1. Field of the Invention
The present invention relates to fuel injectors, and more particularly fuel injectors having coated components.
2. Description of the Related Art
Conventional fuel injectors include metallic components that are attached such that they move jointly within the fuel injectors. For example, during manufacture of some air assist fuel injectors, a poppet of a first material is press fit into a receiving portion of an armature of a second material. During this press fitting process, the poppet and armatures are often galled such that air pockets form between the surface of the armature and the surface of the poppet. After the poppet is press fit to the armature, they are typically welded together. During operation of the fuel injector, the armature and the poppet move in a reciprocating linear motion within the fuel injector. Although the poppet and the armature typically do not move with respect to one another, the base material of the poppet and armature occasionally corrodes near or at the poppet-armature interface where the poppet is attached to the armature. The dissimilar materials, the air pockets, and the weld connection are thought to contribute to galvanic corrosion, crevice corrosion, and intergranular corrosion at the poppet-armature interface of these conventional fuel injectors. Additionally, the poppet-armature interface is thought to be susceptible to stress corrosion cracking as these components are often subjected to tensile stresses and corrosive environments.
In light of the above-described problems of some conventional fuel injectors, embodiments of the present invention generally strive to provide fuel injectors that include a coating at the poppet-armature interface, where the coating helps reduce corrosion of the base material of the poppet and/or the base material of the armature.
Other advantages and features associated with the embodiments of the present invention will become more readily apparent to those skilled in the art from the following detailed description. As will be realized, the invention is capable of other and different embodiments, and its several details are capable of modification in various obvious aspects, all without departing from the invention. Accordingly, the drawings in the description are to be regarded as illustrative in nature, and not limitative.
The fuel injector 100 includes a solenoid coil 114 of conductive wire wrapped around a tubular bobbin 112. The solenoid coil 114 has two ends that are each electrically connected to terminals 122. The solenoid coil 114 is energized by providing current to the terminals 122. The bobbin 112 of the solenoid assembly is a spool on which the conductor of the solenoid coil 114 is wound, and defines a through hole in or near which an armature 172 is electromagnetically actuated as further described below. As is illustrated in
The armature 172 functions as the moving part of an electromagnetic actuator, defined by the solenoid coil 114 and armature 172 combination. As is illustrated in
As is described below, the poppet 202 is attached to the armature 172 at an interface location. Because the poppet 202 is attached to the armature 172, the poppet will move with armature when the armature is actuated by energizing the solenoid coil 114. The poppet 202 is a member that opens and closes to control the discharge of fuel from the fuel injector 100. When the poppet 202 opens and closes, it reciprocates in a channel 208 of the seat 204. In the illustrated embodiment, the poppet 202 includes a stem 212 and a head 214. The head 214 includes an impact surface 220 that abuts the seat 204 when the fuel injector is closed and that is spaced away from the seat 204 when the fuel injector is open. In the preferred embodiment, the impact surface 220 includes an angled and annular face that defines a contact ring, which contacts a surface of the seat 204 to define a seal between the poppet 202 and the seat. The poppet 202 is fabricated from a metallic material, such as iron, aluminum, titanium, and their alloys. In one embodiment, the poppet 202 is an austenitic, ferretic, or martensitic stainless steel. In a preferred embodiment, the poppet is formed of a 400 series stainless steel. Like the armature 172, the poppet 202 is fabricated by casting, molding, forging, machining, and/or other conventional metal working processes.
In the illustrated embodiment, the poppet 202 includes an interior channel 210 that extends from the inlet 182 of the poppet 202 to an outlet 232 of the poppet located upstream of the head 214. In the preferred embodiment, the poppet 202 includes four slot-shaped outlets 232 that are equally spaced from each other and located approximately transverse to a longitudinal axis of the poppet 202. Although it is preferred that the poppet 202 have four slot-shaped outlets 232, other configurations will suffice. For example, the poppet 202 may include one slot-shaped outlet, two circular outlets, five oval outlets, or ten pin sized outlets. Alternative embodiments of the poppet 202 need not include the inlet 182, the outlets 232, and the interior channel 210.
As is described above, the impact surface 220 of the head 214 seats against the seat 204 when the solenoid coil 114 is not energized. When the armature 172 is actuated by energizing the solenoid coil 114, the poppet 202 moves with the armature 172 such that the head 214 is lifted off of the seat 204 in a direction away from the fuel injector 100. Hence, the poppet 202 is an outwardly opening poppet. When the head 214 is lifted off of the seat 204, a seal is broken between the head 214 and the seat 204 such that liquid fuel and gas exiting the outlets 232 exits the fuel injector 100. In an alternative embodiment of the fuel injector 100, the poppet 202 is solid, i.e., it is devoid of an interior channel 210. In this solid-poppet embodiment, the liquid fuel travels exterior the poppet, as is common in many conventional fuel injectors. In another embodiment, the poppet 202 is an inwardly opening poppet. That is, to discharge the fuel from the fuel injector, the poppet and armature move opposite the direction of flow ƒ. Such that the poppet head 214 lifts inwardly off of the seat 204 to discharge fuel from the fuel injector.
Movement of the poppet 202 is guided by a bearing 175 that is located upstream of the outlets 232 with respect to the direction of flow ƒ of the liquid fuel and the gas through the injector 100. Hence, the seat 204 includes a bearing surface that engages a corresponding bearing surface of the poppet 202 to guide movement of the poppet. Because the seat 204 serves as a bearing surface for poppet movement and also absorbs the impact of the head 214 when the poppet 202 opens and closes, the seat 204 is preferably fabricated from a wear and impact resistant material such as hardened 440 stainless steel. In alternative embodiments, seat 204 need not include a bearing surface that guides movement of the poppet. For example, movement of the poppet 202 may be guided at other locations upstream of the seat 204. In an alternative embodiment, the fuel injector includes bearing surfaces between the seat 204 and the poppet 202 and between the armature 172 and the sleeve168.
As is further illustrated in
The spring 170 is located between the armature 172 and the leg 166. More particularly, the spring 170 is located within a recessed bore 171 of the leg 166 that is concentric with the elongated channel 165 of the leg 166. The bore 171 faces the armature 172 and defines the seat for the spring 170. The spring 170 is a compression spring having a first end that abuts the armature 172 and a second end that abuts the leg 166. The bottom of the bore 171 defines the seat for the downstream end of the spring and a recess in the armature 172 defines a seat for the upstream end of the spring 170. The spring 170 functions to bias the armature 172 away from the leg 166. When the solenoid coil 114 is not energized, the spring 170 biases the armature 172 away from the leg 166 and thus the poppet 202 is maintained in a closed position where the head 214 abuts the seat 204. However, when the solenoid coil 114 is energized, the electromagnetic forces cause the armature 172 to overcome the biasing force of the spring 170 such that the armature 172 moves toward the leg 166 until it abuts a stop surface 167 of the leg 166. When the solenoid coil 114 is de-energized, the electromagnetic force is removed and the spring 170 again forces the armature 172 away from the stop surface 167. As will be appreciated, in alternative embodiments of the fuel injector 100, the spring 170 may be located at different positions and still be within the confines of the present invention. For example, in one inwardly-opening embodiment of the fuel injector, the spring 170 is located at the upstream end of the armature and biases the armature toward the leg 166.
In the preferred embodiment, the fuel injector 100 also includes a cap 190 that defines an inlet to the air assist fuel injector 100 for the pressurized gas and liquid fuel. The cap 190 serves to direct the liquid fuel and gas to the passageway 180 of the armature 172. The cap 190 includes one fuel passageway 192 having an inlet that primarily receives liquid fuel and four gas passageways 194 each having an inlet that primarily receives pressurized gas. The liquid fuel passageway 192 is located along the center axis of the cap 190, and the gas passageways 194 are circumferentially and equally spaced about the liquid fuel passageway 192. Alternative embodiments of the air assist fuel injector 100 need not include the cap 190, and alternative embodiments of the cap 190 may include more or fewer passageways 192, 194.
As is described above, the illustrated fuel injector 100 utilizes pressurized gas, such as air, to atomize low pressure fuel. When installed in an engine, the fuel injector 100 is located such that the atomized low pressure fuel that exits the fuel injector 100 is delivered to the internal combustion chamber of an engine, i.e., that part of an engine at which combustion takes place, normally the volume of the cylinder between the piston crown and the cylinder head, although the combustion chamber may extend to a separate cavity outside this volume. For example, the fuel injector 100 may be located in a cavity of a four-stroke internal combustion engine head such that the fuel injector can deliver a metered quantity of atomized liquid fuel to a combustion cylinder of the four-stroke internal combustion engine where it is ignited by a spark plug or otherwise.
Because the fuel injector 100 is an air assist fuel injector, in a typical configuration, the air assist fuel injector 100 is located adjacent a conventional fuel injector (not illustrated), which delivers metered quantities of fuel to the air assist fuel injector. The conventional fuel injector may be located in the cavity of a rail or within a cavity in the head of an engine. The air assist fuel injector 100 is referred to as “air assist” because it preferably utilizes pressurized air to atomize liquid fuel. Although it is preferred that the air assist fuel injector 100 atomize liquid gasoline with pressurized air, it will be appreciated that the air assist fuel injector 100 may atomize many other liquid combustible forms of energy with any variety of gases. For example, the air assist fuel injector 100 may atomize kerosene or liquid methane with pressurized gaseous oxygen, propane, or exhaust gas. Hence, the term “air assist” is a term of art, and as used herein is not intended to dictate that the air assist fuel injector 100 be used only with pressurized air. As mentioned above, in alternative embodiments, the fuel injector 100 is not an air assist fuel injector as it is configured to deliver fuel without the assistance of a gas.
As is described above and as best illustrated in
As is set forth above, the poppet-armature interface location of some conventional fuel injectors is susceptible to corrosion. The embodiments of the present invention strive to address this problem by including a coating 205 on the poppet 202 and/or on the armature 172 over all or at least a portion of the interface location 177.
The coating 205 is a layer of substance spread over and bonded to a surface of the poppet 202 and/or the armature 172 at the interface location 177 and has an increased resistance to corrosion (i.e., corrodes at a slower rate in mils penetration per year) as compared with the base material of the poppet and/or the base material of the armature when each is exposed to a same working environment. This increased resistance to corrosion of the coating 205 may be an increased resistance (as measured relative to the base material of the armature 172 and/or the base material of the poppet 202 without the coating 205) to one or more of the following types of corrosion: uniform corrosive attack; galvanic corrosion; crevice corrosion; pitting corrosion; intergranular corrosion; erosion corrosion; and stress corrosion cracking. The coating 205 is a solid-phase, i.e., non-fluid, after its application and is one or more of numerous coatings that increase corrosion resistance, such as organic coatings, inorganic coatings, and metallic coatings. Suitable organic coatings include dried paints, varnishes, lacquers, and synthetic resins. Suitable inorganic coatings include dried enamels, oxides, and phosphate conversions. Examples of suitable metallic coatings include tin based coatings, cadmium based coatings, gold based coatings, silver based coatings, platinum based coatings, aluminum based coatings, titanium based coatings, zinc based coatings, chromium based coatings, nickel based coatings, carbon based coatings, iron based coatings, and other known coatings. Examples of some preferred classes of metallic coatings include chromium nitride coatings, nickel phosphorous coatings, diamond-like-carbon coatings, nickel coatings, and iron nitride coatings. Suitable coatings may be applied by hot or cold dipping, electroplating, spraying, and by deposition from solution. In the illustrated embodiment the coating 205 is preferably a chromium based coating, commercially available as ARMOLOY-TDC from Armoloy, Inc., Pennsylvania, USA, and is deposited on the cylindrical, exterior surface of the end portion 203 of the poppet 202 via an electrochemical bath. The coating 205 preferably extends from the extreme or most distal end 179 to a location downstream of the interface location 177 as measured with respect to the direction of flow f. Hence, in the illustrated embodiment, the coating 205 extends from the most distal end 179 to a location 10 mm downstream thereof, which is approximately 6 mm downstream of the most downstream end of the interface location 177. In alternative embodiments, the coating 205 does not extend downstream of the interface location 177. In a further embodiment, the coating 205 covers the entire exterior surface of the poppet 202.
In an alternative embodiment, the poppet 202 does not include the coating 205. Rather, the recess 173 of the armature 172 that receives the poppet 202 includes the coating 205. For example, in one embodiment, the interior cylindrical surface 169 of the recess 173 of the conduit 180 is coated with the coating 205. In a further embodiment, the end portion 203 of the poppet 202 and the recess 173 of the armature 172 each include an identical or different coating 205.
By coating at least one of the armature and poppet surfaces at the interface location with the coating 205, the attached components are less likely to become corroded as compared to some conventional configurations. Additionally, the coating 205 provides some lubricity to the components, thereby decreasing the amount of galling that takes place when the poppet 202 is inserted into the armature 172 (or vice versa) which is thought to contribute to the corrosion of some conventional designs.
In an alternative embodiment, the poppet 1202 does not include the coating 1205. Rather, the outside diameter of the cylindrical end portion 1185 of the armature 1172 includes the coating 1205. In a further alternative embodiment, both the inside diameter of the cylindrical portion 1209 of the poppet interior channel 1210 and the outside diameter of the cylindrical end portion 1185 of the armature 1172 include the coating.
In an alternative embodiment, the outside diameter of the first end 3211 of the poppet 3202 does not include the coating. Rather, the inside surfaces of the groove 3181 include the coating.
In an alternative embodiment, the outside diameter of the first end 4211 of the poppet 4202 does not include the coating. Rather, the inside surface of the recess 4173 includes the coating. In a further alternative embodiment, both the outside diameter of the first end portion 4211 of the poppet 4202 and the inside surface of the recess 4173 include the coating.
The principles, preferred embodiments, and modes of operation of the present invention have been described in the foregoing description. However, the invention which is intended to be protected is not to be construed as limited to the particular embodiments disclosed. Further, the embodiments described herein are to be regarded as illustrative rather than restrictive. Variations and changes may be made by others, and equivalents employed, without departing from the spirit of the present invention. Accordingly, it is expressly intended that all such variations, changes, and equivalents which fall within the spirit and scope of the present invention as defined in the claims be embraced thereby.
Number | Name | Date | Kind |
---|---|---|---|
2627259 | Wood et al. | Feb 1953 | A |
3773265 | Kent | Nov 1973 | A |
4075999 | Danis | Feb 1978 | A |
4212602 | Buran et al. | Jul 1980 | A |
4552311 | Casey | Nov 1985 | A |
4714198 | Savkar | Dec 1987 | A |
4867116 | de Freitas Couto Rosa et al. | Sep 1989 | A |
4871434 | Munz et al. | Oct 1989 | A |
5040501 | Lemelson | Aug 1991 | A |
5069189 | Saito | Dec 1991 | A |
5173339 | Singer | Dec 1992 | A |
5226975 | Denton et al. | Jul 1993 | A |
5271823 | Schachameyer et al. | Dec 1993 | A |
5474234 | Maley | Dec 1995 | A |
5752308 | Maley et al. | May 1998 | A |
5819774 | Beardsley et al. | Oct 1998 | A |
5888316 | Erickson | Mar 1999 | A |
5904125 | Enright et al. | May 1999 | A |
5937520 | Earhart et al. | Aug 1999 | A |
5996227 | Reiter et al. | Dec 1999 | A |
6062499 | Nakamura et al. | May 2000 | A |
6145763 | Fleming et al. | Nov 2000 | A |
6302337 | Kimmel | Oct 2001 | B1 |
6311901 | Imoehl et al. | Nov 2001 | B1 |
6484700 | Kimmel et al. | Nov 2002 | B1 |
6561167 | Berndt | May 2003 | B1 |
Number | Date | Country |
---|---|---|
0 818 622 | Nov 2000 | EP |
Number | Date | Country | |
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20030226914 A1 | Dec 2003 | US |