This invention generally relates to spark plugs, and more particularly, to metal shells for spark plugs.
Low carbon steels (e.g., C1005, C1008, and C1010 steels) have been traditionally used as materials for extruded spark plug shells. These materials have lower strength and higher ductility, making them more suitable for deep extrusion. Typically, these low carbon steels are widely used for M12 spark plugs (shell outer diameter of 12 mm or 0.485 inches), as well as larger sized plugs.
With engine downsizing requirements, spark plugs are correspondingly downsizing, with sizes such as M8 and M10 being used more frequently. With this size decrease, there is also a trend of using a thicker ceramic insulator to increase the voltage capability of the spark plugs. This requires the use of thinner but stronger shell materials. To satisfy these requirements, higher strength steel materials for the shell are required. However, higher strength steel can oftentimes be more difficult to manufacture, in processes such as extrusion, to cite one example.
According to one example, there is provided a spark plug shell, comprising: a tubular body of steel material, the tubular body having an axial bore with a longitudinal axis (Lshell), wherein the steel material comprises 0.20-0.55 wt % carbon, inclusive, and includes a grain structure with a plurality of grains, each of the plurality of grains in the grain structure includes a longitudinal axis (LG) along a longest extent of the grain and, for a majority of the plurality of grains in the grain structure, the longitudinal axis (LG) of the grain is aligned with the longitudinal axis (Lshell) of the axial bore of the shell.
According to various embodiments, the spark plug shell may further include any one of the following features or any technically-feasible combination of some or all of these features:
the tubular body includes a terminal end, a free end, and a thread region located between the terminal end and the free end, wherein an outer diameter (ODshell) of the thread region is between 0.30-0.425 inches, inclusive;
According to another example, there is provided a spark plug shell, comprising: a tubular body of steel material, the tubular body having an axial bore with a longitudinal axis (Lshell), wherein the steel material comprises a balance of iron, 0.45-0.50 wt % carbon, 5-30 ppm boron, 0.30-1.00 wt % manganese, 0.001-0.10 wt % titanium, and at least one of 0.02-0.06 wt % aluminum or 0.01-0.30 wt % silicon, where each wt % is inclusive.
According to various embodiments, the spark plug shell may further include any one of the following features or any technically-feasible combination of some or all of these features:
According to another example, there is provided a method of manufacturing a spark plug shell, comprising the steps of: extruding a tubular body from a steel material, wherein the steel material comprises 0.20-0.55 wt % carbon, inclusive, and the tubular body has an axial bore with a longitudinal axis (Lshell); and crimping a hot lock region in the tubular body once an insulator has been inserted into the axial bore, wherein an outer diameter (ODHD) of the hot lock region is between 0.40 inches and 0.50 inches, inclusive.
Preferred exemplary embodiments will hereinafter be described in conjunction with the appended drawings, wherein like designations denote like elements, and wherein:
The spark plug described herein includes a metal shell made from a steel material having an increased carbon content, and advantageously, with the co-addition of boron. The steel material for the spark plug shell is well-suited for extrusion because of its ductility, while maintaining requisite strength. The spark plug shell described herein has a reduced outer diameter at a crimped hot lock region. In smaller spark plugs, such as M8 and M10 plugs, as opposed to M12 and M14 plugs, the proportionate diametric reduction at the hot lock region in particular may be more pronounced. The presently described steel material and extruded spark plug shell can help compensate for this diametric reduction at the hot lock region.
One embodiment of a spark plug is illustrated in
The center electrode 12 and/or the ground electrode 18 may include a nickel-based external cladding layer and a copper-based internal heat conducting core. Some non-limiting examples of nickel-based materials that may be used with the center electrode 12 and/or the ground electrode 18 include alloys composed of nickel (Ni), chromium (Cr), iron (Fe), aluminum (Al), manganese (Mn), silicon (Si), and any suitable alloy or combination thereof (e.g., Inconel 600, 601). The internal heat conducting core may be made of pure copper, copper-based alloys, or some other material with suitable thermal conductivity. Of course, other materials are certainly possible, including center and/or ground electrodes that have more than one internal heat conducting core or no internal heat conducting core at all.
The spark plug shell 16 provides an outer structure for the spark plug 10. The shell 16 includes a main tubular body 28 that axially extends between a free end 30 and a terminal end 32. The tubular body 28 includes axial bore 26 which may include various steps, seats, etc. for accommodating the insulator 14, and has a longitudinal axis Lshen that generally corresponds to the longitudinal axis of the spark plug Lplug. In an advantageous embodiment, the shell 16 is extruded with the various features such as steps, threads, etc. machined into the extruded body 28. However, in some embodiments, the body 28 of the shell 16 may be entirely machined. The shell 16 may also include other features not shown in the drawings, such as a nickel-based or zinc-based coating or cladding layer, to cite a few examples. The tubular body 28 of the shell 16 includes a number of regions along the axial extent of shell 16 between the free end 30 and the terminal end 32: a thread region 34, a seal region 36, a seat region 38, a hot lock region 40, a hex region 42, and a crimp region 44.
The thread region 34 is designed to be installed into an engine so that the firing end extends into a combustion chamber. The thread region 34 may include a plurality of threads 46 (only a few of which are labeled in
As shown, the ODshell at the thread region 34 decreases from about 0.485″ to about 0.350″ from the M12 to the M8 plug. In additional the TShell at the thread region 34 also decreases from about 0.0575″ to about 0.0500″ from the M12 to the M8 plug. At the hot lock region 40, although the thickness THL is about the same between the various plug sizes, the outer diameter ODHL decreases from 0.557″ to 0.494″ from the M12 to the M8 plug. Advantageously, the spark plug 10 has a thread region outer diameter ODshell that is between approximately 0.30″ and 0.425″ inches, inclusive, and a hot lock outer diameter ODHL that is between approximately 0.40″ and 0.50″, inclusive, for M8 and M10 plugs. The diametric reduction of the ODHL as the plug is downsized can highly increase the local stress level for a given pop up load or twist off torque load applied to the plug 10. To maintain the same (or improve) the twist off capability and/or the pop-up strength, an increase in steel strength of about 20-30% is required. In one embodiment, to transition from the M12 to M8 size in the table above, a 27% increase in steel strength is required.
The steel materials and grain structure of the steel material in the body 28 of the shell 16 can help increase the steel strength and provide better structural reinforcement, particularly in the hot lock region 40 where the proportional diametric reduction is more pronounced. In some advantageous embodiments, the steel material has a higher proportion of carbon than other steels often used for spark plug shells. In other advantageous embodiments, the steel material includes the co-addition of carbon and boron in certain amounts to improve ductility while increasing strength. Additionally, in combination with one or more embodiments described herein, the steel material may have a particular grain structure to help impart force tolerance. The described grain structure may be imparted via particular manufacturing processes, such as extrusion, which is not a feasible process for some steel types that do not have the requisite ductility.
In general, the steel material for the spark plug shell 16 includes an iron (Fe) balance, a carbon (C) content of 0.20 to 0.55 weight percent, and a manganese (Mn) content of 0.30 to 1.00 weight percent (all example ranges described herein are inclusive). In a more advantageous embodiment, the carbon content is 0.45 to 0.50 weight percent, with 0.45 weight percent preferred to achieve the mechanical strength necessary to at least partially counteract the diametric reduction of the hot lock region 40. The manganese can be added to the steel material to de-oxidize the steel melts, and can help form manganese sulphide (MnS) with sulfur to benefit machining while also helping to balance potential brittleness from sulfur. In some embodiments, the steel material for the shell 16 includes no or trace amounts of Nickel (Ni), Chromium (Cr), Vanadium (V), and Molybdenum (Mo).
Advantageously, in some embodiments, the steel material contains boron (B). The boron addition can enhance the strength through hardenability. The amount of boron is preferably 5 to 30 parts per million (ppm). To encourage the mechanical strengthening effect of boron, titanium (Ti) can be added, along with aluminum (Al) or silicon (Si) to fix nitrogen and oxygen in the steel.
In one particular embodiment, the steel material has a balance of iron, a carbon content of 0.20 to 0.55 weight percent, a manganese content of 0.30 to 1.00 weight percent, boron in the range of 5 to 30 ppm, a titanium content of 0.001 to 0.10 weight percent, and either an aluminum content of 0.02 to 0.06 weight percent or a silicon content of 0.01 to 0.30 weight percent. In another particular embodiment, the steel material has a balance of iron, a carbon content of 0.25 to 0.55 weight percent, a manganese content of 0.60 to 0.90 weight percent, boron in the range of 5 to 30 ppm, a titanium content of 0.01 to 0.05 weight percent, and an aluminum content of 0.02 to 0.06 weight percent. In yet another embodiment, the steel material has a balance of iron, a carbon content of 0.40 to 0.50 weight percent, a manganese content of 0.60 to 0.90 weight percent, boron in the range of 5 to 30 ppm, a titanium content of 0.01 to 0.10 weight percent, and an aluminum content of 0.02 to 0.06 weight percent. In all of these embodiments, the carbon content may be advantageously limited to 0.45 to 0.50 weight percent, particularly with the co-addition of 5-30 ppm boron, to help achieve the mechanical strength necessary to at least partially counteract the diametric reduction of the hot lock region 40.
With typical M12 plugs that use 1008/1010 steel, for example, the tensile strength is about 300-350 MPa. The example materials disclosed above have a tensile strength of 450-500 MPa to provide more structural mechanical strength to the diametrically reduced areas of the shell 16, such as the hot lock region 40.
Additionally, in some embodiments, the steel material can be annealed. For annealed materials, the tensile strength is about 450 MPa and the yield strength is about 280 MPa. For unannealed steel, the tensile strength is about 600-700 MPa and the yield strength is about 350-400 MPa. If the shell 16 is to be machined and not manufactured using a deep extrusion process, the steel materials do not need to be annealed to maintain their higher strength. If an extrusion process is used, it may be desirable to anneal the steel material.
As schematically shown in
It is to be understood that the foregoing is a description of one or more preferred example embodiments of the invention, and the figures are examples that are not necessarily to scale. The invention is not limited to the particular embodiment(s) disclosed herein, but rather is defined solely by the claims below. Furthermore, the statements contained in the foregoing description relate to particular embodiments and are not to be construed as limitations on the scope of the invention or on the definition of terms used in the claims, except where a term or phrase is expressly defined above. Various other embodiments and various changes and modifications to the disclosed embodiment(s) will become apparent to those skilled in the art. All such other embodiments, changes, and modifications are intended to come within the scope of the appended claims.
As used in this specification and claims, the terms “for example,” “e.g.,” “for instance,” “such as,” and “like,” and the verbs “comprising,” “having,” “including,” and their other verb forms, when used in conjunction with a listing of one or more components or other items, are each to be construed as open-ended, meaning that the listing is not to be considered as excluding other, additional components or items. Other terms are to be construed using their broadest reasonable meaning unless they are used in a context that requires a different interpretation.
This application claims the priority of U.S. provisional application No. 62/832,557, filed Apr. 11, 2019, the entire contents of which is hereby incorporated by reference.
Filing Document | Filing Date | Country | Kind |
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PCT/US2020/027508 | 4/9/2020 | WO | 00 |
Number | Date | Country | |
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62832557 | Apr 2019 | US |