1. Field of the Invention
This invention pertains to ignition systems and more particularly to spark igniters for burners and burner pilots.
2. Description of the Related Art
A gas burner pilot is a device used to create a stable pilot flame by combustion of a low flow rate (relative to the main burner) gaseous fuel-air mixture. The pilot flame is used to light a larger main burner, or a difficult to light fuel. Gas pilot designs normally include an ignition system. One common type of ignition systems used in gas burner pilots, as well as other systems such as flare systems, is a high-energy ignition (HEI).
An HEI system typically utilizes a capacitive discharge exciter to pass large current pulses to a spark rod. The large current pulses are often greater than 1 kA. The spark igniter (also known as spark plug, spark rod or igniter probe) for an HEI system is generally constructed using a center electrode surrounded by an insulator and an outer conducting shell over the insulator such that, at the axially-facing ignition end of the spark rod, an air gap is formed between the center electrode and the outer conduction shell, i.e., a gap between the center electrode and the outer electrode shell or conducting shell. At this air gap, also called a spark gap, a high-energy spark can pass between the center electrode and outer conducting shell. Often a semiconductor material is applied to the insulating material at this gap to facilitate sparking. HEI systems have the ability to maintain powerful high energy sparks in adverse conditions such as cold temperatures, heavy fuels (heavy gases or oils), contamination of the igniter plug with coking or other debris and moisture presence due to steam purging or rain.
Past HEI spark igniter designs produced sparks on an axial-facing surface (referred to herein after as “axial-directed spark igniter”). One variable that affects spark energy is the size of the air gap on the axial-facing surface of the igniter. As the air gap increases, the amount of energy released during the spark event also increases. Air gaps generally range in size from 1 mm to 2 mm.
The center electrode, the electrode shell and semiconductor material erode away as sparking occurs over the course of an igniter's life. An igniter generally reaches the end of its life when either the semiconductor has worn away or when the air gap has become too large due to electrode erosion. Thus, while there is a desire to have relatively large air gaps because fuel ignition is more likely with higher energy release, problems are encountered with increasing the air gap size. Increased air gap size means either a shorter igniter life due to less material used in the center electrode and/or electrode shell or a larger higher-cost igniter due to an increased outer shell diameter and, hence, increased material. It would be desirable to have an igniter allowing for an increased gap size without significantly increasing the size or amount of material used and without adversely affecting igniter life.
In addition to the above considerations, the igniter life can be shortened by the exposure of the semiconductor material to flame radiation. In some burner pilot configurations, the flame may root in a position in which the igniter's semiconductor material is exposed to flame radiation. Flame radiation damages the semiconductor material, which generally reduces the life of an igniter. Accordingly, it would be desirable to avoid this problem in a burner pilot design.
In accordance with one embodiment of the current invention there is provided a spark igniter comprising a plurality of electrodes and an insulator, which are configured to form an elongated body having a first end, a second end and an outer surface extending between the first end and the second end. The spark igniter is configured so as to produce a radially-directed spark.
In accordance with another embodiment of the current invention there is provided a burner pilot comprising a source of electrical energy, a spark igniter, and a housing. The spark igniter has a first end, a second end, an outer surface, a center electrode, an electrode shell and an insulator. The outer surface comprises an end surface at the first end and a side surface extending from the second end toward the first end. The center electrode extends from the second end toward the first end. The electrode shell surrounds the center electrode and forms at least part of the side surface. The insulator is between the center electrode and outer electrode shell. The center electrode, the electrode shell and the insulator are configured to form a spark gap on the side surface, which produces a radially-directed spark, and the center electrode and electrode shell are connected to the source of electrical energy at the second end. The housing has a fuel flow passage which contains the first end of the spark igniter such that the spark gap is within the fuel flow passage.
In accordance with yet another embodiment of the invention, there is provided a method of igniting a fuel gas comprising: introducing the fuel gas into a flow passage having an ignition end wherein the flow passage defines an aperture at the ignition end and wherein the flow passage contains a spark igniter having an elongated igniter body terminating at a first end in a spark tip having a side surface and an end surface and wherein the spark tip is located adjacent to the ignition end of the flow passage; and producing a radially-directed spark to thus ignite the fuel and produce a flame at the ignition end.
The description below and the figures illustrate a spark igniter and burner pilot of the type used in a furnace having a main burner that supplies a fuel and air mixture to the furnace and a burner pilot adjacent to the main burner for igniting the fuel and air mixture. While the invention is described in the context of a burner pilot for such a furnace, it will be appreciated that the inventive spark igniter is more broadly applicable as an ignition system for fuels and can be applied to other systems such as flare systems.
Referring now to
Housing 114 surrounds spark igniter 100. Housing 114 forms a fuel channel 115, which surrounds spark igniter 100. The end 116 of housing 114 forms an opening. Fuel flows through fuel channel 115 and towards the opening in a generally axial direction parallel with the longitudinal axis of spark igniter 100.
As can be seen from
Turning now to
Fuel introduction pipe 218 is in fluid flow communication with a fuel source (not shown) and longitudinal fuel flow passage 212 of tube portion 204. Generally, a fuel-air mixture will be introduced into passage 212 through pipe 218 such that the fuel-air mixture will flow in a generally longitudinal direction towards first end 208 and out opening 214.
Extending longitudinally inside and along longitudinal passage 212 is a spark igniter 300. Generally, spark igniter 300 is held in place by sealing device 220 and structural supports 222. Structural supports 222 can be perforated to limit obstruction of the flow of the fuel and air mixture and can be shaped into swirling or diffusion elements to induce premixing of fuel and air within longitudinal passage 212 and prior to reaching the first end 302 of spark igniter 300.
Spark igniter 300 has a first end or igniter tip 302 located inside tube portion 204 but near the first end 208 of tube portion 204 and a second end 304 extending into electronics enclosure 216. As can best be seen from
As illustrated, spark igniter 300 is a high-energy igniter (HEI) probe. Accordingly, spark igniter 300 should be suitable to pass large current pulses (often greater than 1 kA) from an energy source to the spark gap and, thereby, generate a spark at the spark gap. The purpose of an HEI probe is to provide high ignition power. In applications with low temperatures, heavy fuels (heavy gases or oils), contamination of the igniter plug with coking or other debris, or moisture presence due to steam purging or rain, the main fuel may be difficult to light but an HEI system has the ability to maintain powerful high energy sparks in these adverse conditions.
An HEI system generally has a spark igniter and capacitive discharge system to provide a high-energy pulse to the spark igniter. As illustrated in
Spark igniter 300 is connected at its second end 304 to exciter 224 so that center electrode 306 is connected to a first terminal of exciter 224, generally the high voltage terminal, and electrode shell 310 is connected to a second terminal of exciter 224, generally the low voltage terminal, which can be electrically grounded.
Turning now on
The igniter tip 302 comprises an outer surface 314 comprised of a side surface 316 and end surface 318. The side surface 316 typically extends between the end surface 318 of the igniter tip 302 and the second end 304 of the spark igniter 300. The igniter tip 302 terminates in end surface 318, which is an axially-facing surface, as can be seen from the figures. Generally, the igniter tip in accordance with the invention is configured so that a spark gap 312 is on a radially-facing surface such as side surface 316 of spark igniter 300. In
As shown, insulator 308 extends concentrically around electrode 306 within electrode shell 310 so that the two electrodes do not make electrical contact. Further, spark gap 312 is between the electrode 306 and the electrode shell 310 and extends down to insulator 308 so that electrode 306 and electrode shell 310 do not make electrical contact. Additionally, there can be a semiconductor material 330 deposited on the insulator at the bottom of the spark gap 312. Semiconductor material 330 forms a conductive path between the electrode 306 and the electrode shell 310. This semiconductor can be a film applied to the insulator itself. This semiconductor assists the spark igniter 300 with spark initiation by allowing a low level of current to pass in the semiconductor when the energy source applies an ignition pulse to the electrode 306. This low level current flowing through the semiconductor creates a small ionized air zone above the path of current in the spark gap 312. This small ionized air path is a low impedance pathway for current flow. Once the pathway is established, the electrical energy is able to flow unresisted except for circuit impedance, thereby creating a very high current and energy spark at spark gap 312.
As illustrated in
The spark generated at spark gap 312 is projected perpendicular to the longitudinal axis of spark igniter 300 and outward into the fuel-air mixture flowing through tube portion 204 and will, thus, be projected perpendicular to the flow of the fuel-air mixture, as shown by arrow 313. In the embodiment illustrated, the spark igniter is cylindrical and thus the spark is projected radially outward; however, a similar spark projection, perpendicular to the longitudinal axis, will apply to other configurations, such as a spark igniter having a square, rectangular, triangular or oblong cross-section, and will generally be herein referred to as a “radially-directed spark.” The spark will ignite the fuel-air mixture forming a flame that will be located downstream from end surface 318; that is, the flame will be located on the other side of end surface 318 from spark gap 312. Accordingly, cap 324 will act to shield the spark gap 312 and semiconductor material 330 from flame radiation generated from the flame. Turning now to
Turning now to
Turning now to
In the above embodiments, the semiconductor may be deposited on only a portion of the surface of the insulator in the spark gap to effectively reduce the spark direction. For example, in the embodiment illustrated in
In order to further illustrate the spark igniter of this invention, its operation and the methods of the invention, the following example is given.
Three igniter tips were life tested by repeatedly firing each igniter tip until it no longer fired. Control 1 and Control 2 were axially-directed spark tips and Example 1 was a radially-directed spark tip in accordance with the embodiment of the invention illustrated in
As can be seen from Table I, the inventive radially-directed spark tip (Example 1) had a significantly longer spark life than either of the traditional axially-directed spark tips (Control 1 and Control 2). Example 1 had a 218% longer spark life than Control 1 and a 179% longer spark life than Control 2.
Other embodiments of the current invention will be apparent to those skilled in the art from a consideration of this specification or practice of the invention disclosed herein. Thus, the foregoing specification is considered merely exemplary of the current invention with the true scope thereof being defined by the following claims.
Number | Name | Date | Kind |
---|---|---|---|
2064089 | Stemmeler | Dec 1936 | A |
2214958 | Gotterba et al. | Sep 1940 | A |
2332210 | Frank | Oct 1943 | A |
2501826 | McCarthy et al. | Mar 1950 | A |
2906922 | Huber | Sep 1959 | A |
3073121 | Baker et al. | Jan 1963 | A |
3312848 | Baum | Apr 1967 | A |
4187825 | Loyd, Jr. | Feb 1980 | A |
4621599 | Igashira et al. | Nov 1986 | A |
4695758 | Nishida et al. | Sep 1987 | A |
4711629 | MacDonald | Dec 1987 | A |
5074262 | McAbee | Dec 1991 | A |
6048196 | Collier et al. | Apr 2000 | A |
20110215703 | Maul | Sep 2011 | A1 |
Number | Date | Country |
---|---|---|
545351 | May 1942 | GB |
819256 | Sep 1959 | GB |
848070 | Sep 1960 | GB |
855440 | Nov 1960 | GB |
2361264 | Oct 2001 | GB |
S4719237 | Jul 1972 | JP |
S6158187 | Mar 1986 | JP |
S5888519 | Jun 1986 | JP |
9927303 | Jun 1999 | WO |
Entry |
---|
European search report issued Mar. 3, 2016 in corresponding European application No. 13826537.6, Chentronics Corporation. |
International Search Report and Written Opinion issued in correspohding PCT application No. PCT/US13/52938, Chentronics Corporation (Jan. 13, 2014). |
JP2015-52554 Japanese Search Report dated Mar. 1, 2016. |
Number | Date | Country | |
---|---|---|---|
20140038114 A1 | Feb 2014 | US |