is greater than chemical ignition delay time. At large Da, the combustion reaction releases heat faster than (relatively cool) reactants are combined. Large Da combustion reactions are subject to detonation. Moreover, mixing at large Da is relatively inefficient, which causes combustion over a relatively large range of fuel dilutions and a relatively large range of fuel to oxidant ratios. A large range of fuel to oxidant ratios generally causes the combustion reaction to also exhibit a large range of combustion temperatures (with a correspondingly wide Boltzmann distribution). A large range of combustion temperatures is associated with high carbon monoxide and high NOx output, both of which are undesirable.
  • Da can alternatively be expressed as a ratio of the reaction rate to the convective mass transport rate, and is expressed in the equation
  • Da = k c C 0 n C 0 / τ = k c C 0 ( n - 1 ) τ ;
  • where kc is a reaction rate constant, C0 is an initial concentration, n is the reaction order, and r is a mean residence time.
  • The selected DamkOhler number can be equal to or greater than 1 without causing the combustion reaction 108 to be quenched. In an embodiment, the mixer 110 is operable to cause the selected DamkOhler number to be between 1.1 and 1.7. In a particular embodiment, the mixer 110 is operable to cause the selected DamkOhler number to be about 1.3. Running the mixer 110 at a Da greater than 1 can provide operating margin with respect to transient effects that could cause quenching of the combustion reaction 108.
  • The conductive flame holder 102 is shaped to define an aperture 104 configured to be supported peripherally and adjacent to the fuel jet 112. The mixer 110 can be operated to produce a DamkOhler number selected to form a compact combustion reaction 108 disposed near the aperture 104. For example, the DamkOhler number can be selected to form a compact combustion reaction disposed within the aperture 104.
  • In an embodiment, the charger 106 and the conductive flame holder 102 are configured to cooperate to maintain a current flow channel therebetween in the combustion reaction 108. The current flow channel stabilizes and holds the combustion reaction 108 adjacent to the conductive flame holder 102.
  • In an embodiment, a power supply 122 is operatively coupled to the charger 106 and configured to cause the charger 106 to apply current to the combustion reaction 108. Alternatively, the power supply 122 can be configured to cause the charger 106 to apply a time-varying current to the combustion reaction 108. A time-varying current corresponds to a time-varying charge concentration in the combustion reaction 108, which may be measured as a corresponding electrical potential. The time-varying charge can include a sign-varying charge. The time-varying charge can include a periodic charge waveform having a frequency from about 50 to about 10,000 Hertz. In another embodiment, the time-varying charge can include a periodic charge waveform having a frequency from about 200 to about 800 Hertz. The time-varying charge can include, for example, a square waveform, sine waveform, triangular waveform, truncated triangular waveform, sawtooth waveform, logarithmic waveform, exponential waveform or other arbitrary shape. The inventors have found that waveforms with sharp edges (e.g., square, triangular, or sawtooth waveforms) tend to cause higher visibility (more easily observable) effects in combustion reactions 108.
  • In an embodiment, the charger 106 includes a charge electrode 106 configured to be disposed proximate to the combustion reaction 108. The power supply 122 is configured to apply a voltage to the charge electrode 106. The power supply 122 can be configured to apply a substantially constant voltage or a time-varying voltage, to the charge electrode 106. The time-varying voltage can include a sign-varying voltage. The time-varying voltage can include a periodic voltage waveform having a frequency of about 50 to about 10,000 Hertz. For example, the periodic voltage waveform can have a frequency of about 200 to about 800 Hertz. The time-varying voltage can include a square waveform, sine waveform, triangular waveform, truncated triangular waveform, sawtooth waveform, logarithmic waveform, or exponential waveform. The time-varying voltage applied to the charge electrode 106 includes a waveform having an amplitude of about ±1,000 volts to about ±115,000 volts. For example, the time-varying voltage includes a waveform having an amplitude of about ±8,000 volts to about ±40,000 volts.
  • The power supply 122 also is operatively coupled to the conductive flame holder 102. The power supply 122 is configured to apply a different voltage to the conductive flame holder 102 than to a charger (e.g., charge electrode 106). For example, the conductive flame holder 102 can be held at ground potential. According to an embodiment, the conductive flame holder 102 can be galvanically isolated from voltages other than voltages corresponding to charges received from the combustion reaction 108. The power supply 122 can be additionally or alternatively operatively coupled to the fuel nozzle 116. The fuel nozzle 116 is generally held at ground potential. Alternatively, the fuel nozzle 116 can be galvanically isolated from voltages other than voltages corresponding to charges received from the charger 106 through the combustion reaction 108. In embodiments, the fuel nozzle 116 is held in electrical continuity with the conductive flame holder 102.
  • Optionally, the power supply 122 is configured to apply to the conductive flame holder 102 and/or the fuel nozzle 116 one or more voltages opposite in polarity from charges applied to the combustion reaction 108 by the charger 106. Driving the conductive flame holder 102 to a voltage opposite in polarity to the charges applied to the combustion reaction 108 can provide greater flame attraction to the conductive flame holder 102, and hence greater flame stability compared to holding the conductive flame holder 102 at ground potential. Voltages applied by the power supply 122 can be selected dynamically, for example with larger voltages (and in particular, a larger voltage difference between the charger 106 and the conductive flame holder 102) being applied at higher fuel flow rates. In an embodiment, the power supply 122 is configured to drive the charger 106 to maintain a capacitance-coupled voltage relationship between the charger 106 and the conductive flame holder 102.
  • The electrically stabilized burner 101 can include an electrical insulator 124 disposed between the conductive flame holder 102 and the charger 106. The mixer 110 can be formed integrally with the electrical insulator 124.
  • FIG. 2A is a plan view 201 of a portion of the electrically stabilized burner 101 of FIG. 1, according to an embodiment. FIG. 2B is a side view of a portion of the electrically stabilized burner corresponding to FIG. 2A, according to an embodiment. The mixer 110 further includes one or more fluid passages 103 entering aperture 104 tangentially so as to be configured to impart rotational velocity to impart a stream-wise vortex 202 onto the combustion reaction 108. The one or more fluid passages 103 can be arranged to drive the combustion reaction 108 in the stream-wise vortex 202. A fluid manifold 204 is configured to supply the mixing fluid to the one or more fluid passages 103. The rate of mixing is controlled according to a fluid flow rate through the fluid manifold 204 responsive to a flow control valve 206. A mixer controller 210 is configured to operate the control valve 206 to control the flow of fluid and the rate of mixing. The fluid includes oxidant (e.g., included in any or all of oxygen, air, and flue gas), and/or fuel. Fluid jets projected by the one or more fluid passages 103 can optionally be configured to act as a pilot flame if the main fuel jet 112 is reduced or stopped.
  • FIG. 3 is a perspective view of a portion of an electrically stabilized burner 301, according to an embodiment. The electrically stabilized burner 301 includes a support structure 118 configured to hold the conductive flame holder 102 at a selected distance from a fuel nozzle 116. As described, the distance can be selected to correspond to a desired fuel and oxidant, air, and/or flue gas mixture. An electrical insulator 124 can be disposed between the conductive flame holder 102 and a charger 106. (Optionally, the charger 106 and the conductive flame holder 102 can be separated by an air gap.) In the embodiment 301, the mixer 110 includes one or more fluid passages 103 formed into or through the electrical insulator 124 so as to output a mixing fluid substantially tangentially to the periphery of the aperture 104 defined by the electrical insulator 124. The conductive flame holder 102, the fuel nozzle 116, and the support structure 118 are configured as an integrated unit. Fittings 306 are formed to accept coupling to a fluid manifold (204 shown schematically in FIG. 2). An electrical lug 304 in electrical continuity with the charger 106 is configured for operative coupling to a lead (not shown) from a power supply 122. Some or all of the fuel nozzle 116, support structure 118, conductive flame holder 102, electrical insulator 124, fluid passages 103, charger 106, and electrical lug 304 can be formed as an integrated unit.
  • Various mixer embodiments are contemplated. The embodiments of FIGS. 1, 2A, 2B, and 3 show mixers formed as vortex-generating jet nozzles. As described, oxidant, air, flue gas, or fuel, alone or in combination, can be passed through the one or more fluid passages 103. Alternatively, the mixer 110 can include a plurality of electrodes configured to impart rotational force on charged particles carried by the combustion reaction 108. The resulting movement of the charged particles can, in turn, convey momentum to uncharged particles in the combustion reaction 108.
  • FIG. 4 is a simplified perspective view of an electrically stabilized burner 401, according to another embodiment. A mixer 410 includes a plurality of field electrodes 402 operatively coupled to one or more power supplies 122 and disposed between the charger 106 and the conductive flame holder 102. The plurality of field electrodes 402 can be carried by an electrical insulator 124 or can alternatively be supported within an air gap between the charger 106 and the conductive flame holder 102. The actual number of field electrodes used can be fewer or greater than three. A mixer controller (not shown) is operatively coupled to the one or more power supplies 122. The mixer controller is configured to cause the one or more power supplies 122 to sequentially apply driving voltages to the field electrodes 402. The mixer controller is configured to drive the field electrodes 402 in a manner selected to cause the field electrodes 402 to mix fuel with oxidant, air, and/or flue gas at a selected rate of mixing. For example, the mixer controller can be configured to drive the field electrodes 402 in a sequence selected to cause the field electrodes 402 to sequentially attract and repel charged particles corresponding to a majority polarity of charged particles carried by combustion reaction 108 (the majority polarity of charged particles being supplied by the charger 106). The sequential driving of the charged particles causes circulation of the charged particles and a corresponding stream-wise vortex in the aperture defined by the conductive flame holder 102, field electrodes 402, electrical insulator 124, and/or the charger 106. The resultant circulation of the combustion reaction 108 causes mixing of the fuel with oxidant, air, and/or flue gas at the selected rate.
  • Approaches to electrical vortex generation are described in the U.S. patent application Ser. No. 12/753,047, entitled “SYSTEM AND APPARATUS FOR APPLYING AN ELECTRIC FIELD TO A COMBUSTION VOLUME”, filed Apr. 1, 2010, which is incorporated by reference in its entirety. Compared to the approaches described in U.S. patent application Ser. No. 12/753,047, disclosure herein provides vortex generation by acting on a combustion reaction that carries a majority charge. The majority charge can reduce the amount of rotational inertia that is resisted by charged particles having opposite polarity to the majority charge. For example, for a positively charged combustion reaction, a relatively higher concentration of positively charged particles can be circulated under the influence of the field electrodes 402 than the number that are available in a neutral combustion reaction.
  • The voltage applied to the charger 106 by the power supply 122 can be substantially constant. Alternatively, the voltage applied to the charger 106 by the power supply 122 can be time varying. For example, the time varying voltage can include a periodically varying sign voltage, such as an AC voltage. For an embodiment where a periodically sign-varying voltage is applied to the charger 106, the sequential voltages applied to the field electrodes 402 are also be modified or be made intermittent such that the rotational direction of majority charges in the combustion reaction 108 (not shown) is maintained when the polarity of the majority charge inverts.
  • The electrical insulator 124 and the field electrodes 402 can form an integrated unit or a portion of an integrated unit 401. Some or all of the fuel nozzle 116, support structure 118, conductive flame holder 102, electrical insulator 124), field electrodes 402, charger 106, and/or electrical lug(s) (not shown) can be formed as an integrated unit 401.
  • FIG. 5 is a simplified perspective view of an electrically stabilized burner 501, according to another embodiment. Compared to the embodiment 401 of FIG. 4, in the embodiment 501, the relative locations of the field electrodes 402 and the charger 106 are reversed. A mixer 510 includes a plurality of field electrodes 402 operatively coupled to at least one power supply 122. The charger 106 is disposed between the field electrodes 402 and the conductive flame holder 102. For purposes of illustration, only three field electrodes 402 are shown but more or fewer field electrodes 402 are possible. The mixer controller (not shown) is operatively coupled to at least one power supply 122 and configured to cause the power supply(ies) 122 to apply driving voltages to the field electrodes 402. The mixer controller 210 is configured to cause the power supply(ies) to drive the field electrodes 402 in a manner selected to cause the field electrodes 402 to mix fuel with oxidant, air, and/or flue gas at a selected rate of mixing. For example, the power supply(ies) 122 can drive the field electrodes 402 in a sequence selected to cause the field electrodes 402 to sequentially attract and repel charged particles corresponding to a majority polarity of charged particles carried by combustion reaction 108. The sequential driving of the charged particles can cause circulation of the charged particles and a corresponding stream-wise vortex in an aperture defined by the conductive flame holder 102, field electrodes 402, electrical insulator 124, and/or the charger 106. The resultant circulation of the combustion reaction 108 causes mixing of the fuel with oxidant, air, and/or flue gas at the selected rate.
  • The voltage applied to the charger 106 by the first power supply 122 can be substantially constant. Alternatively, the voltage applied to the charger 106 by the power supply 122 can be time varying. For example, the time varying voltage can include a periodically varying sign voltage, such as an AC voltage. For an embodiment where a periodically sign-varying voltage is applied to the charger 106, the sequential voltages applied to the field electrodes 402 are also be modified or be made intermittent such that the rotational direction of the combustion reaction 108 is maintained when the majority charge polarity is inverted.
  • The field electrodes 402 can be at least partially carried by a second electrical insulator (not shown). The second electrical insulator and the field electrodes 402 can form an integrated unit or a portion of an integrated unit 401. Some or all of the fuel nozzle 116, support structure 118, conductive flame holder 102, first and second electrical insulator(s), field electrodes 402, and/or charger 106 can be formed as an integrated unit 501.
  • FIG. 6 is a simplified perspective view of an electrically stabilized burner 601, according to another embodiment. Compared to the embodiments 401 and 501 shown in FIG. 4 and FIG. 5 respectively, in the embodiment illustrated by 601, a separate charger 106 is omitted. The function of the charger 106 is performed by an integrated field and charge electrodes 602. The mixer 610 includes a plurality of field and charge electrodes 602 operatively coupled to a power supply 122. For purposes of illustration, three field and charge electrodes 602 are shown but the actual number of field and charge electrodes 602 can be different. A mixer controller (not shown) is operatively coupled to one or more power supplies 122 configured to apply driving voltages to the field and charge electrodes 602. The mixer controller 210 is configured to cause the power supply(ies) 122 to apply a bias voltage to the field and charge electrodes 602 superimposed over electrode sequence voltages similar to those described in embodiments illustrated in FIGS. 4 and 5. The electrode sequence voltages sequentially attract and repel charged particles corresponding to a majority polarity of charged particles carried by combustion reaction 108. The bias voltage causes the combustion reaction to carry the majority polarity. As with a conventional charger, the concentration of charges carried by the combustion reaction (which may be measured as a voltage) is proportional to the bias voltage.
  • The bias voltage can be substantially constant. Alternatively, the bias voltage can be time varying. For example, the time varying voltage can include a periodically varying sign voltage, such as an AC voltage. For an embodiment where a periodically sign-varying bias voltage is applied to the field and charge electrodes 602, the sequential voltages (superimposed over the bias voltage) applied to the field and charge electrodes 602 can also be modified or be made intermittent such that the rotational direction of the combustion reaction is maintained.
  • The mixer controller is configured to cause the power supply(ies) 122 to drive the field and charge electrodes 602 in a manner selected to cause the field and charge electrodes 602 to mix the fuel with the oxidant, air, and/or flue gas at a selected rate of mixing. The sequential driving of the charged particles can cause circulation of the charged particles and a corresponding stream-wise vortex 202 in an aperture 104 defined by the conductive flame holder 102, field and charge electrodes 602 and/or electrical insulator (not shown). The resultant circulation of combustion reaction causes mixing of the fuel with oxidant, air, and/or flue gas at the selected rate.
  • The field and charge electrodes 602 can be at least partially carried by an electrical insulator (not shown). The electrical insulator and the field and charge electrodes 602 can form an integrated unit or a portion of an integrated unit 601. Some or all of a fuel nozzle 116, support structure 118, conductive flame holder 102, one or more electrical insulator(s) (not shown), and field and charge electrodes 602 can be formed as an integrated unit 601.
  • Optionally, any of electrically stabilized burner embodiments 101, 201, 301, 401, 501, and 601 can additionally include a second mixer (not shown) configured to mix fuel with oxidant, air, and/or flue gas below the conductive flame holder 102.
  • FIG. 7 is a flowchart showing a method 701 for operating an electrically stabilized burner, according to an embodiment. A fuel jet is projected in step 702. A fuel jet typically diverges from a nozzle at about a 7.5° half angle (15° solid angle). The divergence corresponds to the entrainment of gas or gases adjacent to the fuel jet. For example, oxidant, air, and/or flue gas can be entrained in the fuel jet. The entrainment reduces the concentration of the fuel within the gas stream. For a given fuel and entrained gas, the resultant ratio of fuel to oxidant can be a determinate function of distance along the fuel jet. In a low nitrogen oxide (NOx) burner, for example, it can be advantageous to maintain combustion at a narrow range of fuel dilution at or near a lean flammability limit of the fuel. Step 702 includes entraining oxidant, air, and/or flue gas, in the fuel jet.
  • Step 704 includes supporting a conductive flame holder proximate to a fuel jet at a distance along the fuel jet from the fuel nozzle corresponding to a selected fuel dilution. The selected fuel dilution can correspond substantially to a lean flammability limit of the fuel. Alternatively, supporting a conductive flame holder proximate to a fuel jet at a distance along the fuel jet corresponding to a selected fuel dilution can include supporting the conductive flame holder at a distance such that the dilution in the fuel caused by entrainment (and corresponding to fuel jet expansion) between the fuel nozzle and the conductive flame holder plus the dilution of the fuel caused by subsequent mixing results in a selected fuel dilution near the lean flammability limit of the fuel.
  • Optionally, the method 701 can include the step (not shown) of selecting a fuel dilution. For example, at start-up, a furnace or boiler using the burner can be operated at a relatively rich fuel mixture. A richer fuel mixture is generally more stable when a combustion chamber is cool. Later, after a warm-up period, the fuel dilution can be increased such that the fuel is burned near its lean flammability limit. As described above, operating a burner near the lean flammability limit of the fuel is generally associated with a cooler combustion reaction, and a cooler combustion reaction is generally associated with reduced NOx output. The method 701 can further include (not shown) adjusting the distance along the fuel jet at which the conductive flame holder is supported, wherein the distance corresponds to the selected fuel dilution.
  • Alternatively, the burner described herein can be operated primarily when the furnace or boiler is cool. Later, after the combustion chamber is warmed-up, the combustion reaction can lift from the conductive flame holder to be held at a larger distance from the fuel nozzle by an aerodynamic flame holder (e.g., a bluff body). The combustion reaction can be lifted by removing application of the voltage or charge applied in step 706, or responsive to higher temperatures that cause the conductive flame holder to be less effective at holding the combustion reaction (at a given applied voltage).
  • Proceeding to step 706, a voltage or charge is applied to a combustion reaction supported by the fuel jet. For example, a charger can be disposed near the combustion reaction and raised to a potential to inject a charge into the combustion reaction. According to embodiments, applying a voltage or charge to the combustion reaction includes applying a voltage to the charger.
  • Applying a voltage or charge to the combustion reaction can include the application of a constant voltage to the charger, and hence a substantially constant current to the combustion reaction. The inventors have found that a high voltage (high voltage is defined as equal to or greater than ±1000 volts) should be applied to the charger in order to inject sufficient charge to cause the described phenomena. Either positive or negative voltage may be applied to the combustion reaction. In some experiments, positive voltage was found to be somewhat more effective at holding the flame compared to an equal magnitude negative voltage. In an embodiment, +15,000 volts was applied to a charger formed as a charge electrode in electrical contact with a conductive flame, and the conductive flame holder (described in step 708 below) was held at ground potential. For more demanding conditions (e.g., hotter furnace temperature and/or higher fuel flow velocity), the conductive flame holder can be held at a voltage opposite in polarity to the applied charge polarity. The inventors contemplate a wide range of effective voltages. For example, voltages of ±1000 volts to about ±115,000 volts can be applied to the charger. More particularly, ±8000 volts to about ±40,000 volts can be applied to the charger. At +15,000 volts, current is typically in the range of hundreds of microamps up to hundreds of milliamps. A power supply capable of delivering a maximum power of about 15 Watts to 1500 Watts is generally appropriate, depending on operating conditions. Lower power is required at cooler furnace temperatures and at fuel flow rates corresponding to about 150,000 BTU/hour output.
  • Alternatively, applying a voltage or charge to the combustion reaction in step 706 can include applying a time-varying voltage or charge to the combustion reaction. For example, a time-varying voltage can be applied to a charger. The time-varying voltage can include a periodic voltage waveform having a frequency of about 50 to about 10,000 Hertz. For example, the time-varying voltage can include a periodic voltage waveform having a frequency of about 200 to about 800 Hertz. Applying the time-varying voltage can include applying a square waveform, sine waveform, triangular waveform, truncated triangular waveform, sawtooth waveform, logarithmic waveform, and/or exponential waveform to the charger. The waveform can also have an amplitude of about ±1000 volts to about ±115,000 volts. For example, the waveform can have an amplitude of about ±8000 volts to about ±40,000 volts.
  • Step 706 includes holding the conductive flame holder at a voltage different than the voltage or charge applied to the combustion reaction. Applying a voltage or charge to the combustion reaction can includes applying a time-varying voltage or charge to the combustion reaction and applying a second time-varying voltage to the conductive flame holder, the second time-varying voltage being instantaneously opposite in polarity from the time-varying voltage or charge applied to the combustion reaction. Alternatively, the conductive flame holder can be held substantially at a ground potential, or can be galvanically isolated from ground and from voltages other than the voltage applied to the charger.
  • Step 708 includes stabilizing a combustion reaction supported by the fuel jet proximate to the conductive flame holder. The stabilization can be responsive to at least an intermittent voltage difference between the combustion reaction and the conductive flame holder. For example, step 708 can include exciting at least an intermittent plasma state in the fuel jet responsive to the at least intermittent voltage difference between the combustion reaction and the conductive flame holder. The plasma state can maintain fuel ignition in some embodiments.
  • Step 710 includes mixing the fuel with oxidant (e.g. oxygen), air, and/or flue gas above the conductive flame holder. The fuel and oxidant, air, and/or flue gas can be mixed to maintain a selected DamkOhler number at a location corresponding to the combustion reaction. The selected DamkOhler number can be greater than or equal to 1. For example, the selected DamkOhler number can be in the range from about 1.1 to about 1.7.
  • In step 710, mixing the oxidant, air, and/or flue gas and the fuel includes imparting rotational inertia on the combustion reaction. The rotational inertia can be imparted by injecting one or more jets of gas that include oxidant, air, and/or flue gas into the fuel jet and entrained gas proceeding from the fuel nozzle and into the mixer aperture. Alternatively, mixing the fuel with oxidant, air, and/or flue gas can include applying a rotating electric field to the combustion reaction or the fuel jet above the conductive flame holder. Applying the rotating electric field can include applying a sequential waveform to a plurality of field electrodes.
  • Step 710 further includes mixing the fuel with oxidant, air, and/or flue gas above the conductive flame holder and below a location where the voltage or charge is applied to the combustion reaction (e.g., see FIG. 4). Alternatively, mixing the fuel with oxidant, air, and/or flue gas above the conductive flame holder can include mixing the fuel with oxidant, air, and/or flue gas above a location where the voltage or charge is applied to the combustion reaction or can include mixing the fuel with oxidant, air, and/or flue gas at a location substantially coincident with a location where the voltage or charge is applied to the combustion reaction (e.g., see FIGS. 5, 6).
  • Optionally, the fuel can also be mixed with oxidant, air, and/or flue gas below the conductive flame holder.
  • Steps 706 and 710 can be combined, optionally, such as with an embodiment 601 (see FIG. 6). Applying the voltage or charge to the combustion reaction and mixing the combustion reaction can be performed by at least an overlapping set of field electrodes. The mixing of fuel with oxidant of step 710 can include applying an electric field to the combustion reaction or to the fuel stream above the conductive flame holder. The electric field can be applied with a charger.
  • Proceeding to step 712, heat from the combustion reaction is output. For example, the heat can be output to heat a process material, to heat process equipment, to heat air and/or water, to generate electricity, to generate rotational energy, and/or to generate thrust.
  • While various aspects and embodiments have been disclosed herein, other aspects and embodiments are contemplated. The various aspects and embodiments disclosed herein are for purposes of illustration and are not intended to be limiting, with the true scope and spirit being indicated by the following claims.

Claims (31)

What is claimed is:
1. An electrically stabilized burner, comprising:
a fuel nozzle configured to providing a fuel jet flowing a fuel through a surrounding volume and entraining a first quantity of oxidant, air or flue gas, wherein the fuel and the first quantity of oxidant, air or flue gas are ignited to provide a combustion reaction;
a conductive flame holder configured for mounting proximate the fuel jet;
a mixer configured to mix the fuel and the first quantity of oxidant, air or flue gas above the conductive flame holder; and
wherein the mixer includes a plurality of field electrodes operatively coupled to the mixer controller and disposed such that the conductive flame holder is disposed between the plurality of field electrodes and a fuel nozzle;
wherein the mixer controller further includes a plurality of second power supplies each operatively coupled to one of each of the plurality of field electrodes;
wherein the mixer controller is configured to drive the plurality of field electrodes with a substantially constant bias voltage superimposed over a time-varying mixing voltage sequence; and
wherein the application of the bias voltage is selected to cause the plurality of field electrodes to operate as a charger.
2. The electrically stabilized burner of claim 1, wherein the mixer controller is configured to drive the plurality of field electrodes in a manner selected to cause the plurality of field electrodes to mix the fuel and the first quantity of oxidant, air, or flue gas at a selected rate of mixing.
3. The electrically stabilized burner of claim 1, wherein the mixer controller is configured to drive the plurality of field electrodes in a sequence selected to cause the plurality of field electrodes to form a stream-wise vortex in the combustion reaction to cause mixing of the fuel and the first quantity of oxidant, air, or flue gas.
4. The electrically stabilized burner of claim 1, further comprising a third electrical insulator configured to be disposed peripherally to the combustion reaction or to the fuel and the first quantity of oxidant, air, or flue gas such that the conductive flame holder is disposed between the third electrical insulator and the fuel nozzle;
wherein the plurality of field electrodes are at least partially carried by the third electrical insulator; and
wherein the third electrical insulator and the plurality of field electrodes form an integrated unit or a portion of an integrated unit.
5. The electrically stabilized burner of claim 1, wherein the mixer includes a plurality of field electrodes operatively coupled to the mixer controller and disposed such that the conductive flame holder is disposed between the plurality of field electrodes and a fuel nozzle;
wherein the mixer controller is configured to drive the plurality of field electrodes with a time-varying bias voltage superimposed over a time-varying mixing voltage sequence; and
wherein the application of the time-varying bias voltage is selected to cause the plurality of field electrodes to operate as charger.
6. A method for operating an electrically stabilized burner, comprising the steps of:
providing a fuel jet streaming a fuel;
supporting a conductive flame holder proximate to the fuel jet at a distance along the fuel jet corresponding to a selected fuel dilution;
mixing the fuel with the first quantity of oxidant, air, or flue gas above the conductive flame holder to provide a mixed fuel.
igniting the mixed fuel to provide a combustion reaction;
applying a voltage or charge to the combustion reaction; and
holding the combustion reaction with the conductive flame holder responsive to at least an intermittent voltage difference between the combustion reaction and the conductive flame holder.
7. The method for operating an electrically stabilized burner of claim 6, wherein the selected fuel dilution corresponds to a fuel concentration at or above a lean flammability limit of the fuel.
8. The method for operating an electrically stabilized burner of claim 6, further comprising the step of:
mixing the fuel with the first quantity of oxidant, air, or flue gas at a mixing rate corresponding to a selected Damköhler number between about 1.1 to 1.7 at a location corresponding to the combustion reaction.
9. The method for operating an electrically stabilized burner of claim 6, wherein the step of supporting a conductive flame holder proximate to a fuel jet at a distance along the fuel jet corresponding to a selected fuel dilution includes the step of supporting the conductive flame holder at a distance such that dilution in the fuel caused by fuel jet expansion between a nozzle and the conductive flame holder plus dilution in the fuel jet caused by the step of mixing the fuel with a first quantity of oxidant, air, or flue gas results in a selected fuel dilution near the lean flammability limit of the fuel.
10. The method for operating an electrically stabilized burner of claim 6, wherein the step of mixing the fuel with a first quantity oxidant, air, and/or flue gas includes the step of injecting one or more fluid jets of the second quantity of any or the combination of fuel, oxidant, air, and/or flue gas into the combustion reaction in order to impart rotational inertia to the combustion reaction.
11. The method for operating an electrically stabilized burner of claim 6, wherein the step of mixing the fuel with a first quantity of oxidant, air, or flue gas includes a step of applying a rotating electric field to the combustion reaction or to the mixed fuel above the conductive flame holder.
12. The method for operating an electrically stabilized burner of claim 11, wherein the step of applying a rotating electric field includes a step of applying a sequential voltage waveform to a plurality of field electrodes.
13. The method for operating an electrically stabilized burner of claim 6, wherein the steps of applying a voltage or charge to the combustion reaction and mixing the fuel with a first quantity of oxidant, air, or flue gas above the conductive flame holder is performed by sequentially applying a voltage waveform to at least an overlapping set of field electrodes.
14. The method for operating an electrically stabilized burner of claim 6, wherein the step of mixing the fuel with a first quantity of oxidant, air, or flue gas above the conductive flame holder includes the step of applying an electric field to the combustion reaction or to the mixed fuel above the conductive flame holder.
15. The method for operating an electrically stabilized burner of claim 6, wherein the step of mixing the fuel with a first quantity of oxidant, air, or flue gas includes the step of applying an electric field to the combustion reaction or to the mixed fuel with a charger.
16. The method for operating an electrically stabilized burner of claim 6, wherein the step of mixing the fuel with a first quantity of oxidant, air, or flue gas above the conductive flame holder includes the step of mixing the fuel with the first quantity of oxidant, air, or flue gas above the conductive flame holder and below a location where the voltage or charge is applied to the combustion reaction.
17. The method for operating an electrically stabilized burner of claim 6, wherein the step of mixing the fuel with a first quantity of oxidant, air, or flue gas above the conductive flame holder includes the step of mixing the fuel with the first quantity of oxidant, air, or flue gas above a location where the voltage or charge is applied to the combustion reaction.
18. The method for operating an electrically stabilized burner of claim 6, wherein the step of mixing the fuel with a first quantity of oxidant, air, or flue gas above the conductive flame holder includes the step of mixing the fuel with the first quantity of oxidant, air, or flue gas at a location substantially coincident with a location where the voltage or charge is applied to the combustion reaction.
19. The method for operating an electrically stabilized burner of claim 6, further comprising the step of:
mixing the fuel with a first quantity of oxidant, air, or flue gas at a location below the conductive flame holder.
20. The method for operating an electrically stabilized burner of claim 6, further comprising the steps of:
selecting a fuel and an oxidant stoichiometry; and
adjusting the distance along the fuel jet at which the conductive flame holder is supported to correspond to the selected fuel and oxidant stoichiometry.
21. The method for operating an electrically stabilized burner of claim 6, further comprising the step of:
entraining at least an oxidant in the fuel jet.
22. The method for operating an electrically stabilized burner of claim 21, wherein the step of entraining at least the oxidant in the fuel jet includes entraining a gas including the oxidant.
23. The method for operating an electrically stabilized burner of claim 21, wherein the step of entraining at least the oxidant in the fuel jet includes entraining the oxidant and air or flue gas.
24. The method for operating an electrically stabilized burner of claim 21, wherein entraining at least the oxidant in the fuel jet includes entraining a flue gas.
25. The method for operating an electrically stabilized burner of claim 6, wherein the step of mixing the fuel with the first quantity of oxidant, air, or flue gas further includes the step of mixing the fuel with a flue gas.
26. The method for operating an electrically stabilized burner of claim 6, wherein the step of holding the combustion reaction with the conductive flame holder includes the step of exciting at least an intermittent plasma state in the mixed fuel responsive to the at least an intermittent voltage difference between the combustion reaction and the conductive flame holder.
27. The method for operating an electrically stabilized burner of claim 26, further comprising the step of:
maintaining ignition of the mixed fuel with the plasma state.
28. The method for operating an electrically stabilized burner of claim 6, further comprising the step of:
holding the conductive flame holder at a voltage different than the voltage or charge applied to the combustion reaction.
29. The method for operating an electrically stabilized burner of claim 28, wherein the step of applying a voltage or charge to the combustion reaction includes the step of applying a first time-varying voltage or charge to the combustion reaction and the step of applying a second time-varying voltage to the conductive flame holder, the second time-varying voltage being instantaneously opposite in sign from the time-varying voltage or charge applied to the combustion reaction.
30. The method for operating an electrically stabilized burner of claim 6, further comprising the step of:
holding the conductive flame holder substantially at a ground potential.
31. The method for operating an electrically stabilized burner of claim 15, further comprising the step of:
galvanically isolating the conductive flame holder from ground and from voltages other than the voltage applied to the ionizing electrode.
US15/617,836 2012-07-24 2017-06-08 Apparatus and method for electrically stabilized combustion Abandoned US20170276346A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US15/617,836 US20170276346A1 (en) 2012-07-24 2017-06-08 Apparatus and method for electrically stabilized combustion

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201261675079P 2012-07-24 2012-07-24
US13/950,249 US9702550B2 (en) 2012-07-24 2013-07-24 Electrically stabilized burner
US15/617,836 US20170276346A1 (en) 2012-07-24 2017-06-08 Apparatus and method for electrically stabilized combustion

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US13/950,249 Division US9702550B2 (en) 2012-07-24 2013-07-24 Electrically stabilized burner

Publications (1)

Publication Number Publication Date
US20170276346A1 true US20170276346A1 (en) 2017-09-28

Family

ID=50188057

Family Applications (2)

Application Number Title Priority Date Filing Date
US13/950,249 Expired - Fee Related US9702550B2 (en) 2012-07-24 2013-07-24 Electrically stabilized burner
US15/617,836 Abandoned US20170276346A1 (en) 2012-07-24 2017-06-08 Apparatus and method for electrically stabilized combustion

Family Applications Before (1)

Application Number Title Priority Date Filing Date
US13/950,249 Expired - Fee Related US9702550B2 (en) 2012-07-24 2013-07-24 Electrically stabilized burner

Country Status (3)

Country Link
US (2) US9702550B2 (en)
CN (2) CN108469020B (en)
WO (1) WO2015012872A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10627106B2 (en) 2012-12-26 2020-04-21 Clearsign Technologies Corporation Combustion system with a grid switching electrode
US11073280B2 (en) 2010-04-01 2021-07-27 Clearsign Technologies Corporation Electrodynamic control in a burner system

Families Citing this family (47)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9732958B2 (en) 2010-04-01 2017-08-15 Clearsign Combustion Corporation Electrodynamic control in a burner system
US9696031B2 (en) 2012-03-27 2017-07-04 Clearsign Combustion Corporation System and method for combustion of multiple fuels
US9371994B2 (en) 2013-03-08 2016-06-21 Clearsign Combustion Corporation Method for Electrically-driven classification of combustion particles
US9289780B2 (en) 2012-03-27 2016-03-22 Clearsign Combustion Corporation Electrically-driven particulate agglomeration in a combustion system
US9702550B2 (en) 2012-07-24 2017-07-11 Clearsign Combustion Corporation Electrically stabilized burner
US9310077B2 (en) 2012-07-31 2016-04-12 Clearsign Combustion Corporation Acoustic control of an electrodynamic combustion system
CN104755842B (en) 2012-09-10 2016-11-16 克利尔赛恩燃烧公司 Use the electronic Combustion System of current limliting electrical equipment
US9746180B2 (en) 2012-11-27 2017-08-29 Clearsign Combustion Corporation Multijet burner with charge interaction
US9496688B2 (en) 2012-11-27 2016-11-15 Clearsign Combustion Corporation Precombustion ionization
US9513006B2 (en) 2012-11-27 2016-12-06 Clearsign Combustion Corporation Electrodynamic burner with a flame ionizer
US9562681B2 (en) 2012-12-11 2017-02-07 Clearsign Combustion Corporation Burner having a cast dielectric electrode holder
WO2014099193A1 (en) 2012-12-21 2014-06-26 Clearsign Combustion Corporation Electrical combustion control system including a complementary electrode pair
US9441834B2 (en) 2012-12-28 2016-09-13 Clearsign Combustion Corporation Wirelessly powered electrodynamic combustion control system
US10364984B2 (en) 2013-01-30 2019-07-30 Clearsign Combustion Corporation Burner system including at least one coanda surface and electrodynamic control system, and related methods
US10077899B2 (en) 2013-02-14 2018-09-18 Clearsign Combustion Corporation Startup method and mechanism for a burner having a perforated flame holder
US10119704B2 (en) 2013-02-14 2018-11-06 Clearsign Combustion Corporation Burner system including a non-planar perforated flame holder
CA2892234A1 (en) 2013-02-14 2014-08-21 Clearsign Combustion Corporation Perforated flame holder and burner including a perforated flame holder
US10571124B2 (en) 2013-02-14 2020-02-25 Clearsign Combustion Corporation Selectable dilution low NOx burner
US11460188B2 (en) 2013-02-14 2022-10-04 Clearsign Technologies Corporation Ultra low emissions firetube boiler burner
US10386062B2 (en) 2013-02-14 2019-08-20 Clearsign Combustion Corporation Method for operating a combustion system including a perforated flame holder
US9377189B2 (en) 2013-02-21 2016-06-28 Clearsign Combustion Corporation Methods for operating an oscillating combustor with pulsed charger
US9696034B2 (en) 2013-03-04 2017-07-04 Clearsign Combustion Corporation Combustion system including one or more flame anchoring electrodes and related methods
US9664386B2 (en) 2013-03-05 2017-05-30 Clearsign Combustion Corporation Dynamic flame control
US10190767B2 (en) 2013-03-27 2019-01-29 Clearsign Combustion Corporation Electrically controlled combustion fluid flow
WO2014160830A1 (en) 2013-03-28 2014-10-02 Clearsign Combustion Corporation Battery-powered high-voltage converter circuit with electrical isolation and mechanism for charging the battery
WO2014183135A1 (en) 2013-05-10 2014-11-13 Clearsign Combustion Corporation Combustion system and method for electrically assisted start-up
US9574767B2 (en) 2013-07-29 2017-02-21 Clearsign Combustion Corporation Combustion-powered electrodynamic combustion system
WO2015017084A1 (en) 2013-07-30 2015-02-05 Clearsign Combustion Corporation Combustor having a nonmetallic body with external electrodes
WO2015038245A1 (en) 2013-09-13 2015-03-19 Clearsign Combustion Corporation Transient control of a combustion reaction
WO2015042566A1 (en) 2013-09-23 2015-03-26 Clearsign Combustion Corporation Control of combustion reaction physical extent
WO2015051377A1 (en) 2013-10-04 2015-04-09 Clearsign Combustion Corporation Ionizer for a combustion system
CN105579776B (en) 2013-10-07 2018-07-06 克利尔赛恩燃烧公司 With the premix fuel burner for having hole flame holder
WO2015057740A1 (en) 2013-10-14 2015-04-23 Clearsign Combustion Corporation Flame visualization control for electrodynamic combustion control
CA2928451A1 (en) 2013-11-08 2015-05-14 Clearsign Combustion Corporation Combustion system with flame location actuation
EP3090210A1 (en) * 2013-12-31 2016-11-09 Clearsign Combustion Corporation Method and apparatus for extending flammability limits in a combustion reaction
EP3097365A4 (en) 2014-01-24 2017-10-25 Clearsign Combustion Corporation LOW NOx FIRE TUBE BOILER
WO2016003883A1 (en) 2014-06-30 2016-01-07 Clearsign Combustion Corporation Low inertia power supply for applying voltage to an electrode coupled to a flame
US10458647B2 (en) 2014-08-15 2019-10-29 Clearsign Combustion Corporation Adaptor for providing electrical combustion control to a burner
US9702547B2 (en) 2014-10-15 2017-07-11 Clearsign Combustion Corporation Current gated electrode for applying an electric field to a flame
US10006715B2 (en) 2015-02-17 2018-06-26 Clearsign Combustion Corporation Tunnel burner including a perforated flame holder
US10514165B2 (en) * 2016-07-29 2019-12-24 Clearsign Combustion Corporation Perforated flame holder and system including protection from abrasive or corrosive fuel
US10619845B2 (en) 2016-08-18 2020-04-14 Clearsign Combustion Corporation Cooled ceramic electrode supports
WO2018085152A1 (en) 2016-11-04 2018-05-11 Clearsign Combustion Corporation Plasma pilot
DE102017003388A1 (en) * 2017-04-06 2018-10-11 Linde Aktiengesellschaft Flame rectification method and burner arrangement therefor
US10920979B2 (en) 2018-04-06 2021-02-16 Zeeco, Inc. Low NOx burner and flow momentum enhancing device
US11353212B2 (en) 2019-09-12 2022-06-07 Zeeco, Inc. Low NOxburner apparatus and method
CN112696657B (en) * 2020-12-01 2023-03-10 北方联合电力有限责任公司包头第一热电厂 Boiler blowing-out control system

Family Cites Families (135)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1153182A (en) 1912-12-19 1915-09-07 Frederic W C Schniewind Purification of coal.
US1983430A (en) 1934-04-16 1934-12-04 Clarence S Asheraft Electric arc and method of producing same
US2604936A (en) 1946-01-15 1952-07-29 Metal Carbides Corp Method and apparatus for controlling the generation and application of heat
US2942420A (en) 1957-10-28 1960-06-28 Gen Electric Ignition mechanism
CH359724A (en) 1958-12-11 1962-01-31 Commissariat Energie Atomique Electrical method and device for improving heat exchanges between a gas and an exchange surface
DE1121762B (en) 1960-04-14 1962-01-11 Alberto Wobig Burners for gaseous or liquid fuels
US3087472A (en) 1961-03-30 1963-04-30 Asakawa Yukichi Method and apparatus for the improved combustion of fuels
GB1042014A (en) 1961-11-10 1966-09-07 Kenneth Payne A fuel burner
US3224485A (en) 1963-05-06 1965-12-21 Inter Probe Heat control device and method
US3416870A (en) 1965-11-01 1968-12-17 Exxon Research Engineering Co Apparatus for the application of an a.c. electrostatic field to combustion flames
US3306338A (en) 1965-11-01 1967-02-28 Exxon Research Engineering Co Apparatus for the application of insulated a.c. fields to flares
US3358731A (en) 1966-04-01 1967-12-19 Mobil Oil Corp Liquid fuel surface combustion process and apparatus
US3503348A (en) 1968-08-30 1970-03-31 Hagan Ind Inc Incinerator
US3749545A (en) 1971-11-24 1973-07-31 Univ Ohio State Apparatus and method for controlling liquid fuel sprays for combustion
US3841824A (en) 1972-09-25 1974-10-15 G Bethel Combustion apparatus and process
US3869362A (en) 1973-01-11 1975-03-04 Ebara Mfg Process for removing noxious gas pollutants from effluent gases by irradiation
JPS5819609B2 (en) 1973-07-28 1983-04-19 新日本化学工業株式会社 Manufacturing method of magnesium hydroxide
CA1070622A (en) 1974-08-19 1980-01-29 James J. Schwab Process and apparatus for electrostatic cleaning of gases
FR2290945A1 (en) 1974-11-12 1976-06-11 Paillaud Pierre PROCESS FOR IMPROVING THE ENERGY EFFICIENCY OF A REACTION
DE2456163C2 (en) 1974-11-28 1986-03-13 Daimler-Benz Ag, 7000 Stuttgart Combustion chamber, in particular the piston working chamber of an engine
JPS5343143A (en) 1976-09-30 1978-04-19 Tokai Trw & Co Ignition plug
US4111636A (en) 1976-12-03 1978-09-05 Lawrence P. Weinberger Method and apparatus for reducing pollutant emissions while increasing efficiency of combustion
US4118202A (en) 1977-10-17 1978-10-03 Ball Corporation Pre-primed fuel and method and apparatus for its manufacture
JPS5551918A (en) 1978-10-13 1980-04-16 Nissan Motor Co Ltd Internal combustion engine
US4304096A (en) 1979-05-11 1981-12-08 The Regents Of The University Of Minnesota Method for reducing particulates discharged by combustion means
US4260394A (en) 1979-08-08 1981-04-07 Advanced Energy Dynamics, Inc. Process for reducing the sulfur content of coal
US4362016A (en) 1979-10-15 1982-12-07 Papadopulos Stephen C Pollution control device for automobile exhaust
US4439980A (en) 1981-11-16 1984-04-03 The United States Of America As Represented By The Secretary Of The Navy Electrohydrodynamic (EHD) control of fuel injection in gas turbines
US4649260A (en) 1983-03-16 1987-03-10 Coal-O-Matic Pvba Lighter for stove, open hearth and similar
JPS60216111A (en) 1984-04-11 1985-10-29 Osaka Gas Co Ltd Heating apparatus of combustion type
GB8418056D0 (en) 1984-07-16 1984-08-22 Roberts J P Active control of acoustic instability in combustion chambers
US4675029A (en) 1984-11-21 1987-06-23 Geoenergy International, Corp. Apparatus and method for treating the emission products of a wood burning stove
FR2577304B1 (en) 1985-02-08 1989-12-01 Electricite De France GAS ELECTROBURNER WITH ELECTRICAL ENERGY SUPPLY.
JPS61265404A (en) 1985-05-17 1986-11-25 Osaka Gas Co Ltd Burner
SE460737B (en) 1986-05-12 1989-11-13 Konstantin Mavroudis PANNA FOR FIXED BRAENSLEN, SUPPLIED WITH DEVICES FOR SUPPLY OF SECOND AIR
JPH01111945U (en) * 1988-01-12 1989-07-27
US4995805A (en) 1989-02-24 1991-02-26 Gas Research Institute Method and apparatus for increasing radiant heat production of hydrocarbon fuel combustion systems
US4987839A (en) 1990-05-14 1991-01-29 Wahlco, Inc. Removal of particulate matter from combustion gas streams
EP0712477A1 (en) 1994-06-15 1996-05-22 Thermal Energy Systems, Incorporated Apparatus and method for reducing particulate emissions from combustion processes
NO180315C (en) 1994-07-01 1997-03-26 Torfinn Johnsen Combustion chamber with equipment to improve combustion and reduce harmful substances in the exhaust gas
US5455401A (en) 1994-10-12 1995-10-03 Aerojet General Corporation Plasma torch electrode
DE19542918A1 (en) 1995-11-17 1997-05-22 Asea Brown Boveri Device for damping thermoacoustic pressure vibrations
US6247921B1 (en) 1996-05-23 2001-06-19 American Standard International Inc. Apparatus for generating a spark
JP3054596B2 (en) 1996-10-28 2000-06-19 照夫 新井 burner
FR2794847B1 (en) * 1999-06-08 2001-07-20 Gaz De Petrole PROCESS FOR PREVENTING THE BURNER OF A BURNER FROM EXTINGUISHING AND BURNER FACILITATING ITS IMPLEMENTATION
JP2001021110A (en) 1999-07-06 2001-01-26 Tokyo Gas Co Ltd Method and device for combustion of gas burner
DE10137683C2 (en) 2001-08-01 2003-05-28 Siemens Ag Method and device for influencing combustion processes in fuels
US20030051990A1 (en) 2001-08-15 2003-03-20 Crt Holdings, Inc. System, method, and apparatus for an intense ultraviolet radiation source
US6742340B2 (en) 2002-01-29 2004-06-01 Affordable Turbine Power Company, Inc. Fuel injection control system for a turbine engine
DE50304472D1 (en) * 2002-03-22 2006-09-14 Pyroplasma Kg FUEL BURNING DEVICE
US6736133B2 (en) 2002-04-09 2004-05-18 Hon Technology Inc. Air filtration and sterilization system for a fireplace
US7159646B2 (en) 2002-04-15 2007-01-09 University Of Maryland Electrohydrodynamically (EHD) enhanced heat transfer system and method with an encapsulated electrode
EP1411573A2 (en) 2002-10-16 2004-04-21 Matsushita Electric Industrial Co., Ltd. Burner, hydrogen generator, and fuel cell power generation system
US6640549B1 (en) 2002-12-03 2003-11-04 The United States Of America As Represented By The Secretary Of The Navy Method and device for modulation of a flame
DE10260709B3 (en) 2002-12-23 2004-08-12 Siemens Ag Method and device for influencing combustion processes in fuels
JP2006523294A (en) * 2003-01-22 2006-10-12 ヴァスト・パワー・システムズ・インコーポレーテッド Reactor
CN2791501Y (en) * 2003-06-11 2006-06-28 日本特殊陶业株式会社 Diacharge ignition device for combustion appliance
US7243496B2 (en) 2004-01-29 2007-07-17 Siemens Power Generation, Inc. Electric flame control using corona discharge enhancement
US7377114B1 (en) 2004-06-02 2008-05-27 Kevin P Pearce Turbine engine pulsed fuel injection utilizing stagger injector operation
US6918755B1 (en) 2004-07-20 2005-07-19 Arvin Technologies, Inc. Fuel-fired burner with skewed electrode arrangement
US7226496B2 (en) 2004-11-30 2007-06-05 Ranco Incorporated Of Delaware Spot ventilators and method for spot ventilating bathrooms, kitchens and closets
US7226497B2 (en) 2004-11-30 2007-06-05 Ranco Incorporated Of Delaware Fanless building ventilator
US7182805B2 (en) 2004-11-30 2007-02-27 Ranco Incorporated Of Delaware Corona-discharge air mover and purifier for packaged terminal and room air conditioners
DE102004061300B3 (en) 2004-12-20 2006-07-13 Siemens Ag Method and device for influencing combustion processes
US8082725B2 (en) 2007-04-12 2011-12-27 General Electric Company Electro-dynamic swirler, combustion apparatus and methods using the same
WO2008154592A2 (en) 2007-06-11 2008-12-18 University Of Florida Research Foundation, Inc. Electrodynamic control of blade clearance leakage loss in turbomachinery applications
US20090165436A1 (en) * 2007-12-28 2009-07-02 General Electric Company Premixed, preswirled plasma-assisted pilot
US8245951B2 (en) 2008-04-22 2012-08-21 Applied Nanotech Holdings, Inc. Electrostatic atomizing fuel injector using carbon nanotubes
US8851882B2 (en) 2009-04-03 2014-10-07 Clearsign Combustion Corporation System and apparatus for applying an electric field to a combustion volume
CN201568964U (en) * 2009-10-30 2010-09-01 华南理工大学 Micro-combustor adopting applied electric field
KR20120129907A (en) 2010-01-13 2012-11-28 클리어사인 컨버스천 코포레이션 Method and apparatus for elecrical control of heat transfer
US9732958B2 (en) 2010-04-01 2017-08-15 Clearsign Combustion Corporation Electrodynamic control in a burner system
JP2014507623A (en) 2011-02-09 2014-03-27 クリアサイン コンバスチョン コーポレイション Multiple response electric field control in combustion systems
EP2798270A4 (en) 2011-12-30 2015-08-26 Clearsign Comb Corp Method and apparatus for enhancing flame radiation
US20160123576A1 (en) 2011-12-30 2016-05-05 Clearsign Combustion Corporation Method and apparatus for enhancing flame radiation in a coal-burner retrofit
US20140208758A1 (en) 2011-12-30 2014-07-31 Clearsign Combustion Corporation Gas turbine with extended turbine blade stream adhesion
US9284886B2 (en) 2011-12-30 2016-03-15 Clearsign Combustion Corporation Gas turbine with Coulombic thermal protection
CN104136849A (en) 2012-02-22 2014-11-05 克利尔赛恩燃烧公司 Cooled electrode and burner system including a cooled electrode
US9377195B2 (en) 2012-03-01 2016-06-28 Clearsign Combustion Corporation Inertial electrode and system configured for electrodynamic interaction with a voltage-biased flame
CN104169725B (en) 2012-03-01 2018-04-17 克利尔赛恩燃烧公司 It is configured to the inert electrode interacted electronic with flame and system
US9696031B2 (en) 2012-03-27 2017-07-04 Clearsign Combustion Corporation System and method for combustion of multiple fuels
US9366427B2 (en) 2012-03-27 2016-06-14 Clearsign Combustion Corporation Solid fuel burner with electrodynamic homogenization
US9371994B2 (en) 2013-03-08 2016-06-21 Clearsign Combustion Corporation Method for Electrically-driven classification of combustion particles
US9289780B2 (en) 2012-03-27 2016-03-22 Clearsign Combustion Corporation Electrically-driven particulate agglomeration in a combustion system
US9267680B2 (en) 2012-03-27 2016-02-23 Clearsign Combustion Corporation Multiple fuel combustion system and method
US20150121890A1 (en) 2012-04-30 2015-05-07 Clearsign Combustion Corporation High velocity combustor
WO2013181563A1 (en) 2012-05-31 2013-12-05 Clearsign Combustion Corporation LOW NOx BURNER AND METHOD OF OPERATING A LOW NOx BURNER
US20130323661A1 (en) 2012-06-01 2013-12-05 Clearsign Combustion Corporation Long flame process heater
EP2861341A4 (en) 2012-06-15 2016-02-24 Clearsign Comb Corp Electrically stabilized down-fired flame reactor
US20130333279A1 (en) 2012-06-19 2013-12-19 Clearsign Combustion Corporation Flame enhancement for a rotary kiln
WO2014005143A1 (en) 2012-06-29 2014-01-03 Clearsign Combustion Corporation Combustion system with a corona electrode
US9702550B2 (en) 2012-07-24 2017-07-11 Clearsign Combustion Corporation Electrically stabilized burner
US9310077B2 (en) 2012-07-31 2016-04-12 Clearsign Combustion Corporation Acoustic control of an electrodynamic combustion system
US8911699B2 (en) 2012-08-14 2014-12-16 Clearsign Combustion Corporation Charge-induced selective reduction of nitrogen
US20140051030A1 (en) 2012-08-16 2014-02-20 Clearsign Combustion Corporation System and sacrificial electrode for applying electricity to a combustion reaction
US20150219333A1 (en) 2012-08-27 2015-08-06 Clearsign Combustion Corporation Electrodynamic combustion system with variable gain electrodes
CN104755842B (en) 2012-09-10 2016-11-16 克利尔赛恩燃烧公司 Use the electronic Combustion System of current limliting electrical equipment
CN202766490U (en) * 2012-09-12 2013-03-06 衢州市广源生活垃圾液化技术研究所 Plasma gasification spray gun
US20140080070A1 (en) 2012-09-18 2014-03-20 Clearsign Combustion Corporation Close-coupled step-up voltage converter and electrode for a combustion system
US20140076212A1 (en) 2012-09-20 2014-03-20 Clearsign Combustion Corporation Method and apparatus for treating a combustion product stream
US20140162195A1 (en) 2012-10-23 2014-06-12 Clearsign Combustion Corporation System for safe power loss for an electrodynamic burner
US20160161115A1 (en) 2012-10-23 2016-06-09 Clearsign Combustion Corporation Burner with electrodynamic flame position control system
US9746180B2 (en) 2012-11-27 2017-08-29 Clearsign Combustion Corporation Multijet burner with charge interaction
US9496688B2 (en) 2012-11-27 2016-11-15 Clearsign Combustion Corporation Precombustion ionization
US20170009985A9 (en) 2012-11-27 2017-01-12 Clearsign Combustion Corporation Charged ion flows for combustion control
US9513006B2 (en) 2012-11-27 2016-12-06 Clearsign Combustion Corporation Electrodynamic burner with a flame ionizer
US9562681B2 (en) 2012-12-11 2017-02-07 Clearsign Combustion Corporation Burner having a cast dielectric electrode holder
US20140170576A1 (en) 2012-12-12 2014-06-19 Clearsign Combustion Corporation Contained flame flare stack
US20140170569A1 (en) 2012-12-12 2014-06-19 Clearsign Combustion Corporation Electrically controlled combustion system with contact electrostatic charge generation
US20140170571A1 (en) 2012-12-13 2014-06-19 Clearsign Combustion Corporation Combustion control electrode assemblies, systems, and methods of manufacturing and use
US20140170575A1 (en) 2012-12-14 2014-06-19 Clearsign Combustion Corporation Ionizer for a combustion system, including foam electrode structure
WO2014099193A1 (en) 2012-12-21 2014-06-26 Clearsign Combustion Corporation Electrical combustion control system including a complementary electrode pair
WO2014105990A1 (en) 2012-12-26 2014-07-03 Clearsign Combustion Corporation Combustion system with a grid switching electrode
US9441834B2 (en) 2012-12-28 2016-09-13 Clearsign Combustion Corporation Wirelessly powered electrodynamic combustion control system
US20140196368A1 (en) 2013-01-16 2014-07-17 Clearsign Combustion Corporation Gasifier having at least one charge transfer electrode and methods of use thereof
US9469819B2 (en) 2013-01-16 2016-10-18 Clearsign Combustion Corporation Gasifier configured to electrodynamically agitate charged chemical species in a reaction region and related methods
US10364984B2 (en) 2013-01-30 2019-07-30 Clearsign Combustion Corporation Burner system including at least one coanda surface and electrodynamic control system, and related methods
US20140216401A1 (en) 2013-02-04 2014-08-07 Clearsign Combustion Corporation Combustion system configured to generate and charge at least one series of fuel pulses, and related methods
US20140227649A1 (en) 2013-02-12 2014-08-14 Clearsign Combustion Corporation Method and apparatus for delivering a high voltage to a flame-coupled electrode
US20140227646A1 (en) 2013-02-13 2014-08-14 Clearsign Combustion Corporation Combustion system including at least one fuel flow equalizer
US20140227645A1 (en) 2013-02-14 2014-08-14 Clearsign Combustion Corporation Burner systems configured to control at least one geometric characteristic of a flame and related methods
CA2892234A1 (en) 2013-02-14 2014-08-21 Clearsign Combustion Corporation Perforated flame holder and burner including a perforated flame holder
US9377189B2 (en) 2013-02-21 2016-06-28 Clearsign Combustion Corporation Methods for operating an oscillating combustor with pulsed charger
US9696034B2 (en) 2013-03-04 2017-07-04 Clearsign Combustion Corporation Combustion system including one or more flame anchoring electrodes and related methods
US9664386B2 (en) 2013-03-05 2017-05-30 Clearsign Combustion Corporation Dynamic flame control
US20140255856A1 (en) 2013-03-06 2014-09-11 Clearsign Combustion Corporation Flame control in the buoyancy-dominated fluid dynamics region
US20140272731A1 (en) 2013-03-15 2014-09-18 Clearsign Combustion Corporation Flame control in the momentum-dominated fluid dynamics region
US20150276211A1 (en) 2013-03-18 2015-10-01 Clearsign Combustion Corporation Flame control in the flame-holding region
US20160040872A1 (en) 2013-03-20 2016-02-11 Clearsign Combustion Corporation Electrically stabilized swirl-stabilized burner
WO2014160662A1 (en) 2013-03-23 2014-10-02 Clearsign Combustion Corporation Premixed flame location control
US20140295094A1 (en) 2013-03-26 2014-10-02 Clearsign Combustion Corporation Combustion deposition systems and methods of use
US10190767B2 (en) 2013-03-27 2019-01-29 Clearsign Combustion Corporation Electrically controlled combustion fluid flow
WO2014160830A1 (en) 2013-03-28 2014-10-02 Clearsign Combustion Corporation Battery-powered high-voltage converter circuit with electrical isolation and mechanism for charging the battery
WO2014183135A1 (en) 2013-05-10 2014-11-13 Clearsign Combustion Corporation Combustion system and method for electrically assisted start-up
US20140335460A1 (en) 2013-05-13 2014-11-13 Clearsign Combustion Corporation Electrically enhanced combustion control system with multiple power sources and method of operation

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11073280B2 (en) 2010-04-01 2021-07-27 Clearsign Technologies Corporation Electrodynamic control in a burner system
US10627106B2 (en) 2012-12-26 2020-04-21 Clearsign Technologies Corporation Combustion system with a grid switching electrode

Also Published As

Publication number Publication date
CN105247284A (en) 2016-01-13
CN108469020B (en) 2020-08-18
WO2015012872A1 (en) 2015-01-29
CN105247284B (en) 2018-04-03
CN108469020A (en) 2018-08-31
US9702550B2 (en) 2017-07-11
US20140065558A1 (en) 2014-03-06

Similar Documents

Publication Publication Date Title
US20170276346A1 (en) Apparatus and method for electrically stabilized combustion
US10753605B2 (en) Low NOx burner
US10047950B2 (en) Oscillating combustor with pulsed charger
US7243496B2 (en) Electric flame control using corona discharge enhancement
Kim et al. Plasma-discharge stabilization of jet diffusion flames
US9879858B2 (en) Inertial electrode and system configured for electrodynamic interaction with a flame
US20150079524A1 (en) LIFTED FLAME LOW NOx BURNER WITH FLAME POSITION CONTROL
US8601819B2 (en) Method and device for the combustion of hydrocarbon-containing fuels
US20150147706A1 (en) Electrodynamic burner with a flame ionizer
De Giorgi et al. Improvement of lean flame stability of inverse methane/air diffusion flame by using coaxial dielectric plasma discharge actuators
JP2009162478A (en) Premixed, preswirled plasma-assisted pilot
Bradley et al. Electrical coronas and burner flame stability
Ju et al. Effect of rotating gliding arc plasma on lean blow-off limit and flame structure of bluff body and swirl-stabilized premixed flames
KR100713708B1 (en) Alternating Current High Voltage Adoptive Combustion System for increasing a Flame Stabilization Region
KR101751984B1 (en) Streamer induction type combustor for improving flame stability
Kim et al. Flame stabilization using a plasma discharge in a lifted jet flame
KR20240130404A (en) High voltage applied combustor
Wang et al. Process of Multiple Channel Gliding Arc Assisted Combustion Near Lean Blow-out Limit
Krickis et al. Gas Combustion Efficiency Enhancement: Application Study of Intense Elestrostatic Field
Guan et al. Effects of electric field waveforms on a lifted non-premixed jet flame
CN104395673B (en) Low-NOx combustor and the method for operation low-NOx combustor
De Giorgi et al. Experimental Characterization Of A Plasma Assisted Lifted Flame
Barmina et al. Electric field effects on the combustion characteristics of renewable fuel
Choi et al. Response of counterflow diffusion flames to low frequency AC electric fields
Versailles et al. Application of Dielectric Barrier Discharge to Improve the Flashback Limit of a Lean Premixed Dump Combustor

Legal Events

Date Code Title Description
AS Assignment

Owner name: CLEARSIGN COMBUSTION CORPORATION, WASHINGTON

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:COLANNINO, JOSEPH;BREIDENTHAL, ROBERT E.;KRICHTAFOVITCH, IGOR A.;AND OTHERS;SIGNING DATES FROM 20131016 TO 20131105;REEL/FRAME:042751/0883

STCB Information on status: application discontinuation

Free format text: EXPRESSLY ABANDONED -- DURING EXAMINATION