US3330985A - High voltage igniter with fluid feed through the insulator core center - Google Patents
High voltage igniter with fluid feed through the insulator core center Download PDFInfo
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- US3330985A US3330985A US506662A US50666265A US3330985A US 3330985 A US3330985 A US 3330985A US 506662 A US506662 A US 506662A US 50666265 A US50666265 A US 50666265A US 3330985 A US3330985 A US 3330985A
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- insulator
- annular space
- igniter
- gas
- high voltage
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/264—Ignition
- F02C7/266—Electric
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23Q—IGNITION; EXTINGUISHING-DEVICES
- F23Q3/00—Igniters using electrically-produced sparks
- F23Q3/006—Details
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Definitions
- ABSTRACT OF THE DISCLOSURE This invention relates to a high voltage igniter for gas turbine engines in which the construction provides for a stream of gas to pass between the walls of the insulator centerbore and the firing tip portion of the center electrode during sparking thereby increasing the projections and the energy release of the spark are.
- This invention relates to a high voltage igniter for gas turbine engines and more particularly to increasing the energy release of the spark from the igniter.
- a high voltage igniter is required to deliver high quantities of electrical energy into the combustion chamber of the jet engine. This high energy is required to ignite air-fuel mixtures under conditions adverse to ignition of the engine, such as low temperatures, high air velocities, poorly atomized fuel droplets, etc. Although energies of 1 to joules are stored in the power source, only 15 to of this stored energy is actually delivered to the spark are due to the low efiiciency of the ignition system.
- the high voltage igniter has a passageway through the metal shell and the insulator which connects the annular space separating the center electrode from the insulator to an oxidizing gas source. Gas from the gas source passes through the passageway in the shell and the insulator to the annular space separating the center electrode from the insulator and then out of the end of the insulator and past the sparking tip portion of the center electrode.
- the gas flow increases the projection of the spark arc.
- the gas flow about the electrodes also removes the incandescent gas plasma from the gap region thereby increasing the energy release of the spark arc.
- FIGURE 1 is a side view in elevation of a high voltage igniter positioned in the gas turbine engine
- FIGURE 2 is a side view of an improved high voltage igniter having a passageway to receive air from the turbine secondary air chamber in cross section;
- FIGURE 3 is an enlarged view of the firing tip portion of the improved high voltage igniter.
- FIGURE 4 is a side view of an improved high voltage igniter having an air passageway to receive air from a separate source.
- FIGURE 1 shows the igniter 10 installed in the engine case 12 of the gas turbine so that the ground electrode portion 14 projects through the combustion liner 16 to the combustion chamber 18.
- the air pressure in the combustion chamber 18 is p.s.i.
- Air from the compressor 20 also flows through the secondary chamber 24 at a pressure of 102 to 106 p.s.i.
- Air passing through the secondary chamber 24 also flows through the igniter openings 26 and 28.
- Igniter openings 26 are vent holes which are widely used in igniters for cooling purposes. Opening 28 in the shell of the igniter 10 provides the opening through which the air required for this invention enters the igniter 10 as will be more fully discussed hereinafter.
- FIGURE 2 is an enlarged view of the high voltage igniter 10 showing a conventional outer tubular metal shell 30 having the lower end portion thereof constituting an annular ground electrode 32.
- the ground electrode 32 may be made of any suitable high temperature erosion resistant metal or metal alloy. Inconel containing approximately 76% by weight nickel, 16% by weight chromium, and 6% by weight iron is used in the preferred embodiment.
- a tubular two-piece alumina base ceramic insulator Positioned within the metal shell 30 and the ground electrode 32 is a tubular two-piece alumina base ceramic insulator having an upper portion 34 and a lower portion 36.
- the upper portion 34 is in contact with an upper annular gasket 38 which presses against the shell 30.
- Below the upper gasket 38 is an upper annular space 40 which separates the lower end of the upper insulator portion 34 from the shell 30 and provides a passageway for the flow of air.
- the lower insulator portion 36 fits snugly against the lower annular gasket 42 which rests against the upper end 44 of the ground electrode 32, the upper end 44 being held in locking relationship by the lower end 46 of the shell 30.
- an outer annular space 48 which separates the ground electrode 32 from the lower insulator portion 36 and provides a passageway for the flow of air.
- the insulator portions 34 and 36 have a centerbore 50 therethrough. Positioned within the insulator centerbore 50 is a center electrode 52.
- the center electrode 52 is separated from the upper insulator portion 34 and the lower insulator portion 36 by an inner annular space 54.
- the inner annular space 54 provides a passageway for the flow of air.
- the lower end of the center electrode 52 is the firing tip portion 56.
- the inner annular space 54 separating the center electrode 52 from the insulator lower portion 36 becomes very narrow about the firing tip portion 56 of the center electrode 52.
- the annular space 54 at the end of the lower insulator portion 36 becomes the opening 58 having a width of approximately 0.001 to 0.010 inch which is shown more clearly in FIGURE 3.
- the width of the opening 58 is not critical.
- the opening 58 is smaller, that is, in the range of .001 inch when the pressure is higher and larger, say in the range of 0.010 inch when the pressure is smaller.
- the pressure of the gas and the opening 58 must be such so as to project the gas about the space immediately surrounding the end of the firing tip portion 56.
- One of the primary purposes of this gas is to remove the incandescent gases which are present in the electrode region.
- the incandescent gases present in the electrode region lower the arc resistance between the firing tip portion 56 and the ground electrode 32.
- the incandescent gases allow the current to flow more easily thereby causing a reduction in the energy of the spark arc.
- the voltage drop is not lowered and the corresponding reduction of energy brought about by the lowering of the are resistance is eliminated.
- the gas coming out of the opening 58 causes an increase in the projection of the are thereby effecting an increase in the energy of the spark arc.
- the gas flow between the center electrode 52 and the insulator cools the electrodes thereby increasing the life of the electrodes. This gas also increases the length of the center electrode 52 life by causing the are to wander over the entire surface of the firing tip portion 56 of the center electrode 52.
- the ground electrode 32 has openings 26 which permit air to flow through the outer annular space 48 between the ground electrode 32 and the lower insulator portion 36 to cool these two pieces respectively. These vents, as indicated earlier, are well known in the art and their primary purpose is to cool the lower end of the igniter.
- the opening 28 in the shell 30 permits the air to enter the shell 30 and fiow through the upper annular space 40 and from there through the space 57 separating the upper insulator portion 34 from the lower insulator portion 36, and from there into the inner annular space 54 separating the center electrode 52 from the lower insulator portion 36.
- the gas proceeds to fiow down the inner annular space 54 until it reaches the opening 58.
- the gas flows out of the opening 58 around the end of the firing tip portion 56 and carries away any incandescent gases in the spark gap region 60 which have been ionized by previous spark arcs.
- FIGURE 4 shows the preferred embodiment of this invention wherein gas from a separate source 62 is introduced into igniter 10 by means of a standard tubing fitting 64 attached to the shell 30 at opening 66.
- the pressure of the gas from the separate source must be greater than the 100 p.s.i. pressure in the combustion chamber. It has been observed that beneficial results have been obtained by passing air from the separate source having a pressure as low as 102 p.s.i. However, better results are obtained with much higher pressures, for example in the range of 100 p.s.i. greater than the combustion chamber pressure. For example, a pressure of 200 p.s.i. increased the energy of the spark an appreciable amount. Pressures greater than 200 p.s.i.
- the pressure of the gas from the separate source can range from 2 to 250 p.s.i. greater than the combustion chamber pressure with 75 to 125 p.s.i. being preferred.
- Air is the preferred gas, however other oxidizing gases can be used; for example, oxygen, fluorine, and the like.
- gas from the separate source 62 passes through the tube 68 through the standard fitting 64 through the opening 66. The air then passes down the upper annular space 40 through the insulator opening 57 to the inner annular space 54.
- the gas then goes through the opening 58 adjacent to the center electrode firing tip 56 to increase the energy of the spark are by removing the incandescent gas plasma and by increasing the projection of the arc, as well as increasing the life of the center electrode by cooling the electrodes and by causing the arc to wander over the firing tip portion of the center electrode.
- the increase in the spark are energy of the igniter was observed by two methods.
- the first method involved measuring the voltage and current discharge of the spark arc during the 4 or half-cycle loop life of the spark arc.
- the instantaneous values of the voltage and current referred to above were multiplied together to give the power at each interval.
- the energy was determined by integrating the power over the discharge time. It was observed that the power increase of the spark are obtained by the igniter in the preferred embodiment was in the range of 50%.
- Another indication of the energy release is the projection of the spark are from the electrode end of the igniter. Pictures were taken during the ignition of an igniter operating in accordance with this invention and a standard igniter. It was observed that the projection of the flame increased between 80 and 100% when using the igniter disclosed in this invention.
- a high voltage igniter plug comprising an alumina base ceramic insulator having a centerbore therethrough, a stationary center electrode positioned longitudinally within said insulator centerbore and having a firing tip portion, said center electrode being separated over a substantial length from said insulator by an annular space, and means communicating said annular space with an oxidizing gas source, said annular space providing a passageway for the flow of said oxidizing gas about said firing tip portion during sparking to increase the energy release of the spark are from said plug.
- a high voltage igniter plug comprising an outer annular shell having an annular ground electrode connected to the lower end thereof, said shell having an opening therein to permit the fiow of gas therethrough,
- a two-piece tubular ceramic insulator positioned longitudinally within said shell and having a centerbore therethrough, said two-piece ceramic insulator having an upper portion and a lower portion, said upper portion being separated over a substantial length from said shell by an outer annular space, said outer annular space being connected to said opening in said shell, said upper portion having an opening therein to permit the flow of gas therethrough,
- a center electrode positioned longitudinally within said insulator centerbore and having a firing tip portion at the lower end thereof, said center electrode being separated from said insulator over a substantial length by an inner annular space, said firing tip portion of said electrode being separated from the lower end of said insulator by a narrow opening, said inner annular space being connected to said outer annular space by said insulator opening,
- said openings combining with said inner annular space and said outer annular space to provide a passageway for the flow of gas about said firing tip portion to increase the energy release of the spark are from said plug.
- a separate source of oxidizing gas and a high voltage igniter plug comprising an alumina base ceramic insulator having a centerbore therethrough, a stationary center electrode positioned longitudinally within said insulator centerbore and having a firing tip portion, said center electrode being separated over a substantial length from said insulator by an annular space, and means communicating said annular space with said oxidizing gas source, said annular space providing a passageway for the flow of said oxidizing gas about said firing tip portion during sparking to increase the energy release of the spark are from said plug.
- a separate source of oxidizing gas and a high voltage igniter plug comprising an outer annular shell having an annular ground electrode connected to the lower end thereof, said shell having an opening therein to permit the flow of gas therethrough, said opening connected to said separate source of oxidizing gas,
- a two-piece tubular ceramic insulator positioned longitudinally within said shell and having a centerbore therethrough, said two-piece ceramic insulator having an upper portion and a lower portion, said upper portion being separated over a substantial'length from said shell by an outer annular space, said outer annular space being connected to said opening in said 5 6 shell, said upper portion having an opening therein and said outer annular space to provide a passageto permit the flow of gas therethrough, way for the flow of said oxidizing gas about said a center electrode positioned longitudinally within said firing tip portion to increase the energy release of the insulator centerbore and having a firing tip portion spark are from said plug.
Description
July 11, 1967 w. J. JOHNSTON 3,330,985
HIGH VOLTAGE IGNITER WITH FLUID FEED THROUGH THE INSULATOR CORE CENTER Filed Nov. 8, 1965 y MW/ -ll Iii v INVENTOR. 1 24 2022: Jfifins/ozz A 7'TORNEY United States Patent 3,330,985 HIGH VOLTAGE IGNITER WI'I'H FLUID FEED THROUGH THE INSULATOR CORE CENTER William J. Johnston, Flint, Mich, assignor to General Motors Corporation, Detroit, Mich, a corporation of Delaware Filed Nov. 8, 1965, Ser. No. 506,662 3 Claims. (Cl. 313-120) ABSTRACT OF THE DISCLOSURE This invention relates to a high voltage igniter for gas turbine engines in which the construction provides for a stream of gas to pass between the walls of the insulator centerbore and the firing tip portion of the center electrode during sparking thereby increasing the projections and the energy release of the spark are. i
This invention relates to a high voltage igniter for gas turbine engines and more particularly to increasing the energy release of the spark from the igniter.
A high voltage igniter is required to deliver high quantities of electrical energy into the combustion chamber of the jet engine. This high energy is required to ignite air-fuel mixtures under conditions adverse to ignition of the engine, such as low temperatures, high air velocities, poorly atomized fuel droplets, etc. Although energies of 1 to joules are stored in the power source, only 15 to of this stored energy is actually delivered to the spark are due to the low efiiciency of the ignition system.
It is a basic object of this invention to increase the projection of the spark arc of the igniter and thereby increase the energy release of the spark arc and increase the life of the igniter.
These and other objects are accomplished by passing an oxidizing gas through an annular space between the center electrode and the insulator during the ignition cycle. In general, the high voltage igniter has a passageway through the metal shell and the insulator which connects the annular space separating the center electrode from the insulator to an oxidizing gas source. Gas from the gas source passes through the passageway in the shell and the insulator to the annular space separating the center electrode from the insulator and then out of the end of the insulator and past the sparking tip portion of the center electrode. When the high voltage igniter is energized, the gas flow increases the projection of the spark arc. The gas flow about the electrodes also removes the incandescent gas plasma from the gap region thereby increasing the energy release of the spark arc.
Other objects and advantages of this invention will be apparent from the following detailed description, reference being made to the accompanying drawings wherein several preferred embodiments of this invention are shown.
In the drawings:
FIGURE 1 is a side view in elevation of a high voltage igniter positioned in the gas turbine engine;
FIGURE 2 is a side view of an improved high voltage igniter having a passageway to receive air from the turbine secondary air chamber in cross section;
FIGURE 3 is an enlarged view of the firing tip portion of the improved high voltage igniter; and
FIGURE 4 is a side view of an improved high voltage igniter having an air passageway to receive air from a separate source.
Referring to the drawings, FIGURE 1 shows the igniter 10 installed in the engine case 12 of the gas turbine so that the ground electrode portion 14 projects through the combustion liner 16 to the combustion chamber 18. Air from the compressor 20 at a pressure of 102 to 106 p.s.i. flows through a fuel nozzle 22, the fuel is vaporized into droplets on its way to the combustion chamber 13. The air pressure in the combustion chamber 18 is p.s.i. Air from the compressor 20 also flows through the secondary chamber 24 at a pressure of 102 to 106 p.s.i. Air passing through the secondary chamber 24 also flows through the igniter openings 26 and 28. Igniter openings 26 are vent holes which are widely used in igniters for cooling purposes. Opening 28 in the shell of the igniter 10 provides the opening through which the air required for this invention enters the igniter 10 as will be more fully discussed hereinafter.
FIGURE 2 is an enlarged view of the high voltage igniter 10 showing a conventional outer tubular metal shell 30 having the lower end portion thereof constituting an annular ground electrode 32. The ground electrode 32 may be made of any suitable high temperature erosion resistant metal or metal alloy. Inconel containing approximately 76% by weight nickel, 16% by weight chromium, and 6% by weight iron is used in the preferred embodiment.
Positioned within the metal shell 30 and the ground electrode 32 is a tubular two-piece alumina base ceramic insulator having an upper portion 34 and a lower portion 36. The upper portion 34 is in contact with an upper annular gasket 38 which presses against the shell 30. Below the upper gasket 38 is an upper annular space 40 which separates the lower end of the upper insulator portion 34 from the shell 30 and provides a passageway for the flow of air. The lower insulator portion 36 fits snugly against the lower annular gasket 42 which rests against the upper end 44 of the ground electrode 32, the upper end 44 being held in locking relationship by the lower end 46 of the shell 30. Below the lower gasket 42 is an outer annular space 48 which separates the ground electrode 32 from the lower insulator portion 36 and provides a passageway for the flow of air. The insulator portions 34 and 36 have a centerbore 50 therethrough. Positioned within the insulator centerbore 50 is a center electrode 52. The center electrode 52 is separated from the upper insulator portion 34 and the lower insulator portion 36 by an inner annular space 54. The inner annular space 54 provides a passageway for the flow of air. The lower end of the center electrode 52 is the firing tip portion 56. The inner annular space 54 separating the center electrode 52 from the insulator lower portion 36 becomes very narrow about the firing tip portion 56 of the center electrode 52. The annular space 54 at the end of the lower insulator portion 36 becomes the opening 58 having a width of approximately 0.001 to 0.010 inch which is shown more clearly in FIGURE 3. The width of the opening 58 is not critical. The opening 58 is smaller, that is, in the range of .001 inch when the pressure is higher and larger, say in the range of 0.010 inch when the pressure is smaller. The pressure of the gas and the opening 58 must be such so as to project the gas about the space immediately surrounding the end of the firing tip portion 56. One of the primary purposes of this gas is to remove the incandescent gases which are present in the electrode region. The incandescent gases present in the electrode region lower the arc resistance between the firing tip portion 56 and the ground electrode 32. By lowering the arc resistance between the two electrodes, the incandescent gases allow the current to flow more easily thereby causing a reduction in the energy of the spark arc. By removing the incandescent gases the voltage drop is not lowered and the corresponding reduction of energy brought about by the lowering of the are resistance is eliminated. The gas coming out of the opening 58 causes an increase in the projection of the are thereby effecting an increase in the energy of the spark arc. The gas flow between the center electrode 52 and the insulator cools the electrodes thereby increasing the life of the electrodes. This gas also increases the length of the center electrode 52 life by causing the are to wander over the entire surface of the firing tip portion 56 of the center electrode 52.
The ground electrode 32 has openings 26 which permit air to flow through the outer annular space 48 between the ground electrode 32 and the lower insulator portion 36 to cool these two pieces respectively. These vents, as indicated earlier, are well known in the art and their primary purpose is to cool the lower end of the igniter. The opening 28 in the shell 30 permits the air to enter the shell 30 and fiow through the upper annular space 40 and from there through the space 57 separating the upper insulator portion 34 from the lower insulator portion 36, and from there into the inner annular space 54 separating the center electrode 52 from the lower insulator portion 36. The gas proceeds to fiow down the inner annular space 54 until it reaches the opening 58. The gas flows out of the opening 58 around the end of the firing tip portion 56 and carries away any incandescent gases in the spark gap region 60 which have been ionized by previous spark arcs.
FIGURE 4 shows the preferred embodiment of this invention wherein gas from a separate source 62 is introduced into igniter 10 by means of a standard tubing fitting 64 attached to the shell 30 at opening 66. The pressure of the gas from the separate source must be greater than the 100 p.s.i. pressure in the combustion chamber. It has been observed that beneficial results have been obtained by passing air from the separate source having a pressure as low as 102 p.s.i. However, better results are obtained with much higher pressures, for example in the range of 100 p.s.i. greater than the combustion chamber pressure. For example, a pressure of 200 p.s.i. increased the energy of the spark an appreciable amount. Pressures greater than 200 p.s.i. did not yield energy gains much different than with 200 p.s.i. The pressure of the gas from the separate source can range from 2 to 250 p.s.i. greater than the combustion chamber pressure with 75 to 125 p.s.i. being preferred. Air is the preferred gas, however other oxidizing gases can be used; for example, oxygen, fluorine, and the like. In this embodiment gas from the separate source 62 passes through the tube 68 through the standard fitting 64 through the opening 66. The air then passes down the upper annular space 40 through the insulator opening 57 to the inner annular space 54. The gas then goes through the opening 58 adjacent to the center electrode firing tip 56 to increase the energy of the spark are by removing the incandescent gas plasma and by increasing the projection of the arc, as well as increasing the life of the center electrode by cooling the electrodes and by causing the arc to wander over the firing tip portion of the center electrode.
The increase in the spark are energy of the igniter was observed by two methods. The first method involved measuring the voltage and current discharge of the spark arc during the 4 or half-cycle loop life of the spark arc.
The instantaneous values of the voltage and current referred to above were multiplied together to give the power at each interval. The energy was determined by integrating the power over the discharge time. It was observed that the power increase of the spark are obtained by the igniter in the preferred embodiment was in the range of 50%. Another indication of the energy release is the projection of the spark are from the electrode end of the igniter. Pictures were taken during the ignition of an igniter operating in accordance with this invention and a standard igniter. It was observed that the projection of the flame increased between 80 and 100% when using the igniter disclosed in this invention.
While the invention has been described in terms of certain specific examples, it is to be understood that the scope of the invention is not limited thereby except as defined in the following claims.
I claim:
1. A high voltage igniter plug comprising an alumina base ceramic insulator having a centerbore therethrough, a stationary center electrode positioned longitudinally within said insulator centerbore and having a firing tip portion, said center electrode being separated over a substantial length from said insulator by an annular space, and means communicating said annular space with an oxidizing gas source, said annular space providing a passageway for the flow of said oxidizing gas about said firing tip portion during sparking to increase the energy release of the spark are from said plug.
2. A high voltage igniter plug comprising an outer annular shell having an annular ground electrode connected to the lower end thereof, said shell having an opening therein to permit the fiow of gas therethrough,
a two-piece tubular ceramic insulator positioned longitudinally within said shell and having a centerbore therethrough, said two-piece ceramic insulator having an upper portion and a lower portion, said upper portion being separated over a substantial length from said shell by an outer annular space, said outer annular space being connected to said opening in said shell, said upper portion having an opening therein to permit the flow of gas therethrough,
a center electrode positioned longitudinally within said insulator centerbore and having a firing tip portion at the lower end thereof, said center electrode being separated from said insulator over a substantial length by an inner annular space, said firing tip portion of said electrode being separated from the lower end of said insulator by a narrow opening, said inner annular space being connected to said outer annular space by said insulator opening,
said openings combining with said inner annular space and said outer annular space to provide a passageway for the flow of gas about said firing tip portion to increase the energy release of the spark are from said plug.
3. An igniter plug as defined in claim 2 wherein said narrow opening ranges in width from 0.001 to 0.010 inch.
4. The combination of a separate source of oxidizing gas and a high voltage igniter plug comprising an alumina base ceramic insulator having a centerbore therethrough, a stationary center electrode positioned longitudinally within said insulator centerbore and having a firing tip portion, said center electrode being separated over a substantial length from said insulator by an annular space, and means communicating said annular space with said oxidizing gas source, said annular space providing a passageway for the flow of said oxidizing gas about said firing tip portion during sparking to increase the energy release of the spark are from said plug.
5. The combination as defined in claim 4 wherein the pressure from said separate gas source ranges from 2 to 250 p.s.i. greater than the pressure in the turbine combustion chamber.
6. The combination as defined in claim 4 wherein said separate gas source is air.
7. The combination as defined in claim 4 wherein said separate gas source is oxygen.
8. The combination of a separate source of oxidizing gas and a high voltage igniter plug comprising an outer annular shell having an annular ground electrode connected to the lower end thereof, said shell having an opening therein to permit the flow of gas therethrough, said opening connected to said separate source of oxidizing gas,
a two-piece tubular ceramic insulator positioned longitudinally within said shell and having a centerbore therethrough, said two-piece ceramic insulator having an upper portion and a lower portion, said upper portion being separated over a substantial'length from said shell by an outer annular space, said outer annular space being connected to said opening in said 5 6 shell, said upper portion having an opening therein and said outer annular space to provide a passageto permit the flow of gas therethrough, way for the flow of said oxidizing gas about said a center electrode positioned longitudinally within said firing tip portion to increase the energy release of the insulator centerbore and having a firing tip portion spark are from said plug.
at the lower end thereof, said center electrode being separated from said insulator over a substantial length References Cited bydan 1inrtierdanigular space, 1saliidfliringtgp portion 0; UNITED STATES PATENTS sal e co ro e eing separa e rom e ower en of said insulator by a narrow opening, said inner an- 26301O7 3/1953 F 161d 313 120 nular space being connected to said outer annular 10 JAMES W. LAWRENCE, Primary Examiner. space by said lnsulator opening,
said openings combining with said inner annular space 0 CAM BELL, Assistant Examiner.
Claims (1)
1. A HIGH VOLTAGE IGNITER PLUG COMPRISING AN ALUMINA BASE CERAMIC INSULATOR HAVING A CENTERBORE THERETHROUGH, A STATIONARY CENTER ELECTRODE POSITIONED LONGITUDINALLY WITHIN SAID INSULATOR CENTERBORE AND HAVING A FIRING TIP PORTION, SAID CENTER ELECTRODE BEING SEPARATED OVER A SUBSTANTIAL LENGTH FROM SAID INSULATOR BY AN ANNULAR SPACE, AND MEANS COMMUNICATING SAID ANNULAR SPACE WITH AN OXIDIZING GAS SOURCE, SAID ANNULAR SPACE PROVIDING A PASSAGEWAY FOR THE FLOW OF SAID OXIDIZING GAS ABOUT SAID FIRING TIP PORTION DURING SPARKING TO INCREASE THE ENERGY RELEASE OF THE SPARK ARC FROM SAID PLUG.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
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US506662A US3330985A (en) | 1965-11-08 | 1965-11-08 | High voltage igniter with fluid feed through the insulator core center |
GB43499/66A GB1087537A (en) | 1965-11-08 | 1966-09-29 | High voltage igniter plug |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US506662A US3330985A (en) | 1965-11-08 | 1965-11-08 | High voltage igniter with fluid feed through the insulator core center |
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US3330985A true US3330985A (en) | 1967-07-11 |
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US506662A Expired - Lifetime US3330985A (en) | 1965-11-08 | 1965-11-08 | High voltage igniter with fluid feed through the insulator core center |
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US3521105A (en) * | 1967-09-25 | 1970-07-21 | Harry E Franks | Ignition device having elongated planar parallel electrodes between which a pulse of ionizable gas is passed |
US3990834A (en) * | 1973-09-17 | 1976-11-09 | General Electric Company | Cooled igniter |
US4264844A (en) * | 1978-09-29 | 1981-04-28 | Axe Gavin C H | Electrical igniters |
US4277724A (en) * | 1979-10-18 | 1981-07-07 | The Economy Engine Company | Integral spark plug coil for automotive-type plug |
US4597260A (en) * | 1981-04-17 | 1986-07-01 | Williams International Corporation | Oxygen starting assist system |
EP0212079A1 (en) * | 1985-08-13 | 1987-03-04 | Unison Industries Limited Partnership | Igniter with improved isulator support |
US4938019A (en) * | 1987-10-16 | 1990-07-03 | Fuel Systems Textron Inc. | Fuel nozzle and igniter assembly |
US4954743A (en) * | 1987-12-15 | 1990-09-04 | Ngk Spark Plug Co., Ltd. | Igniter plug structure having semicircular grooves |
US5402637A (en) * | 1993-07-13 | 1995-04-04 | Cooper Industries | Igniter plug extender for a turbine engine combustor |
US20060059885A1 (en) * | 2004-09-08 | 2006-03-23 | Johnson Howard R | Two piece jet engine igniter assembly |
WO2006114436A1 (en) * | 2005-04-28 | 2006-11-02 | Siemens Aktiengesellschaft | Lead arrangement for a combustor unit |
EP1798398A2 (en) * | 2005-12-16 | 2007-06-20 | General Electric Company | A cooling apparatus for a gas turbine engine igniter lead |
US20080054777A1 (en) * | 2006-09-06 | 2008-03-06 | Callahan Richard E | Extension spark plug |
US20080218053A1 (en) * | 2007-03-07 | 2008-09-11 | Callahan Richard E | 14 mm extension spark plug |
EP1619369A3 (en) * | 2004-07-20 | 2011-12-14 | General Electric Company | Methods and apparatus for cooling turbine engine combustor ignition devices |
US20120110975A1 (en) * | 2010-11-10 | 2012-05-10 | United Technologies Corporation | Igniter with integral pressure sensing line |
US20120279195A1 (en) * | 2011-05-03 | 2012-11-08 | Muzaffer Sutcu | Gas turbine igniter |
US20150040575A1 (en) * | 2013-08-12 | 2015-02-12 | Unison Industries, Llc | Fuel igniter assembly having heat-dissipating element and methods of using same |
FR3068766A1 (en) * | 2017-07-10 | 2019-01-11 | Office National D'etudes Et Recherches Aerospatiales | COMBUSTION IGNITION OR STABILIZATION SYSTEM |
EP4235087A3 (en) * | 2019-05-10 | 2023-10-11 | Hamilton Sundstrand Corporation | Multi-use torpedo propulsion system starter |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH03205775A (en) * | 1989-12-29 | 1991-09-09 | Ngk Spark Plug Co Ltd | Ignitor plug |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2630107A (en) * | 1949-12-15 | 1953-03-03 | Andrew R Cochrane | Spark plug |
-
1965
- 1965-11-08 US US506662A patent/US3330985A/en not_active Expired - Lifetime
-
1966
- 1966-09-29 GB GB43499/66A patent/GB1087537A/en not_active Expired
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2630107A (en) * | 1949-12-15 | 1953-03-03 | Andrew R Cochrane | Spark plug |
Cited By (30)
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US3521105A (en) * | 1967-09-25 | 1970-07-21 | Harry E Franks | Ignition device having elongated planar parallel electrodes between which a pulse of ionizable gas is passed |
US3990834A (en) * | 1973-09-17 | 1976-11-09 | General Electric Company | Cooled igniter |
US4264844A (en) * | 1978-09-29 | 1981-04-28 | Axe Gavin C H | Electrical igniters |
US4277724A (en) * | 1979-10-18 | 1981-07-07 | The Economy Engine Company | Integral spark plug coil for automotive-type plug |
US4597260A (en) * | 1981-04-17 | 1986-07-01 | Williams International Corporation | Oxygen starting assist system |
EP0212079A1 (en) * | 1985-08-13 | 1987-03-04 | Unison Industries Limited Partnership | Igniter with improved isulator support |
US4938019A (en) * | 1987-10-16 | 1990-07-03 | Fuel Systems Textron Inc. | Fuel nozzle and igniter assembly |
DE3841941C2 (en) * | 1987-12-15 | 2000-08-10 | Ngk Spark Plug Co | spark plug |
US4954743A (en) * | 1987-12-15 | 1990-09-04 | Ngk Spark Plug Co., Ltd. | Igniter plug structure having semicircular grooves |
US5402637A (en) * | 1993-07-13 | 1995-04-04 | Cooper Industries | Igniter plug extender for a turbine engine combustor |
EP1619369A3 (en) * | 2004-07-20 | 2011-12-14 | General Electric Company | Methods and apparatus for cooling turbine engine combustor ignition devices |
US20060059885A1 (en) * | 2004-09-08 | 2006-03-23 | Johnson Howard R | Two piece jet engine igniter assembly |
US7065956B2 (en) | 2004-09-08 | 2006-06-27 | Howard Johnson | Two piece jet engine igniter assembly |
WO2006114436A1 (en) * | 2005-04-28 | 2006-11-02 | Siemens Aktiengesellschaft | Lead arrangement for a combustor unit |
EP1717515A1 (en) * | 2005-04-28 | 2006-11-02 | Siemens Aktiengesellschaft | Lead arrangement for a combustor unit |
US20100180569A1 (en) * | 2005-04-28 | 2010-07-22 | Siemens Aktiengesellschaft | Lead Arrangement for a Combustor Unit |
EP1798398A2 (en) * | 2005-12-16 | 2007-06-20 | General Electric Company | A cooling apparatus for a gas turbine engine igniter lead |
EP1798398A3 (en) * | 2005-12-16 | 2013-08-07 | General Electric Company | A cooling apparatus for a gas turbine engine igniter lead |
US20080054777A1 (en) * | 2006-09-06 | 2008-03-06 | Callahan Richard E | Extension spark plug |
US7768183B2 (en) | 2006-09-06 | 2010-08-03 | Federal Mogul World Wide, Inc. | Extension spark plug |
US7825573B2 (en) | 2007-03-07 | 2010-11-02 | Federal-Mogul Ignition Company | 14 mm extension spark plug |
US20080218053A1 (en) * | 2007-03-07 | 2008-09-11 | Callahan Richard E | 14 mm extension spark plug |
US20120110975A1 (en) * | 2010-11-10 | 2012-05-10 | United Technologies Corporation | Igniter with integral pressure sensing line |
US8733078B2 (en) * | 2010-11-10 | 2014-05-27 | United Technologies Corporation | Igniter with integral pressure sensing line |
US20120279195A1 (en) * | 2011-05-03 | 2012-11-08 | Muzaffer Sutcu | Gas turbine igniter |
US9140193B2 (en) * | 2011-05-03 | 2015-09-22 | Siemens Energy, Inc. | Gas turbine igniter with structure to reduce radial movement of igniter rod |
US20150040575A1 (en) * | 2013-08-12 | 2015-02-12 | Unison Industries, Llc | Fuel igniter assembly having heat-dissipating element and methods of using same |
US9803554B2 (en) * | 2013-08-12 | 2017-10-31 | Unison Industries, Llc | Fuel igniter assembly having heat-dissipating element and methods of using same |
FR3068766A1 (en) * | 2017-07-10 | 2019-01-11 | Office National D'etudes Et Recherches Aerospatiales | COMBUSTION IGNITION OR STABILIZATION SYSTEM |
EP4235087A3 (en) * | 2019-05-10 | 2023-10-11 | Hamilton Sundstrand Corporation | Multi-use torpedo propulsion system starter |
Also Published As
Publication number | Publication date |
---|---|
GB1087537A (en) | 1967-10-18 |
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