US2286610A - Safety pilot burner - Google Patents

Safety pilot burner Download PDF

Info

Publication number
US2286610A
US2286610A US300438A US30043839A US2286610A US 2286610 A US2286610 A US 2286610A US 300438 A US300438 A US 300438A US 30043839 A US30043839 A US 30043839A US 2286610 A US2286610 A US 2286610A
Authority
US
United States
Prior art keywords
pilot burner
apertures
jet
fuel
relay
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
US300438A
Inventor
Theodore B Focke
Allen K Phelps
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.)
Perfection Stove Co
Original Assignee
Perfection Stove 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 Perfection Stove Co filed Critical Perfection Stove Co
Priority to US300438A priority Critical patent/US2286610A/en
Application granted granted Critical
Publication of US2286610A publication Critical patent/US2286610A/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
    • F23N5/10Systems for controlling combustion using devices responsive to thermal changes or to thermal expansion of a medium using thermocouples
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23QIGNITION; EXTINGUISHING-DEVICES
    • F23Q9/00Pilot flame igniters
    • F23Q9/08Pilot flame igniters with interlock with main fuel supply
    • F23Q9/12Pilot flame igniters with interlock with main fuel supply to permit the supply to the main burner in dependence upon existence of pilot flame
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N2239/00Fuels
    • F23N2239/06Liquid fuels

Definitions

  • This invention relates, generally, to fluid fuel combustion apparatus, and it has to do particularly with a novel form of pilot burner for use with such apparatus and a safety control system involving the same.
  • our invention has, as its primary object, to provide, in combination with one or more main fluid fuel burners, a unique fluid fuel pilot burner and a control system involving the same by which a supply of fuel to the main burner or burners is permittedonly in case the pilot burner is functioning properly to light said main burner or burners.
  • Another object is to provide a convenient and reliable lighting means for the pilot burner; and, according to one form of the invention, to combine with such lighting means a control that acts to shut off the fuel supply to the pilot burner in case its flame accidentally becomes extinguish l, and which serves to re-establish the fuel supply to the pilot burner upon subsequent actuation of the lighting means.
  • a plural jet pilot burner including means for effectively communicating combustion from one jet to another; to .combine therewith an igniter arranged in lighting relation to one of said jets, and a heat energized instrumentality that controls the supply of fuel to the main burner or I" burners and is arranged in heat receiving relation to another jet, and, still more limitedly, to provide, in association with a plurality of main burners, an elongated pilot burner possessing the foregoing features arranged with the igniter at one end, the heat energized instrumentality at the other, and the lighting jets for the main burners therebetween so as to insure against delivery of fuel to the main burners unless the pilot burner is properly functioning.
  • the invention in its broader'aspect, isappli cable to one or more main burners, or to, a multiple main burner of two or more independent sections or units.
  • a mixture of primary air and gas is supplied to each burner or unit through an inducer 5 whose outer end incorporates the usual shutter-con trolled air mixer B into which fluid, fuel or gas is projected through a nipple 9 from a manifold 10.
  • each inducer 5, with a burner mounted thereon is supported through The pilot burner assemsupported from the base l2, in operative relation to the main burners, by standards iii to the upper ends of which are connected. by bolts i3, brackets body and cover with a part of the cover broken away;
  • Fig. 5 is a section on the line 55 of Fig. 4 on a scale twice that of the latter view;
  • apertures are relatively small and comparatively.
  • the front wall of' the cover is cut away at its ends, as indicated atfll, and intermediate its ends is provided with a notch s2, soas not to interfere with the lighting jets projected from the apertures 26, 2'! and 28.
  • include laterally extending flanges or ledges 48 and ll, respectively, and supported by a mounting 48 from the ledge 48 is an electric igniter designated generally by the reference numeral 85.
  • the igniter consists of a body 88 of suitable insulating refractory material, and a resistor coil 81 disposed within a groove thereof.
  • the ends of the coil are connected to screws 48 that extend through the body and have nuts applied to their ends, thereby to provide binding posts-for
  • the parts are so arranged as to dispose the igniter in line with the aperture 34 so that a jet of fuel issuing therefrom will impinge against the resistance coil and be ignited thereby when said coil is energized.
  • combustion from this igniting jet will be instantly transmitted through fuel escaping from the adjacent slot 38 to the jet of fuel projected from the aperture 26.
  • the flame from the last mentioned jet is propagated along the line of perforations 28 beneath the cover 30 to the jets of fuel issuing from the apertures 21, and 28, from the latter of which combustion is transmitted by the fuel issuing from the slot 31 to that issuing from the aperture 35, the latter providing what may be termed the heating jet.
  • is a heat energized instrumentality or thermosensitive element 58, the one illustrated being a thermocouple which has the capacity to generate electric current when heated. This element is arranged for impingement against it of the aforesaid heating J'et.
  • fluid fuel is supplied from a suitable source to the main burners I, 2 and 3 through a pipe 55 that is connected to the manifold l0.
  • a pipe 55 that is connected to the manifold l0.
  • an automatic valve 56 that is biased toward closed position, as by gravity, and is adapted to be opened by electrical means, such as a solenoid 51.
  • a pipe 58 is shown as leading from the pipe 55, in advance of the valve 58, to the pilot burner, and the supply pipe may be equipped with a manual valve 58 in advance of its connection with the pipe 58.
  • the 60 designates a transformer, the primary winding 80 of which is in the house circuit that may be of the usual I I8 volts and is represented by the conductors GI and 82.
  • the secondary winding 88 of the transformer is placed in circuit with the igniter 45 through conductors 83 and 64, the latter including a push button switch 85.
  • the thermocouple 50 is placed in' circuit with the winding of a relay I0, whose armature H is normally held away from the core of the relay by a light spring 72. When energized, the relay moves the armature ll into engagement with a contact 13. represents a thermostatic switch or so-called room thermostat that is subjected to the heat output of the combustion apparatus or furnace.
  • the room thermostat under the influence of a temperature of given value for the maintenance of which it is set, and with the main burners out of operation and only the pilot burner functioning, is in condition to maintain the circuit in which it is included open.
  • gas will issue from the several :Iet apertures of the pilot burner, the igniting jet impinging against the resistance coil of the .igniter 45.
  • the push button switch-65 is closed thereby to establish a circuit through the secondary winding of the transformer, the conductor 63, igniter 45, and conductor 84.
  • thermocouple 50 When the coil becomes sufliciently hot, it will ignite the gas issuing from the aperture 84, and combustion will be communicated therefrom across the slot 38 to the aperture 26 and along the row of perforations 28 to the apertures 21 and 28 and across the slot 81 to the aperture 35, the flame of the jet issuing from the latter aperture impinging against the thermocouple 50. When sufficiently heated, the thermocouple will generate current in the circuit represented by the conductors 81 and 68 and including the winding of the relay 10, thereby to energize the relay and attract the armature II so as to engage it with the contact 13.
  • the movable contact member I6 of said thermostat will swing into engagement with the contact member 11, thereby to close the circuit including, besides the room thermostat, the secondary winding of the transformer, the solenoid 51, and the armature of the relay 10, said circuit being represented by the conductors I8, 18, and 8
  • the relay III will function to maintain the circuit including the room thermostat and the solenoid 5! closed at the relay, thus placing the automatic valve 55 solely under the influence of the room thermostat to be opened when occasion requires.
  • a pipe 58" that conducts gas from the supply pipe 55 to the pilot burner includes an automatic valve 85 that is biased toward closed position and is adapted to be opened by a solenoid 88.
  • thermocouple 88 is arranged in intimate heat exchanging relation to the igniter 45 and is desirably in the path of the Jet of gas issuing from the aperture 34.
  • the thermocouple 88 is placed in circuit with the winding of a relay 8
  • the armature 82 will be at-' tracted and swung into engagement with a contact member 84.
  • are placed in circuit with the secondary winding 60 of the transformer through conductors 86, 81 and88.
  • the supply of gas to the pilot burner will be shut off by the automatic valve 85.
  • the push button switch aaeaeio 65 is closed thereby to energize the igniter d5.
  • the relay 9! will be energized, thereby to swing the aperture 92 into engagement with the contact 94, establishing the circuit that includes the secondary winding of the transformer and the winding of the solenoid 86.
  • the valve 85 Upon energization of the solenoid 88, the valve 85 will be opened to supply fuel to the pilot burner, and when the pilot burner is once in operation, the heat from the flame of the igniting jet will maintain the thermocouple 88 hot, thereby to supply current to the relay 9! and maintain closed the circuit including the solenoid 86 that acts, under such conditions, to hold the automatic valve 85 open. Should the flame of the pilot burner become accidentally extinguished, the thermocouple 88 will cool, thereby to deenergize the relay and open the circuit that includes the winding of the solenoid 88 and, as a consequence, allow the valve 85 to close.
  • a safety pilot burner comprising an elongated hollow bcdy having jet apertures spaced therealong and rows of perforations between apertures, a stationary cover extending along the body and permanently overhanging said perforations and cut away adjacent each aperture to prevent interference with the jet projected therefrom, and means for admitting fluid fuel to the body.
  • a safety pilot burner comprising a hollow elongated body having a plurality of jet apertures in its front wall spaced apart longitudinally thereof, one of said apertures being adjacent each end of the body, said front wall being provided also with perforations in series between said apertures, a stationary cover extending along the body and permanently overhanging said perforations and cut away adjacent each aperture to prevent interference with the jet issuing therefrom, the rear wall of the body being provided with apertures substantially diametrically opposite those apertures of the front wall that are adjacent the ends of the body, the bottom wall of the body having openings between the apertures of the rear wall and the corresponding apertures of the front wall, and means for admitting fluid fuel to the body.
  • a safety pilot burner comprising a hollow tures, a stationary cover fixed with respect to the body and permanently overhanging the front wall thereof and having a part extending downwardly in opposed relation to said wall, said part being cut away opposite each aperture, the rear wall of the body being provided with apertures substantially diametrically opposite those apertures of the front wall that are adjacent the ends of the body, the bottom wall of the body having openings between the apertures of the rear wall and the corresponding apertures of the front wall, and means for admitting fluid fuel to the body.
  • a safety pilot burner comprising a hollow elongated body having a plurality of jet aperelongated body having a plurality of jet apertures in its front wall spaced apart longitudinally tures in its front wall spaced apart longitudinally.
  • one of said apertures being adjacent each end of the body, said front wall having rows of perforations between said apertures, a stationary cover permanently overhanging the front portion of the body in opposed relation to the front wall thereof and cut away opposite each aperture, the rear wall of the body being provided with apertures substantially diametrically opposite those apertures of the front wall that are adjacent the ends of the body, the bottom wall of the body having openings between the corresponding apertures of the front and rear walls, supporting means secured to the body, one in the region of each of the apertures of the rear wall, and means for admitting fluid fuel to the body.
  • a safety pilot burner comprising a straight cylindricaltubular body closed at its ends, an inducer communicating with the body for admitting a fluid fuel mixture thereto, the front wall of the body being provided with jet apertures spaced apart longitudinally thereof, one of said apertures being located adjacent each end of the body, said front wall being provided also with perforations in series between said apertures, the rear wall of the body having jet apertures substantially diametrically opposite the apertures of the front wall that are adjacent the ends of the body while the bottom wall of the body has openings between the corresponding apertures of the front and rear walls, a cover fixedly attached to the top of the body and permanently overhanging the front side thereof and including a wall spaced from the front wall of the body in opposed relation thereto, said wall of the cover being cut away adjacent eachaperture of the front wall of the body to prevent interference with a jet issuing therefrom, and brackets secured to the body adjacentthe ends thereof, each bracket including a supporting part in the region of one of the apertures in the rear wall of the body.

Description

June 16, 1942. T. B. FOCKE ET AL SAFETY PILOT BURNER 7 Filed 001;; 20, 1939 3 Sheets-Shed l ATTORNEYS.
FIG. 2.
' INVENTORS. THEODORE B. FOCKE' ALLEN. K PHELPS June 16, 1942.
T. B. FOCKE ET AL SAFETY PILOT BURNER Filed Oct. 20, 1939 3 Sheeis-Shegt 2 FIG. 3.
INVENTORS. TH EODOBE- 5. FOCKE ALLEN I. PHELPS M,M m
ATTORNEYS.
June 16, 1942. T. B. FOCKE ET AL 2,286,610
SAFETY P ILOT BURNER Filed Oct. 20, 1959 3 h et s INVENTORS. THEODORE B FOCKE- BY ALLEN K. PHELPS ATTORNEYS.
Patented June 16, 1942 SAFETY PILOT BURNER Theodore B. Focke, Cleveland Heights, and Allen K. Phelps, East Cleveland, Ohio, assignors to Perfection Stove Company, Cleveland, Ohio, a
corporation of Ohio Application October 20, 1939, Serial No. 300,438
5 Claims.
This invention relates, generally, to fluid fuel combustion apparatus, and it has to do particularly with a novel form of pilot burner for use with such apparatus and a safety control system involving the same.
To the end of safety, our invention has, as its primary object, to provide, in combination with one or more main fluid fuel burners, a unique fluid fuel pilot burner and a control system involving the same by which a supply of fuel to the main burner or burners is permittedonly in case the pilot burner is functioning properly to light said main burner or burners.
Another object is to provide a convenient and reliable lighting means for the pilot burner; and, according to one form of the invention, to combine with such lighting means a control that acts to shut off the fuel supply to the pilot burner in case its flame accidentally becomes extinguish l, and which serves to re-establish the fuel supply to the pilot burner upon subsequent actuation of the lighting means.
Further and more limited objects are: to provide, in conjunctf on with one or more main burners, a plural jet pilot burner including means for effectively communicating combustion from one jet to another; to .combine therewith an igniter arranged in lighting relation to one of said jets, and a heat energized instrumentality that controls the supply of fuel to the main burner or I" burners and is arranged in heat receiving relation to another jet, and, still more limitedly, to provide, in association with a plurality of main burners, an elongated pilot burner possessing the foregoing features arranged with the igniter at one end, the heat energized instrumentality at the other, and the lighting jets for the main burners therebetween so as to insure against delivery of fuel to the main burners unless the pilot burner is properly functioning.
The foregoing objects and advantages, with others hereinafter appearing. including simplicity and economy of construction, facility of assembly and installation, reliability and durability are attained in the embodiments of the invention a diagrammatic representation of one form of the invention; and Fig. 7 is a similar view-showing.
- another form thereof.
' legs H from a base l2.
bly, designated generally by the numeral I5, is
While our invention is applicable to various kinds of combustion apparatus, we have selected as an illustration of a practical application its incorporation in the combustion apparatus of a gas fired furnace. Only such elements of the apparatus are included in the drawings as are essential to a proper disclosure of the invention, and in this connection it may be explained that the diagrams of Figs. 6 and '7 have been simplified by omitting therefrom all features ordinarily included in such control systems but which have no bearing on the instant invention.
The invention, in its broader'aspect, isappli cable to one or more main burners, or to, a multiple main burner of two or more independent sections or units. According to the illustrative embodiments herein disclosed, there are three such burners or units, designated l, 2 and 3. A mixture of primary air and gas is supplied to each burner or unit through an inducer 5 whose outer end incorporates the usual shutter-con trolled air mixer B into which fluid, fuel or gas is projected through a nipple 9 from a manifold 10. Asshown in Fig. 2, each inducer 5, with a burner mounted thereon, is supported through The pilot burner assemsupported from the base l2, in operative relation to the main burners, by standards iii to the upper ends of which are connected. by bolts i3, brackets body and cover with a part of the cover broken away; Fig. 5 is a section on the line 55 of Fig. 4 on a scale twice that of the latter view; Fig. 6
apertures are relatively small and comparatively.
closely spaced perforations 29 that provide the fuel to transmit combustion from one jet to an- 3 7 other, this end being further served by an over;- hanging cover 36 that is substantially L-sloaped;
in cross section and has the rear edge ,ofits,
wall welded or otherwise secured to thetop the burner body. The front wall of' the cover is cut away at its ends, as indicated atfll, and intermediate its ends is provided with a notch s2, soas not to interfere with the lighting jets projected from the apertures 26, 2'! and 28.
the attachment of conductors.
I joins the body 25 toward one end thereof, The
brackets 20 and 2| include laterally extending flanges or ledges 48 and ll, respectively, and supported by a mounting 48 from the ledge 48 is an electric igniter designated generally by the reference numeral 85.
The igniter consists of a body 88 of suitable insulating refractory material, and a resistor coil 81 disposed within a groove thereof. The ends of the coil are connected to screws 48 that extend through the body and have nuts applied to their ends, thereby to provide binding posts-for The parts are so arranged as to dispose the igniter in line with the aperture 34 so that a jet of fuel issuing therefrom will impinge against the resistance coil and be ignited thereby when said coil is energized. As will be readily understood, combustion from this igniting jet will be instantly transmitted through fuel escaping from the adjacent slot 38 to the jet of fuel projected from the aperture 26. The flame from the last mentioned jet is propagated along the line of perforations 28 beneath the cover 30 to the jets of fuel issuing from the apertures 21, and 28, from the latter of which combustion is transmitted by the fuel issuing from the slot 31 to that issuing from the aperture 35, the latter providing what may be termed the heating jet. Supported by the flange or ledge ll of the bracket 2| is a heat energized instrumentality or thermosensitive element 58, the one illustrated being a thermocouple which has the capacity to generate electric current when heated. This element is arranged for impingement against it of the aforesaid heating J'et.
Referring now to the diagram of Fig. 6, fluid fuel is supplied from a suitable source to the main burners I, 2 and 3 through a pipe 55 that is connected to the manifold l0. Included in the gas supply line or pipe 55 is an automatic valve 56 that is biased toward closed position, as by gravity, and is adapted to be opened by electrical means, such as a solenoid 51. A pipe 58 is shown as leading from the pipe 55, in advance of the valve 58, to the pilot burner, and the supply pipe may be equipped with a manual valve 58 in advance of its connection with the pipe 58.
60 designates a transformer, the primary winding 80 of which is in the house circuit that may be of the usual I I8 volts and is represented by the conductors GI and 82. The secondary winding 88 of the transformer is placed in circuit with the igniter 45 through conductors 83 and 64, the latter including a push button switch 85. Through conductors 81 and 88, the thermocouple 50 is placed in' circuit with the winding of a relay I0, whose armature H is normally held away from the core of the relay by a light spring 72. When energized, the relay moves the armature ll into engagement with a contact 13. represents a thermostatic switch or so-called room thermostat that is subjected to the heat output of the combustion apparatus or furnace.
According to the simplified control system herein disclosed for illustrative purposes, the room thermostat, under the influence of a temperature of given value for the maintenance of which it is set, and with the main burners out of operation and only the pilot burner functioning, is in condition to maintain the circuit in which it is included open. Assuming that the manual valve 58 is adjusted to supply fuel to the apparatus, gas will issue from the several :Iet apertures of the pilot burner, the igniting jet impinging against the resistance coil of the .igniter 45. To start the apparatus in operation, the push button switch-65 is closed thereby to establish a circuit through the secondary winding of the transformer, the conductor 63, igniter 45, and conductor 84. When the coil becomes sufliciently hot, it will ignite the gas issuing from the aperture 84, and combustion will be communicated therefrom across the slot 38 to the aperture 26 and along the row of perforations 28 to the apertures 21 and 28 and across the slot 81 to the aperture 35, the flame of the jet issuing from the latter aperture impinging against the thermocouple 50. When sufficiently heated, the thermocouple will generate current in the circuit represented by the conductors 81 and 68 and including the winding of the relay 10, thereby to energize the relay and attract the armature II so as to engage it with the contact 13. Assuming, now, that the temperature to which the room thermostat is subjected has fallen below the aforesaid given value, the movable contact member I6 of said thermostat will swing into engagement with the contact member 11, thereby to close the circuit including, besides the room thermostat, the secondary winding of the transformer, the solenoid 51, and the armature of the relay 10, said circuit being represented by the conductors I8, 18, and 8|.
It will be seen, therefore, that as long as the pilot burner is operating and heating the thermocouple 50, the relay III will function to maintain the circuit including the room thermostat and the solenoid 5! closed at the relay, thus placing the automatic valve 55 solely under the influence of the room thermostat to be opened when occasion requires.
The modification of the invention illustrated in Fig. 7 diflers from that shown in Fig. 6 only by the inclusion of an automatic valve for controlling the supply of fuel to the pilot burner, and a thermocouple, in association with the igniter 45, with its relay and necessary circuits. Therefore, in the diagram of Fig. 7, all parts corresponding to those of the diagram of Fig. 6 will be designated by the same reference numerals. In the form of the invention shown in Fig. '7, a pipe 58" that conducts gas from the supply pipe 55 to the pilot burner includes an automatic valve 85 that is biased toward closed position and is adapted to be opened by a solenoid 88. A thermocouple 88 is arranged in intimate heat exchanging relation to the igniter 45 and is desirably in the path of the Jet of gas issuing from the aperture 34. Through conductors 88 and 80, the thermocouple 88 is placed in circuit with the winding of a relay 8| whose armature 82 is held away from the core of the relay by a light spring 93. When the relay is energized, the armature 82 will be at-' tracted and swung into engagement with a contact member 84. The winding of the solenoid 86 and the armature of the relay 8| are placed in circuit with the secondary winding 60 of the transformer through conductors 86, 81 and88.
When the-parts are cold, the supply of gas to the pilot burner will be shut off by the automatic valve 85. When it is desired to set the apparatus in operation, the push button switch aaeaeio 65 is closed thereby to energize the igniter d5. When the temperature of the igniter becomes suficiently high to transmit enough heat to the thermocouple 88 to cause it to generate current, the relay 9! will be energized, thereby to swing the aperture 92 into engagement with the contact 94, establishing the circuit that includes the secondary winding of the transformer and the winding of the solenoid 86. Upon energization of the solenoid 88, the valve 85 will be opened to supply fuel to the pilot burner, and when the pilot burner is once in operation, the heat from the flame of the igniting jet will maintain the thermocouple 88 hot, thereby to supply current to the relay 9! and maintain closed the circuit including the solenoid 86 that acts, under such conditions, to hold the automatic valve 85 open. Should the flame of the pilot burner become accidentally extinguished, the thermocouple 88 will cool, thereby to deenergize the relay and open the circuit that includes the winding of the solenoid 88 and, as a consequence, allow the valve 85 to close.
Having thus described our invention, what we claim is:
1. A safety pilot burner comprising an elongated hollow bcdy having jet apertures spaced therealong and rows of perforations between apertures, a stationary cover extending along the body and permanently overhanging said perforations and cut away adjacent each aperture to prevent interference with the jet projected therefrom, and means for admitting fluid fuel to the body.
2. A safety pilot burner comprising a hollow elongated body having a plurality of jet apertures in its front wall spaced apart longitudinally thereof, one of said apertures being adjacent each end of the body, said front wall being provided also with perforations in series between said apertures, a stationary cover extending along the body and permanently overhanging said perforations and cut away adjacent each aperture to prevent interference with the jet issuing therefrom, the rear wall of the body being provided with apertures substantially diametrically opposite those apertures of the front wall that are adjacent the ends of the body, the bottom wall of the body having openings between the apertures of the rear wall and the corresponding apertures of the front wall, and means for admitting fluid fuel to the body.
3. A safety pilot burner comprising a hollow tures, a stationary cover fixed with respect to the body and permanently overhanging the front wall thereof and having a part extending downwardly in opposed relation to said wall, said part being cut away opposite each aperture, the rear wall of the body being provided with apertures substantially diametrically opposite those apertures of the front wall that are adjacent the ends of the body, the bottom wall of the body having openings between the apertures of the rear wall and the corresponding apertures of the front wall, and means for admitting fluid fuel to the body.
4. A safety pilot burner comprising a hollow elongated body having a plurality of jet aperelongated body having a plurality of jet apertures in its front wall spaced apart longitudinally tures in its front wall spaced apart longitudinally.
thereof, one of said apertures being adjacent each end of the body, said front wall having rows of perforations between said apertures, a stationary cover permanently overhanging the front portion of the body in opposed relation to the front wall thereof and cut away opposite each aperture, the rear wall of the body being provided with apertures substantially diametrically opposite those apertures of the front wall that are adjacent the ends of the body, the bottom wall of the body having openings between the corresponding apertures of the front and rear walls, supporting means secured to the body, one in the region of each of the apertures of the rear wall, and means for admitting fluid fuel to the body.
5. A safety pilot burner comprising a straight cylindricaltubular body closed at its ends, an inducer communicating with the body for admitting a fluid fuel mixture thereto, the front wall of the body being provided with jet apertures spaced apart longitudinally thereof, one of said apertures being located adjacent each end of the body, said front wall being provided also with perforations in series between said apertures, the rear wall of the body having jet apertures substantially diametrically opposite the apertures of the front wall that are adjacent the ends of the body while the bottom wall of the body has openings between the corresponding apertures of the front and rear walls, a cover fixedly attached to the top of the body and permanently overhanging the front side thereof and including a wall spaced from the front wall of the body in opposed relation thereto, said wall of the cover being cut away adjacent eachaperture of the front wall of the body to prevent interference with a jet issuing therefrom, and brackets secured to the body adjacentthe ends thereof, each bracket including a supporting part in the region of one of the apertures in the rear wall of the body.
' THEODORE B. FOCKE.
ALLEN K. PHELPS.
US300438A 1939-10-20 1939-10-20 Safety pilot burner Expired - Lifetime US2286610A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US300438A US2286610A (en) 1939-10-20 1939-10-20 Safety pilot burner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US300438A US2286610A (en) 1939-10-20 1939-10-20 Safety pilot burner

Publications (1)

Publication Number Publication Date
US2286610A true US2286610A (en) 1942-06-16

Family

ID=23159097

Family Applications (1)

Application Number Title Priority Date Filing Date
US300438A Expired - Lifetime US2286610A (en) 1939-10-20 1939-10-20 Safety pilot burner

Country Status (1)

Country Link
US (1) US2286610A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2539075A (en) * 1946-10-26 1951-01-23 L J Mueller Furnace Company Gas burner igniter
US2557927A (en) * 1951-06-26 Oven lighting system
US2715940A (en) * 1946-06-17 1955-08-23 Roper Corp Geo D Oven lighting system
US2823741A (en) * 1953-03-26 1958-02-18 Baso Inc Multiple burner control
US2850084A (en) * 1954-03-19 1958-09-02 Robertshaw Fulton Coutrols Com Electric ignition device for gaseous fuel
US2889872A (en) * 1954-03-29 1959-06-09 Gen Electric Multiple pilot control for burner systems
US3288196A (en) * 1963-02-14 1966-11-29 Vaillant Joh Kg Combined bunsen burner, more particularly for gas water heaters
US4887959A (en) * 1988-11-17 1989-12-19 Rheem Manufacturing Company Gas furnace with improved ignition
US20080289619A1 (en) * 2003-02-21 2008-11-27 Middleby Corporation Charbroiler
US20090165778A1 (en) * 2007-12-11 2009-07-02 Garland Commercial Industries Llc Energy efficient char-broiler

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2557927A (en) * 1951-06-26 Oven lighting system
US2715940A (en) * 1946-06-17 1955-08-23 Roper Corp Geo D Oven lighting system
US2539075A (en) * 1946-10-26 1951-01-23 L J Mueller Furnace Company Gas burner igniter
US2823741A (en) * 1953-03-26 1958-02-18 Baso Inc Multiple burner control
US2850084A (en) * 1954-03-19 1958-09-02 Robertshaw Fulton Coutrols Com Electric ignition device for gaseous fuel
US2889872A (en) * 1954-03-29 1959-06-09 Gen Electric Multiple pilot control for burner systems
US3288196A (en) * 1963-02-14 1966-11-29 Vaillant Joh Kg Combined bunsen burner, more particularly for gas water heaters
US4887959A (en) * 1988-11-17 1989-12-19 Rheem Manufacturing Company Gas furnace with improved ignition
US20080289619A1 (en) * 2003-02-21 2008-11-27 Middleby Corporation Charbroiler
US20090165778A1 (en) * 2007-12-11 2009-07-02 Garland Commercial Industries Llc Energy efficient char-broiler

Similar Documents

Publication Publication Date Title
US2351277A (en) Safety device
US2416766A (en) Fuel supply and ignition control for combustion apparatus
US1535240A (en) Controller for fuel igniters
US2286610A (en) Safety pilot burner
US2361530A (en) Control system for ovens
US2125473A (en) Gas burner control system
US1985991A (en) Protective system for oil burners
US2078576A (en) Gas lighter
US2150415A (en) Igniting mechanism for gas burners
US2192631A (en) Automatic fuel ignition
US2275279A (en) Automatic lighter
US2176647A (en) Fuel igniting device for burners
US2296340A (en) Safety control apparatus for gaseous fuel burners
US2263767A (en) Ignition system and pilot control
US2370205A (en) Burner control apparatus
US2438275A (en) Fuel supply control means for combustion apparatus
US2248737A (en) Pilot control
US3938936A (en) Fluid control system
US2098383A (en) Heating system
US3502419A (en) Flame-proving ignition system for gas burners
US3153440A (en) Electric igniting and fuel supply control arrangement for fuel burners
US1673404A (en) Controlling means for burners
US2157109A (en) Apparatus for controlling flow of fuel to a heating device
US2303183A (en) Thermocouple and pilot burner
US2889872A (en) Multiple pilot control for burner systems