US3681001A - Fluid fuel igniter control system - Google Patents
Fluid fuel igniter control system Download PDFInfo
- Publication number
- US3681001A US3681001A US37450A US3681001DA US3681001A US 3681001 A US3681001 A US 3681001A US 37450 A US37450 A US 37450A US 3681001D A US3681001D A US 3681001DA US 3681001 A US3681001 A US 3681001A
- Authority
- US
- United States
- Prior art keywords
- capacitance
- capacitor
- primary winding
- voltage
- electrodes
- 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.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23Q—IGNITION; EXTINGUISHING-DEVICES
- F23Q3/00—Igniters using electrically-produced sparks
- F23Q3/004—Using semiconductor elements
Definitions
- ABSTRACT Fuel burner spark ignition generator having a high voltage transformer secondary connected to the electrodes of a spark gap, and a primary connected in series with a capacitance, and means for charging the capacitance, and effecting a discharge of the capacitance through the transformer primary, upon the elapse of a predetermined time during the charging of the capacitance.
- This invention relates to oil burner ignition and control systems, and more particularly to a system employing solid state circuitry.
- spark discharges are used as a means of igniting an oil-fueled burner it is important for safety reasons and for long-life of electrodes, that the spark discharge electrodes be located, relative to the combustible mixture of air and oil, so that oil is unable to impinge upon the electrodes. This location is necessary since oil on the electrodes quickly results in the formation of carbon deposits on the electrodes. Such deposits in time build up sufficiently to bridge the electrode gap completely so that a spark discharge cannot occur. Further, as the spark discharge gap narrows from its proper gap length because of carbon formation, the spark discharge will not be deflected adequately by the flow of combustion air, and ignition will become sporadic with attendant unsafe and unpleasant conditions resulting.
- a satisfactory electric ignition means for ignition of an oil burner must be able to produce a spark of sufficient energy and duration so that the rapid flow of combustion air past the spark discharge electrodes and oil nozzle into the combustion chamber will deflect the spark into the finemist of oil surrounding the cone of oil sprayed out of the oil nozzle.
- Another object of the present invention is to assemble both the spark voltage generator and the oil burner control on a single base, contained in a single housing of sufficiently small size to allow mounting in the same space and location as occupied heretofor by an ignition transformer alone.
- Yet another object of the present invention is to simplify both the installation and the servicing of oil burner ignition and control by providing in a single housing an integrated system which may be readily removed for repairs, requires no separate mounting, and needs no interconnecting cables.
- a still further objective of the present invention is to provide a single unit of considerably less weight by integration of a spark voltage generator using capacitor discharge principles with a control using semiconductor devices.
- the present invention is also directed to a circuit using a time-delay circuit to provide a specific period of time for burner ignition,-failing which, the system is turned off and the circuit is put in a lock-out condition requiring manual reset.
- the circuit is further provided with protection against ignition attempts when red-hot refractory heat conditions exist within the combustion chamber.
- FIG. 1 is a schematic diagram showing the detailed circuitry of the control interconnected with other elements of a complete burner system
- FIG. 2 is a schematic diagram showing the detailed circuitry of one capacitor discharge spark discharge voltage generator
- FIG. 3 is a schematic diagram showing the detailed circuitry of a second capacitor discharge spark discharge voltage generator
- FIG. 4 is a schematic diagram showing the detailed circuitry of a third capacitor discharge spark discharge voltage generator
- FIG. 5 is a view of the relative positions of an oil burner nozzle, flow of air and spark electrodes indicating the manner in which the spark discharge is deflected by the air flow into the oil mist sprayed out of the nozzle so that oil cannot impinge on the electrodes.
- terminals of lines 1 and 2 connected to a 117 volt AC supply.
- a step down transformer 3, diode 4 and capacitor 5 provide a control operating voltage at thermostat switch 6 of about 24 volts DC, that is available so long as terminals of lines 1 and 2 are connected to the supply line.
- the lines 1 and 2 are connected to an ignition unit by leads 41 and 42, the circuitry of which may be that shown in FIGS. 2, 3 or 4, a burner motor 30 which may drive a blower and fuel pump and to the solenoid 31, of a combustible fluid fuel supply valve 32.
- the burner nozzle 33 is located in suitable relation to the spark gap 34 and 35.
- the line 2 is provided with a symmetrical or silicon gated switch 29, sometimes also referred to as a bidirectional triode thyristor or bidirectional controlled rectifier, for controlling current flow to the ignition unit 45, motor 30 and fuel valve solenoid 31.
- the thyristor may be of the type known under the trade name Triac.
- a cadmium sulphide cell 40 is located in sensing position to sense burner operation.
- thermostatic switch 6 in order to initiate burner operation, it is essential that thermostatic switch 6 be closed, and that cell 40 be dark.
- switch 6 closes, a positive DC potential is applied to resistors 7, 11, 17 and 27. If cell 40 is dark and so has a very high resistance, the base of NPN transistor 13 will immediately draw current through resistor 7 and zener diode 10, thereby causing transistor 13 to saturate with a collector to emitter voltage of less than 0.2 volts. When transistor 13 saturates, the base of transistor 16 cannot draw current and remains 'cut off.
- Capacitor 15, connected from the base of transistor 16 to the common line 2, provides a very short delay so that when switch 6 first closes, the base of transistor 13 will draw current before the base of transistor 16, thereby assuring that transistor 13 saturates and transistor 16 remains cut off. With transistor 16 in a cut-off state, the base of NPN transistor 28 will draw current through resistor 17, resistor 26, its own baseemitter section and the gate-anode section of bidirectional triode thyristor 29 and transistor 28 will saturate.
- thyristor 29 When transistor 28 saturates the gate of thyristor 29 will draw current from the positive DC voltage source through resistor 27 and the collectoremitter section of transistor 28, thereby allowing the anode 1 anode 2 region of thyristor 29 to conduct in either direction, depending upon the varying polarity of the AC voltage applied. When thyristor 29 conducts,
- AC voltage is applied to ignition unit 45, motor 30 and solenoid 31 thereby energizing them to operate in their normal mode.
- Solenoid 31 opens fuel valve 32
- motor 30 drives a blower fan and a full pump to cause an appropriate fuel/air mixture to issue at burner nozzle 33
- igniter unit 45 provides spark discharge voltage at electrodes 34 and 35 to cause sparks to occur between the electrodes. Electrodes 34 and 35 are located in a fixed position so that the sparks will ignite the fuel air mixture issuing at nozzle 33.
- capacitor 19 charges slowly through resistor 17 and resistor 18, the charging time being determined principallyby resistor 18 and the value of capacitor 19.
- capacitor 19 is charged to the breakdown voltage of zener diode 20
- the base of NPN transistor 21 draws current and this transistor saturates, thereby causing PNP transistor 22 to saturate.
- transistor 22 saturates it allows the base of transistor 21 to draw current through resistor 23 and the emitter collector section of transistor 22, thereby locking transistors 21 and 22 in a state of saturation.
- the base voltage of transistor 28 drops to a low value and transistor 28 cuts-off thereby cutting off thyristor 29.
- resistors 23 and 24 are both connected to the constantly available source of positive DC voltage at the junction of diode 4 and capacitor 5, the lookout circuit stays in lock-out regardless of whether or not switch 6 is open or closed.
- the lock-out circuit is reset by switch 46B which when momentarily closed first causes the base voltage of transistor 21 to drop to the voltage drop across diode 36, this being sufficiently low to cause transistor 21 to cut off and in turn causing transistor 22 to cut off also; and second, allows capacitor 19 to discharge through diode 38, resistor 37 and switch 46B.
- diode 39 The purpose of diode 39 is to provide a unilateral path for current to flow through cell 40 from resistor 18.
- the purpose of switch section 46A is to ensure that the thyristor is cut-ofl during manual reset.
- cell 40 may remain illuminated by dull or infra red light from the refractory in the combustion chamber of the burner. lf switch 6 closes while cell 40 is so illuminated, capacitor 8 and resistor 9'are shunted by the low resistance of the cell, and the beam of transistor 13 will not draw sufficient current to saturate and thus transistor 13 will not draw sufficient current to saturate and thus transistor 16 will saturate and prevent the system from turning on the thyristor.
- capacitor 8 charges through resistor 7 and the combination of resistor 9 in parallel with resistor 14, in series with the saturated collector emitter of transistor 16, results in a voltage drop due to charging current across resistor 9, sufficient to cause transistor 13 to saturate, therebycutting off transistor 16 to let the normal control sequences take place.
- switch 6 closes to provide DC voltage to the control circuit. If the cadmium sulphide cell 40 is dark, i.e., not illuminated, its resistance is very high and consequently the flip-flop control circuit consisting of components 7 through 17 will allow NPN transistor 28 to saturate thereby causing current to flow in the gate-anode 1 section of thyristor 29 which in turn causes the thyristor 29 to become bidirectionally conductive.
- the thyristor 29 When the thyristor 29 conducts, it turns on the AC voltage from terminals 1 and 2 to ignition unit 45, to blower motor 30 and to fuel valve solenoid 31, thereby causing a fuel/air mixture to issue at bumer nozzle 33 to be ignited by the spark occurring at electrodes 34 and 35, the resulting flame, in turn, illuminating cell 40.
- cell 40 When cell 40 is illuminated its internal resistance is very low and this low resistance prevents the timing and lock-out circuit consisting of components 18 through 24 from functioning. The burner will continue to run until switch 6 opens.
- Ignitor unit 46 may consist of a conventional AC line-operated transformer, a fast-sparking capacitive-discharge type of generator such as illustrated schematically in FIG. 2, or a high-energy capacitive-discharge generator such as in FIG. 3 or FIG. 4, all three types being described in detail hereunder.
- capacitor 58 charges from the positive DC point 65 through inductor 56, diode 57, capacitor 58 and the primary winding of ignition transformer 59.
- Capacitor 58 charges initially from the positive DC point 65 through inductor 56, diode 57 and on through the primary winding of transformer 59 to the negative DC point 66.
- capacitor 61 charges through resistor 60 until the breakdown voltage of gas discharge tube 62 is reached. When the gas discharge tube 62 conducts, it allows current to flow in the gate of silicon controlled rectifier 63 to make the anodecathode region of rectifier 63 conduct, thereby discharging capacitor 58 through the primary of transformer 59, the discharge current causing a very high voltage to be induced in the secondary of transformer 59.
- Diode 64 allows the flow of reverse oscillatory current after the initial discharge.
- rectifier 63 When rectifier 63 conducts, it also connects the cathode of diode 57 to the negative DC point 66.
- inductor 56 As current tries to flow from positive point 65 through inductor 56 and diode 57 to negative point 66 it is resisted by the inductive effect of inductor 56 which does not allow the magnitude of the current to reach a high value before the silicon controlled rectifier 63 is turned off by the reverse oscillatory voltage across the primary of transformer 59.
- rectifier 63 cuts off, the magnetic field around inductor 56 collapses to induce a voltage of such polarity that capacitor 58 is charged to almost twice the DC supply voltage.
- resistor 60 and capacitor 61 are selected so that the time to charge capacitor 61 to the breakdown voltage of gas tube 63 is slightly longer than the charging time of capacitor 58. Spark-discharge voltage will be produced continuously in the above described manner as long as AC voltage is connected to terminals 41 and 42.
- the spark discharge voltage from the secondary winding of transformer 59 is connected to terminals 43 and 44 and may be connected through appropriate means to the electrodes of a spark gap as illustrated, for example, in FIG. 1.
- the charging path for capacitor 84 starts at positive point 92 through diode 82 and resistor 83 to capacitor 84 and returns through primary winding 85 of transformer 91 to negative point 93.
- the values of capacitor 76 and primary 77 are such as to induce a very fast rising but short-lived high voltage in secondary winding whereas the values of capacitor 84 and winding 85 are chosen to induce a slower rising but much longer lastingvoltage in secondary winding 90, the purpose of this arrangement being to initially ionize a spark gap with the fast-rising voltage and to provide a long lasting, high energy content spark with the slower rising voltage.
- Capacitor 76 is discharged into winding 77 through the silicon controlled rectifier 81 which acts as a gate triggered by the timing network consisting of resistor 78, connected to positive point 92 to allow charging current to flow into capacitor 79 and on to negative point 93.
- the charge on capacitor 79 reaches the breakdown voltage of gas discharge tube 80, gas tube 80 conducts to allow gate current to flow in the silicon controlled rectifier 81 thus turning the rectifier on and causing capacitor 76 to discharge through winding 77.
- Capacitor 84 is discharged into winding 85 through silicon controlled rectifier 89 which is gate triggered by the timing network consisting of resistor 86 connected to positive point 92 to allow charging current to flow into capacitor 87 and on to negative point 93.
- the charge on capacitor 87' reaches the breakdown voltage of gas discharge tube 88, gas tube 88 conducts to allow current to flow in the gate of the silicon controlled rectifier 89 and thereby turning the rectifier on and causing capacitor 84 to discharge through winding 85.
- the values of resistor 78 and capacitor 79 are such that the gas tube 80 will conduct after the peak value of the DC pulses has been reached but before the DC pulse drops to zero.
- the values of resistor 86 and capacitor 87 are such that gas tube 88 conducts a few microseconds after gas tube 80, thus permitting the fast-rising output voltage to commence first.
- FIG. 4 there is shown, what may be referred to as a preferred embodiment of a spark discharge voltage generator to produce spark discharges of sufficient energy and duration for oil burner ignition.
- this voltage generator When this voltage generator is connected into the circuit described in FIG. 1, it has line voltage applied to terminals 41 and 42 as previously described.
- capacitor 163 may be charged to twice the peak value of line voltage on each cycle of the line voltage.
- Diode 10S, resistor 106, capacitor 107 and gas discharge tube 108 form a pulsing network to trigger the gate of silicon controlled rectifier 109, which triggering causes the anode-cathode section of rectifier 109 to become conductive.
- the pulse rate is deter-' mined primarily by the values of resistor 106 and capacitor 107 and may be adjusted to provide a maximum pulse rate equal to supply line frequency or as much slower a rate as may be desired, each triggering pulse occurring when the charge on capacitor 107 reaches the breakdown or ionizing voltage of gas tube 108.
- Capacitor 107 will then begin to recharge, drawing charging current through diode 105 and resistor 106 on each half cycle of line voltage when terminal 41 is positive.
- capacitor 103 discharges through rectifier 109 and the primary winding of transformer 104, the discharge current inducing a very high voltage in the secondary winding. Since capacitor 103 and the primary of transformer 104 form a parallel resonant circuit, the discharge of capacitor 103 will be the first halfcycle of an oscillation.
- the magnetic field in transformer 104 will start to fall and will induce in the primary winding a voltage of reverse polarity thus starting the second halfcycle of the same oscillation, the reverse voltage causing silicon controlled rectifier 109 to cut-off and at the same time causing capacitor 103 to charge again through diodes 101 and 102. Also on this second halfcycle of the oscillation a very high voltage of reverse polarity is induced in the secondary winding of transformer 104 thus causing the air gap between the spark electrodes to remain ionized although with a reversal of current flow.
- the high voltage induced in the secondary winding is essentially sine-wave in shape with its rate of increase from zero being determined primarily by the resonant frequency of capacitor 103 and the inductance of primary winding with the secondary winding open-circuited.
- FIG. 5 there is illustrated a nozzle 33 providing a conical spray pattern 121 which intersects the annulus of air, following arrow A, flowing around the nozzle.
- the moving airstream may be employed to deflect the spark into the oil mist of the conical pattern, as indicated at 125.
- a spark ignition voltage generator comprising a transformer having a high voltage secondary winding adapted to be connected to said electrodes, and a first primary winding connected in series with a first capacitance, first means for charging said first capacitance first means for repetitively discharging said first capacitor through said first primary winding, and a second primary winding connected in series with a second capacitance, second means for charging said second capacitance, and second means for repetitively discharging said second capacitance, second means for charging said second capacitance, and second means for repetitively discharging said second capacitance, second means for charging said second capacitance, and second means for repetitively discharging said second capacitance through said second primary winding with means for effecting the repetitive discharges of said second capacitance through said second primary winding a
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Abstract
Fuel burner spark ignition generator having a high voltage transformer secondary connected to the electrodes of a spark gap, and a primary connected in series with a capacitance, and means for charging the capacitance, and effecting a discharge of the capacitance through the transformer primary, upon the elapse of a predetermined time during the charging of the capacitance.
Description
United States Patent Potts [54] FLUID FUEL IGNITER CONTROL SYSTEM [72] inventor: William F. Potts, Liverpool, N.Y.
[73] Assignee: Liberty Combustion Corporation,
Syracuse, N.Y.
[22] Filed: May 15, 1970 [21] Appl. No.: 37,450
Related U.S. Application Data [60] Division of Ser. No. 586,593, Sept. 26, 1966,
and a continuation of Ser. No. 739,606, April,
52 U.S. c1 ..43l/264,3l7/96 51 mm ..F23q 3/00 58 Field of Search .....431/74, 264, 265, 18; 317/96 [56] References Cited UNITED STATES PATENTS 1,762,555 6/1930 Kiefer ..431/264X 2,655,209 10/1953 Newton ..431/265 1151 3,681,001 [4 1 Aug. 1,1972
2,817,395 12/1957 Lutz et al. ..431/265 X 2,985,797 5/1961 Williams et al. ..315/209 3,142,332 6/1964 Weber et al. ..317/96 3,027,933 4/1962 Hearst ..431/78 3,238,992 3/1966 Forbes ..236/21 3,291,183 12/1966 Fairley ..431/74 X 3,377,125 4/1968 3,400,302 9/ 1 968 Miller ..317/96 Primary Examiner-Frederick L. Matteson Assistant Examiner-Harry B. Ramey AttomeyF. P. Keiper [57] ABSTRACT Fuel burner spark ignition generator having a high voltage transformer secondary connected to the electrodes of a spark gap, and a primary connected in series with a capacitance, and means for charging the capacitance, and effecting a discharge of the capacitance through the transformer primary, upon the elapse of a predetermined time during the charging of the capacitance.
1 Claim, 5 Drawing Figures PAIENIEuA'uc 1 m2 SHEET 1 0F 3 INVENTOR. WILLIAM F POTTS.
ATTORNEV PATENTEDAus 1 I972 SHEET 2 [IF 3 INVENTOR. WILLIAM F. POTTS ATTORNEY FLUID FUEL IGNITER CONTROL SYSTEM This application is a division of application Ser. No. 586,593 filed Sept. 26, 1966, and a continuation of application Ser. No. 739,606 filed Apr. 2, 1968.
This invention relates to oil burner ignition and control systems, and more particularly to a system employing solid state circuitry.
Where electric spark discharges are used as a means of igniting an oil-fueled burner it is important for safety reasons and for long-life of electrodes, that the spark discharge electrodes be located, relative to the combustible mixture of air and oil, so that oil is unable to impinge upon the electrodes. This location is necessary since oil on the electrodes quickly results in the formation of carbon deposits on the electrodes. Such deposits in time build up sufficiently to bridge the electrode gap completely so that a spark discharge cannot occur. Further, as the spark discharge gap narrows from its proper gap length because of carbon formation, the spark discharge will not be deflected adequately by the flow of combustion air, and ignition will become sporadic with attendant unsafe and unpleasant conditions resulting. Accordingly a satisfactory electric ignition means for ignition of an oil burner must be able to produce a spark of sufficient energy and duration so that the rapid flow of combustion air past the spark discharge electrodes and oil nozzle into the combustion chamber will deflect the spark into the finemist of oil surrounding the cone of oil sprayed out of the oil nozzle.
Electrical spark ignition transformers and associated burner controls designed for use on ordinary oil burners, because of their nature and characteristics, have been contained in separate housings, positioned in separate locations and interconnected by additionally provided cabling. Furthermore, burners, transformers and controls are frequently manufactured by different companies and so may not be brought together as a burner system until they are installed in a heating unit, thereby leaving system performance in the hands of installation (i.e. non-factory) personnel. Additionally, both installation and servicing are complicated by interconnecting cables, separate locations for the equipments, more weight, more boxes and involve more vide an oil burner control of improved reliability with no moving parts by the use of electronic semiconductor circuitry and components.
Another object of the present invention is to assemble both the spark voltage generator and the oil burner control on a single base, contained in a single housing of sufficiently small size to allow mounting in the same space and location as occupied heretofor by an ignition transformer alone.
Yet another object of the present invention is to simplify both the installation and the servicing of oil burner ignition and control by providing in a single housing an integrated system which may be readily removed for repairs, requires no separate mounting, and needs no interconnecting cables.
A still further objective of the present invention is to provide a single unit of considerably less weight by integration of a spark voltage generator using capacitor discharge principles with a control using semiconductor devices.
The present invention is also directed to a circuit using a time-delay circuit to provide a specific period of time for burner ignition,-failing which, the system is turned off and the circuit is put in a lock-out condition requiring manual reset. The circuit is further provided with protection against ignition attempts when red-hot refractory heat conditions exist within the combustion chamber.
The above and other objects and novel features of the invention will appear more fully hereinafter from the following detailed description when taken in conjunction with the accompanying drawings. It is expressly understood that the drawings are employed for purposes of illustration only and are not designed as a definition of the limits of the invention, reference being had for this purpose to the appended claims.
In the drawings, wherein like reference characters indicate like parts:
FIG. 1 is a schematic diagram showing the detailed circuitry of the control interconnected with other elements of a complete burner system;
FIG. 2 is a schematic diagram showing the detailed circuitry of one capacitor discharge spark discharge voltage generator;
FIG. 3 is a schematic diagram showing the detailed circuitry of a second capacitor discharge spark discharge voltage generator;
FIG. 4 is a schematic diagram showing the detailed circuitry of a third capacitor discharge spark discharge voltage generator;
FIG. 5 is a view of the relative positions of an oil burner nozzle, flow of air and spark electrodes indicating the manner in which the spark discharge is deflected by the air flow into the oil mist sprayed out of the nozzle so that oil cannot impinge on the electrodes.
Referring to the drawings and particularly FIG. 1, there are shown terminals of lines 1 and 2 connected to a 117 volt AC supply. A step down transformer 3, diode 4 and capacitor 5 provide a control operating voltage at thermostat switch 6 of about 24 volts DC, that is available so long as terminals of lines 1 and 2 are connected to the supply line. The lines 1 and 2 are connected to an ignition unit by leads 41 and 42, the circuitry of which may be that shown in FIGS. 2, 3 or 4, a burner motor 30 which may drive a blower and fuel pump and to the solenoid 31, of a combustible fluid fuel supply valve 32. The burner nozzle 33 is located in suitable relation to the spark gap 34 and 35. The line 2 is provided with a symmetrical or silicon gated switch 29, sometimes also referred to as a bidirectional triode thyristor or bidirectional controlled rectifier, for controlling current flow to the ignition unit 45, motor 30 and fuel valve solenoid 31. The thyristor may be of the type known under the trade name Triac. A cadmium sulphide cell 40 is located in sensing position to sense burner operation. t
in order to initiate burner operation, it is essential that thermostatic switch 6 be closed, and that cell 40 be dark. When switch 6 closes, a positive DC potential is applied to resistors 7, 11, 17 and 27. If cell 40 is dark and so has a very high resistance, the base of NPN transistor 13 will immediately draw current through resistor 7 and zener diode 10, thereby causing transistor 13 to saturate with a collector to emitter voltage of less than 0.2 volts. When transistor 13 saturates, the base of transistor 16 cannot draw current and remains 'cut off. Capacitor 15, connected from the base of transistor 16 to the common line 2, provides a very short delay so that when switch 6 first closes, the base of transistor 13 will draw current before the base of transistor 16, thereby assuring that transistor 13 saturates and transistor 16 remains cut off. With transistor 16 in a cut-off state, the base of NPN transistor 28 will draw current through resistor 17, resistor 26, its own baseemitter section and the gate-anode section of bidirectional triode thyristor 29 and transistor 28 will saturate. When transistor 28 saturates the gate of thyristor 29 will draw current from the positive DC voltage source through resistor 27 and the collectoremitter section of transistor 28, thereby allowing the anode 1 anode 2 region of thyristor 29 to conduct in either direction, depending upon the varying polarity of the AC voltage applied. When thyristor 29 conducts,
AC voltage is applied to ignition unit 45, motor 30 and solenoid 31 thereby energizing them to operate in their normal mode. Solenoid 31 opens fuel valve 32, motor 30 drives a blower fan and a full pump to cause an appropriate fuel/air mixture to issue at burner nozzle 33, and igniter unit 45 provides spark discharge voltage at electrodes 34 and 35 to cause sparks to occur between the electrodes. Electrodes 34 and 35 are located in a fixed position so that the sparks will ignite the fuel air mixture issuing at nozzle 33.-
When transistor 16 is cut-off and cell 40 remains dark, for failure of the burner to ignite, capacitor 19 charges slowly through resistor 17 and resistor 18, the charging time being determined principallyby resistor 18 and the value of capacitor 19. When capacitor 19 is charged to the breakdown voltage of zener diode 20, the base of NPN transistor 21 draws current and this transistor saturates, thereby causing PNP transistor 22 to saturate. When transistor 22 saturates it allows the base of transistor 21 to draw current through resistor 23 and the emitter collector section of transistor 22, thereby locking transistors 21 and 22 in a state of saturation. With transistor 21 in saturation, the base voltage of transistor 28 drops to a low value and transistor 28 cuts-off thereby cutting off thyristor 29. Since resistors 23 and 24 are both connected to the constantly available source of positive DC voltage at the junction of diode 4 and capacitor 5, the lookout circuit stays in lock-out regardless of whether or not switch 6 is open or closed. The lock-out circuit is reset by switch 46B which when momentarily closed first causes the base voltage of transistor 21 to drop to the voltage drop across diode 36, this being sufficiently low to cause transistor 21 to cut off and in turn causing transistor 22 to cut off also; and second, allows capacitor 19 to discharge through diode 38, resistor 37 and switch 46B.
The purpose of diode 39 is to provide a unilateral path for current to flow through cell 40 from resistor 18. The purpose of switch section 46A is to ensure that the thyristor is cut-ofl during manual reset.
When a flame results from the ignition of the fuel/air mixture at nozzle 33, cell 40, located in a suitable fixed position, is illuminated by the flame, and the internal resistance of cell 40 decreases to a relatively low value, drawing sufficient current through resistors 17 and 18 so that capacitors 19 cannot charge sufficiently to reach the breakdown voltage of zener diode 20 with the result that the lookout circuit does not operate. So long as switch 6 is closed and cell 40 is illuminated by flame, the burner will continue to burn. During a burning period should the flame be extinguished for any reason and remain extinguished, cell 40 will go dark and capacitor 19 will charge up slowly to the point where zener diode 20 will conduct to put the system into lockout.
Under certain conditions after switch 6 has opened, cell 40 may remain illuminated by dull or infra red light from the refractory in the combustion chamber of the burner. lf switch 6 closes while cell 40 is so illuminated, capacitor 8 and resistor 9'are shunted by the low resistance of the cell, and the beam of transistor 13 will not draw sufficient current to saturate and thus transistor 13 will not draw sufficient current to saturate and thus transistor 16 will saturate and prevent the system from turning on the thyristor. After a time when cell 40 becomes dark and its internal resistance increases greatly, capacitor 8 charges through resistor 7 and the combination of resistor 9 in parallel with resistor 14, in series with the saturated collector emitter of transistor 16, results in a voltage drop due to charging current across resistor 9, sufficient to cause transistor 13 to saturate, therebycutting off transistor 16 to let the normal control sequences take place.
In operation, when heat is required, switch 6 closes to provide DC voltage to the control circuit. If the cadmium sulphide cell 40 is dark, i.e., not illuminated, its resistance is very high and consequently the flip-flop control circuit consisting of components 7 through 17 will allow NPN transistor 28 to saturate thereby causing current to flow in the gate-anode 1 section of thyristor 29 which in turn causes the thyristor 29 to become bidirectionally conductive. When the thyristor 29 conducts, it turns on the AC voltage from terminals 1 and 2 to ignition unit 45, to blower motor 30 and to fuel valve solenoid 31, thereby causing a fuel/air mixture to issue at bumer nozzle 33 to be ignited by the spark occurring at electrodes 34 and 35, the resulting flame, in turn, illuminating cell 40. When cell 40 is illuminated its internal resistance is very low and this low resistance prevents the timing and lock-out circuit consisting of components 18 through 24 from functioning. The burner will continue to run until switch 6 opens.
If the fuel/air mixture fails to ignite, cell 40 will remain at a very high resistance and the timing-lockout circuit will run to the end of the timing period at which point the lockout circuit will operate to shut the system off and keep it locked off until reset switch 46 is manually closed momentarily.
If, when switch 6 first closes, cell 40 is illuminated the flip-flop circuit will change over to put transistor 16 into saturation, thereby preventing the thyristor 29 from conducting and preventing the AC voltage from reaching motor 30, ignitor 45 and solenoid 31 as previously described. Ignitor unit 46 may consist of a conventional AC line-operated transformer, a fast-sparking capacitive-discharge type of generator such as illustrated schematically in FIG. 2, or a high-energy capacitive-discharge generator such as in FIG. 3 or FIG. 4, all three types being described in detail hereunder.
With reference to FIG. 2, when an AC voltage, nominally of 117 volts, is applied to terminals 41 and 42, the full-wave rectifier consisting of diodes 50, 51, 52 and 53 and filter resistor 54 and capacitor 55, provide a DC voltage, nominally of 150 volts, reference point 65 being positive and reference point 66 being negative.
In operation, capacitor 58 charges from the positive DC point 65 through inductor 56, diode 57, capacitor 58 and the primary winding of ignition transformer 59. Capacitor 58 charges initially from the positive DC point 65 through inductor 56, diode 57 and on through the primary winding of transformer 59 to the negative DC point 66. At the same time capacitor 61 charges through resistor 60 until the breakdown voltage of gas discharge tube 62 is reached. When the gas discharge tube 62 conducts, it allows current to flow in the gate of silicon controlled rectifier 63 to make the anodecathode region of rectifier 63 conduct, thereby discharging capacitor 58 through the primary of transformer 59, the discharge current causing a very high voltage to be induced in the secondary of transformer 59. Diode 64 allows the flow of reverse oscillatory current after the initial discharge. When rectifier 63 conducts, it also connects the cathode of diode 57 to the negative DC point 66. However, as current tries to flow from positive point 65 through inductor 56 and diode 57 to negative point 66 it is resisted by the inductive effect of inductor 56 which does not allow the magnitude of the current to reach a high value before the silicon controlled rectifier 63 is turned off by the reverse oscillatory voltage across the primary of transformer 59. When rectifier 63 cuts off, the magnetic field around inductor 56 collapses to induce a voltage of such polarity that capacitor 58 is charged to almost twice the DC supply voltage. The values of resistor 60 and capacitor 61 are selected so that the time to charge capacitor 61 to the breakdown voltage of gas tube 63 is slightly longer than the charging time of capacitor 58. Spark-discharge voltage will be produced continuously in the above described manner as long as AC voltage is connected to terminals 41 and 42. The spark discharge voltage from the secondary winding of transformer 59 is connected to terminals 43 and 44 and may be connected through appropriate means to the electrodes of a spark gap as illustrated, for example, in FIG. 1.
With reference to FIG. 3, when an AC voltage, nominally of 117 volts is connected to terminals 41 and 42, it is rectified by a full wave bridge rectifier consist ing of diodes 70, 71, 72, 73 to produce a continuous series of half-sinewave DC pulses at twice supply voltage frequency, between reference point 92 which is positive and reference point 93 which is negative. As each DC pulse increases from zero to its maximum value both capacitor 76 and capacitor 84 will charge to a value close to the peak value of the DC pulse. The charging path for capacitor 76 starts with positive point 92, through diode 741, resistor 75 through capacitor 76 and primary winding 77 of transformer 91 to negative point 93. The charging path for capacitor 84 starts at positive point 92 through diode 82 and resistor 83 to capacitor 84 and returns through primary winding 85 of transformer 91 to negative point 93. The values of capacitor 76 and primary 77 are such as to induce a very fast rising but short-lived high voltage in secondary winding whereas the values of capacitor 84 and winding 85 are chosen to induce a slower rising but much longer lastingvoltage in secondary winding 90, the purpose of this arrangement being to initially ionize a spark gap with the fast-rising voltage and to provide a long lasting, high energy content spark with the slower rising voltage. Capacitor 76 is discharged into winding 77 through the silicon controlled rectifier 81 which acts as a gate triggered by the timing network consisting of resistor 78, connected to positive point 92 to allow charging current to flow into capacitor 79 and on to negative point 93. When the charge on capacitor 79 reaches the breakdown voltage of gas discharge tube 80, gas tube 80 conducts to allow gate current to flow in the silicon controlled rectifier 81 thus turning the rectifier on and causing capacitor 76 to discharge through winding 77.
In FIG. 4 there is shown, what may be referred to as a preferred embodiment of a spark discharge voltage generator to produce spark discharges of sufficient energy and duration for oil burner ignition. When this voltage generator is connected into the circuit described in FIG. 1, it has line voltage applied to terminals 41 and 42 as previously described.
When terminal 42 is positive, capacitor will charge to the peak value, nominally volts, of the line voltage, the plate of capacitor 100 connected to the cathode of diode 101 always being positive, the other plate always being negative. When terminal 41 is positive, the line voltage adds to the charge on capacitor 100 to charge capacitor 103 to twice the peak value of line voltage, capacitor 103 charging through diode 162 and the primary of winding of transformer 104. The plate of capacitor 103 connected to the cathode of diode 1112 is positively charged while the other plate is negatively charged. Thus, in this arrangement, capacitor 163 may be charged to twice the peak value of line voltage on each cycle of the line voltage.
Diode 10S, resistor 106, capacitor 107 and gas discharge tube 108 form a pulsing network to trigger the gate of silicon controlled rectifier 109, which triggering causes the anode-cathode section of rectifier 109 to become conductive. The pulse rate is deter-' mined primarily by the values of resistor 106 and capacitor 107 and may be adjusted to provide a maximum pulse rate equal to supply line frequency or as much slower a rate as may be desired, each triggering pulse occurring when the charge on capacitor 107 reaches the breakdown or ionizing voltage of gas tube 108. Capacitor 107 will then begin to recharge, drawing charging current through diode 105 and resistor 106 on each half cycle of line voltage when terminal 41 is positive.
When the anode-cathode section of silicon controlled rectifier 109 is made conductive by the flow of gate current, capacitor 103 discharges through rectifier 109 and the primary winding of transformer 104, the discharge current inducing a very high voltage in the secondary winding. Since capacitor 103 and the primary of transformer 104 form a parallel resonant circuit, the discharge of capacitor 103 will be the first halfcycle of an oscillation. When the charge on capacitor 103 falls to zero, the magnetic field in transformer 104 will start to fall and will induce in the primary winding a voltage of reverse polarity thus starting the second halfcycle of the same oscillation, the reverse voltage causing silicon controlled rectifier 109 to cut-off and at the same time causing capacitor 103 to charge again through diodes 101 and 102. Also on this second halfcycle of the oscillation a very high voltage of reverse polarity is induced in the secondary winding of transformer 104 thus causing the air gap between the spark electrodes to remain ionized although with a reversal of current flow.
The high voltage induced in the secondary winding is essentially sine-wave in shape with its rate of increase from zero being determined primarily by the resonant frequency of capacitor 103 and the inductance of primary winding with the secondary winding open-circuited. With the high secondary voltage connected to a pair of spark electrodes, as illustrated in FIG. 1, when the secondary voltage reaches a value great enough to the air gap between the electrodes.
In FIG. 5, there is illustrated a nozzle 33 providing a conical spray pattern 121 which intersects the annulus of air, following arrow A, flowing around the nozzle. By locating the spark electrodes 34 and 35, in the airstream but outside the conical spray pattern 121, and by providing a sufficient ionization in the spark gap region, the moving airstream may be employed to deflect the spark into the oil mist of the conical pattern, as indicated at 125.
While a single embodiment with variations of the invention has been illustrated and described, it is to be understood that the i vention is not limited thereto. As various changes in t e construction and arrangement may be made without departing from the spirit of the invention, as will be apparent to those skilled in the art, reference will be had to the appended claims for a definition of the limits of the invention. I
I claim: I
1. For use in igniting an oil fueled burner of the type having a nozzle adapted to emit a cone spray of oil, an air blower adapted to produce an air stream in the general direction of the axis of the cone and electrodes forming an air spark gap positioned so that said spark gap is located immediately outside of the cone spray and within the air stream, a spark ignition voltage generator comprising a transformer having a high voltage secondary winding adapted to be connected to said electrodes, and a first primary winding connected in series with a first capacitance, first means for charging said first capacitance first means for repetitively discharging said first capacitor through said first primary winding, and a second primary winding connected in series with a second capacitance, second means for charging said second capacitance, and second means for repetitively discharging said second capacitance, second means for charging said second capacitance, and second means for repetitively discharging said second capacitance through said second primary winding with means for effecting the repetitive discharges of said second capacitance through said second primary winding a short time following the discharge of the first named capacitance, wherein said first primary winding and said first capacitance are proportioned to produce an electric arc at said electrodes of short duration and wherein said second primary winding and second capacitance are proportioned to provide for the continuation of said electrical are for a significant period whereby the said are and the resulting incandescent matter are deflected into the fuel area by the airstream to ignite the oil spray.
Claims (1)
1. For use in igniting an oil fueled burner of the type having a nozzle adapted to emit a cone spray of oil, an air blower adapted to produce an air stream in the general direction of the axis of the cone and electrodes forming an air spark gap positioned so that said spark gap is located immediately outside of the cone spray and within the air stream, a spark ignition voltage generator comprising a transformer having a high voltage secondary winding adapted to be connected to said electrodes, and a first primary winding connected in series with a first capacitance, first means for charging said first capacitance first means for repetitively discharging said first capacitor through said first primary winding, and a second primary winding connected in series with a second capacitance, second means for charging said second capacitance, and second means for repetitively discharging said second capacitance, second means for charging said second capacitance, and second means for repetitively discharging said second capacitance through said second primary winding with means for effecting the repetitive discharges of said second capacitance through said second primary winding a short time following the discharge of the first named capacitance, wherein said first primary winding and said first capacitance are proportioned to produce an electric arc at said electrodes of short duration and wherein said second primary winding and second capacitance are proportioned to provide for the continuation of said electrical arc for a significant period whereby the said arc and the resulting incandescent matter are deflected into the fuel area by the airstream to ignite the oil spray.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US3745070A | 1970-05-15 | 1970-05-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3681001A true US3681001A (en) | 1972-08-01 |
Family
ID=21894417
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US37450A Expired - Lifetime US3681001A (en) | 1970-05-15 | 1970-05-15 | Fluid fuel igniter control system |
Country Status (1)
Country | Link |
---|---|
US (1) | US3681001A (en) |
Cited By (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3716758A (en) * | 1971-03-12 | 1973-02-13 | Fiat Spa | Thyristor ignition control device |
US3889160A (en) * | 1972-09-06 | 1975-06-10 | Braun Ag | Spark-producing arrangement for a lighter with a battery |
US3949273A (en) * | 1974-06-20 | 1976-04-06 | Sundstrand Corporation | Burner ignition system |
US4382773A (en) * | 1979-06-05 | 1983-05-10 | Societe Bourguignonne De Mecanique | Safety ignition device notably for burner valve |
US5561350A (en) * | 1988-11-15 | 1996-10-01 | Unison Industries | Ignition System for a turbine engine |
US5754011A (en) * | 1995-07-14 | 1998-05-19 | Unison Industries Limited Partnership | Method and apparatus for controllably generating sparks in an ignition system or the like |
US6292347B1 (en) * | 1998-08-04 | 2001-09-18 | Stmicroelectronics S.A. | Electric arc generation circuit |
US6449138B2 (en) * | 1998-05-12 | 2002-09-10 | Miller Europe S.P.A. | Electric gas-lighter |
US6670777B1 (en) | 2002-06-28 | 2003-12-30 | Woodward Governor Company | Ignition system and method |
US20050276000A1 (en) * | 2004-06-15 | 2005-12-15 | Wilmot Theodore S | Solid state turbine engine ignition exciter having elevated temperature operational capabiltiy |
US20060257805A1 (en) * | 2005-05-12 | 2006-11-16 | Honeywell International Inc. | Adaptive spark ignition and flame sensing signal generation system |
US20070188971A1 (en) * | 2006-02-15 | 2007-08-16 | Honeywell International Inc. | Circuit diagnostics from flame sensing ac component |
US20070224557A1 (en) * | 2006-03-22 | 2007-09-27 | I-Hua Huang | Controller for re-igniting |
US20090009344A1 (en) * | 2007-07-03 | 2009-01-08 | Honeywell International Inc. | Flame rod drive signal generator and system |
US20090136883A1 (en) * | 2007-07-03 | 2009-05-28 | Honeywell International Inc. | Low cost high speed spark voltage and flame drive signal generator |
US20100013644A1 (en) * | 2005-05-12 | 2010-01-21 | Honeywell International Inc. | Flame sensing voltage dependent on application |
US20100265075A1 (en) * | 2005-05-12 | 2010-10-21 | Honeywell International Inc. | Leakage detection and compensation system |
US9494320B2 (en) | 2013-01-11 | 2016-11-15 | Honeywell International Inc. | Method and system for starting an intermittent flame-powered pilot combustion system |
US10042375B2 (en) | 2014-09-30 | 2018-08-07 | Honeywell International Inc. | Universal opto-coupled voltage system |
US10208954B2 (en) | 2013-01-11 | 2019-02-19 | Ademco Inc. | Method and system for controlling an ignition sequence for an intermittent flame-powered pilot combustion system |
US10288286B2 (en) | 2014-09-30 | 2019-05-14 | Honeywell International Inc. | Modular flame amplifier system with remote sensing |
US10402358B2 (en) | 2014-09-30 | 2019-09-03 | Honeywell International Inc. | Module auto addressing in platform bus |
US10473329B2 (en) | 2017-12-22 | 2019-11-12 | Honeywell International Inc. | Flame sense circuit with variable bias |
US10678204B2 (en) | 2014-09-30 | 2020-06-09 | Honeywell International Inc. | Universal analog cell for connecting the inputs and outputs of devices |
US10935237B2 (en) | 2018-12-28 | 2021-03-02 | Honeywell International Inc. | Leakage detection in a flame sense circuit |
US11236930B2 (en) | 2018-05-01 | 2022-02-01 | Ademco Inc. | Method and system for controlling an intermittent pilot water heater system |
US11656000B2 (en) | 2019-08-14 | 2023-05-23 | Ademco Inc. | Burner control system |
US11739982B2 (en) | 2019-08-14 | 2023-08-29 | Ademco Inc. | Control system for an intermittent pilot water heater |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1762555A (en) * | 1926-11-18 | 1930-06-10 | Sundstrand Engineering Co | Oil burner |
US2655209A (en) * | 1950-04-07 | 1953-10-13 | David L Newton | Oil burner |
US2817395A (en) * | 1955-10-19 | 1957-12-24 | White Rodgers Company | Burner control system |
US2985797A (en) * | 1958-10-30 | 1961-05-23 | Westinghouse Electric Corp | Application of semiconductors to ignition circuitry |
US3027933A (en) * | 1959-02-05 | 1962-04-03 | Automatic Burner Corp | Oil burner construction |
US3142332A (en) * | 1962-12-14 | 1964-07-28 | American Gas Ass | Gas burner ignition system |
US3238992A (en) * | 1964-01-24 | 1966-03-08 | American Radiator & Standard | Solid-state control system |
US3291183A (en) * | 1965-09-13 | 1966-12-13 | Controls Co Of America | Spark ignition and flame sensing circuit |
US3377125A (en) * | 1966-06-16 | 1968-04-09 | American Gas Ass | Electrical ignition system for gaseous fuel burners and the like |
US3400302A (en) * | 1966-04-01 | 1968-09-03 | Ranco Inc | Electric igniter system for fuel burners and the like |
-
1970
- 1970-05-15 US US37450A patent/US3681001A/en not_active Expired - Lifetime
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1762555A (en) * | 1926-11-18 | 1930-06-10 | Sundstrand Engineering Co | Oil burner |
US2655209A (en) * | 1950-04-07 | 1953-10-13 | David L Newton | Oil burner |
US2817395A (en) * | 1955-10-19 | 1957-12-24 | White Rodgers Company | Burner control system |
US2985797A (en) * | 1958-10-30 | 1961-05-23 | Westinghouse Electric Corp | Application of semiconductors to ignition circuitry |
US3027933A (en) * | 1959-02-05 | 1962-04-03 | Automatic Burner Corp | Oil burner construction |
US3142332A (en) * | 1962-12-14 | 1964-07-28 | American Gas Ass | Gas burner ignition system |
US3238992A (en) * | 1964-01-24 | 1966-03-08 | American Radiator & Standard | Solid-state control system |
US3291183A (en) * | 1965-09-13 | 1966-12-13 | Controls Co Of America | Spark ignition and flame sensing circuit |
US3400302A (en) * | 1966-04-01 | 1968-09-03 | Ranco Inc | Electric igniter system for fuel burners and the like |
US3377125A (en) * | 1966-06-16 | 1968-04-09 | American Gas Ass | Electrical ignition system for gaseous fuel burners and the like |
Cited By (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3716758A (en) * | 1971-03-12 | 1973-02-13 | Fiat Spa | Thyristor ignition control device |
US3889160A (en) * | 1972-09-06 | 1975-06-10 | Braun Ag | Spark-producing arrangement for a lighter with a battery |
US3949273A (en) * | 1974-06-20 | 1976-04-06 | Sundstrand Corporation | Burner ignition system |
US4382773A (en) * | 1979-06-05 | 1983-05-10 | Societe Bourguignonne De Mecanique | Safety ignition device notably for burner valve |
US5561350A (en) * | 1988-11-15 | 1996-10-01 | Unison Industries | Ignition System for a turbine engine |
US6034483A (en) * | 1995-07-14 | 2000-03-07 | Unison Industries, Inc. | Method for generating and controlling spark plume characteristics |
US6353293B1 (en) | 1995-07-14 | 2002-03-05 | Unison Industries | Method and apparatus for controllably generating sparks in an ignition system or the like |
US20020101188A1 (en) * | 1995-07-14 | 2002-08-01 | Unison Industries, Inc. | Method and apparatus for controllably generating sparks in an ingnition system or the like |
US7095181B2 (en) | 1995-07-14 | 2006-08-22 | Unsion Industries | Method and apparatus for controllably generating sparks in an ignition system or the like |
US5754011A (en) * | 1995-07-14 | 1998-05-19 | Unison Industries Limited Partnership | Method and apparatus for controllably generating sparks in an ignition system or the like |
US6449138B2 (en) * | 1998-05-12 | 2002-09-10 | Miller Europe S.P.A. | Electric gas-lighter |
US6292347B1 (en) * | 1998-08-04 | 2001-09-18 | Stmicroelectronics S.A. | Electric arc generation circuit |
US6670777B1 (en) | 2002-06-28 | 2003-12-30 | Woodward Governor Company | Ignition system and method |
US7355300B2 (en) | 2004-06-15 | 2008-04-08 | Woodward Governor Company | Solid state turbine engine ignition exciter having elevated temperature operational capability |
US20050276000A1 (en) * | 2004-06-15 | 2005-12-15 | Wilmot Theodore S | Solid state turbine engine ignition exciter having elevated temperature operational capabiltiy |
US20100013644A1 (en) * | 2005-05-12 | 2010-01-21 | Honeywell International Inc. | Flame sensing voltage dependent on application |
US20060257805A1 (en) * | 2005-05-12 | 2006-11-16 | Honeywell International Inc. | Adaptive spark ignition and flame sensing signal generation system |
US20100265075A1 (en) * | 2005-05-12 | 2010-10-21 | Honeywell International Inc. | Leakage detection and compensation system |
US8066508B2 (en) * | 2005-05-12 | 2011-11-29 | Honeywell International Inc. | Adaptive spark ignition and flame sensing signal generation system |
US8310801B2 (en) | 2005-05-12 | 2012-11-13 | Honeywell International, Inc. | Flame sensing voltage dependent on application |
US8659437B2 (en) | 2005-05-12 | 2014-02-25 | Honeywell International Inc. | Leakage detection and compensation system |
US20070188971A1 (en) * | 2006-02-15 | 2007-08-16 | Honeywell International Inc. | Circuit diagnostics from flame sensing ac component |
US8875557B2 (en) | 2006-02-15 | 2014-11-04 | Honeywell International Inc. | Circuit diagnostics from flame sensing AC component |
US20070224557A1 (en) * | 2006-03-22 | 2007-09-27 | I-Hua Huang | Controller for re-igniting |
US20090009344A1 (en) * | 2007-07-03 | 2009-01-08 | Honeywell International Inc. | Flame rod drive signal generator and system |
US20090136883A1 (en) * | 2007-07-03 | 2009-05-28 | Honeywell International Inc. | Low cost high speed spark voltage and flame drive signal generator |
US8085521B2 (en) | 2007-07-03 | 2011-12-27 | Honeywell International Inc. | Flame rod drive signal generator and system |
US8300381B2 (en) | 2007-07-03 | 2012-10-30 | Honeywell International Inc. | Low cost high speed spark voltage and flame drive signal generator |
US9494320B2 (en) | 2013-01-11 | 2016-11-15 | Honeywell International Inc. | Method and system for starting an intermittent flame-powered pilot combustion system |
US10429068B2 (en) | 2013-01-11 | 2019-10-01 | Ademco Inc. | Method and system for starting an intermittent flame-powered pilot combustion system |
US10208954B2 (en) | 2013-01-11 | 2019-02-19 | Ademco Inc. | Method and system for controlling an ignition sequence for an intermittent flame-powered pilot combustion system |
US11719436B2 (en) | 2013-01-11 | 2023-08-08 | Ademco Inc. | Method and system for controlling an ignition sequence for an intermittent flame-powered pilot combustion system |
US11268695B2 (en) | 2013-01-11 | 2022-03-08 | Ademco Inc. | Method and system for starting an intermittent flame-powered pilot combustion system |
US10402358B2 (en) | 2014-09-30 | 2019-09-03 | Honeywell International Inc. | Module auto addressing in platform bus |
US10678204B2 (en) | 2014-09-30 | 2020-06-09 | Honeywell International Inc. | Universal analog cell for connecting the inputs and outputs of devices |
US10042375B2 (en) | 2014-09-30 | 2018-08-07 | Honeywell International Inc. | Universal opto-coupled voltage system |
US10288286B2 (en) | 2014-09-30 | 2019-05-14 | Honeywell International Inc. | Modular flame amplifier system with remote sensing |
US10473329B2 (en) | 2017-12-22 | 2019-11-12 | Honeywell International Inc. | Flame sense circuit with variable bias |
US11236930B2 (en) | 2018-05-01 | 2022-02-01 | Ademco Inc. | Method and system for controlling an intermittent pilot water heater system |
US11719467B2 (en) | 2018-05-01 | 2023-08-08 | Ademco Inc. | Method and system for controlling an intermittent pilot water heater system |
US10935237B2 (en) | 2018-12-28 | 2021-03-02 | Honeywell International Inc. | Leakage detection in a flame sense circuit |
US11656000B2 (en) | 2019-08-14 | 2023-05-23 | Ademco Inc. | Burner control system |
US11739982B2 (en) | 2019-08-14 | 2023-08-29 | Ademco Inc. | Control system for an intermittent pilot water heater |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3681001A (en) | Fluid fuel igniter control system | |
US3425780A (en) | Fluid fuel igniter control system | |
US3377125A (en) | Electrical ignition system for gaseous fuel burners and the like | |
JPS5838696B2 (en) | fuel igniter | |
US3877864A (en) | Spark igniter system for gas appliance pilot ignition | |
CA1051768A (en) | Spark ignited recycling ignition system with interlocking gas valve control | |
US3975136A (en) | Burner control system | |
US3766441A (en) | Controlling and monitoring combustible gases | |
US3529910A (en) | Reignite system | |
US2544477A (en) | Spark type ignition system for combustion engines | |
US3589848A (en) | Oil burner control system | |
US3938937A (en) | Fuel ignition control arrangement | |
US3726630A (en) | Flame ignition | |
US4161387A (en) | Detection devices especially for the detection of flames | |
US3718423A (en) | Automatic fuel ignition system | |
US4231732A (en) | Gas burner control system | |
US3441356A (en) | Pulsed spark gas ignition and fuel control system | |
US4535380A (en) | Ignition system | |
US3734676A (en) | Electrically energizable control system for a fuel burner | |
US3806305A (en) | Solid state spark ignition circuit with automatic shut-off | |
US3561900A (en) | Igniter system | |
US3514240A (en) | Fluid fuel ignition control system | |
US3920376A (en) | Control system for a fuel burner | |
US3142332A (en) | Gas burner ignition system | |
US3510236A (en) | Ignition control |