US2684115A - Fuel burner safety control using flame conduction - Google Patents

Fuel burner safety control using flame conduction Download PDF

Info

Publication number
US2684115A
US2684115A US103767A US10376749A US2684115A US 2684115 A US2684115 A US 2684115A US 103767 A US103767 A US 103767A US 10376749 A US10376749 A US 10376749A US 2684115 A US2684115 A US 2684115A
Authority
US
United States
Prior art keywords
flame
winding
anode
saturating
burner
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
Application number
US103767A
Inventor
Jr Fred E Cairns
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.)
General Controls Co
Original Assignee
General Controls Co
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 General Controls Co filed Critical General Controls Co
Priority to US103767A priority Critical patent/US2684115A/en
Application granted granted Critical
Publication of US2684115A publication Critical patent/US2684115A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N5/00Systems for controlling combustion
    • F23N5/02Systems for controlling combustion using devices responsive to thermal changes or to thermal expansion of a medium
    • F23N5/12Systems for controlling combustion using devices responsive to thermal changes or to thermal expansion of a medium using ionisation-sensitive elements, i.e. flame rods
    • F23N5/123Systems for controlling combustion using devices responsive to thermal changes or to thermal expansion of a medium using ionisation-sensitive elements, i.e. flame rods using electronic means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N2229/00Flame sensors
    • F23N2229/12Flame sensors with flame rectification current detecting means

Definitions

  • This invention relates to a burner control for automatically opening a burner valve upon establishment of a pilot flame, and for automatically causing the burner valve to close upon extinguishment of a pilot flame.
  • This automatic control in this instance, is effected by utilizing the electric conductivity of a flame; thus, the pilot flame is made a part of an electric circuit that controls the flow of current to an electrically operated valve supplying fuel to the main burner.
  • the single figure is a diagrammatic representation of a system incorporating the invention.
  • a main burner l is shown supplied with gaseous fuel from a conduit 2.
  • This conduit 2 is controlled by a Passage of fuel to the main burner I is controlled by an eleetromagnetically operated valve 4.
  • a pilot burner is arranged in proximity to the main burner l, and is connected to the conduit 2 between the valves 3 and 4.
  • the pilot burner 5 is shown somewhat exaggerated in size in relation to the main burner I.
  • the electromagnetically operated Valve 4 has a circuit energized by a secondary winding 43 of a transformer 33.
  • the transformer 33 may be 2 Claims. (Cl. 158--123) of the cored type.
  • thermostatically operated switching means 25 In this energization circuit are thermostatically operated switching means 25, a limit control switching means 26, and two series connected coil sections ll and 32.
  • the coil sections 4! and 42 are respectively wound upon branch legs of a core of a saturable reactor 40.
  • a primary transformer winding 34 of the transformer 33 may be connected to a source of alternating current supplied by mains 12.
  • the supply of energy is controlled by a circuit controller 35.
  • a saturating coil 36 is wound upon the central leg of the core oil.
  • the saturable reactor 4% is such that when its core so is unsaturated, the combined impedance of the coils 4i and 42 is sufliciently high to prevent operation of the electromagnetically operated valve 4.
  • the reactance oi the coils ill and A2 is reduced, and the valve i may be operated by a substantial alternating current.
  • flame electrodes 38 and 3! control an electronic emission device 6, the output circuit of which includes the saturating winding 35.
  • the electronic emission device 5 includes a cathode 1 indirectly heated by heater 8, an anode 9, and a control electrode Ill.
  • the cathode l of the electronic emission device 6 is connected to an intermediate point of another secondary transformer winding 32 of the transformer 33.
  • One terminal of this winding 32 is connected through the saturating coil 36 to the anode ii.
  • a bypass condenser 39 shunts the coil St.
  • the other terminal of this winding 32 is connected to the control electrode It by way of a high resistance 37.
  • a grid leak condenser 38 bridges this resistance. Energy is transmitted to the secondary winding 32 upon energization of the primary winding 34.
  • the cathode heater 8 is connected across a section of the secondary winding 32.
  • the pilot flame H In order to make it possible for current to flow in the output circuit of the electronic emission device 6 and to pass a saturating current through the coil 36 to operate the valve 4, the pilot flame H must be in existence. Under such circumstances, the flame electrodes 38 and ti cause the control electrode to assume a positive potential during that half cycle in which the anode 9 is positive.
  • the electrodes 30 and 31 are arranged to be in the flame ll and in the direction of flame propagation.
  • electrode .30 is nearer the root of the flame H, and electrode 3
  • Electrode 30 is directly connected to the control electrode Ii), and theelectrode 3! is similarly directly connected to'the anode 9.
  • the pilot flame l I when in existence, provides .a conducting medium to complete .an electrical conducting path between the .anode 3 and the The arrangement of the electrodes 3G and 3! is such that the current flows quite readily through the flame ll fromanode 9 to the control electrode if].
  • the control electrode 10 then assumes the potential of the anode 9 when the anode is positive.
  • a rectified current flows between the oathode l and the anode 3 in response to the existence of a pilot flame l i.
  • This space current energizes the saturating coil 35, and the saturation .of the core permits operation-of the valve means 4.
  • Initiation of the operation of the system requires opening of the valve .3 and the closing of the circuit controller 35. Assuming pilot .flame H to be in existence, and the switching devices 25 and 2% closed, the main burner is supplied with fuel and may be lighted by the pilot flame.
  • the limit switch 25 ma be arranged to .open upon a predetermined condition, such as the attainment of a definite pressure or level, or the like, and switch 25 may be caused to respond .to temperature. Forspace heating, the limit switch 26 may be omitted.
  • a control system for a main burner and a pilot burner electrically operated valvemeans for controlling the flow of fuel to .the main burner; first and second electrical transducers, each having an electrical output; a circuit for the electromagnetically operated valve means, including the output of said first electrical transducer, and a reactor coil in .series therewith; a magnetic core for said reactor .coil; .a saturating winding for saturating said magnetic core; the impedance of said reactor coil permitting effective energization of said electromagnetically operated means only when the core is substantially saturated; a circuit for said saturating winding, including the output of saidsecond-electrical transducer and an electronic emission device having a cathode, an anode, and a control electrode, said cathode, anode, and the output of said second transducer being in series with said saturating winding; means forming a biasing circuit for said electronic emission device for normally imposing a bias on said control electrode such as to prevent conduction of current
  • pair of electrodes adapted to project into the flame of said pilot burner and along the direction of flame propagation; a connection between one of said electrodes and said anode; a connection between the other of said electrodes and said control electrode; and means for energizing said transducers.
  • a control system for a main burner and a pilot burner electrically operated valve means for controlling the flow of fuel to the main burner; .a circuit for the electromagnetically operated valve means, including a first transformer winding, and a .reactorcoil in series therewith; a magnetic core for said reactor coil; a saturating winding .for saturating said magnetic core; the impedance of said reactor coil permitting ef-- fective energization of said electromagnetically operated valve means only when the core is substantially saturated; a circuit for said saturating winding, including a second transformer winding and an electronic emission device having a cathode, an anode, and a control electrode, said cathode, anode, and one portion of said second transformer winding being in series with said saturating winding; means forming a biasing circuit for said electronic emission device, comprising a resistor and another portion of said second transformer winding, said resistor and said other portion of said second transformer winding being in series with

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)

Description

y 1954 F. E. CAIRNS, JR 2,684,115
FUEL BURNER SAFETY CONTROL USING FLAME CONDUCTION Filed July 9, 1949 F250 5. cn/elva IN V EN TOR.
prime/V59 shut-off valve 3.
Patented July 20, 1954 FUEL BURNER SAFETY CONTROL USING FLAME CONDUCTION Fred E. Cairns, in, North Hollywood, Calif., assignor to General Controls 00., Glendale, Calif., a corporation of California Application July 9, 1949, Serial N o. 103,767
This invention relates to a burner control for automatically opening a burner valve upon establishment of a pilot flame, and for automatically causing the burner valve to close upon extinguishment of a pilot flame.
This automatic control, in this instance, is effected by utilizing the electric conductivity of a flame; thus, the pilot flame is made a part of an electric circuit that controls the flow of current to an electrically operated valve supplying fuel to the main burner.
It is one of the objects of this invention to utilize the conducting property of the flame in conjunction with an electronic emission device for causing an operative current to flow to the main burner valve.
It is another object of this invention to provide a control system of this character in which the rectifying property of a flame is employed in a simple and effective manner to control the supply of power to an electromagnet.
It is another object of this invention to employ flame conduction for controlling the rate of current flow in an output circuit of an electronic emission device, in which the output circuit includes a reactance that is decreased sharply in value when the flame is in existence.
This invention possesses many other advantages, and has other objects which may be made more clearly apparent from a consideration of one embodiment of the invention. For this purpose, there is shown one form in the drawings accompanying and forming part of the present specification. This form will now be described in detail, illustrating the general principles of the invention; but it is to be understood that such detailed description is not to be taken in a limiting sense, since the scope of the invention is defined by the appended claims.
The single figure is a diagrammatic representation of a system incorporating the invention.
In the system shown in the drawing, a main burner l is shown supplied with gaseous fuel from a conduit 2. This conduit 2 is controlled by a Passage of fuel to the main burner I is controlled by an eleetromagnetically operated valve 4.
A pilot burner is arranged in proximity to the main burner l, and is connected to the conduit 2 between the valves 3 and 4. The pilot burner 5 is shown somewhat exaggerated in size in relation to the main burner I.
The electromagnetically operated Valve 4 has a circuit energized by a secondary winding 43 of a transformer 33. The transformer 33 may be 2 Claims. (Cl. 158--123) of the cored type. In this energization circuit are thermostatically operated switching means 25, a limit control switching means 26, and two series connected coil sections ll and 32. The coil sections 4! and 42 are respectively wound upon branch legs of a core of a saturable reactor 40.
A primary transformer winding 34 of the transformer 33 may be connected to a source of alternating current supplied by mains 12. The supply of energy is controlled by a circuit controller 35.
A saturating coil 36 is wound upon the central leg of the core oil. The saturable reactor 4% is such that when its core so is unsaturated, the combined impedance of the coils 4i and 42 is sufliciently high to prevent operation of the electromagnetically operated valve 4. However, when the core 66 is substantially saturated, the reactance oi the coils ill and A2 is reduced, and the valve i may be operated by a substantial alternating current.
saturating current flows through the saturating coil 36 only in the event that a pilot flame i l is in existence. For this purpose, flame electrodes 38 and 3! control an electronic emission device 6, the output circuit of which includes the saturating winding 35.
The electronic emission device 5 includes a cathode 1 indirectly heated by heater 8, an anode 9, and a control electrode Ill. The cathode l of the electronic emission device 6 is connected to an intermediate point of another secondary transformer winding 32 of the transformer 33. One terminal of this winding 32 is connected through the saturating coil 36 to the anode ii. A bypass condenser 39 shunts the coil St. The other terminal of this winding 32 is connected to the control electrode It by way of a high resistance 37. A grid leak condenser 38 bridges this resistance. Energy is transmitted to the secondary winding 32 upon energization of the primary winding 34. The cathode heater 8 is connected across a section of the secondary winding 32.
During a cycle in which the right-hand terminal of the winding 32 is positive, there is a sufficient positive potential impressed upon the anode 9 to permit the passage of a space current. However, the space current is normally controlled by the control electrode H which is maintained at a negative potential. This is efiected because the left-hand terminal or" the winding 32 is negative with respect to the right-hand terminal thereof during this portion of the cycle. During that half of the cycle in which the right-hand terminal of winding 82 is negative, no space curcontrol electrode It.
rent can flow, since the cathode 1 is at a higher potential than the anode 9.
In order to make it possible for current to flow in the output circuit of the electronic emission device 6 and to pass a saturating current through the coil 36 to operate the valve 4, the pilot flame H must be in existence. Under such circumstances, the flame electrodes 38 and ti cause the control electrode to assume a positive potential during that half cycle in which the anode 9 is positive.
For this purpose, the electrodes 30 and 31 are arranged to be in the flame ll and in the direction of flame propagation. Thus, electrode .30 is nearer the root of the flame H, and electrode 3| is nearer the tip. Electrode 30 is directly connected to the control electrode Ii), and theelectrode 3! is similarly directly connected to'the anode 9.
The pilot flame l I, when in existence, provides .a conducting medium to complete .an electrical conducting path between the .anode 3 and the The arrangement of the electrodes 3G and 3! is such that the current flows quite readily through the flame ll fromanode 9 to the control electrode if].
The control electrode 10 then assumes the potential of the anode 9 when the anode is positive. Thus, a rectified current flows between the oathode l and the anode 3 in response to the existence of a pilot flame l i. This space current energizes the saturating coil 35, and the saturation .of the core permits operation-of the valve means 4.
As soon as the flame H is extinguished, either accidentally or otherwise, a conducting medium 1 between electrodes 33 and M is no longer provided, and the potential of the control electrode l6 returns to a negative value whenever the anode is positive. Thus, no substantial current can pass to the saturating winding 36,, and the valve means closes.
Initiation of the operation of the system requires opening of the valve .3 and the closing of the circuit controller 35. Assuming pilot .flame H to be in existence, and the switching devices 25 and 2% closed, the main burner is supplied with fuel and may be lighted by the pilot flame. The limit switch 25 ma be arranged to .open upon a predetermined condition, such as the attainment of a definite pressure or level, or the like, and switch 25 may be caused to respond .to temperature. Forspace heating, the limit switch 26 may be omitted.
What I claim is:
1. In a control system for a main burner and a pilot burner: electrically operated valvemeans for controlling the flow of fuel to .the main burner; first and second electrical transducers, each having an electrical output; a circuit for the electromagnetically operated valve means, including the output of said first electrical transducer, and a reactor coil in .series therewith; a magnetic core for said reactor .coil; .a saturating winding for saturating said magnetic core; the impedance of said reactor coil permitting effective energization of said electromagnetically operated means only when the core is substantially saturated; a circuit for said saturating winding, including the output of saidsecond-electrical transducer and an electronic emission device having a cathode, an anode, and a control electrode, said cathode, anode, and the output of said second transducer being in series with said saturating winding; means forming a biasing circuit for said electronic emission device for normally imposing a bias on said control electrode such as to prevent conduction of current between said anode and said cathode; a. pair of electrodes adapted to project into the flame of said pilot burner and along the direction of flame propagation; a connection between one of said electrodes and said anode; a connection between the other of said electrodes and said control electrode; and means for energizing said transducers.
.2. In a control system for a main burner and a pilot burner: electrically operated valve means for controlling the flow of fuel to the main burner; .a circuit for the electromagnetically operated valve means, including a first transformer winding, and a .reactorcoil in series therewith; a magnetic core for said reactor coil; a saturating winding .for saturating said magnetic core; the impedance of said reactor coil permitting ef-- fective energization of said electromagnetically operated valve means only when the core is substantially saturated; a circuit for said saturating winding, including a second transformer winding and an electronic emission device having a cathode, an anode, and a control electrode, said cathode, anode, and one portion of said second transformer winding being in series with said saturating winding; means forming a biasing circuit for said electronic emission device, comprising a resistor and another portion of said second transformer winding, said resistor and said other portion of said second transformer winding being in series with said cathode and said control electrode for normally imposing a Joias onsaid control electrode such as to prevent conduction of current between said anode and said cathode; a pair of electrodes adapted to project into the flame of said pilot burner and along the direction of flame propagation; a con- .nection between one of said electrodes and said anode; .a connection between the other of said electrodes and :said control electrode; an energizing transformer winding; and means magnetically coupling said energizing transformer winding with said first and second transformer windings.
References Cited ill-17116 ,file of this patent UNITED STATES PATENTS
US103767A 1949-07-09 1949-07-09 Fuel burner safety control using flame conduction Expired - Lifetime US2684115A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US103767A US2684115A (en) 1949-07-09 1949-07-09 Fuel burner safety control using flame conduction

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US103767A US2684115A (en) 1949-07-09 1949-07-09 Fuel burner safety control using flame conduction

Publications (1)

Publication Number Publication Date
US2684115A true US2684115A (en) 1954-07-20

Family

ID=22296942

Family Applications (1)

Application Number Title Priority Date Filing Date
US103767A Expired - Lifetime US2684115A (en) 1949-07-09 1949-07-09 Fuel burner safety control using flame conduction

Country Status (1)

Country Link
US (1) US2684115A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2832929A (en) * 1953-06-15 1958-04-29 Gen Controls Co Flame safety amplifier
US2898981A (en) * 1954-12-24 1959-08-11 Barber Colman Co Flame detection apparatus
US2908325A (en) * 1954-10-27 1959-10-13 Baso Inc Control apparatus
US2964686A (en) * 1954-12-06 1960-12-13 Thomas E Maddox Fuel burning safety devices
US3462233A (en) * 1967-12-01 1969-08-19 Penn Controls Fuel burner control utilizing silicon controlled rectifier
US4457692A (en) * 1983-08-22 1984-07-03 Honeywell Inc. Dual firing rate flame sensing system
US4552528A (en) * 1983-04-07 1985-11-12 Societe Anonyme: Construction Electriques R.V. Current generator for the supply and detection of operation of a gas burner and control device applying same
US20070224558A1 (en) * 2006-03-08 2007-09-27 American Flame, Inc. Gas flow and combustion control system
US9546788B2 (en) * 2012-06-07 2017-01-17 Chentronics, Llc Combined high energy igniter and flame detector

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1809280A (en) * 1928-05-26 1931-06-09 Westinghouse Electric & Mfg Co Safety system
US2106249A (en) * 1933-09-27 1938-01-25 Cosma Lab Company Flame sensitive current controlling article
US2112736A (en) * 1935-12-18 1938-03-29 Gen Electric Flame detector
US2170497A (en) * 1936-01-29 1939-08-22 Honeywell Regulator Co Fuel combustion control system
US2243071A (en) * 1939-04-01 1941-05-27 Gen Electric Furnace control system
US2260977A (en) * 1940-08-14 1941-10-28 Brown Instr Co Control apparatus
US2299501A (en) * 1941-03-01 1942-10-20 Gen Electric Control system
US2306578A (en) * 1938-06-17 1942-12-29 Milwaukee Gas Specialty Co Control apparatus
US2343001A (en) * 1936-01-02 1944-02-29 Theodore A Cohen Control apparatus
US2374610A (en) * 1942-06-02 1945-04-24 Bristol Company Control apparatus
US2379873A (en) * 1943-01-09 1945-07-10 Honeywell Regulator Co Electronic control device
US2379872A (en) * 1943-01-09 1945-07-10 Honeywell Regulator Co Electronic control apparatus
US2455350A (en) * 1942-07-11 1948-12-07 Honeywell Regulator Co Control device

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1809280A (en) * 1928-05-26 1931-06-09 Westinghouse Electric & Mfg Co Safety system
US2106249A (en) * 1933-09-27 1938-01-25 Cosma Lab Company Flame sensitive current controlling article
US2112736A (en) * 1935-12-18 1938-03-29 Gen Electric Flame detector
US2343001A (en) * 1936-01-02 1944-02-29 Theodore A Cohen Control apparatus
US2170497A (en) * 1936-01-29 1939-08-22 Honeywell Regulator Co Fuel combustion control system
US2306578A (en) * 1938-06-17 1942-12-29 Milwaukee Gas Specialty Co Control apparatus
US2243071A (en) * 1939-04-01 1941-05-27 Gen Electric Furnace control system
US2260977A (en) * 1940-08-14 1941-10-28 Brown Instr Co Control apparatus
US2299501A (en) * 1941-03-01 1942-10-20 Gen Electric Control system
US2374610A (en) * 1942-06-02 1945-04-24 Bristol Company Control apparatus
US2455350A (en) * 1942-07-11 1948-12-07 Honeywell Regulator Co Control device
US2379873A (en) * 1943-01-09 1945-07-10 Honeywell Regulator Co Electronic control device
US2379872A (en) * 1943-01-09 1945-07-10 Honeywell Regulator Co Electronic control apparatus

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2832929A (en) * 1953-06-15 1958-04-29 Gen Controls Co Flame safety amplifier
US2908325A (en) * 1954-10-27 1959-10-13 Baso Inc Control apparatus
US2964686A (en) * 1954-12-06 1960-12-13 Thomas E Maddox Fuel burning safety devices
US2898981A (en) * 1954-12-24 1959-08-11 Barber Colman Co Flame detection apparatus
US3462233A (en) * 1967-12-01 1969-08-19 Penn Controls Fuel burner control utilizing silicon controlled rectifier
US4552528A (en) * 1983-04-07 1985-11-12 Societe Anonyme: Construction Electriques R.V. Current generator for the supply and detection of operation of a gas burner and control device applying same
US4457692A (en) * 1983-08-22 1984-07-03 Honeywell Inc. Dual firing rate flame sensing system
US20070224558A1 (en) * 2006-03-08 2007-09-27 American Flame, Inc. Gas flow and combustion control system
US9546788B2 (en) * 2012-06-07 2017-01-17 Chentronics, Llc Combined high energy igniter and flame detector

Similar Documents

Publication Publication Date Title
US2112736A (en) Flame detector
US2684115A (en) Fuel burner safety control using flame conduction
NL6612620A (en)
US2640920A (en) Safety fuel burner control system utilizing flame conduction
US2260977A (en) Control apparatus
US2384696A (en) Control system
US2081091A (en) Burner control system
US3384440A (en) Ignition devices
US2691705A (en) Safety control system for fuel burners
US2464945A (en) Control system for fluid pressure servomotors
US3938937A (en) Fuel ignition control arrangement
US2765119A (en) Saturable core reactor with thermistor control
US2408954A (en) Fuel supply system
US2357609A (en) Control system
US3042781A (en) Control circuit
US2449185A (en) Safety control system for fuel burners
US2395666A (en) Electric ignition control
US3174528A (en) Staring burner control system
US3501253A (en) Automatic ignition systems
US2379873A (en) Electronic control device
US2625216A (en) Control and ignition system for fuel burners
US2181970A (en) Fuel combustion control system
US2177883A (en) Electric discharge apparatus
US2529740A (en) Safety control system for fluid fuel burners
US3845582A (en) Control device for gas burner