1. Field of the Invention
The present invention relates to a plasma arc torch and, more particularly, to a plasma arc torch with improved electrode cooling and/or safety provisions.
2. Description of Related Art
Blowback type plasma torches are generally configured such that an electrode and a nozzle can be brought into contact with each other to ignite an arc, whereafter, the electrode is separated from the nozzle so as to draw the arc therebetween. A fluid, such as air, is concurrently provided under pressure through the nozzle, wherein the air flow interacts with the drawn arc so as to form a plasma. The plasma flowing through the nozzle is then directed at a workpiece to perform a cutting function.
In some instances, the fluid for forming the plasma is also used to cool the electrode and nozzle. That is, the formation of the plasma generally requires a limited amount of, for example, air. As such, the remainder of the fluid can be used for other purposes, such as to cool the electrode and nozzle that are heated by passage of the arc and by the plasma. Cooling of the electrode and nozzle may provide, for example, greater plasma stability and cutting performance, and may also lengthen the service life of the torch components. In some instances, such torches may also be configured to have a relatively compact size, with respect to both the components and the overall assembly. Accordingly, another consideration with these torches is safety, since the torch must incorporate a power feed for providing the arc, and must provide sufficient cooling to prevent catastrophic failure of the torch due to overheating. These considerations must also be implemented in the components of the torch assembly, since proper cooperation of the torch components may also be critical to safety and efficient performance.
Thus, there exists a need for a plasma arc torch, particularly a blowback type of plasma arc torch, having improved electrode and/or nozzle cooling characteristics for providing, for example, greater plasma stability, enhanced and/or consistent cutting performance, and an improved service life. Such a blowback type plasma torch should also facilitate safety, for example, by providing components configured to be formed into a torch assembly in a precise and consistent manner.
The above and other needs are met by the present invention which, in one embodiment, provides a plasma torch having a tubular member with opposing first and second ends and defining a bore extending axially between the ends, as well as a nozzle operably engaged with the first end of the tubular member. A movable member is movably engaged with the tubular member axially within the bore, and includes a first end disposed toward the nozzle and an opposing second end. A piston member is operably engaged with the movable member away from the first end thereof. An electrode, having a first portion defining a bore, is configured to be received by the first end of the movable member, wherein the electrode also has a second portion extending outwardly from the first end of the movable member toward the nozzle. The electrode further includes a radially outward-extending medial flange disposed between the first and second portions axially outward of the first end of the movable member. The electrode is configured to be movable by the piston member, via the movable member, between an inoperable position where the electrode is in contact with the nozzle and an operable position where the electrode is separated from the nozzle and the medial flange is in contact with the first end of the tubular member.
Embodiments of the present invention thus provide a blowback type of plasma arc torch having improved electrode and/or nozzle cooling characteristics. Such a blowback type plasma torch also facilitates safety, for example, by providing components configured to be formed into a torch assembly in a precise and consistent manner, whereby proper assembly or reassembly of the torch may be readily assured. These and other significant advantages are provided by embodiments of the present invention, as described further herein.
Having thus described the invention in general terms, reference will now be made to the accompanying drawings, which are not necessarily drawn to scale, and wherein:
The present inventions now will be described more fully hereinafter with reference to the accompanying drawings, in which some, but not all embodiments of the invention are shown. Indeed, these inventions may be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will satisfy applicable legal requirements. Like numbers refer to like elements throughout.
A piston member 50 includes a piston portion 55 having a shaft portion 60 engaged therewith and extending axially therefrom. The piston member 50 is configured to be received within the tubular member 20 such that the piston portion 55 is axially movable within the piston bore 25 and the shaft portion 60 is axially movable within the shaft bore 30. The piston member 50 is normally biased toward the shaft bore 30 by, for example, a biasing member 70 acting against the piston portion 55. The piston portion 55 may also include, for example, a sealing ring 75 extending around the circumference thereof so as to form a movable seal with the inner surface of the portion of the tubular member 20 defining the piston bore 25. One skilled in the art will appreciate, however, that the piston portion 55 may be movably sealed with respect to the piston bore 25 in many different manners consistent with the spirit and scope of the present invention.
The portion of the shaft bore 30 disposed between the end surface 40 and the holes 45 in the tubular member 20 is generally configured to be closely toleranced with respect to the outer dimensions of the shaft portion 60 of the piston member 55, but with sufficient clearance to allow the shaft portion 60 to move axially therethrough. However, the portion of the shaft bore 30 disposed between the piston bore 25 and the holes 45 is generally oversized with respect to the shaft portion 60 of the piston member 50. Accordingly, a pressurized fluid such as, for example, air, from a fluid source (not shown) introduced through the inlet channel 65 into the bore cannot escape axially past the sealing ring 75 surrounding the piston portion 55 within the piston bore 25 and will thus flow axially between the shaft portion 60 and shaft bore 30, from the piston bore 25 to the holes 45 in the tubular member 20. Due to the close tolerance between the shaft portion 60 and the shaft bore 30, between the holes 45 and the end surface 40, the pressurized air will tend to flow through the holes 45.
In some instances, the end 80 of the shaft portion 60, opposite the piston portion 55, is generally tubular and internally threaded. The end 80 of the shaft portion 60 may also define one or more holes 85 disposed medially between the end 80 of the shaft portion 60 and the piston portion 55, with the holes 85 extending through the wall of the end 80 of the shaft portion 60. Thus, some of the pressurized air will also tend to flow through the holes 85 defined by the shaft portion 60 and into the end 80, in addition to outwardly of the tubular member 20 through the holes 45 extending therethrough. The internally threaded end 80 is further configured to receive a hollow electrode 90. The hollow electrode 90 generally includes a tubular holder 95 with opposed first and second portions 100, 105. The first portion 100 is configured to receive an emissive element 110 therein, for example, in a friction fit. The second portion 105 is at least partially externally threaded, with the threads 115 extending toward the first portion 100, wherein the threads 115 are configured to correspond to the internally threaded end 80 of the shaft portion 60. In one embodiment, the second portion 105 includes only several threads 115 medially disposed along the second portion 105.
Following termination of the threads 115 and medially between the first and second portions 100, 105, the holder 95 forms a radially outward extending flange 120. The flange 120 extends radially outward so as to extend past the internally threaded end 80 of the shaft portion 60. Thus, when the second portion 105 of the holder 95 is threaded into the internally threaded end 80 of the shaft portion 60, the flange 120 functions to stop the axial threaded engagement between the second portion 105 and the internally threaded end 80 upon contact with the internally threaded end 80. In this manner, such an embodiment of the present invention advantageously indicates to the assembler that the holder 95 has been completely and properly engaged with the shaft portion 60. That is, failure of the flange 120 to contact the end of the shaft portion 60 when axial progress of the threaded engagement is halted, would indicate to the assembler, for example, that the electrode 90 is cross-threaded in the shaft portion 60 or that either of the threads are damaged, or that there is some other impediment to full engagement between the components. The assembler will thus be notified of a possible safety and/or operational hazard risk before the remainder of the torch 10 is assembled.
In some instances, the flange 120 may also be configured to extend radially outward to a sufficient extent, for example, to be greater than the inner diameter of the tubular member 20, such that the flange 120 is capable of engaging the end surface 40 of the tubular member 20. In such an instance, the flange 120 also functions to limit the extent of axial travel of the shaft portion 60 of the piston member 50 toward the piston bore 25. That is, in addition to the flange 120 providing an indicator of complete and proper engagement between the holder 95 and the shaft portion 60, the flange 120 of a properly installed and/or assembled electrode 90 also limits the extent of axial travel of the shaft portion 60 and, as such, the axial travel of the piston portion 55. As a result, the properly installed and/or assembled electrode 90 may allow closer tolerances with respect to other components of the torch 10 wherein, for example, the axial travel of the piston portion 55 may be limited with respect to the axial travel of a properly installed and/or assembled electrode 90 due to the flange 120, thereby advantageously allowing, for instance, a more compact torch 10 to be constructed. In such an instance, the indicator function provided by the flange 120 may also serve to prevent the piston portion 55 from reaching its axial travel limit prior to the flange 120 limiting the axial travel thereof. That is, if the electrode 90 is not properly installed, whereby the flange 120 contacts the end of the shaft portion 60, the piston portion 55 may limit the axial travel of the electrode 90 and the electrode 90 may not “blow back” to the full operative position upon actuation of the torch 10. The flange 120 thus functions to ensure that such a condition will not occur.
As shown in
In some instances, a heat shield 130 extends about the tubular member 20 and is radially spaced apart from the tubular member 20, along at least a portion of the tubular member 20 defining the shaft bore 30. The heat shield 130 extends axially toward the end surface 40, and may be externally threaded. The nozzle 140 defines an axial nozzle bore 145 (through which the plasma is emitted) and is configured to generally surround the first portion 100 of the hollow electrode 90 carrying the emissive element 110. A shield cup 150 is configured to extend over the nozzle 140 and includes internal threads configured to interact with the external threads of the heat shield 130 so as to secure the nozzle 140 to the end surface 40 of the tubular member 20. For example, the nozzle 140 may be configured to extend axially through the shield cup 150, with the nozzle 140 having a retaining flange for interacting with the shield cup 150 in order to retain and secure the nozzle 140. One skilled in the art will appreciate, however, that there may be many different configurations of the components involved in securing the nozzle 140 with respect to the end surface 40 of the tubular member 20. For example, the heat shield 130 and the shield cup 150 may be provided as an integral assembly. In other instances, for instance, the shield cup 150 and the nozzle 140 may be an integral assembly. Accordingly, the configurations provided herein are for example only and are not intended to be limiting in this respect.
Further to the described configuration shown in
The nozzle 140, the axial spacer 135 (if used), and the end surface 40 of the tubular member 20 thus cooperate to form the plasma chamber 155 in the torch 10. The electrode 90 is axially movable within the plasma chamber 155 between an inoperative position (as shown in
In general, a blowback torch of the type described first requires the application of a voltage between the emissive element 110/electrode 90 and the nozzle 140, with the electrode 90 in the inoperative position. Subsequently, the pressurized air is introduced through the inlet channel 65 with sufficient pressure to act on the piston portion 55 of the piston member 50 so as to force the piston member 50, and thus the electrode 90, away from the nozzle 140. The pressurized air acting on the piston portion 55 thus provides the “blowback” and moves the electrode 90 to the operative position, whereby separation of the emissive element 110/electrode 90 from the nozzle 140 draws the arc therebetween. At the same time, the air flowing through the one or more holes 125 defined by the holder 95, via the shaft bore 30, the one or more holes 85 defined by the end 80 of the shaft portion 60 and the holder 95, enters the plasma chamber 155 and thus forms the plasma which exits the plasma chamber 155 through the nozzle bore 145 so as to allow the operator to cut the workpiece. Any of the pressurized air flowing through the holes 45 defined by the tubular member 20 flows into a space defined by the heat shield 130 and shield cup 150 so as to, for example, provide cooling of those components. In some instances, the shield cup 150 may define one or more apertures (not shown) angularly spaced apart about the nozzle 140, wherein, for example, such apertures may be configured such that the air flowing therethrough provides cooling for the external surface of the nozzle 140 disposed outside the shield cup 150.
In the operating position, any of the pressurized air flowing through the hollow electrode 90 and through the one or more holes 125 defined thereby, is directed into and through the plasma chamber 155, and eventually out the nozzle bore 145. In instances, where the one or more holes 125 defined by the holder 95 are radially canted, the pressurized air emitted therefrom may be caused to swirl around the plasma chamber 155. Since the pressurized air introduced through the air inlet channel 65 flows through the interior of the hollow electrode 90, as well as around the exterior of the first end 100 of the hollow electrode 90 in which the emissive element 100 is received, improved cooling for the electrode 90 and/or nozzle 140 of the blowback torch 10 may be realized, in addition to improved control and consistency of the plasma flow. Extended service life of the electrode 90, emissive element 110, and/or the nozzle 140 may also be realized.
Many modifications and other embodiments of the inventions set forth herein will come to mind to one skilled in the art to which these inventions pertain having the benefit of the teachings presented in the foregoing descriptions and the associated drawings. Therefore, it is to be understood that the inventions are not to be limited to the specific embodiments disclosed and that modifications and other embodiments are intended to be included within the scope of the appended claims. Although specific terms are employed herein, they are used in a generic and descriptive sense only and not for purposes of limitation.