Consumable Cartridge for a Plasma Arc Cutting System
20200023456 ยท 2020-01-23
Inventors
Cpc classification
B23K10/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
B23K10/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The invention features a frame for a plasma arc torch cartridge. The frame includes a thermally conductive frame body having a longitudinal axis, a first end configured to connect to a first consumable component, and a second end configured to mate with a second consumable component. The frame body surrounds at least a portion of the second consumable component. The frame also includes a set of flow passages formed within the frame body. The set of flow passages fluidly connects an internal surface of the frame body and an external surface of the frame body. The set of flow holes is configured to impart a fluid flow pattern about the second consumable component.
Claims
1. A plasma arc torch cartridge having an electrode, a nozzle, and a shield, the cartridge further comprising: an inner portion relative to a longitudinal axis of the cartridge comprising copper, the inner portion including at least a portion of the shield, the nozzle, and the electrode; and an outer portion relative to the longitudinal axis, the outer portion at least substantially free of copper, the outer portion surrounding the copper inner portion and including at least a portion of the shield and a portion of the nozzle.
2. The cartridge of claim 1 wherein the electrode is a spring electrode.
3. The cartridge of claim 1 further including a set of swirl holes, wherein the cartridge cap extends within a base of the nozzle toward the set of swirl holes.
4. The cartridge of claim 1 wherein a base of the nozzle is metallic or anodized.
5. The cartridge of claim 1 further comprising a retaining cap connected to the cartridge frame.
6. The cartridge of claim 5 wherein the retaining cap is formed of a plastic.
7. The cartridge of claim 5 wherein the nozzle and the electrode are connected to the retaining cap via a base of the nozzle.
8. The cartridge of claim 1 further comprising a shield connected to the cartridge frame.
9. The cartridge of claim 8 wherein the shield is connected to the cartridge frame via a shield insulator.
10. The cartridge of claim 9 wherein the shield insulator is electrically insulative.
11. The cartridge of claim 9 wherein the shield insulator is thermally conductive.
12. The cartridge of claim 9 wherein the shield insulator includes anodized aluminum.
13. The cartridge of claim 8 wherein the shield has a heat capacity to current ratio of about 2-4 W/m- K-A.
14. The cartridge of claim 1 further including a sleeve disposed about a portion of the electrode.
15. The cartridge of claim 14 wherein the sleeve includes an anodized layer formed to electrically isolate the electrode from a base of the nozzle.
16. The cartridge of claim 14 wherein the sleeve includes a set of flow surfaces.
17. The cartridge of claim 1 further including a cap insert connected to the second end of the cartridge frame, the cap insert substantially orienting the electrode and retaining the electrode within the cartridge frame.
18. A consumable assembly for a plasma arc torch, the consumable assembly comprising: a metallic assembly body extending along a longitudinal axis through the metallic assembly body from a first end to a second end, the metallic assembly body defining a heat sink having a plurality of swirl holes shaped to impart a flow pattern within or around the heat sink; a nozzle having a base and in physical communication with the first end of the heat sink; and an electrode disposed within a portion of the heat sink and a portion of the nozzle.
19. The consumable assembly of claim 18 wherein the nozzle and the electrode are integrally formed as a part of within a consumable cartridge.
20. The consumable assembly of claim 18 wherein the electrode is a spring electrode.
21. The consumable assembly of claim 18 further including a cartridge cap, the cartridge cap extending within the base of the nozzle toward the set of swirl holes.
22. The consumable assembly of claim 18 wherein the metallic assembly body is anodized.
23. The consumable assembly of claim 18 further comprising a retaining cap directly connected to the metallic assembly body.
24. The consumable assembly of claim 23 wherein the nozzle and the electrode are connected to the retaining cap via the metallic assembly body.
25. The consumable assembly of claim 18 further comprising a shield connected to the metallic assembly body.
26. The consumable assembly of claim 25 wherein the shield is connected to the metallic assembly body via a shield insulator.
27. The consumable assembly of claim 26 wherein the shield insulator is press fit to at least one of the shield and the base of the nozzle.
28. The consumable assembly of claim 26 wherein the shield insulator is electrically insulative.
29. The consumable assembly of claim 26 wherein the shield insulator is thermally conductive.
30. The consumable assembly of claim 26 wherein the shield insulator includes anodized aluminum.
31. The consumable assembly of claim 25 wherein the shield has a heat capacity to current ratio of about 2-4 W/m- K-A.
32. The consumable assembly of claim 18 further including a sleeve disposed about a portion of the electrode.
33. The consumable assembly of claim 32 wherein the sleeve includes an anodized layer formed to electrically isolate the electrode from the base of the nozzle.
34. The consumable assembly of claim 32 wherein the sleeve includes a set of flow surfaces.
35. The consumable assembly of claim 18 further including a cap insert connected to the second end of the metallic assembly body, the cap insert configured to orient the electrode and retain the electrode within the metallic assembly body.
36. The consumable assembly of claim 35 further comprising a seal disposed within the cap insert.
37. A method of cooling a plasma arc torch, the method comprising: providing a composite consumable having a heat sink defining a plurality of holes, the composite consumable having integrated components including an electrode, a nozzle and a shield; installing the composite consumable in the plasma arc torch; and flowing a cooling fluid through the plurality of holes, the cooling fluid forming a fluid flow pattern that cools at least one of the electrode, nozzle or shield, thereby removing at least one watt of power from the plasma arc torch during operation.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0029] The foregoing discussion will be understood more readily from the following detailed description of the invention when taken in conjunction with the accompanying drawings.
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DETAILED DESCRIPTION OF THE DRAWINGS
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[0050] For example, the nozzle body 216 can be formed from a conductive material (e.g., a highly conductive material such as aluminum) and can be attached to (e.g., can be in direct physical contact with) other parts of the cartridge 200. In some embodiments, the nozzle body 216 is in thermal communication with certain parts of the cartridge 200 (e.g., via thermal conduction) but electrically isolated from certain parts (e.g., either the same parts or other parts with which the nozzle body 216 is in thermal communication). For example, the nozzle body 216 can function as a heat sink for the nozzle orifice 218 while remaining electrically isolated from the nozzle shield 212. Such a configuration can enhance cooling performance (for example, of the nozzle and the electrode) and reduce manufacturing costs by comparison to previously used materials (e.g., Vespel). In some embodiments, the cartridge has a region with a thermal conductivity of between about 200-400 Watts per meter per degree Kelvin (for example, aluminum may have a thermal conductivity of between 200-250 W/m- K, while copper may have a thermal conductivity of between 350-400 W/m- K). In some embodiments, aluminum can be relaced with a steel alloy, e.g. SS304. In some embodiments, the consumable cartridge has a heat capacity to current ratio of 2-4 W/m- K-A. In some embodiments, the cartridge has an inner portion (e.g., designated by dotted lines 290A, 290B in
[0051] In addition, the nozzle body 216 includes a set of inlet swirl holes 228 (e.g., swirl holes 228A and 228B). In some embodiments, the set of inlet swirl holes 228 includes five swirl holes, or optionally between three and ten swirl holes. The swirl holes 228 can be radially offset to impart a swirl flow (e.g., radial and tangential velocity components) to gases flowing therethrough (e.g., a shield gas, plasma gas, and/or a plenum gas). In this configuration, the nozzle body 216 provides the swirl function previously provided by a swirl ring, thus eliminating the need for a traditional swirl ring. In addition, in some embodiments the nozzle body 216 is formed via a molding process, thus eliminating the need for expensive and time-consuming drilling procedures to create the swirl holes. In some embodiments, the nozzle shield 212 includes an angle 232 that helps redirect fluid flow away from the plasma arc during operation and helps to provide impingement cooling (e.g., gas flowing from holes 212 into angle 232).
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[0053] In addition, the cartridge 240 uses a molded, slotted swirl feature 266 to achieve the swirling function instead of using holes drilled in the nozzle body. For example, during operation gas can flow along path 265 as shown, with gas flowing out of the slots 266 and into the plasma chamber to form the swirl gas about the plasma arc. During operation, gas may also flow through molded gas shield channel 254, further cooling the nozzle body. Slots 266 form a set of swirl holes once the nozzle body, nozzle orifice, and/or nozzle liner are connected. Gas delivered to the slots is conveyed from the torch through a chamber defined by an internal surface of the nozzle body and an external surface of the nozzle liner (which, in combination, form the swirl holes). Such a configuration eliminates post-process machining steps and the associated expenses. In addition, the cartridge 240 includes a radial swage connection 258 between the nozzle orifice and the nozzle body. The radial swage connection 258 provides a robust connection interface to allow contact to be maintained between the nozzle orifice and the nozzle body, but also exposes significant surface area for heat to be conducted from the nozzle orifice to the nozzle body. Finally, in this embodiment, the electrode sleeve is removed and replaced with a more traditional heat exchanger.
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[0056] A number of features of the inner cartridge assembly 300 can enhance its cooling capabilities. First, the nozzle body 308 can be made of aluminum, which can enhance heat conduction over previous materials (e.g., Vespel) and configurations as described above. Second, the nozzle orifice 324 can be made of copper and can be pressed onto the nozzle body 308. In such embodiments, the nozzle body 308 can serve as a heat sink for the copper nozzle orifice 324. Third, improved gas flow surfaces, can assist in cooling, e.g., with shield gas flowing forward through holes 328A, 328B just outside of the press area. A press fit arrangement can also provide improved thermal conduction paths between torch parts as a result of relatively tight tolerances between the surfaces of the parts. In some embodiments, the press fit arrangement includes an interference fit and/or a tabbed or interlocking fit having one or more step-like features. In addition, the small size of the press fit design has the additional advantages of reducing manufacturing and/or material costs and simplifying manufacture and assembly of the components (e.g., by having fewer parts).
[0057] The nozzle shield 304 can also be made of copper and can be pressed onto an anodized aluminum insulator 314 at a surface 305A. This assembly can then be pressed onto the nozzle body 308 at a press fit surface 305B. In such embodiments, the shield insulator 314 connects the nozzle body 308 to the shield 304. In some embodiments, the shield insulator 314 is press fit to the nozzle body 308. In some embodiments, the shield insulator 314 is an electrically insulative ring and/or includes a set of press-fit surfaces 305A, 305B that connect the shield 304 and the nozzle body 308. The shield insulator 314 can connect the nozzle body 308 to the shield 304 such that the nozzle body 308 and the shield 304 are electrically insulated from one another while still transferring thermal energy to one another. In some embodiments, the press fit surfaces may be knurled to further enhance thermal conduction between components (e.g., between nozzle body 308 and nozzle orifice 324, between nozzle body 308 and shield 304, etc.). In some embodiments, using a two-piece shield insulator can increase (e.g., double) electrical insulation abilities as a result of increasing contact surfaces.
[0058] The nozzle shield 304 can be considerably smaller than previous shields, allowing for efficient manufacture and assembly of components, improved durability, and greater assurances of proper orientation of cartridge parts relative to one another. By way of example, for a 45-amp system, a prior art stock shield might have a diameter of about one inch and a mass of about 0.04 pounds, whereas a cartridge shield in accordance with the current invention can have a diameter of about 0.5 inches with a mass of less than 0.01 pounds (e.g., about 0.007 pounds). For a 105-amp system, a prior art stock shield might have a diameter of about one inch with a mass of about 0.05 pounds, whereas a cartridge shield in accordance with the current invention can have a diameter of about a half inch with a mass of about 0.01 pounds (e.g., 0.013 pounds).
[0059] The smaller size configuration can carry significant advantages. First, components having a reduced mass have a reduced heat capacity, which allows the components to be rapidly cooled during post-flow and/or allows more heat to be transferred to the cooling gas during operation. Second, a smaller shield can attain comparatively higher temperatures during operation and can transfer more heat to the cooling gas. In some embodiments, the nozzle shield 304 is exposed to a cold gas entering the shield area, e.g., via shield flow holes 328, which can further reduce the temperature. The flow holes 328 can each have a total cross sectional area of at least about one square inch.
[0060] In some embodiments, the electrode 320 includes a base made of copper. In some embodiments, the electrode 320 base has a small diameter with a pressed-on insulator sleeve 332 made of anodized aluminum and/or plastic used for electrical isolation. In some embodiments, a cooling gas flow channel or gap 336 exists between the insulator sleeve 332 and the nozzle body 308. In some embodiments, a cool gas flows in the gap 336. In some embodiments, a dumbbell configuration 340 defined by two end contacts 340A, 340B is used, which can reduce or minimize contact area between the nozzle body 308 and the insulator sleeve 332 and can reduce friction between parts.
[0061] In some embodiments, the sleeve 332 contacts the electrode 320, which can be part of a separate current path from the nozzle body 308 and/or a different portion of the current path from the nozzle body 308. In some embodiments, the electrode 320 and the nozzle orifice 324 can be electrically separated by a gap to create the arc and/or to ensure proper orientation of the parts in the torch. In such embodiments, the nozzle body 308 and the electrode 320 can be in physical contact between the sleeve 332 and the nozzle body 308. In such embodiments, insulative layers are needed in this region so that current is directed to pass through the emitting element 322.
[0062] In some embodiments, a wall of the nozzle body 342 near which the electrode 320 moves can stay comparatively cool during operation as gas flow passes both on the inside of the nozzle body 308 and directly across an exterior surface 344 of the nozzle orifice 324. The material choice (e.g., aluminum or another metal) for the nozzle body 342 design provides for a better conduction path and heat sink ability as compared with previous materials such as Vespel. Such factors assist in cooling the electrode isolation piece and allow the electrode to function even after a deep pit is formed in the emitting element from electrode use.
[0063] In some embodiments, a lock ring 316 (or isolation ring) forms an interface 346 between the cartridge 300 and the torch. In some embodiments, the lock ring 316 can be made of anodized aluminum. The lock ring 316 can be pressed into the nozzle body to trap the moveable electrode 320. The lock ring 316 can contain the components within the cartridge 300 and electrically isolate the torch. In some embodiments, the lock ring 316 is replaced by heat shrinking or gluing. In some embodiments, the lock ring 316 is shaped to orient the cartridge 300 (e.g., axially), to optimize gas flow, to enable electrical connection to the cathode, and/or to provide electrical isolation.
[0064] In various embodiments described herein, the cartridges or consumable assemblies are about 3.5 inches in length and 1.1 inches in diameter. In some embodiments, the retaining cap is considered part of the torch, e.g., not a consumable component. In such configurations, machining steps can be minimized, with no machining necessary after assembly (as compared to some torch assemblies that require a final machining step to achieve functional axiality of the cartridge). In some embodiments, the reduction in swirl holes can minimize drilling operations compared to prior art swirl rings. In some embodiments, replacing Vespel with aluminum can significantly reduce manufacturing costs of the cartridge. In some embodiments, copper is used only in certain locations in the electrode, nozzle, and/or orifice, which can reduce manufacturing costs. For example, copper can be concentrated primarily in an inner core or region to achieve the heat and current conduction benefits described above while minimizing the regions using the more expensive copper material.
[0065] In some embodiments, the anodized layer formed on select cartridge components can be created using a hard anodizing technique. An anodized layer formed using a Sulfuric hard anodizing process can be formed using an electrolytic solution of sulfuric acid. For example, an electrolytic solution of sulfuric acid at approximately 32 degrees Fahrenheit and a current density of about 23 to 37 Amperes per square foot can be used. The process can be run for about 20 to 120 minutes, depending on the alloy used and the desired coating thickness. A coating having a thickness of about 10 to 50 microns can be produced. This hard anodized coating can provide high corrosion resistance (e.g., 336+hours salt spray resistance), high durability (e.g. 60-70 Rockwell C-scale rating), and electrical insulation (e.g. 800 V/mil thickness). The hard anodize coating can be dyed, which does not necessarily produce the vibrant colors that a sulfuric anodize produces.
[0066] The anodizing process can provide a surface conversion of Aluminum to Al.sub.2O.sub.3. The anodizing process can provide a hard dielectric shell of about 0.003 inches thick (including both 50% build up (e.g. deposits on the part) and 50% penetration (e.g. material change to the exposed surfaces of the component). The hard dielectric shell can provide good atmospheric corrosion resistance. For extreme environments a 5% dichromate solution sealing is recommended, which can produce fair abrasion resistance. In some embodiments, a plurality of anodized disks can be pressed or heat shrunk together. Using a plurality of disks can create adjustable electrical isolation, e.g. because each disk increases electrical isolation linearly (via each coating/layer introduced by the new surfaces of each disk). By using multiple layers, electrical isolation capability can be made very strong. In some embodiments, plastics, ceramics, lava, or Vespel can be used in place of any or all of the anodized portions/components discussed herein.
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[0068] The plastic based cartridge 100 can include an aluminum nozzle body 116, to which other parts attach directly or indirectlye.g., a nozzle orifice 118, a shield 120, and an electrode 124 having an emitting element 126. The nozzle orifice 118 can be pressed into the nozzle body 116, for example at press fit junction 122. As above, the nozzle body 116 can have inlet swirl holes 128 (e.g., 128A and 128B as shown) and/or holes 130 directed forward (e.g., toward the front of the cartridge) through which shield gas can pass. The shield 120 can be made of copper and/or snapped onto a high temperature thermoplastic insulator. The shield/insulator assembly can be fastened to (e.g., snapped onto) the nozzle body 116. The electrode 124 can be made of copper. The electrode 124 can include an aluminum sleeve 132 having cooling holes (e.g. upper cooling gas flow channel 134 and lower cooling gas flow channel 136) pressed onto it. The high temperature thermoplastic sleeve 108 can be connected to (e.g., snapped onto) the electrode aluminum sleeve 132. The electrode 124 can be moveable within the nozzle body 116. The high temperature thermoplastic cap 104 can be snapped into the nozzle body to trap the electrode. The useful life of the cartridge parts can be arranged such that the useful lives of the individual parts are similar to one another. At the end of the cartridge's life, the entire cartridge 100 can be discarded (e.g., recycled), with no parts reused.
[0069] In some embodiments, the front plastic component 112 connects to and electrically isolates the shield 120 from the nozzle body 116. In some embodiments, the nozzle body 116 includes five shield cooling holes to supply cooling gas to the shield. In some embodiments, the sleeve plastic component 108 can be stressed during operation while both the front plastic component 112 and the rear plastic component 104 face milder conditions. These conditional variations can make it desirable to use different plastics for the front, middle and/or rear plastic portions. In some embodiments, the sleeve plastic portion 108 can be exposed to large thermal extremes, while the front plastic component 112 and the rear plastic component 104 can face comparatively lower temperatures during operation. As a result, the sleeve plastic component 108 can be formed of a more robust material/plastic (which involves increased cost and difficulty to manage) while the front and/or rear components 104, 112 can be formed of a separate slightly less robust material/plastic (which involves decreased cost and difficulty to manage). In some embodiments, the torch is hottest toward the front. In some embodiments, plastics that can withstand high temperatures can be used toward the front, but these materials are often more expensive. Less expensive materials can be used in cooler areas of the torch.
[0070] It is also possible to use anodized aluminum, ceramics, lava, or Vespel in place of any or all of these plastic portions/components. In some embodiments, cooling holes 134, 136 in the aluminum electrode sleeve 132 allow cooling gas to flow between the electrode 124 and nozzle body 116. The cooling holes 134, 136 can have different diameters within the sleeve 132 to achieve desired flow characteristics (e.g., increased flow, increased pressure, turbulent flow, laminar flow, etc.) for a given cartridge. In some embodiments, the electrode sleeve 132 can be shorter or longer (as shown in
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[0076] The cartridge designs shown and described above in
[0077] In some embodiments, cartridges are replaced as units, with no need to further assemble appropriate consumable stackups or select appropriate consumable combinations. In some embodiments, the length of the emitting element can be adjusted to match the life of the nozzle such that the cartridge parts reach the end of their useful lives at approximately the same time. In some embodiments, cut quality can be similar to that achieved using current consumables. In some embodiments, a spring need not be used with the electrode. Elimination of the spring may reduce manufacturing costs by eliminating the spring and thumbtack components on the top of the spring electrode. In some embodiments, machining steps can be minimized, with no machining necessary after assembly (as compared to some torch assemblies that require a final machining step to achieve functional axiality of the cartridge). In some embodiments, the reduction in swirl holes can minimize drilling operations compared to prior art swirl rings (the cross sectional area of these larger holes is roughly equivalent to the cross sectional area of all previous smaller holes). In some embodiments, particular components are or may optionally be molded or moldable, e.g., do not require machining. Thus, threading on the retaining cap and/or other components is not necessary to attach the components (e.g., cartridge consumable assembly), as the components can be already press fit together.
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[0085] While the invention has been particularly shown and described with reference to specific preferred embodiments, it should be understood by those skilled in the art that various changes in form and detail may be made therein without departing from the spirit and scope of the invention as defined by the following claims. In particular, the dimensions shown and discussed herein are offered by way of example only and are not intended to be construed as limiting. In addition, the materials described are exemplary, and other materials can be used while remaining within the spirit and scope of the technology.