US3918878A - Apparatus and method of ignition for combustible gases - Google Patents

Apparatus and method of ignition for combustible gases Download PDF

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US3918878A
US3918878A US389251A US38925173A US3918878A US 3918878 A US3918878 A US 3918878A US 389251 A US389251 A US 389251A US 38925173 A US38925173 A US 38925173A US 3918878 A US3918878 A US 3918878A
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gas
igniter
leads
ignition
chamber
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Warren A Rice
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Chemotronics International Inc
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23QIGNITION; EXTINGUISHING-DEVICES
    • F23Q7/00Incandescent ignition; Igniters using electrically-produced heat, e.g. lighters for cigarettes; Electrically-heated glowing plugs
    • F23Q7/06Incandescent ignition; Igniters using electrically-produced heat, e.g. lighters for cigarettes; Electrically-heated glowing plugs structurally associated with fluid-fuel burners
    • F23Q7/10Incandescent ignition; Igniters using electrically-produced heat, e.g. lighters for cigarettes; Electrically-heated glowing plugs structurally associated with fluid-fuel burners for gaseous fuel, e.g. in welding appliances
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression
    • F02B1/02Engines characterised by fuel-air mixture compression with positive ignition
    • F02B1/04Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into cylinder

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  • Pappas & McLeod 1 1 ABSTRACT A method and apparatus is described for igniting combustible gases by the zone heating of a pressure resistant. electrically conductive material with spaced apart electrical contacts on a surface of the material opposite the gases. After the ignition of the gases. the heated zone cools or is cooled and additional combustible gases can then be reintroduced for ignition by the same method.
  • the material is preferably in the form of a small diameter metal tube with a portion of its length being electrically heated.
  • the apparatus and method are particularly useful in the dcburring of articles by controlling the ignition of the explosive gases in a rapidly and repetitively opened and sealed chamber for deburring articles by causing ignition of the gases in the sealed chamber at only that operatorselected portion of the cycle after maximum desired unexploded gas charge pressure has been obtained.
  • the present invention relates to an electrical apparatus for igniting combustible gases.
  • the present invention relates to an apparatus with means which electrically heat a zone of a pressure resistant, electrically conductive material to a temperature adjacent to the gases sufficient for ignition.
  • the pressure resistant material is preferably in the form of a metal tubeconnected with a sealed chamber such that the combustible gases inside the chamber can be ignited from inside the tube.
  • the prior art has utilized heated tubes to ignite combustible gases usually in the operation of Otto or Diesel engines.
  • the igniter means is externally heated such as with a flame or electrically prior to the introduction of combustible gases to initially ignite the combustible gas as it is introduced intothe chambers. Once the engine is running at a steady state the external heating source is removed and the igniter is maintained in a heated state at or above the combustible gas autoignition temperature by the repeated exposure to the periodically igniting gases.
  • the patents to Nash US. Pat. No. 563,051
  • Vierling U.S. Pat. No. 2,996,056
  • an object of the present invention to provide an igniter apparatus and method of ignition of combustible gases which allows for operator-selected control of the ignition of the combustible gases. Further, it is an object .of the present invention to provide an igniter apparatus which can be rapidly cycled without concern about premature ignition of the combusti- *ble' gases. It-is further an object of the present invention to provide igniters which-will withstand severe repetitive gas explosion conditions without failure.
  • FIG. I is a schematic illustration of the steps in the method of the present invention particularly showing the external heating of a zone of a material in contact with a combustible gas and also schematically showing a form of external cooling of the material using cooling gas or other fluid exposure, which can be forced air or liquid or which can be accomplished by other convective means. 7
  • FIG. II is a front cross sectional view of a thermal deburring chamber illustrating a tubular igniter apparatus connected to a current source with spaced apart cooled electrically conductive electrodes defining a heating zone of the tube.
  • FIG. III is a front exploded perspective view of the preferred igniter apparatus of the present invention.
  • FIG. IV is a front view of the preferred assembled igniter apparatus illustrated in FIG. III.
  • the leads such that a zone of the heatable igniter material is heated to produce ignition on the combustible gas side of the material when the leads are supplied from a current source; and heat transfer means in thermal contact with the heated zone of the igniter material for cooling the heated zone to below the ignition temperature of the combustible gas after the thermal energy release and pressure rise in the combustible gas in the chamber occurs by removing the heat.
  • the present invention also relates to the method of igniting a combustible gas to produce a rapid thermal energy release and pressure rise which comprises: providing an ignit- ,able gas adjacent to an electrically conductive igniter material having sufficient mechanical strength when heated to withstand a rapid thermal energy release and pressure rise in a gas adjacent to the igniter material; heating the igniter material by passing an electric current through a zone defined by spaced apart electrically conductive low resistance leads connected to a current source to ignite the combustible gas; and cooling the heated zone of the igniter material to below the ignition temperature after the combustible gas has ignited.
  • the igniter material of the present invention is conductive and is spot or zone heated electrically. This material can be in various forms but is preferably a tube.
  • the igniter materials are preferably composed of high mechanical strength, and corrosion resistant metals such as the nickel-chrome alloys. Inconel is a particularly useful material since it is able to repetitively withi stand the thermal cycling and the pressures generated by explosive gases when heated to the ignition temperathe American Society for Metals Handbook Vol. I (I961 i
  • the gases which can be ignited by the method and apparatus of the present invention are combustible mixtures of an oxidizable material and an oxidizer material. Typical oxidizable gases are hydrogen. lower alkanes, alkcncs and alkynes, such as those containing 1 to 4 carbon atoms, ammonia, hydrazine, hydrogen sulfide, carbon monoxide and various other rapidly oxidizable compounds.
  • Oxidizer compounds which can be used include air, oxygen, the halogens, such as fluorine and chlorine, ozone and various perchlorates and nitrogen oxides. Particularly preferred are the compositions shown in US. Pat. No. 3,475,229.
  • Step 1 an ignitable gas 11 is provided adjacent to an electrically conductive material 10.
  • Step 2 the material is contacted with electrically conductive leads l2 and 12a connected to a current source 13.
  • the leads l2 and 12a heat the material 10 to the ignition temperature of the gas 11.
  • the distance is preferably between about I and 30 millimeters between the leads l2 and 12a.
  • fluid means 15, such as air is used to cool the material 10 to below the combustible gas 11 ignition temperature.
  • the steps of the method can be performed by a specifically designed replaceable separate assembly.
  • a confined space 19 is formed by mating tooling 20 and chamber 21.
  • a pressure responsive seal 22 is mounted on the tooling 20 in contact with the lower lip 21a of the chamber 21.
  • Conduit 23 with valve means 24 are provided leading to the confined space 21 for gas inlet and outlet.
  • the tooling 20 is mounted on ram means 25 for closure of the tooling 20 with the chamber 21.
  • the confined space 19 is provided with an ignition tube 26 mounted on the chamber 21 with the closed end extending from the chamber 21.
  • the tube was about 300 millimeters long, 3 millimeters inside diameter and 6 millimeters outside diameter.
  • Two spaced apart cooled electrodes 27 and 28 are mounted on the tube 26. Cooling of the electrodes was provided by tubes 33 and 34 around the electrodes 27 and 28.
  • the electrodes 27 and 28 were spaced apart about 10 millimeters.
  • the first electrode 28 was about 100 millimeters from the chamber end of the tube 26.
  • the tube 26 can be mounted on the tooling 20 or on the conduit 23 (not shown).
  • the electrodes 27 and 28 are connected to a current source 29.
  • the ram 25' is pulled down and an article 31 with burrs 32 is mounted on the tooling 20.
  • the ram 25 is then moved upward so that the tooling 20 and seal 22 close the chamber 21 on the lip 21a.
  • the valve 24 is opened to allow combustible gas to enter the confined space 19 and to fill the tube 26 and then closed.
  • the current source 29 is then activated to ignite the gas by heating the tube 26 between the spaced apart electrodes 27 and 28.
  • FIGS. III and IV The preferred apparatus of the present invention is illustrated in FIGS. III and IV.
  • the apparatus is similar in operation to that shown in FIG. II but modified to provide improved operating life.
  • a heating zone 40 on a tube 41 with a closed end 42 is defined by copper bushings 43 and 43a, l9 millimeters in diameter,
  • bushings 43 and 43a are slightly oversize in inside diameter to permit silver soldering.
  • the heating zone was 13 millimeters long.
  • the tube 4] inside and outside diameters were 3.2 and 6.4 millimeters respectively.
  • Clamped around bushing 43 are two opposing copper bus bars 44 and 45 secured together by bolts 46 and threaded retaining plate 58.
  • the copper to copper contact of the bus bars 44 and 45 and bushing 43 and 43a prevents corrosion, which would result from using dissimilar metals, and helps to uniformly distribute the current around and into the tube 41.
  • the extended portions of the bus bars 44 and 45 are provided with coiled cooling tubes 47 and 48 brazed to the bus bars 44 and 45.
  • the ends of the bus bars 44 and 45 are provided with bolts 49 and 50 for mounting electrically conductive leads 51 and 52.
  • the closed end 42 of the tube 41 is provided with an insulating positioning bracket 53 secured by bolts 54 and 57 to a portion of the chamber or other fixed part of the equipment (not shown).
  • the bracket 53 loosely surrounds the tube 41 to allow the tube 41 to elongate on heating without bending.
  • the open end of the tube 41 is provided with a hexagonal fitting 55 with threads 56.
  • electrical leads 51 and 52 are connected to a current source (not shown) and water or other cooling fluid is supplied through the tubes 47 and 48 to cool the bus bars 44 and 45.
  • Current is supplied equally at the identical potential through leads 51 and 52 through zone 40 from the bus bars 44 and 45 and through bushings 43 to ring 43a from the current source (not shown). The zone 40 is thus heated to ignite the combustible gas provided inside the tube 41.
  • FIGS. Ill and IV will function reliably for long periods of time and many firings without cracking of the tube 41, particularly in the heating zone 40.
  • the reason for this is that there are relatively uniform mechanical and thermal stresses on the heated zone because of the construction and mounting of the apparatus.
  • the electrical leads 51 and 52; cooling tubes 47 and 48 and other tube 41 compo nents are arranged to minimize mechanical stress on the zone 40.
  • Other bus bar means and cooling means providing this result will occur to those skilled in the art.
  • the heated tube is so designed and located so as to minimize the heat rise of the tube from the explosion in the chamber and is also designed to maximize the heat loss when the current is turned off after the explosion. This is necessary because the tube must be below the ignition temperature of the gas mixture between the selected ignition periods.
  • the method of igniting a combustible gas to pro'- cute a rapid thermal energy release and pressure rise which comprises:
  • heat transfer means is forced air in contact with the igniter material on the side opposite the gas side of the surface.
  • the igniter apparatus adapted to be fitted on a combustible gas containing chamber to produce ignition of the gas with a consequent rapid thermal energy release and pressure rise which comprises:
  • an integral heatable electrically conductive igniter material provided with means adapted to be fitted to a gas ignition chamber and being of sufficient mechanical strength to be able to withstand a rapid thermal energy release and pressure rise in a gas on one side of the material and with a surface permit- 7 ting cooling heat transfer on the side opposite the combustible gas side of the material;
  • electrically conductive low resistance leads connected to the igniter material to form a conductive path between the leads through the material such that a zone of the heatable igniter material between the leads is heated to produce ignition on the combustible gas side of the material when the leads are supplied from a current source;
  • heat transfer means mounted adjacent to the surface opposite the combustible gas side of the material and in thermal contact with the heated zone of the igniter material for cooling the heated zone to below the ignition temperature of the combustible gas by removing the heat after the thermal energy release and pressure rise in the combustible gas in the chamber occurs.
  • the igniter material is in the form of a tube with sides extending from the means adapted to be fitted to the chamber to a closed end and an open end at the end with the means adapted to be fitted to the chamber and wherein the leads are connected to the exterior sides of the tube opposite the gas combustion side of the igniter material to provide the heatable zones.

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

A method and apparatus is described for igniting combustible gases by the zone heating of a pressure resistant, electrically conductive material with spaced apart electrical contacts on a surface of the material opposite the gases. After the ignition of the gases, the heated zone cools or is cooled and additional combustible gases can then be reintroduced for ignition by the same method. The material is preferably in the form of a small diameter metal tube with a portion of its length being electrically heated. The apparatus and method are particularly useful in the deburring of articles by controlling the ignition of the explosive gases in a rapidly and repetitively opened and sealed chamber for deburring articles by causing ignition of the gases in the sealed chamber at only that operator-selected portion of the cycle after maximum desired unexploded gas charge pressure has been obtained.

Description

United States Patent Rice [5 APPARATUS AND METHOD OF IGNITION FOR COMBUSTIBLE GASES [75] Inventor: Warren A. Rice, Dexter, Mich.
173] Assignee: Chemotronics International. Inc.,
Ann Arbor, Mich.
[221 Filed: Aug. 17, 1973 [21] Appl. No: 389,251
[52] US. Cl 431/6; 123/169 C; 431/258; 317/82; 317/98 [51] Int. Cl. F23N 5/20; F23N 5/22 [58] Field of Search 431/6. 263. 258; 317/82. 317/98; 165/47; 123/169 C [56] References Cited UNITED STATES PATENTS 2.017.364 10/1935 Anderson 123/169 c 2.273.651 2/1942 Lude 123/169 C 2.526.169 10/1950 Steeg 431/263 X 3.071.182 1/1963 Delano... 431/6 3.191.659 6/1965 Weiss 431/258 X 3.245.457 4/1966 Smith et al.... 431/6 3.662.222 5/1972 Ray 317/98 FOREIGN PATENTS OR APPLICATIONS 571.170 5/1924 France 123/169 C PROV/DING A COMBUS TIBLE STEP 64$ ADJACENT 44/ 54 5c TIP/(Al 4 Y CONDUCT/4 E (OOL/A/G. #547250 zen/5 /4 w/n/ #547 TRANSFER Fay/0 4464/16 /5 70 cooL MATER/AL /0 STEP 3 561.991 5/1957 Italy 431/258 Primary Eraminer-Charles J. Myhre Assistant Examiner-William C. Anderson Attorney, Agent, or FirnzMiller. Morriss. Pappas & McLeod 1 1 ABSTRACT A method and apparatus is described for igniting combustible gases by the zone heating of a pressure resistant. electrically conductive material with spaced apart electrical contacts on a surface of the material opposite the gases. After the ignition of the gases. the heated zone cools or is cooled and additional combustible gases can then be reintroduced for ignition by the same method. The material is preferably in the form of a small diameter metal tube with a portion of its length being electrically heated. The apparatus and method are particularly useful in the dcburring of articles by controlling the ignition of the explosive gases in a rapidly and repetitively opened and sealed chamber for deburring articles by causing ignition of the gases in the sealed chamber at only that operatorselected portion of the cycle after maximum desired unexploded gas charge pressure has been obtained.
11 Claims, 4 Drawing Figures US. Patent N0v.11, 1 975 sheet'zofz 3,918,878
APPARATUS AND METHOD OF IGNITION ,FOR
COMBUSTIBLE GASES SUMMARY OF INVENTION The present invention relates to an electrical apparatus for igniting combustible gases. In particular, the present invention relates to an apparatus with means which electrically heat a zone of a pressure resistant, electrically conductive material to a temperature adjacent to the gases sufficient for ignition. The pressure resistant material is preferably in the form of a metal tubeconnected with a sealed chamber such that the combustible gases inside the chamber can be ignited from inside the tube.
PRIOR ART U. S. Pat. Nos. 3,475,229 and 3,666,252 show a method and various apparatus for thermally deburring articles by igniting a combustible gas in a sealed chamber. The chamber in the preferred equipment is opened for article removal and recycled rapidly on a continuous basis. Such chambers can have preignition combustible gas charge pressures of up to 2,000 pounds per square inch (141 kilogram per square centimeter) or more and generate large internally confined explosion pressures which can be on the order of 55 times the initial preignition charge pressure. Such conditions cause rapid deterioration and destruction of conventional igniter devices such as spark or glow plugs since they are designed to operate under much less severe ignition conditions.
The prior art has utilized heated tubes to ignite combustible gases usually in the operation of Otto or Diesel engines. In these devices, the igniter means is externally heated such as with a flame or electrically prior to the introduction of combustible gases to initially ignite the combustible gas as it is introduced intothe chambers. Once the engine is running at a steady state the external heating source is removed and the igniter is maintained in a heated state at or above the combustible gas autoignition temperature by the repeated exposure to the periodically igniting gases. The patents to Nash (US. Pat. No. 563,051) and Vierling (U.S. Pat. No. 2,996,056) are illustrative.
In these prior art heated tube devices,.provision to minimize external cooling of the igniter was made since this would stop the periodic ignition of the combustible gas. Further, in initiating thegas combustion in these devices, no attempt is made to selectively heat only a zone of the igniter, since it would ultimately be completely heated by the operation of the engine in any event. Thus, the priorart heated tube devices are heatedto or above the combustible gas ignition temperature prior to the introduction of the combustible gas to the igniter.
It is-therefore an object of the present invention to provide an igniter apparatus and method of ignition of combustible gases which allows for operator-selected control of the ignition of the combustible gases. Further, it is an object .of the present invention to provide an igniter apparatus which can be rapidly cycled without concern about premature ignition of the combusti- *ble' gases. It-is further an object of the present invention to provide igniters which-will withstand severe repetitive gas explosion conditions without failure. These and other objects will become increasingly apparent to those skilled in the art from the following description and by reference to the following drawings.
IN THE DRAWINGS:
FIG. I is a schematic illustration of the steps in the method of the present invention particularly showing the external heating of a zone of a material in contact with a combustible gas and also schematically showing a form of external cooling of the material using cooling gas or other fluid exposure, which can be forced air or liquid or which can be accomplished by other convective means. 7
FIG. II is a front cross sectional view of a thermal deburring chamber illustrating a tubular igniter apparatus connected to a current source with spaced apart cooled electrically conductive electrodes defining a heating zone of the tube.
FIG. III is a front exploded perspective view of the preferred igniter apparatus of the present invention.
FIG. IV is a front view of the preferred assembled igniter apparatus illustrated in FIG. III.
GENERAL DESCRIPTION the leads such that a zone of the heatable igniter material is heated to produce ignition on the combustible gas side of the material when the leads are supplied from a current source; and heat transfer means in thermal contact with the heated zone of the igniter material for cooling the heated zone to below the ignition temperature of the combustible gas after the thermal energy release and pressure rise in the combustible gas in the chamber occurs by removing the heat. The present invention also relates to the method of igniting a combustible gas to produce a rapid thermal energy release and pressure rise which comprises: providing an ignit- ,able gas adjacent to an electrically conductive igniter material having sufficient mechanical strength when heated to withstand a rapid thermal energy release and pressure rise in a gas adjacent to the igniter material; heating the igniter material by passing an electric current through a zone defined by spaced apart electrically conductive low resistance leads connected to a current source to ignite the combustible gas; and cooling the heated zone of the igniter material to below the ignition temperature after the combustible gas has ignited.
The igniter material of the present invention is conductive and is spot or zone heated electrically. This material can be in various forms but is preferably a tube. The igniter materials are preferably composed of high mechanical strength, and corrosion resistant metals such as the nickel-chrome alloys. Inconel is a particularly useful material since it is able to repetitively withi stand the thermal cycling and the pressures generated by explosive gases when heated to the ignition temperathe American Society for Metals Handbook Vol. I (I961 i The gases which can be ignited by the method and apparatus of the present invention are combustible mixtures of an oxidizable material and an oxidizer material. Typical oxidizable gases are hydrogen. lower alkanes, alkcncs and alkynes, such as those containing 1 to 4 carbon atoms, ammonia, hydrazine, hydrogen sulfide, carbon monoxide and various other rapidly oxidizable compounds.
Oxidizer compounds which can be used include air, oxygen, the halogens, such as fluorine and chlorine, ozone and various perchlorates and nitrogen oxides. Particularly preferred are the compositions shown in US. Pat. No. 3,475,229.
Referring to FIG. I, the steps in the method and ignitcr of the present invention are illustrated. In Step 1 an ignitable gas 11 is provided adjacent to an electrically conductive material 10. In Step 2, the material is contacted with electrically conductive leads l2 and 12a connected to a current source 13. The leads l2 and 12a heat the material 10 to the ignition temperature of the gas 11. The distance is preferably between about I and 30 millimeters between the leads l2 and 12a. In Step 3, fluid means 15, such as air, is used to cool the material 10 to below the combustible gas 11 ignition temperature. The steps of the method can be performed by a specifically designed replaceable separate assembly.
Referring to FIG. I], a confined space 19 is formed by mating tooling 20 and chamber 21. A pressure responsive seal 22 is mounted on the tooling 20 in contact with the lower lip 21a of the chamber 21. Conduit 23 with valve means 24 are provided leading to the confined space 21 for gas inlet and outlet. The tooling 20 is mounted on ram means 25 for closure of the tooling 20 with the chamber 21. The confined space 19 is provided with an ignition tube 26 mounted on the chamber 21 with the closed end extending from the chamber 21. The tube was about 300 millimeters long, 3 millimeters inside diameter and 6 millimeters outside diameter. Two spaced apart cooled electrodes 27 and 28 are mounted on the tube 26. Cooling of the electrodes was provided by tubes 33 and 34 around the electrodes 27 and 28. The electrodes 27 and 28 were spaced apart about 10 millimeters. The first electrode 28 was about 100 millimeters from the chamber end of the tube 26.
The tube 26 can be mounted on the tooling 20 or on the conduit 23 (not shown). The electrodes 27 and 28 are connected to a current source 29.
In operation of the device of FIG. II, the ram 25' is pulled down and an article 31 with burrs 32 is mounted on the tooling 20. The ram 25 is then moved upward so that the tooling 20 and seal 22 close the chamber 21 on the lip 21a. The valve 24 is opened to allow combustible gas to enter the confined space 19 and to fill the tube 26 and then closed. The current source 29 is then activated to ignite the gas by heating the tube 26 between the spaced apart electrodes 27 and 28.
SPECIFIC DESCRIPTION The preferred apparatus of the present invention is illustrated in FIGS. III and IV. The apparatus is similar in operation to that shown in FIG. II but modified to provide improved operating life. A heating zone 40 on a tube 41 with a closed end 42 is defined by copper bushings 43 and 43a, l9 millimeters in diameter,
mounted on the tube 4] by silver soldering. This mating of the bushings 43 and 43a to thctubc 4l, prevents corrosion at that interface. The bushings 43 and 43a are slightly oversize in inside diameter to permit silver soldering. The heating zone was 13 millimeters long. The tube 4] inside and outside diameters were 3.2 and 6.4 millimeters respectively. The further assemblies on bushings 43 and 43a are identical and only one set will be described. Clamped around bushing 43 are two opposing copper bus bars 44 and 45 secured together by bolts 46 and threaded retaining plate 58. The copper to copper contact of the bus bars 44 and 45 and bushing 43 and 43a prevents corrosion, which would result from using dissimilar metals, and helps to uniformly distribute the current around and into the tube 41. The extended portions of the bus bars 44 and 45 are provided with coiled cooling tubes 47 and 48 brazed to the bus bars 44 and 45.
The ends of the bus bars 44 and 45 are provided with bolts 49 and 50 for mounting electrically conductive leads 51 and 52. The closed end 42 of the tube 41 is provided with an insulating positioning bracket 53 secured by bolts 54 and 57 to a portion of the chamber or other fixed part of the equipment (not shown). The bracket 53 loosely surrounds the tube 41 to allow the tube 41 to elongate on heating without bending. The open end of the tube 41 is provided with a hexagonal fitting 55 with threads 56.
In operation of the apparatus of FIGS. III and IV, fitted to a chamber, electrical leads 51 and 52 are connected to a current source (not shown) and water or other cooling fluid is supplied through the tubes 47 and 48 to cool the bus bars 44 and 45. Current is supplied equally at the identical potential through leads 51 and 52 through zone 40 from the bus bars 44 and 45 and through bushings 43 to ring 43a from the current source (not shown). The zone 40 is thus heated to ignite the combustible gas provided inside the tube 41.
It has been found that the device of FIGS. Ill and IV will function reliably for long periods of time and many firings without cracking of the tube 41, particularly in the heating zone 40. The reason for this is that there are relatively uniform mechanical and thermal stresses on the heated zone because of the construction and mounting of the apparatus. The electrical leads 51 and 52; cooling tubes 47 and 48 and other tube 41 compo nents are arranged to minimize mechanical stress on the zone 40. Other bus bar means and cooling means providing this result will occur to those skilled in the art.
The heated tube is so designed and located so as to minimize the heat rise of the tube from the explosion in the chamber and is also designed to maximize the heat loss when the current is turned off after the explosion. This is necessary because the tube must be below the ignition temperature of the gas mixture between the selected ignition periods.
I claim: I
l. The method of igniting a combustible gas to pro'- duce a rapid thermal energy release and pressure rise which comprises:
a. providing an ignitable gas adjacent to and on one side of an electrically conductive igniter material having sufficient mechanical strength when heated to withstand a rapid thermal energy release and pressure rise in the gas adjacent to the igniter material and having sufficient surface on the side opposite the gas to permit cooling;
b. heating the igniter material by passing an electric current through the material such that a zone between spaced apart electrically conductive low resistance leads connected to a current source is heated to ignite the combustible gas; and
c. cooling the heated zone of the igniter material using a heat transfer means on the surface opposite the gas to below the ignition temperature after the combustible gas has ignited.
2. The method of claim 1 wherein the conductive leads are moved into and out of contact with the igniter material.
3. The method of claim 1 wherein the combustible gas is provided in contact with the igniter material inside a sealed chamber.
4. The method of claim 1 wherein heat transfer means is forced air in contact with the igniter material on the side opposite the gas side of the surface.
5. The igniter apparatus adapted to be fitted on a combustible gas containing chamber to produce ignition of the gas with a consequent rapid thermal energy release and pressure rise which comprises:
a. an integral heatable electrically conductive igniter material provided with means adapted to be fitted to a gas ignition chamber and being of sufficient mechanical strength to be able to withstand a rapid thermal energy release and pressure rise in a gas on one side of the material and with a surface permit- 7 ting cooling heat transfer on the side opposite the combustible gas side of the material;
b. electrically conductive low resistance leads connected to the igniter material to form a conductive path between the leads through the material such that a zone of the heatable igniter material between the leads is heated to produce ignition on the combustible gas side of the material when the leads are supplied from a current source; and
. heat transfer means mounted adjacent to the surface opposite the combustible gas side of the material and in thermal contact with the heated zone of the igniter material for cooling the heated zone to below the ignition temperature of the combustible gas by removing the heat after the thermal energy release and pressure rise in the combustible gas in the chamber occurs.
6. The apparatus of claim 5 wherein the igniter material is in the form of a tube with sides extending from the means adapted to be fitted to the chamber to a closed end and an open end at the end with the means adapted to be fitted to the chamber and wherein the leads are connected to the exterior sides of the tube opposite the gas combustion side of the igniter material to provide the heatable zones.
7. The apparatus of claim 5 wherein the heated zone of the igniter material is adapted to fit inside the chamber. 1 I v g 8. The apparatus of claim 5 wherein the electrically conductive leads are provided with fluid cooling.
9. The apparatus of claim 5 wherein the heat transfer means is air cooled surfaces mounted adjacent the heated zone.
10. The apparatus of claim 9 wherein the air cooled surfaces are electrically conductive and the leads are connected to the ignition means surface through the cooled surfaces.
11. The apparatus of claim 5 wherein a current source is connected to the leads and wherein the igniter material is fitted to the chamber.

Claims (11)

1. THE METHOD OF IGNITING A COMBUSTIBLE GAS TO PRODUCE A RAPID THERMAL ENERGY RELEASE AND PRESSURE RISE WHICH COMPRISES: A. PROVIDING AN IGNITABLE GAS ADJACENT TO AND ON ONE SIDE OF AN ELECTRICALLY CONDUCTIVE INGNITER MATERIAL HAVING SUFFICIENT MECHINICAL STRENGTH WHEN HEATED TO WITHSTAND A RAPID TERMAL ENERGY RELEASE AND PRESSURE RISE IN THE GAS ADJACENT TO THE IGNITER MATERIAL AND HAVING SUFFICIENT SURFACE ON THE SIDE OPPOSITE THE GAS TO PERMIT COOLING: B. HEATING THE IGNITER MATERIAL BY PASSING AN ELECTRIC CURRENT THROUGH THE MATERIAL SUCH THAT A ZONE BETWEEN SPACED APART ELECTRICALLY CONDUCTIVE LOW RESISTANCE LEADS CON-
2. The method of claim 1 wherein the conductive leads are moved into and out of contact with the igniter material.
3. The method of claim 1 wherein the combustible gas is provided in contact with the igniter material inside a sealed chamber.
4. The method of claim 1 wherein heat transfer means is forced air in contact with the igniter material on the side opposite the gas side of the surface.
5. The igniter apparatus adapted to be fitted on a combustible gas containing chamber to produce ignition of the gas with a consequent rapid thermal energy release and pressure rise which comprises: a. an integral heatable electrically conductive igniter material provided with means adapted to be fitted to a gas ignition chamber and being of sufficient mechanical strength to be able to withstand a rapid thermal energy release and pressure rise in a gas on one side of the material and with a surface permitting cooling heat transfer on the side opposite the combustible gas side of the material; b. electrically conductive low resistance leads connected to the igniter material to form a conductive path between the leads through the material such that a zone of the heatable igniter material between the leads is heated to produce ignition on the combustible gas side of the material when the leads are supplied from a current source; and c. heat transfer means mounted adjacent to the surface opposite the combustible gas side of the material and in thermal contact with the heated zone of the igniter material for cooling the heated zone to below the ignition temperature of the combustible gas by removing the heat after the thermal energy release and pressure rise in the combustible gas in the chamber occurs.
6. The apparatus of claim 5 wherein the igniter material is in the form of a tube with sides extending from the means adapted to be fitted to the chamber to a closed end and an open end at the end with the means adapted to be fitted to the chamber and wherein the leads are connected to the exterior sides of the tube opposite the gas combustion side of the igniter material to provide the heatable zones.
7. The apparatus of claim 5 wherein the heated zone of the igniter material is adapted to fit inside the chamber.
8. The apparatus of claim 5 wherein the electrically conductive leads are provided with fluid cooling.
9. The apparatus of claim 5 wherein the heat transfer means is air cooled surfaces mounted adjacent the heated zone.
10. The apparatus of claim 9 wherein the air cooled surfaces are electrically conductive and the leads are connected to the ignition means surface through the cooled surfaces.
11. The apparatus of claim 5 wherein a current source is connected to the leads and wherein the igniter material is fitted to the chamber.
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0005694A2 (en) * 1978-05-22 1979-11-28 Nicolas Gath Ground fault protective circuit interrupter
US4778376A (en) * 1983-01-19 1988-10-18 United Kingdom Atomic Energy Authority Gas ignition
US4971571A (en) * 1990-03-15 1990-11-20 Amp Incorporated Self-locking pin field connector
US20150337793A1 (en) * 2013-02-11 2015-11-26 Contour Hardening, Inc. Combustion ignition system

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US2017364A (en) * 1934-08-03 1935-10-15 Anderson August Eugene Spark plug with supported gap
US2273651A (en) * 1940-09-26 1942-02-17 Thoma & Gould Sales Company Spark plug
US2526169A (en) * 1948-09-04 1950-10-17 Gen Motors Corp Air-cooled igniter plug
US3071182A (en) * 1960-02-03 1963-01-01 Arthur G Steinmetz Compact fuel burner with electric ignition means
US3191659A (en) * 1958-04-07 1965-06-29 American Thermocatalytic Corp Radiant gas burner
US3245457A (en) * 1962-11-07 1966-04-12 Hunter Method of igniting liquid fuel
US3662222A (en) * 1970-05-07 1972-05-09 Itt Electric resistance wire igniter with a cooling terminal posts construction

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Publication number Priority date Publication date Assignee Title
US2017364A (en) * 1934-08-03 1935-10-15 Anderson August Eugene Spark plug with supported gap
US2273651A (en) * 1940-09-26 1942-02-17 Thoma & Gould Sales Company Spark plug
US2526169A (en) * 1948-09-04 1950-10-17 Gen Motors Corp Air-cooled igniter plug
US3191659A (en) * 1958-04-07 1965-06-29 American Thermocatalytic Corp Radiant gas burner
US3071182A (en) * 1960-02-03 1963-01-01 Arthur G Steinmetz Compact fuel burner with electric ignition means
US3245457A (en) * 1962-11-07 1966-04-12 Hunter Method of igniting liquid fuel
US3662222A (en) * 1970-05-07 1972-05-09 Itt Electric resistance wire igniter with a cooling terminal posts construction

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0005694A2 (en) * 1978-05-22 1979-11-28 Nicolas Gath Ground fault protective circuit interrupter
EP0005694A3 (en) * 1978-05-22 1979-12-12 Nicolas Gath Ground fault protective circuit interrupter
US4778376A (en) * 1983-01-19 1988-10-18 United Kingdom Atomic Energy Authority Gas ignition
US4971571A (en) * 1990-03-15 1990-11-20 Amp Incorporated Self-locking pin field connector
US20150337793A1 (en) * 2013-02-11 2015-11-26 Contour Hardening, Inc. Combustion ignition system

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