US2526933A - Aviation spark plug - Google Patents

Aviation spark plug Download PDF

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Publication number
US2526933A
US2526933A US775729A US77572947A US2526933A US 2526933 A US2526933 A US 2526933A US 775729 A US775729 A US 775729A US 77572947 A US77572947 A US 77572947A US 2526933 A US2526933 A US 2526933A
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Prior art keywords
spark plug
barrel
potential
liner
center electrode
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Expired - Lifetime
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US775729A
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Robert K Christie
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Federal Mogul Ignition LLC
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Champion Spark Plug Co
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    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B15/00Suppression or limitation of noise or interference
    • H04B15/02Reducing interference from electric apparatus by means located at or near the interfering apparatus
    • H04B15/025Reducing interference from ignition apparatus of fuel engines

Definitions

  • This invention relates to a spark plug of the type used in aircraft engines and is particularly directed to means to reduce or eliminate the formation of corona and accidental electrical discharge Within the spark plug body.
  • Figure 1 is a central vertical section of a spark plug embodying the present invention
  • Fig. 2 is a section on line 2 2 of Fig. 1
  • Fig. 3 is a 'fragmentary sectional View, 'somewhat enlarged, ,Y
  • Fig. 4 is a plan view of an electrode bridging disc
  • Fig. 5 is a fragmentary sectional view of a modified form of the invention applied to a conventional radio shielded spark plug.
  • a spark plug constructed in accordance with the invention is shown in Fig. 1, and ⁇ includes a shell i0 having a threaded part Il for engagement with an engine cylinder head.
  • a shield barrel l2 eX- tends upwardly from the shell l0 and is mechanically and electrically united with the shell so that it is at ground potential.
  • Fixed in the shell l0 is a, core i4 which is held in place in any suitable manner, preferably by a malleable locking sleeve which is compressed and deformed so that a part of the metal of which the locking ring is composed flows into a groove in the core.
  • the construction of the shield barrel and the manner of locking the assembled parts in place form no part of the present invention.
  • the upper end of the shield barrel receives a conventional ignition harness (not shown) -With a connector cable protruding into the upper end of the barrel to make electrical contact with a center electrode i3.
  • the center electrode assembly may be of any suitable construction and may include a small series resistor I9 disposed between the cable tip and the electrode proper.
  • the electrode may be held in the core and sealed against gas leakage by a body of compacted powder 2 l. At its firing end the center electrode cooperates with ksuitable ground electrodes 22 carried by the shell I0.
  • the connector cable is at high potential it is necessary to provide an insulating lining for the shield barrel.
  • a single ceramic member 26 is used, that serves not only to support and insulate the center electrode, but also to line the shield barrel.
  • the unitary piece there are, of course, no joints to be sealed, there is no problem of dissimilar thermal expansion and no problem of non-uniform potential gradients through closely adjacent insulating parts.
  • the exterior of the shield barrel liner is at ground potential and there is little or no increase in potential as the axis of the spark plug is approached.
  • the interior of the liner is very close to ground potential while the metallic connector parts adjacent the upper end of the center electrode are at the highest potential in the entire system.
  • the surrounding air thus becomes the determining factor as to electrical breakdown. At high altitudes this air is raried and is easily ionizable. Further there are always surfaces having low radii of curvature, if not sharp points, adjacent which corona formation can begin readily. Once begun the corona spreads until it reaches the insulating sleeve at which time the inner part of the sleevehas assumed maximum potential and the outside has ⁇ remained at ground potential.
  • the thicknessof the sleeve is. alwaysenough so that 'no breakdown occurs through a uniform -section, but the corona spreads throughout the barrel so that ashover occurs usually around the end of the sleeve, either at the top or the bottom.
  • the exterior of the single insulating member 26 is at ground potential, and uniformity in this direction may be further assured by coating the exterior of the piece with metal 29 either in the form of foil or by sputtering or otherwise.
  • a metallic bridging disc 30 is provided which overlies the center electrode and extends radially :towards the ceramic piece 2S. .formed with an expansion ridge 3l and is nor- .mally of such diameter as to lie closely against :the interior wall of the ceramic core and shield .liner 26.
  • the two parts are joined together by .a mass which adheres to both, indicated at 32, 'which preferably comprises a body of glass formed
  • the disc 30 is 4by melting a mass of glass in place so that it unites both with the metallic disc and with the normal glaze of the insulator.
  • the disc at its lower side is fixed either to the 4center electrode or to the series resistor I9 if one is used. In either event the disc assumes the high potential of the cable tip when the spark plug is in use.
  • the inside surface of the ceramic core and liner portion 2S is likewise at high potential so that the entire potential drop occurs across the ceramic liner with no intervening air gaps. Under these circumstances, and because of the relatively smooth surface of the metal disc, the formation of corona is very unlikely.
  • radial expansion of disc 3i] is taken in the ridge 3i which can, at the same time, allow for axial expansion of the center electrode parts without disturbing the seal 32.
  • the center electrode of a conventional radio shielded spark plug is indicated at 5i), the liner for the shield barrel at 5
  • a connector cable 53 extends into the barrel and carries a tip 54 of insulating material and a metal grommet 55 to which the conductor 55 is soldered.
  • a connector spring 5'1 contacts the center electrode 59 and is also in electrical contact with a shoulder 58 on the grommet 55. Also fixed in place by shoulder 58 is a mass of resilient conducting material 59 formed preferably as a cup having a normal diameter greater than the bore into which it is inserted.
  • the conducting material 59 is preferably a plastic material known commercially as conducting rubber and, while retaining the resilient properties of rubber, has an electrical resistance of the order of -50 ohms per inch.
  • the outer face of the cup of conducting rubber is thus at a potential very close to that of the conductor 56 and is in close compressive contact with the inner surface of liner 5
  • the present invention provides a spark plug structure in which electrical failure caused by ionization of air Within the barrel or by failure at a joint between adjacent elements is practically eliminated. While two preferred embodiments of the invention have been shown and described, it should be expressly understood that numerous modications and changes may be made without departing from the invention as defined in the appended claims.
  • a spark plug of the class described a grounded metallic shell, a functionally integral barrel member extending from said shell, a. ceramic liner for said barrel member having its exterior at the same potential as said barrel, a center electrode assembly mounted in said shell but insulated therefrom and terminating within said ceramic liner, and an expansible metallic conducting member electrically connected to the top of said center electrode assembly and to the interior of said ceramic liner whereby the interior of said liner, at the juncture, is at electrode potential.
  • a grounded metallic shell a functionally integral barrel member extending from said shell, a ceramic liner for said barrel member having its exterior at the same potential as said barrel, a center electrode assembly mounted in said shell but insulated therefrom and terminating within said ceramic liner, and an expansible metal disc having its center portion electrically connected to said center electrode assembly and a peripheral seal connecting said disc to the interior of said ceramic liner whereby the interior of said liner, at the seal line, is at electrode potential.
  • peripheral seal for said metal disc comprises a fused mass which is united to the interior of said ceramic liner.
  • a grounded metallic shell a functionally integral barrel member extending from said shell, a unitary ceramic member fixed in said shell and locked against movement relative thereto, a portion of said ceramic member extending into said barrel as a liner, said last portion being in the form of a tube the exterior of which is at the same potential as said barrel member, a center electrode assembly mounted in said ceramic member and terminating below the upper end thereof, and expansible means to establish an area on the interior of said ceramic member which is at substantially the same potential as said center electrode.

Description

Oct. 24, 1950 R. K. CHRISTIE AVIATION SPARK PLUG Filed sept. 2:5, 1947 Z 4 569,1 0 J 5555.5 5 E E 7 A# T. N/////// ////%V/ llllll A .,W/// 1111 i l INI /EN TOR. @auf da@ BY Patented Oct. 24, 1950 AVIATION SPARK PLUG Robert K. Christie, Toledo, Ohio, assignor to Champion Spark Plug Company, Toledo, Ohio, a corporation of Delaware Application September 23, 1947, Serial No. 775,729
Claims.
This invention relates to a spark plug of the type used in aircraft engines and is particularly directed to means to reduce or eliminate the formation of corona and accidental electrical discharge Within the spark plug body.
In the operation of aircraft engines at high altitude, difliculty has been encountered due to disruptive electrical discharge within the barrel portion of radio shielded spark plugs withfwhich the engines are commonly equipped. Such discharge, of course, prevents normal engine ignition and results in loss of power. Various expedients have been tried in an effort to eliminate this dif culty. In certain instances attempts have been made to eliminate the easily ionizable raried air from the spark plug barrel, and in other instances it has been attempted to maintain normal atmospheric pressure in the barrel as well as in the entire ignition harness. While a degree of success has been attained by these expedients, their adoption is costly and is attended by certain disadvantages.
It is the primary object of the present invention to eliminate the formation of corona in a radio shielded aircraft spark plug by so adjusting the potential gradients existing therein that disruptive discharge does not occur.
Other objects and advantages of the invention will become apparent from the following specillcation, reference being had to the accompanying drawings in which:
Figure 1 is a central vertical section of a spark plug embodying the present invention; Fig. 2 is a section on line 2 2 of Fig. 1; Fig. 3 is a 'fragmentary sectional View, 'somewhat enlarged, ,Y
of a portion of the spark plug shown in Fig. l; Fig. 4 is a plan view of an electrode bridging disc, and Fig. 5 is a fragmentary sectional view of a modified form of the invention applied to a conventional radio shielded spark plug.
Referring t0 the drawings, one form of a spark plug constructed in accordance with the invention is shown in Fig. 1, and `includes a shell i0 having a threaded part Il for engagement with an engine cylinder head. A shield barrel l2 eX- tends upwardly from the shell l0 and is mechanically and electrically united with the shell so that it is at ground potential. Fixed in the shell l0 is a, core i4 which is held in place in any suitable manner, preferably by a malleable locking sleeve which is compressed and deformed so that a part of the metal of which the locking ring is composed flows into a groove in the core. The construction of the shield barrel and the manner of locking the assembled parts in place form no part of the present invention.
The upper end of the shield barrel receives a conventional ignition harness (not shown) -With a connector cable protruding into the upper end of the barrel to make electrical contact with a center electrode i3. (See Fig. 5.) The center electrode assembly may be of any suitable construction and may include a small series resistor I9 disposed between the cable tip and the electrode proper. The electrode may be held in the core and sealed against gas leakage by a body of compacted powder 2 l. At its firing end the center electrode cooperates with ksuitable ground electrodes 22 carried by the shell I0.
Since the connector cable is at high potential it is necessary to provide an insulating lining for the shield barrel. In the present instance a single ceramic member 26 is used, that serves not only to support and insulate the center electrode, but also to line the shield barrel. In the unitary piece there are, of course, no joints to be sealed, there is no problem of dissimilar thermal expansion and no problem of non-uniform potential gradients through closely adjacent insulating parts.
In the known shielded spark plugs the exterior of the shield barrel liner is at ground potential and there is little or no increase in potential as the axis of the spark plug is approached. Thus the interior of the liner is very close to ground potential while the metallic connector parts adjacent the upper end of the center electrode are at the highest potential in the entire system. The surrounding air thus becomes the determining factor as to electrical breakdown. At high altitudes this air is raried and is easily ionizable. Further there are always surfaces having low radii of curvature, if not sharp points, adjacent which corona formation can begin readily. Once begun the corona spreads until it reaches the insulating sleeve at which time the inner part of the sleevehas assumed maximum potential and the outside has `remained at ground potential. The thicknessof the sleeve is. alwaysenough so that 'no breakdown occurs through a uniform -section, but the corona spreads throughout the barrel so that ashover occurs usually around the end of the sleeve, either at the top or the bottom.
In the present invention the exterior of the single insulating member 26 is at ground potential, and uniformity in this direction may be further assured by coating the exterior of the piece with metal 29 either in the form of foil or by sputtering or otherwise.
In the form of the invention shown in Figs. 1 to 4, a metallic bridging disc 30 is provided which overlies the center electrode and extends radially :towards the ceramic piece 2S. .formed with an expansion ridge 3l and is nor- .mally of such diameter as to lie closely against :the interior wall of the ceramic core and shield .liner 26. The two parts are joined together by .a mass which adheres to both, indicated at 32, 'which preferably comprises a body of glass formed The disc 30 is 4by melting a mass of glass in place so that it unites both with the metallic disc and with the normal glaze of the insulator.
The disc at its lower side is fixed either to the 4center electrode or to the series resistor I9 if one is used. In either event the disc assumes the high potential of the cable tip when the spark plug is in use. Thus the inside surface of the ceramic core and liner portion 2S is likewise at high potential so that the entire potential drop occurs across the ceramic liner with no intervening air gaps. Under these circumstances, and because of the relatively smooth surface of the metal disc, the formation of corona is very unlikely. As the spark plug heats in use, radial expansion of disc 3i] is taken in the ridge 3i which can, at the same time, allow for axial expansion of the center electrode parts without disturbing the seal 32.
In the modified form of the invention shown in Fig. 5, the center electrode of a conventional radio shielded spark plug is indicated at 5i), the liner for the shield barrel at 5| and the barrel itself at 52. A connector cable 53 extends into the barrel and carries a tip 54 of insulating material and a metal grommet 55 to which the conductor 55 is soldered. A connector spring 5'1 contacts the center electrode 59 and is also in electrical contact with a shoulder 58 on the grommet 55. Also fixed in place by shoulder 58 is a mass of resilient conducting material 59 formed preferably as a cup having a normal diameter greater than the bore into which it is inserted.
The conducting material 59 is preferably a plastic material known commercially as conducting rubber and, while retaining the resilient properties of rubber, has an electrical resistance of the order of -50 ohms per inch. The outer face of the cup of conducting rubber is thus at a potential very close to that of the conductor 56 and is in close compressive contact with the inner surface of liner 5| so that-this surface is also at or near electrode potential. or no dielectric stress in the air around the upper end of the center electrode 5U, corona formation is effectively inhibited.
It will thus be seen that the present invention provides a spark plug structure in which electrical failure caused by ionization of air Within the barrel or by failure at a joint between adjacent elements is practically eliminated. While two preferred embodiments of the invention have been shown and described, it should be expressly understood that numerous modications and changes may be made without departing from the invention as defined in the appended claims.
Having thus described my invention, what I Since there is little Ill 4 claim as new, and desire to secure by United States Letters Patent, is:
1.`In a spark plug of the class described, a grounded metallic shell, a functionally integral barrel member extending from said shell, a. ceramic liner for said barrel member having its exterior at the same potential as said barrel, a center electrode assembly mounted in said shell but insulated therefrom and terminating within said ceramic liner, and an expansible metallic conducting member electrically connected to the top of said center electrode assembly and to the interior of said ceramic liner whereby the interior of said liner, at the juncture, is at electrode potential.
2. In a spark plug of the class described, a grounded metallic shell, a functionally integral barrel member extending from said shell, a ceramic liner for said barrel member having its exterior at the same potential as said barrel, a center electrode assembly mounted in said shell but insulated therefrom and terminating within said ceramic liner, and an expansible metal disc having its center portion electrically connected to said center electrode assembly and a peripheral seal connecting said disc to the interior of said ceramic liner whereby the interior of said liner, at the seal line, is at electrode potential.
3. A device in accordance with claim 2 in which said peripheral seal for said metal disc comprises a fused mass which is united to the interior of said ceramic liner.
4. In a spark plug of the class described, a grounded metallic shell, a functionally integral barrel member extending from said shell, a unitary ceramic member fixed in said shell and locked against movement relative thereto, a portion of said ceramic member extending into said barrel as a liner, said last portion being in the form of a tube the exterior of which is at the same potential as said barrel member, a center electrode assembly mounted in said ceramic member and terminating below the upper end thereof, and expansible means to establish an area on the interior of said ceramic member which is at substantially the same potential as said center electrode.
5. A spark plug in accordance with claim 4 in which said last means comprises a mass of conductive rubber.
ROBERT K. CHRISTIE.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,988,859 Shumaker Jan. 22, 1935 2,258,810 Rabezzana et al. Oct. 14, 1941 2,368,889 Setterblade Feb. 6, 1945 2,377,213 Danziger May 29, 1945 2,436,973 Pereles Mar. 2, 1948
US775729A 1947-09-23 1947-09-23 Aviation spark plug Expired - Lifetime US2526933A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2878299A (en) * 1954-12-23 1959-03-17 Allan M Starr Spark plug
US3146301A (en) * 1958-04-21 1964-08-25 Bendix Corp Spark discharge device
US3771006A (en) * 1972-02-14 1973-11-06 N Berry Ignition circuit radiation suppression structure
US20130264935A1 (en) * 2012-04-10 2013-10-10 Ngk Spark Plug Co., Ltd. Electrode-attached insulator and spark plug

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1988859A (en) * 1931-07-07 1935-01-22 Raymond L Shumaker Spark plug shield
US2258810A (en) * 1940-01-05 1941-10-14 Gen Motors Corp Shielded aircraft spark plug
US2368889A (en) * 1941-10-10 1945-02-06 Wright Aeronautical Corp Shielded spark plug
US2377213A (en) * 1943-07-09 1945-05-29 Henry L Crowley & Company Inc Electrical device
US2436973A (en) * 1943-04-10 1948-03-02 Pereles Maurice Spark plug

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1988859A (en) * 1931-07-07 1935-01-22 Raymond L Shumaker Spark plug shield
US2258810A (en) * 1940-01-05 1941-10-14 Gen Motors Corp Shielded aircraft spark plug
US2368889A (en) * 1941-10-10 1945-02-06 Wright Aeronautical Corp Shielded spark plug
US2436973A (en) * 1943-04-10 1948-03-02 Pereles Maurice Spark plug
US2377213A (en) * 1943-07-09 1945-05-29 Henry L Crowley & Company Inc Electrical device

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2878299A (en) * 1954-12-23 1959-03-17 Allan M Starr Spark plug
US3146301A (en) * 1958-04-21 1964-08-25 Bendix Corp Spark discharge device
US3771006A (en) * 1972-02-14 1973-11-06 N Berry Ignition circuit radiation suppression structure
US20130264935A1 (en) * 2012-04-10 2013-10-10 Ngk Spark Plug Co., Ltd. Electrode-attached insulator and spark plug
US8933618B2 (en) * 2012-04-10 2015-01-13 Ngk Spark Plug Co., Ltd. Electrode-attached insulator and spark plug

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