US2485699A - Shielded spakk plug - Google Patents

Shielded spakk plug Download PDF

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US2485699A
US2485699A US2485699DA US2485699A US 2485699 A US2485699 A US 2485699A US 2485699D A US2485699D A US 2485699DA US 2485699 A US2485699 A US 2485699A
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core
spark plug
shell
shielded
barrel
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01TSPARK GAPS; OVERVOLTAGE ARRESTERS USING SPARK GAPS; SPARKING PLUGS; CORONA DEVICES; GENERATING IONS TO BE INTRODUCED INTO NON-ENCLOSED GASES
    • H01T13/00Sparking plugs
    • H01T13/02Details
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/04Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of riveting
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B2200/00Constructional details of connections not covered for in other groups of this subclass
    • F16B2200/10Details of socket shapes
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49908Joining by deforming
    • Y10T29/49925Inward deformation of aperture or hollow body wall
    • Y10T29/49927Hollow body is axially joined cup or tube
    • Y10T29/49929Joined to rod
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49908Joining by deforming
    • Y10T29/49925Inward deformation of aperture or hollow body wall
    • Y10T29/49934Inward deformation of aperture or hollow body wall by axially applying force
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/49Member deformed in situ
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/70Interfitted members
    • Y10T403/7075Interfitted members including discrete retainer
    • Y10T403/7077Interfitted members including discrete retainer for telescoping members

Definitions

  • SHIELDED SPARK PLUG Filed Nov. 22, 1946 INVENTOR. file/ 1 M BY I QNAQ Q a Patented Oct. 25, 1949 SHIELDED SPARK PLUG Robert K. Christie, Toledo, Ohio, assignor to Champion Spark Plug Company, Toledo, Ohio, a corporation of Delaware Application November 22, 1946, Serial No. 711,497
  • This invention relates to a shielded spark plug of the type used in aircraft and is particularly directed to a manner of assembling the component parts of such a spark plug.
  • Another object of the invention is to provide a shielded spark plug in which the parts are assembled under pressure.
  • Figure 1 is a side elevation, with parts in section, of a spark plug embodying the present invention, the parts being shown during assembly;
  • Fig. 2 is a top view of a locking sleeve;
  • Fig. 3 is a section on line 33 of Fig. 2;
  • Fig. 4 is a view similar to Fig. 3 showing the sleeve in its compressed form;
  • Fig. 5 is a central vertical section of a spark plug insulator, and
  • Fig. 6 is a section on line 6-6 of Fig. 1.
  • a spark plug embodying the invention comprises generally a shell l0 threaded for engagement with an engine cylinder head, a core H within the shell and a shield barrel I2 extending upwardly around the upper end of the core to form a recess in which electrical connection to the usual ignition lead is established.
  • the shell [0 is provided with the usual hex portion [3 by which the spark plug is positioned in an engine.
  • a center electrode I4 is fixed in the center of the core and projects outwardly therefrom to form a spark discharge gap with one or more side electrodes I5.
  • the shield barrel l2 has, at its top, a threaded area I 6 for engagement with an ignition harness, then an integral shoulder I1, next, a portion of uniform diameter, and at its lower end a reduced axial extension Ill.
  • the outside diameter of the major portion of the barrel corresponds to the inside diameter of the upper part of the shell I0 so that the two parts fit into close telescoping engagement over a part of the length of the barrel and shell.
  • the shell I0 is further provided with an intermediate bore l9 the diameter of which corresponds to the outside diameter of the axial extension l8 of the barrel l2.
  • the bore l9 terminates in a shoulder 20 and receives a locking sleeve 2
  • is preferably made of copper or other malleable metal of high heat conductivity and as shown in Figs. 3 and 4 is initially a uniform cylindrical member having an undercut or groove 22 in one of its surfaces.
  • groove 22 is in the outside surface of the
  • the core II is slipped into the barrel I2 and the locking ring 22 dropped into the bore l9 of the shell.
  • the barrel and core are then inserted the proper distance so that, the center electrode I4 properly coincides with the side electrodes.
  • the parts are then put into a press one element of which may conveniently bear against the under side of the hex portion -l3 and the opposite element of which places a closing force on shoulder I! as indicated in Fig. 1.
  • the core is now held firmly in place with relation to the locking ring. While the press is still closed or after the operation has been transferred to another press and the parts are under pressure, the assembly is completed by brazing or otherwise uniting the barrel l2 and the shell [0. The braze is indicated at 30 in Fig. 1. It will be seen that, in efiect, the plunger used to compress the locking ring remains in place as a part of the assembly and is not withdrawn as is the usual practice.
  • the groove 24 is made rounded so that the meta1 with which it is filled does not exert a direct tensile stress on the core when it expands under heat.
  • the metal has a much greater rate of thermal expansion than does the core.
  • this type are ordinarily fabricated is relatively weak in tension but very strong in compression. It will be apparent that forces tending to move the core axially in either direction with respect to the shell put the core in compression. Cores locked in this manner have been found to resist pressures in the order of 12,000 pounds per square inch in the barrel, being about the limit of bursting strength of the barrel, without appreciable unseating.
  • the present invention thus provides a spark plug assembly which is readily accomplished, strong in resistance to displacement of the parts
  • the material of which cores of and yet unlikely to be destroyed by heating and cooling cycles in use is readily accomplished. While the invention has been described in conjunction with a specific form and disposition of the parts, it should be expressly understood that it is capable of numerous modifications and changes without departing from the spirit of the appended claims.
  • a shell having an internal shoulder, a core received in said shell and having a circumferential groove, a locking sleeve for uniting said shell and core comprising an initially substantially cylindrical body of malleable metal seated on said shoulder and having a circumferential weakening groove in one of its surfaces adjacent the groove in said core, and means actuated by external pressure to deform said locking ring in such a manner that the shell and core are functionally united and a portion of the metal of the ring flows into the groove in said core.
  • a spark plug as defined in claim 1 in which the circumferential groove in said core is so rounded in cross section that thermal expansion of the locking sleeve material does not set up tensile stresses in the core material.

Description

Oct. 25, 1949. I R CHRISTIE 2,485,699
SHIELDED SPARK PLUG Filed Nov. 22, 1946 INVENTOR. file/=1 M BY I QNAQ Q a Patented Oct. 25, 1949 SHIELDED SPARK PLUG Robert K. Christie, Toledo, Ohio, assignor to Champion Spark Plug Company, Toledo, Ohio, a corporation of Delaware Application November 22, 1946, Serial No. 711,497
2 Claims. (01. 123-169) This invention relates to a shielded spark plug of the type used in aircraft and is particularly directed to a manner of assembling the component parts of such a spark plug.
It has heretofore been proposed to use a sleeve of malleable metal, either formed in situ or separately introduced and compressed, as a sealing and holding medium between the core and shell of a spark plug. The bond formed by such a sleeve is quite satisfactory in use and because of its high thermal conductivity has proved useful in installations where it is important that heat pass rapidly away from the core into the shell.
At high altitudes the tendency for a radio shielded spark plug to fail is increased because of the formation of corona within the upper portion of the barrel to the extent that an electrically conductive path is formed between a part at high potential and some other plug part that is at a lower potential. To overcome this tendency to flash-over, many expedients have been tried including attempts to occlude air from the barrel by completely filling this space with some flexible and deformable insulating substance such as a silicone resin. While the introduction of such material successfully prevents the ionization of a complete discharge path it poses other problems. For example, the thermal expansion of the confined resin body is so great that pressures exceeding 9000 pounds per square inch may be developed which are more than suflicient to unseat a core held by a metal sleeve seal.
It is the primary object of the present invention to provide a shielded spark plug in which the core is held in place so firmly that it cannot be unseated by any pressure likely to be encountered in practice.
Another object of the invention is to provide a shielded spark plug in which the parts are assembled under pressure.
Other objects and advantages of the invention will become apparent from the following specification, reference being had to the accompanying drawings in which:
Figure 1 is a side elevation, with parts in section, of a spark plug embodying the present invention, the parts being shown during assembly; Fig. 2 is a top view of a locking sleeve; Fig. 3 is a section on line 33 of Fig. 2; Fig. 4 is a view similar to Fig. 3 showing the sleeve in its compressed form; and Fig. 5 is a central vertical section of a spark plug insulator, and Fig. 6 is a section on line 6-6 of Fig. 1.
Referring to the drawings, a spark plug embodying the invention comprises generally a shell l0 threaded for engagement with an engine cylinder head, a core H within the shell and a shield barrel I2 extending upwardly around the upper end of the core to form a recess in which electrical connection to the usual ignition lead is established. The shell [0 is provided with the usual hex portion [3 by which the spark plug is positioned in an engine.
A center electrode I4 is fixed in the center of the core and projects outwardly therefrom to form a spark discharge gap with one or more side electrodes I5.
The shield barrel l2 has, at its top, a threaded area I 6 for engagement with an ignition harness, then an integral shoulder I1, next, a portion of uniform diameter, and at its lower end a reduced axial extension Ill. The outside diameter of the major portion of the barrel corresponds to the inside diameter of the upper part of the shell I0 so that the two parts fit into close telescoping engagement over a part of the length of the barrel and shell.
The shell I0 is further provided with an intermediate bore l9 the diameter of which corresponds to the outside diameter of the axial extension l8 of the barrel l2. The bore l9 terminates in a shoulder 20 and receives a locking sleeve 2| between the end of extension l8 and the shoulder.
The locking sleeve 2| is preferably made of copper or other malleable metal of high heat conductivity and as shown in Figs. 3 and 4 is initially a uniform cylindrical member having an undercut or groove 22 in one of its surfaces. In the form shown groove 22 is in the outside surface of the In assembling the parts the core II is slipped into the barrel I2 and the locking ring 22 dropped into the bore l9 of the shell. The barrel and core are then inserted the proper distance so that, the center electrode I4 properly coincides with the side electrodes. The parts are then put into a press one element of which may conveniently bear against the under side of the hex portion -l3 and the opposite element of which places a closing force on shoulder I! as indicated in Fig. 1. It will be "seen that as the press is closed, all of the force is exerted by the axial extension [8 of the barrel [2 to compress the locking sleeve 2| against shoulder 20. Being of a malleable metal the sleeve 2| is deformed and flows into groove 24. This action is facilitated by groove 22 in the locking sleeve since this latter roove is initially opposite the groove in the core and deformation of the locking sleeve will start at this point of smallest section.
The core is now held firmly in place with relation to the locking ring. While the press is still closed or after the operation has been transferred to another press and the parts are under pressure, the assembly is completed by brazing or otherwise uniting the barrel l2 and the shell [0. The braze is indicated at 30 in Fig. 1. It will be seen that, in efiect, the plunger used to compress the locking ring remains in place as a part of the assembly and is not withdrawn as is the usual practice.
As previously stated, the groove 24 is made rounded so that the meta1 with which it is filled does not exert a direct tensile stress on the core when it expands under heat. The metal has a much greater rate of thermal expansion than does the core. this type are ordinarily fabricated is relatively weak in tension but very strong in compression. It will be apparent that forces tending to move the core axially in either direction with respect to the shell put the core in compression. Cores locked in this manner have been found to resist pressures in the order of 12,000 pounds per square inch in the barrel, being about the limit of bursting strength of the barrel, without appreciable unseating.
The present invention thus provides a spark plug assembly which is readily accomplished, strong in resistance to displacement of the parts The material of which cores of and yet unlikely to be destroyed by heating and cooling cycles in use. While the invention has been described in conjunction with a specific form and disposition of the parts, it should be expressly understood that it is capable of numerous modifications and changes without departing from the spirit of the appended claims.
Having thus described my invention, what I claim as new and desire to secure b United States Letters Patent is:
1. In a spark plug of the type described, a shell having an internal shoulder, a core received in said shell and having a circumferential groove, a locking sleeve for uniting said shell and core comprising an initially substantially cylindrical body of malleable metal seated on said shoulder and having a circumferential weakening groove in one of its surfaces adjacent the groove in said core, and means actuated by external pressure to deform said locking ring in such a manner that the shell and core are functionally united and a portion of the metal of the ring flows into the groove in said core.
2. A spark plug as defined in claim 1 in which the circumferential groove in said core is so rounded in cross section that thermal expansion of the locking sleeve material does not set up tensile stresses in the core material.
- ROBERT K. CHRISTIE.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,356,104; Tognola Aug. 15, 1944 2,416,643 Rinehart Feb. 25, 1947
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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2835517A (en) * 1953-09-25 1958-05-20 Uster Spindel Motoren Maschf Holding device
US2854744A (en) * 1956-02-17 1958-10-07 Sydney R Crockett Method of locking and sealing tubular structures
US3055100A (en) * 1957-07-01 1962-09-25 Zeller Corp Method of forming interlocking joint between telescoped members
US3748723A (en) * 1970-12-03 1973-07-31 Shinko Wire Co Ltd Method of anchoring wires and strands in prestressed concrete
US4249298A (en) * 1978-03-27 1981-02-10 Hitachi, Ltd. Method for connecting two members
US20040062598A1 (en) * 2000-11-25 2004-04-01 Juergen Bassler Workpiece

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2356104A (en) * 1941-10-11 1944-08-15 Bendix Aviat Corp Spark plug and method of making the same
US2416643A (en) * 1945-04-03 1947-02-25 Carlton H Rinehart Spark plug

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2356104A (en) * 1941-10-11 1944-08-15 Bendix Aviat Corp Spark plug and method of making the same
US2416643A (en) * 1945-04-03 1947-02-25 Carlton H Rinehart Spark plug

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2835517A (en) * 1953-09-25 1958-05-20 Uster Spindel Motoren Maschf Holding device
US2854744A (en) * 1956-02-17 1958-10-07 Sydney R Crockett Method of locking and sealing tubular structures
US3055100A (en) * 1957-07-01 1962-09-25 Zeller Corp Method of forming interlocking joint between telescoped members
US3748723A (en) * 1970-12-03 1973-07-31 Shinko Wire Co Ltd Method of anchoring wires and strands in prestressed concrete
US4249298A (en) * 1978-03-27 1981-02-10 Hitachi, Ltd. Method for connecting two members
US20040062598A1 (en) * 2000-11-25 2004-04-01 Juergen Bassler Workpiece

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