TECHNICAL FIELD
This disclosure generally relates to spark plugs and other ignition devices for internal combustion engines and, in particular, to a firing pad that is attached to an electrode.
BACKGROUND
Spark plugs can be used to initiate combustion in internal combustion engines.
Spark plugs typically ignite a gas, such as an air/fuel mixture, in an engine cylinder or combustion chamber by producing a spark across a spark gap defined between two or more electrodes. Ignition of the gas by the spark causes a combustion reaction in the engine cylinder that causes the power stroke of the engine. The high temperatures, high electrical voltages, rapid repetition of combustion reactions, and the presence of corrosive materials in the combustion gases can create a harsh environment in which the spark plug functions. This harsh environment can contribute to erosion and corrosion of the electrodes and can negatively affect the performance of the spark plug over time, potentially leading to a misfire or some other undesirable condition.
To reduce erosion and corrosion of the spark plug electrodes, various types of noble metals and their alloys—such as those made from platinum and iridium—have been used. These materials, however, can be costly. Thus, spark plug manufacturers sometimes attempt to minimize the amount of precious metals used with an electrode by using such materials only at a firing tip of the electrodes where a spark jumps across a spark gap.
SUMMARY
According to one embodiment, a spark plug includes a shell, an insulator, a center electrode, a ground electrode, and a firing pad. The shell has an axial bore, and the insulator has an axial bore. The insulator is disposed partially or more within the shell's axial bore. The center electrode is disposed partially or more within the insulator's axial bore. The ground electrode is attached to the shell and is composed of a nickel-based alloy material. The firing pad is attached to the ground electrode and is composed of a platinum-based alloy material containing at least 25 wt. % of nickel. The firing pad has a protrusion that projects from a bottom side of the firing pad. The protrusion concentrates current flow therethrough when a resistance welding process is performed. The attachment between the firing pad and the ground electrode includes a resistance-welded weldment and lacks a laser-welded weldment. The protrusion facilitates the absence of the laser-welded weldment in the attachment between the firing pad and ground electrode.
According to another embodiment, a method of preparing a ground electrode and firing pad assembly includes several steps. One step involves locating a firing pad on a ground electrode. The firing pad has a protrusion projecting from a bottom side of the firing pad. The protrusion makes line-to-surface contact with the ground electrode. Another step involves passing electrical current through the line-to-surface contact between the protrusion and the ground electrode while pressing the firing pad and ground electrode together. The firing pad at least partially sinks into the ground electrode when passing electrical current and produces a surface-to-surface contact between the protrusion and ground electrode. The firing pad thereafter being attached to the ground electrode and establishing the ground electrode and firing pad assembly.
According to yet another embodiment, a spark plug includes a shell, an insulator, a center electrode, a ground electrode, a firing pad, and a resistance-welded expulsion. The shell has an axial bore, and the insulator has an axial bore. The insulator is disposed partially or more within the shell's axial bore. The center electrode is disposed partially or more within the insulator's axial bore. The ground electrode is attached to the shell.
The firing pad is attached to the ground electrode. The firing pad has a single protrusion that projects from a bottom side of the firing pad. The single protrusion spans across the bottom side and is received in a depression of the ground electrode upon attachment between the firing pad and ground electrode. The firing pad has a first sparking surface that exchanges sparks during use of the spark plug. The resistance-welded expulsion partly or more surrounds a peripheral edge of the firing pad. The resistance-welded expulsion has a second sparking surface that is generally in-line with the first sparking surface of the firing pad. The second sparking surface exchanges sparks during use of the spark plug.
BRIEF DESCRIPTION OF THE DRAWINGS
Preferred exemplary embodiments of the invention will hereinafter be described in conjunction with the appended drawings, wherein like designations denote like elements, and wherein:
FIG. 1 is a sectional view of an exemplary spark plug;
FIG. 2 is an enlarged view of a firing end of the spark plug of FIG. 1, where the firing end includes an exemplary firing pad;
FIG. 3 is an enlarged view of an exemplary ground electrode with the firing pad of FIG. 2;
FIGS. 4-7 are enlarged views of other exemplary ground electrodes and firing pads;
FIG. 8 is a perspective view of an embodiment of a firing pad with a pair of rails;
FIG. 9 is a perspective view of an embodiment of a firing pad with multi-layers;
FIG. 10 is a schematic of an exemplary method of preparing a ground electrode and firing pad assembly;
FIG. 11 is a microscopic image of a sectional view of an embodiment of a firing pad attached to a ground electrode;
FIG. 12 is a cross-sectional view of the firing pad and ground electrode of FIG. 11;
FIG. 13 is a perspective view of the firing pad of FIG. 11; and
FIG. 14 depicts the firing pad and ground electrode of FIG. 11 in the midst of being prepared via a resistance weld arbor.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
The firing pads and electrodes described herein can be used in spark plugs and other ignition devices including industrial plugs, aviation igniters, or any other device that is used to ignite an air/fuel mixture in an engine. This includes spark plugs used in automotive internal combustion engines, and particularly in engines equipped to provide gasoline direct injection (GDI), engines operating under lean burning strategies, engines operating under fuel efficient strategies, engines operating under reduced emission strategies, or a combination of these. The various firing pads and electrodes may provide improved ignitability, effective pad retention, increased pad exposure to air/fuel mixture, and cost effective solutions for the use of noble metal, to cite some possible improvements. As used herein, the terms axial, radial, and circumferential describe directions with respect to the generally cylindrical shape of the spark plug of FIG. 1 and with reference to a center axis A of the spark plug, unless otherwise specified.
Referring to FIG. 1, a spark plug 10 includes a center electrode (CE) base or body 12, an insulator 14, a metallic shell 16, and a ground electrode (GE) base or body 18. Other components can include a terminal stud, an internal resistor, various gaskets, and internal seals, all of which are known to those skilled in the art. The CE body 12 is generally disposed within an axial bore 20 of the insulator 14, and has an end portion exposed outside of the insulator at a firing end of the spark plug 10. In one example, the CE body 12 is made of a nickel (Ni) alloy material that serves as an external or cladding portion of the body, and includes a copper (Cu) or Cu alloy material that serves as an internal core of the body; other materials and configurations are possible including a non-cored body of a single material. The insulator 14 is generally disposed within an axial bore 22 of the metallic shell 16, and has an end nose portion exposed outside of the shell at the firing end of the spark plug 10. The insulator 14 is made of a material, such as a ceramic material, that electrically insulates the CE body 12 from the metallic shell 16. The metallic shell 16 provides an outer structure of the spark plug 10, and has threads for installation in an engine.
Referring now to FIGS. 1 and 2, the GE body 18 is attached to a free end of the metallic shell 16 at an attachment interface 24 and, as a finished product, may have a generally L-shape. At an end portion nearest a spark gap G, the GE body 18 is axially spaced from the CE body 12 and from a CE firing tip 26 (if one is provided). Like the CE body, the GE body 18 may be made of a Ni alloy material that serves as an external or cladding portion of the body, and can include a Cu or Cu alloy material that serves as an internal core of the body; other examples are possible including non-cored bodies of a single material. Some non-limiting examples of Ni alloy materials that may be used with the CE body 12, GE body 18, or both, include an alloy composed of one or more of Ni, chromium (Cr), iron (Fe), manganese (Mn), silicon (Si), or another element; and more specific examples include materials commonly known as Inconel® 600 or 601. In cross-sectional profile, the GE body 18 can have a generally rectangular shape or some other suitable profile. The GE body 18 has an axially-facing working surface 28 that generally confronts and opposes the CE body 12 or the CE firing tip 26 across the spark gap G.
As mentioned, in the embodiment shown in the figures, the spark plug 10 includes the optional CE firing tip 26 that is attached to an axially-facing working surface 30 of the CE body 12 and exchanges sparks across the spark gap G. Referring particularly to FIG. 2, the CE firing tip 26 shown here has a two-piece and generally rivet-like construction and includes a first piece 32 (rivet head) welded to a second piece 34 (rivet stem). The first piece 32 may be directly attached to the CE body 12, and the second piece 34 may be directly attached to the first piece so that an axially-facing sparking surface 36 is provided for exchanging sparks across the spark gap G. The first piece 32 can be made of a Ni-alloy material, and the second piece 34 can be made of a noble metal-alloy material such as one including iridium (Ir), platinum (Pt), or ruthenium (Ru), Other materials for the first and second pieces 32, 34 are possible. In other embodiments not shown in the drawings, for example, a discrete CE firing tip is omitted, in which case sparks are exchanged from the CE body 12 itself. The optional firing tip 26 could have a one-piece or single-material construction and it could have different shapes including non-rivet-like shapes such as cylinders, bars, columns, wires, balls, mounds, cones, flat pads, rings, or sleeves, to cite several possibilities. The present spark plug is not limited to any particular firing end arrangement, as the firing pads described herein could be used with any number of firing end arrangements, including those with or without CE firing tips.
The spark plug 10 further includes a firing pad 38 made of a precious metal material and attached via welding to the working surface 28 of the GE body 18 for exchanging sparks across the spark gap G. Compared to previously-known firing tips, a side surface or periphery 40 of the firing pad 38 is closer in proximity to, and in some embodiments precisely at, a free end surface 42 of the GE body 18. This provides an increased exposure and availability of the firing pad 38 to air/fuel mixture during a sparking event, with the shifted position of the firing pad and thereby greater absence of the GE body 18 between the free end surface 42 and the side surface 40. Ignitability and flame kernel growth are therefore enhanced because the spark exchanged with or by the firing pad 38 is more readily accessible to the injected air/fuel mixture, and there is minimized obstruction to flame kernel growth from the GE body 18 at the free end surface 42, among other possible improvements and causes. Furthermore, the greater absence of the GE body 18 between the free end surface 42 and the side surface 40 minimizes thermal mass and hence reduces the capacity of stored heat thereat, which could potentially degrade retention between the GE body and firing pad 38 over time. In other words, it has been found that in some cases more heat will remain with the GE body 18 at the firing pad 38 if the GE body spans beyond the firing pad's side surface 40, and the heat could weaken the attachment between the GE body and firing pad. The ability to position the firing pad 38 closer to the free end surface 42 can be contributed to the geometry of the firing pad and the location of a solidified weldment 44 relative to the side surface 40, among other possible factors.
In one previously-known precious metal firing tip, a so-called seam weld is performed in which a laser beam is emitted directly at and directly strikes a periphery of the firing tip at an interfacial boundary between the firing tip and the ground electrode body. The resulting solidified weld pool at the seam spans outwardly of the firing tip's periphery and bleeds over and onto the ground electrode body for a not insubstantial distance away from the firing tip. While seam welds are suitable in some spark plugs, this means that the firing tip should be positioned a sufficient distance away from the free end surface of the ground electrode body so that the seam weld can be performed and in order to ensure retention capabilities. This also means that a subsequent trimming operation of the free end portion of the ground electrode body cannot be performed through the solidified weld pool without jeopardizing the retention effect provided by the seam weld and increasing wear, tear, and dulling on the trimming equipment caused by cutting through the hardened weld pool. The seam weld thereby precludes the firing tip from being positioned as close to the free end surface of the ground electrode body as desired in some circumstances. As will be described below, the firing pad 38, on the other hand, can be positioned adjacent and even precisely at the free end surface 42 without the restrictions associated with seam welds. A trimming operation can also be performed without compromising the retention effect provided by the weldment 44.
Referring still to FIG. 3, a distance D dimension taken between the side surface 40 of the firing pad 38 and the free end surface 42 of the GE body 18 can be less than that of the previously-known firing tips with seam welds, and can help ensure enhanced ignitability and flame kernel growth during a sparking event. The distance D, as used herein, is the shortest geometrically straight-line distance between the side surface 40 and the free end surface 42; in the embodiment of FIG. 3, the distance D happens to be a lateral distance measured orthogonal to the parallel surfaces 40, 42 and in a plane parallel to the working surface 28, but in other embodiments the distance D need not necessarily be orthogonal to surfaces of the firing pad and GE body and can reside in different planes; indeed, as described below in different embodiments, the distance D could be zero. The exact value of the distance D can vary in different embodiments, but establishes a flush or nearly flush relationship between the free end surface 42 and the side surface 40. In some non-limiting examples, the distance D can be less than or equal to approximately 0.7 millimeters (mm), can be less than or equal to approximately 0.25 mm, can be less than or equal to approximately 0.15 mm, or can be greater than 0 but still less than or equal to approximately 0.7 mm or 0.25 mm. It has been found that keeping the value of the distance D within these amounts provides greater exposure of the firing pad 38 and hence improved ignitability and flame kernel growth, and better thermal management of the GE body 18. For instance, when the value of the distance D falls outside of these amounts, the spark exchanged with or by the firing pad may not be as readily accessible to the air/fuel mixture as desired, and ignitability and flame kernel growth may in-turn not be enhanced as desired.
Similarly, enhanced ignitability and flame kernel growth and better thermal management are provided when certain relationships are satisfied that relate to the distance D. In some non-limiting examples, the distance D taken between the side surface 40 and the free end surface 42 can range between approximately 0% to 500% of a thickness dimension T (FIG. 2) of the firing pad 38. Though the thickness dimension T is shown in FIG. 2 after the firing pad 38 is attached to the GE body 18, the thickness dimension T referred to herein is actually a measurement taken before the pad is attached to the GE body. And in some non-limiting examples, the thickness T dimension of the firing pad 38 ranges between approximately 0.05 mm and 0.2 mm; ranges between approximately 0.1 mm and 0.16 mm; or is approximately 0.13 mm; other thickness ranges and values are possible in other examples. Further, the distance D can range between approximately 0% to 200% of the thickness of the firing pad 38, can range between approximately 100% to 500% of the thickness of the pad, or can range between approximately 100% to 200% of the thickness of the pad. Still, other relationships can involve a width dimension W (FIG. 3) of the weldment 44. In a non-limiting example, the distance D can range between approximately 0% to 150% of the width W, can range between approximately 50% to 150% of the width W, can range between approximately 50% to 100% of the width W, or can range between approximately 100% to 150% of the width W. And in some non-limiting examples, the width W of the weldment 44 can range between approximately 0.14 mm and 0.30 mm. As used herein, values within the ranges include the lower and upper limit values of the ranges so that, for example, the range of 0% to 500% includes the values 0% and 500%.
Referring now to FIG. 4, in another embodiment the firing pad 38 can have a diamond orientation, and a free end portion 46 of the GE body 18 can be trimmed. In the diamond orientation, and from FIG. 3 to FIG. 4, the firing pad 38 is turned about its center so that a first corner 48 and a second corner 50 are in alignment with a lengthwise extent of the GE body 18. The example firing pad 38 has a generally square shape and hence, in the diamond orientation, its greatest dimension across its sparking surface between the corners 48, 50 is in-line with a direction of bending of the GE body 18 to the L-shape about the lengthwise extent; this facilitates spark-gapping alignment between the firing pad 38 and the CE firing tip 26 (if one is provided), as the dimension between the corners 48, 50 can often be greater than the diameter of the CE firing tip so that the pad and tip can be more readily overlapped during bending. Further, in the diamond orientation, a first side surface 52 and a second side surface 54 of the firing pad 38 are generally directed toward the free end surface 42 of the GE body 18 and toward an open side 56 (see FIG. 1) of the spark plug firing end.
The free end portion 46 of the GE body 18 can be trimmed or tapered in the radial direction via a cutting or severing process. The trimming can be carried out via a cutting blade, a laser, or some other way. In other embodiments, the firing pad 38 can have a diamond orientation without the radial trimming and instead with a free end portion like that of FIG. 3. The trimming provides the free end portion 46 of FIG. 4 with a first free end surface 58 and a second free end surface 60 that intersect at a free end corner 62. The first and second free end surfaces 58, 60 can be cut at approximately forty-five degree angles relative to the lengthwise extent of the GE body 18 and thereby can define an approximate ninety degree angle relative to each other at the free end corner 62. The free end corner 62 can remain pointed after the cutting process, or can be rounded off some.
Like the embodiment of FIG. 3, the side surfaces 52, 54 of the firing pad 38 of FIG. 4 are closer in proximity to—and in some cases precisely at—the respective free end surfaces 58, 60 compared to previously-known firing tips with seam welds. The corners 48, 62 can be similarly closer in proximity and in some cases precisely at each other. This too provides the enhanced ignitability and flame kernel growth and better thermal management described above. In this embodiment, a first distance D1 dimension is taken between the parallel first side surface 52 and the first free end surface 58, a second distance D2 dimension is taken between the parallel second side surface 54 and the second free end surface 60, and a third distance D3 dimension is taken between the first corner 48 and the free end corner 62. The distances D1, D2, and D3 of FIG. 4 are similar to the distance D of FIG. 3, and the description of the distance D′s measurement, values, and relationships above apply here for the distances D1, D2, and D3. Whatever their values or relationships, the distances D1, D2, and D3 need not necessarily be equal to one another so that, for example, the first distance D1 could be less than or equal to approximately 0.7 mm, while the second distance D2 could range between approximately 100% to 200% of the thickness of the firing pad 38. Furthermore, because the diamond orientation provides two side surfaces (first and second 52, 54) directed toward the open side 56 as opposed to a single side surface as in the embodiment of FIG. 3, the diamond orientation may provide an even more enhanced ignitability and flame kernel growth than that provided by the embodiment of FIG. 3, though this is not necessarily always the case. It is currently believed that one reason for this even greater enhancement is because sparks are sometimes more readily exchanged with or by surface edges and intersections, and the surface edges and intersections of FIG. 4 are more readily accessible to the injected air/fuel mixture via the distances D1, D2, and D3.
Referring now to FIG. 5, in another embodiment the trimming of the free end portion 46 of the GE body 18 can also be performed through the firing pad 38 itself, as opposed to the embodiment of FIG. 4 in which the firing pad is untrimmed after its attachment and in its state of use. The trimming here, or pre-trim, provides the free end portion 46 with the first free end surface 58, the second free end surface 60, and a third free end surface 64. As is described in greater detail below, the weldment 44 can be located inboard of the pad's side surfaces and thereby producing an outboard and substantially unattached portion 66. In this embodiment, the trimming process is performed through a section of the unattached portion 66. The cut or sever providing the first free end surface 58 goes physically through the unattached portion 66 adjacent a first side surface 68, the cut or sever providing the second free end surface 60 goes physically through the unattached portion adjacent a second side surface 70, and the cut or sever providing the third free end surface 64 goes physically through the unattached portion adjacent a third side surface and produces a newly formed third side surface, or trimmed side surface, 72 of the firing pad 38. The surfaces 64, 72 are parallel and flush in this embodiment, while the surfaces 58, 68 and 60, 70 are non-parallel.
Where the trimming goes through the unattached portion 66, the distance D dimension as previously presented has a value of zero. In other words, the respective side surfaces of the firing pad 38 and free end surfaces of the GE body 18 are flush and aligned with each other and, in a sense, can be continuations of the same surface. For example, a part of the first side surface 68 is newly-formed via the trimming and is precisely at the first free end surface 58, and therefore the distance D dimension is zero; likewise, a part of the second side surface 70 is newly-formed and is precisely at the second free end surface 60, giving the distance D dimension also a zero value; and the entire third side surface 72 is precisely at and aligned with the third free end surface 64, giving the distance D dimension a zero value. In the embodiment of FIG. 5, the trimming is not performed through the weldment 44, though it could be. As before, the zero values of the distances D in this embodiment provide the enhanced ignitability and flame kernel growth and better thermal management described above.
The trimming process could also be performed through the unattached portions in the embodiments of FIGS. 3 and 4, and would then give the distances D, D1, D2, and D3 a zero value.
Referring now to FIG. 6, in yet another embodiment the trimming of the free end portion 46 of the GE body 18 can be performed through a section of the weldment 44. The trimming here is arcuate and provides a rounded off free end surface 74 of the free end portion 46. The cut or sever goes physically through an outwardly-most section of the weldment 44 and produces a side surface 76 of the firing pad 38. In this embodiment, while the trimming is indeed made through the weldment 44, it does not substantially affect the retention capabilities provided by the weldment between the firing pad 38 and GE body 18. The distance D dimension here has, similar to earlier embodiments, a value of zero, and therefore provides enhanced ignitability and flame kernel growth and better thermal management. It is possible for the trimming to occur just beyond the weldment 44, as in the case of FIG. 5, so that the weldment remains completely intact.
Referring now to FIG. 7, in yet another embodiment, the firing pad 38 has a generally circular shape, and the free end portion 46 is trimmed at its sides but not at its top. As in earlier embodiments, the description of the distance D's measurement, values, and relationships above apply here for the distances D1, D2, and D3, and the distances D1, D2, and D3 need not necessarily be equal to one another. And, as in earlier embodiments, the cut or sever could go physically through the firing pad 38.
Referring back to FIGS. 2 and 3, the firing pad 38 is provided as a thin pad in the sense that its greatest width dimension across a sparking surface 78 is usually several times or more larger than its greatest axial thickness dimension T through the firing pad. The thin pad is different than many previously-known firing tip configurations with so-called fine wire constructions in which the greatest width dimension across the sparking surface of the wire (i.e., the diameter) is less than the thickness dimension of the wire (i.e., the axial height). Its thinness gives the firing pad 38 a relatively large sparking surface 78 with respect to the total amount of precious metal used, resulting in cost savings, particularly when compared to previously-known fine wire tips. The sparking surface 78 directly confronts and opposes a complementary sparking surface on the CE (with or without discrete firing tip 26), between which sparks are exchanged across the spark gap G during operation of the spark plug 10.
As shown in FIG. 3, the weldment 44 may be a single continuous weld or molten bond that is located entirely inboard or radially inward of a peripheral edge P and the side surface 40, and that generally follows the shape of the peripheral edge P, in this case a square. In other embodiments not shown in the figures, the weldment 44 need not be located wholly inboard of the peripheral edge P and could instead be made up of discrete individual weldments (i.e., non-continuous welds); for example, the weldment could begin and/or end outboard of the peripheral edge P on the GE body 18 (i.e., weld starting and stopping points on the GE body itself), and could be discrete lines that span entirely across the firing pad 38 and criss-cross one another. In the embodiment of FIG. 3, by its inboard location and continuity, a first or inner unfused portion 80 is defined within the radially-inward confines of the weldment 44, and the unattached portion 66 is defined radially-outward of the weldment and spans to the peripheral edge P. Furthermore, the weldment 44 provides an improved retention of the firing pad 38 and an improved consistency among welds of manufactured spark plugs, compared to the previously-known seam welds.
The firing pad 38 is preferably made from a noble metal material and can be formed into its thin shape before or after it is welded to the GE body 18. The firing pad 38 can be made from a pure precious metal or a precious metal alloy, such as those containing platinum (Pt), iridium (Ir), ruthenium (Ru), or a combination thereof. In some non-limiting examples, the firing pad 38 is made from a Pt alloy containing between approximately 10 wt % and 30 wt % Ni and/or Ir and the balance being Pt, or one containing between approximately 1 wt % and 10 wt % tungsten (W) and the balance being Pt; in either of the preceding Pt-alloy examples, other materials like Ir, Ru, rhodium (Rh), rhenium (Re), or a combination thereof could also be included. Other materials are possible for the firing pad 38, including pure Pt, pure Ir, pure Ru, to name a few. Before being welded to the GE body 18, the firing pad 38 can be produced by way of various processes and steps including heating, melting, and metalworking In one example, the firing pad 38 is stamped, cut, or otherwise formed from a thin sheet or tape of precious metal material; in another example, the firing pad is cut or sliced from a wire of precious metal material with a diamond saw or other severing tool, which can then be further flattened or metalworked to refine its shape.
The firing pad 38 can be attached to the GE body 18 by a number of welding types, techniques, processes, steps, etc. The exact attachment method employed can depend upon, among other considerations, the materials used for the firing pad 38 and for the GE body 18, and the exact shape and size of the firing pad. In one example, a fiber laser welding type and technique can be performed, as well as other laser welding types and techniques that use Nd:YAG, CO2, diode, disk, and hybrid laser equipment, with or without shielding gas (e.g., argon) in order to protect the molten weld pool. In the fiber laser example, the fiber laser emits a relatively concentrated and high energy density beam that can create the weldment 44, also called a keyhole weldment; other laser beams can also produce a suitably concentrated and high energy density beam and keyhole weld. The beam can be a non-pulsed or continuous wave beam, a pulsed beam, or some other type. In the embodiments of the figures, the beam's point of entry is at the sparking surface 78, and the thermal energy emitted penetrates entirely through the thickness T of the firing pad 38 and penetrates into the GE body 18 vertically below the surface-to-surface interface. The beam can be aimed at a generally orthogonal angle relative to the sparking surface 78, or can be aimed at another non-orthogonal angle. In a specific example, the laser weld beam has a repetition rate of 500 Hz, a pulse period of 2 ms, a pulse width of 0.7 ms, a duty cycle of 35%, a welding speed of 25 mm/s, a pulse-to-pulse distance of 0.05 mm, a gas flow rate of 30 SCFH, and a laser power of 70-100 W; of course, in other examples other parameters are possible for the laser weld beam.
In another example attachment method, resistance welding is performed as a preliminary tack weld before laser welding, or as the sole and primary weld for attachment without laser welding. In either instance, and now referring to FIG. 8, a first and second protrusion in the form of rails 43, 45 can project from a bottom surface 47 of the firing pad 38. The bottom surface 47 confronts the working surface 28 of the GE body 18 in assembly. During the resistance welding process, electrical current flow is concentrated through the rails 43, 45, and hence increased heat is generated at the rails. In this way, resistance welding is facilitated at the rails 43, 45 and a stronger weld can be formed between the firing pad 38 and the GE body 18 compared to a resistance weld without protrusions. This may also inhibit or altogether preclude separation between the firing pad 38 and the GE body 18, as the increased welding temperature at the rails 43, 45 may allow the firing pad to settle flushly against the working surface 28. In FIG. 8, the rails 43, 45 are rounded, geometrically linear, and span completely across the bottom surface 47, but this is merely one example. In other examples, protrusions could be v-shaped, the rails could be truncated compared to FIG. 8, there could be more or less than two protrusions, and/or the protrusions could simply be knob-like protuberances. Whatever their form, the protrusion has a height H that can differ from embodiment to embodiment. In specific examples, the height H could range between approximately one-half of a thousandth of an inch (0.0005 inches, or 0.0127 mm) to two thousandths of an inch (0.002 inches, or 0.0508 mm), or the height H could be one-half the thickness dimension T of the firing pad 38. Of course, in other embodiments the height H can have other values. Furthermore, the firing pad 38 may be cleaned to remove oil, dirt, and other contaminants from the pad's exterior surfaces before welding; this too may facilitate welding and the formation of a stronger weld.
In any of the embodiments presented in this description, the firing pad 38 could be provided in the form of a multi-layer firing pad as shown in FIG. 9. Whether a multi-layer construction is employed in a particular embodiment may depend upon, among other factors, the exact materials selected for the firing pad and the underlying electrode body and their compatibility in terms of welding and thermal transfer properties. The example of FIG. 9 includes a base metal layer 49 and a precious metal layer 51. The base metal layer 49 acts as a backing to provide strength and rigidity to the thinner precious metal layer 51, and is preferably made of a material that enhances initial weldability and subsequent retention to the GE body 18. In other words, in some cases the precious metal material may be more easily attached and retained to the material of the base metal layer 49 than directly to the GE body 18 (such as in the case when manufacturing thin, multi-layered ribbons). Examples of materials for the base metal layer 49 include Ni-alloys that can contain Cr, Fe, aluminum (Al), Mn, Si, and/or another element; and more specific examples include Inconel® 600 or 601. The precious metal layer 51, on the other hand, exchanges sparks across the spark gap G as previously described and can be made of the pure precious metals or the precious metal alloys presented above for the firing pad 38. Again, the multi-layer firing pad of FIG. 9 can be employed in any of the embodiments of FIGS. 3-7 in place of the single-material firing pads, as well as any of the embodiments detailed in this description.
During manufacturing of the spark plug 10, the GE body 18 and the firing pad 38 can be prepared and assembled together in different ways. In one example, and referring to FIG. 10, at a step 100 the GE body 18 is attached to the metallic shell 16 at the attachment interface 24 via a resistance welding process. The schematic in the figure shows the GE body 18 in an unfinished state and before it is bent to its final L-shape. At a step 200, the firing pad 38 is preliminarily attached to the free end portion 46 of the GE body 18 via a tack or resistance weld—in this example, the firing pad has a diamond orientation. At this step, the distances D1, D2, and D3 between the firing pad's side surfaces and the GE body's free end surfaces may or may not satisfy the values and relationships previously described. At a step 300, the free end portion 46 is trimmed via a cutting or severing process. The trimming in this example is similar to that described in connection with FIG. 4. And here, the distances D1, D2, and D3 satisfy the values and relationships described above so that the firing pad 38 and GE body 18 provide enhanced ignitability and flame kernel growth and better thermal management. Lastly in FIG. 10, at a step 400 the firing pad 38 is more permanently attached to the free end portion 46 via a laser weld that produces the weldment 44. After the step 400 a bending and gapping process can be performed to bring the GE body 18 to its finished L-shape.
Other preparation and assembly processes can have more, less, and/or different steps than those described with FIG. 10. For example, a laser welding process could be performed prior to the trimming step and—as described earlier in connection with FIG. 5—the cut or sever could then go through the unattached portion 66. In another example, there need not be a preliminary attachment and instead just the more permanent laser weld before or after trimming, or the preliminary attachment could be provided in another way such as by mechanical clamping. In yet another example, the trimming step need not be performed and the firing pad 38 need not have a diamond orientation—this could produce the embodiment of FIG. 3. And in another example, the laser welding could be omitted and instead a resistance weld could provide the permanent attachment of step 400.
Thermal testing was conducted in order to observe retention performance between the firing pad 38 and an electrode body. In the testing, the firing pad 38 and electrode body were attached to each other with laser welding similar to the embodiment of FIG. 3, with a firing pad of Pt30Ni. In general, the thermal testing subjected the firing pad 38, electrode body, and weldment 44 to an increased temperature for a relatively brief period of time, and then allowed them to cool to ambient temperature. The testing was meant to mimic expansion and contraction thermal stresses that are more extreme than those experienced in application in a typical internal combustion engine. In the example testing conducted, a sample spark plug was mounted in a collar-like structure made of brass material. The collar structure was secured to the shell of the sample spark plug and did not make direct abutment with the electrode body; the mount structure acted as a heat sink and facilitated cooling. An induction heater was then used to heat the attached firing pad 38 and electrode body up to approximately 1,700° F. for about twenty seconds. After that, the firing pad 38 and electrode body were allowed to cool at rest down to about room temperature or slightly above room temperature. This rise and fall in temperature constituted a single test cycle, and the thermal testing was conducted on numerous sample spark plugs. On average, the sample spark plugs were capable of enduring over one-hundred-and-seventy-five cycles without exhibiting significant cracking, separation, or other conditions that could negatively impact retention between the firing pad 38 and the electrode body. One-hundred-and-seventy-five cycles is considerably greater than the one-hundred-and-twenty-five cycles oftentimes deemed acceptable for such products, and was unexpected in view of how thin the firing pads were. The cycles endured in the testing here is also comparable to pads with much greater thicknesses than the thin firing pads tested—this too was unexpected. It should be appreciated that not all testing will yield these exact results, as different testing parameters, samples, equipment, as well as other factors, can alter the outcome of testing performance.
Referring now to FIGS. 11-14, another embodiment of the firing pad 38 has a protrusion 90 projecting from a bottom side 92 (FIG. 13) of the firing pad 38. As described in more detail below, electrical current flow is concentrated through the protrusion 90 amid a resistance welding process, and hence increased heat is generated at the protrusion 90. In this way, the protrusion 90 facilitates attachment between the firing pad 38 and the GE body 18 via resistance welding only and without performing laser welding, while still satisfying the attachment and retention demands of production spark plugs. In the embodiment presented by FIGS. 11-14, there is a single protrusion 90. It has been found in some cases that a single protrusion—like the one in the figures provides better retention and attachment capabilities than multiple protrusions. The single protrusion 90 can provide a greater displacement into the GE body 18 compared to, for instance, a double or triple protrusion, although the double or triple protrusions are still suitable in other embodiments (i.e., the double protrusion was previously described in connection with FIG. 8, and the described subject matter applies for the firing pad 38 of FIGS. 11-14 in some embodiments). Without intending to be bound to any theories of causation, it has been shown that once surface-to-surface contact is established between the firing pad 38 and the GE body 18 in the midst of resistance welding, formation of a resistance-welded weldment measurably declines and might halt altogether. And since the single protrusion takes a longer time during resistance welding to establish surface-to-surface contact, it displaces more into the GE body 18 and an improved retention and attachment between the firing pad 38 and GE body 18 is achieved. Moreover, the single protrusion may concentrate electrical current flow to a greater degree than multiple protrusions, which might also contribute to the improved retention and attachment.
Referring now particularly to FIG. 13, the protrusion 90 has a generally rounded wedge-like shape. A somewhat thickened material portion of the firing pad 38 opposite the sparking surface 78 makes-up the protrusion 90. The broken line numbered 47 in FIG. 13 approximates the bottom surface 47 of the embodiment of FIG. 8 and is depicted in FIG. 13 for demonstrative purposes in order to better elucidate the protrusion 90. The portion above the broken line 47 constitutes the protrusion 90. In this embodiment, the protrusion 90 spans completely across the bottom side 92 on all sides of the firing pad 38. The protrusion 90 has a crest 94 spanning between a first side 96 of the firing pad 38 and a second side 98 of the firing pad 38. As perhaps illustrated best in FIG. 13, the crest 94 is the highest part of the protrusion 90 (“highest” is used here with reference to the firing pad's orientation in FIG. 13; in FIG. 12, in contrast, the crest 94 is the lowest part of the protrusion 90). The crest 94 is the thickest section of the firing pad 38, measured between the sparking surface 78 and bottom side 92. From the crest 94, the protrusion 90 tapers in thickness toward a third side 100 of the firing pad 38 and tapers in thickness toward a fourth side 102 of the firing pad 38. A first sloped surface 104 slants continuously from the crest 94 and to the third side 100, and a second sloped surface 106 slants continuously from the crest 94 and to the fourth side 102. In other embodiments, the protrusion 90 could have different designs and constructions than that illustrated in FIGS. 11-14; for example, the protrusion 90 can have a sharper wedge-like shape so that it resembles a V-shape in sectional profile, and/or the protrusion 90 need not span completely across the bottom side 92 and instead its sloped surfaces 104, 106 and/or its crest 94 can stop short of the firing pad's sides.
In the embodiment of FIGS. 11-14, the firing pad 38 is preferably made of a Pt-based alloy material containing at least 25 wt. % of Ni, and more preferably containing Pt in an amount between approximately 65 wt. % and approximately 75 wt. % and Ni in an amount between approximately 25 wt. % and approximately 35 wt. %. Still, even more preferably the firing pad 38 of FIGS. 11-14 can be made of a Pt-based alloy material containing approximately 70 wt. % Pt and approximately 30 wt. % Ni (i.e., Pt30Ni). Yet other embodiments can include Pt-based alloy materials that include other elements, such as one or more of the following: tungsten (W), palladium (Pd), rhodium (Rh), iridium (Ir), and/or rhenium (Re). In general, platinum has a greater expense than nickel, and exhibits a greater durability and erosion resistance than nickel when put in use in a spark plug. It is desirable to reduce the amount of platinum in spark plug tips to save costs, and yet not jeopardize durability and sparking performance. In this regard, it has been shown that the firing pad's relatively large sparking surface 78 enhances overall durability of the firing pad 38—most likely due to the greater extent of surface area available to exchange sparks during use. With the enhanced durability, a reduced amount of platinum can be provided and a greater amount of nickel (e.g., Pt30Ni) without seeing an appreciable loss in sparking performance or no loss at all. In other words, the greater extent of surface area accounts for the reduced platinum and the attendant jeopardized durability that might otherwise occur. Suitable sparking performance is maintained and a cost savings can be realized. Still, in other embodiments, the firing pad 38 of FIGS. 11-14 can have the multi-layer construction as described in connection with FIG. 9; in these embodiments, the base metal layer would be composed of the Ni-based alloys previously described, and the precious metal layer would be composed of the Pt-based alloy materials described above in this paragraph.
Moreover, the increased amount of nickel permits the performance of resistance welding only, without laser welding, to attach the firing pad 38 and GE body 18. As mentioned earlier, the protrusion 90 also contributes to the ability to forego laser welding. Removing laser welding from the attachment and retention efforts increases manufacturing efficiencies and saves costs. The increased amount of nickel improves compatibility between the materials of the firing pad 38 and GE body 18 in terms of weldability and retention. As described earlier, the GE body 18 is typically made of a Ni alloy material such as Inconel® 600 or 601. Retention is improved since the materials of the firing pad 38 and GE body 18 exhibit less of a difference between their respective coefficients of thermal expansion, and expand and contract relative to each other during use to a lesser extent.
The resistance welding process employed to attach the firing pad 38 and GE body 18 can involve a first preliminary resistance weld (sometimes referred to as a tack weld) and a second and subsequent permanent resistance weld. Still, the resistance welding process may only involve a single resistance weld. FIG. 14 depicts a schematic representation of a weld arbor 108 that can be used to carry out the resistance welding process. Of course, other equipment may be utilized in the resistance welding process such as another weld arbor or resistance welding electrode positioned on an opposite side of the GE body 18 and opposite the weld arbor 108. The weld arbor 108 has a plate 110 with a face surface 112 that confronts and contacts the sparking surface 78 of the firing pad 38 amid the resistance welding process, as shown in FIG. 14. At the beginning of the resistance welding process, the firing pad 38 is located against the working surface 28 of the GE body 18 with the bottom side 92 and protrusion 90 abutting the working surface 28. Since the crest 94 is the lowest part of the protrusion 90, the crest 94 makes line-to-surface contact with the working surface 28. Although the working surface 28 is shown in FIGS. 11, 12, and 14 with a depression 114, before electrical current is passed the working surface 28 is planar and without any depressions, and hence the line-to-surface contact can be made. The line-to-surface contact may be the only abutment being made between the firing pad 38 and GE body 18 at this point in the resistance welding process.
Once in place, electrical current may be initiated and passed from the weld arbor 108 and through the firing pad 38. At the same time, the weld arbor 108 may exert a pressing force against the firing pad 38. As the material of the GE body 18 begins to soften, the firing pad 38 sinks into the working surface 28 and into the GE body 18. The depression 114 is formed and surface-to-surface contact is established between the firing pad 38 and its protrusion 90 and the GE body 18 and the now-formed depression 114. As previously mentioned, the depression 114 is not pre-formed and is instead established during the resistance welding process. Because the protrusion 90 is what forms the depression 114, the shapes of the protrusion 90 and depression 114 closely complement each other as shown in FIGS. 11, 12, and 14.
As the firing pad 38 is pressed and sunk into the GE body 18, molten material is displaced from therebetween and makes its way toward the peripheral edge P of the firing pad 38. As illustrated in FIG. 14, the displaced material comes into abutment with the face surface 112 of the plate 110 and its movement is hence partly confined thereby. The displaced material may completely surround the peripheral edge P of the firing pad 38, or may mostly be situated at the third and fourth sides 100, 102 via a route that follows the first and second sloped surfaces 104, 106. Once solidified, the displaced material establishes a resistance-welded expulsion 116. The resistance-welded expulsion 116 can be composed of a mixture of materials from both the GE body 18 and firing pad 38, and can largely be made up of nickel material. As perhaps illustrated best by FIG. 12, an upper-most and exposed surface 118 of the resistance-welded expulsion 116 is in-line with the sparking surface 78 of the firing pad 38. Indeed, during use of the associated spark plug, the surface 118 exchanges sparks and thus also constitutes a sparking surface of the firing pad 38. Furthermore, because the resistance-welded expulsion 116 can be made of largely nickel material, it can be more readily cut through via the trimming processes described above than materials containing larger amounts of noble metal material. Lastly, once the resistance welding process is completed, a heat-affected zone 120 is formed within the GE body 18 and underneath the firing pad 38. The heat-affected zone 120 is the result of material partially or more melted during the resistance welding process. As shown in FIG. 12, the heat-affected zone 120 may be generally confined within an interfacial boundary between the firing pad 38 and the resistance-welded expulsion 116.
It is to be understood that the foregoing is a description of one or more preferred exemplary embodiments of the invention. 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.
Patent Application
20150236482
