This invention relates to a systems and methods for hot wire processing. More specifically, the subject invention relates to systems and methods for orbital hot wire cladding.
In a typical laser hot wire or filler wire process between a wire and workpiece, a laser heats and melts a workpiece to form a molten puddle. A filler wire is advanced towards a workpiece and the molten puddle. The wire is resistance-heated by a separate energy source such that the wire approaches or reaches its melting point and contacts the molten puddle. The heated wire is fed into the molten puddle for carrying out the hot wire process. Accordingly, transfer of the filler wire to the workpiece occurs by simply melting the filler wire into the molten puddle.
In the case of joining pipe members of dissimilar materials it is sometimes desirable to clad or apply a layer of metal alloy material, such as for example, a nickel alloy at the pipe ends to act as an intermediate or “butter” layer at the pipe ends before they are welded together. Moreover, it is generally desirable to minimize the admixture between the layer and the material of the pipes. Accordingly, it generally desired to minimize the thickness of the intermediate layer.
Further limitations and disadvantages of conventional, traditional, and proposed approaches will become apparent to one of skill in the art, through comparison of such approaches with embodiments of the present invention as set forth in the remainder of the present application with reference to the drawings.
Embodiments of the present invention include an orbital hot wire system for carrying out a hot wire process about the exterior of a pipe end. The system includes a torch assembly having a laser optics subassembly and a contact tube subassembly. A track is configured for mounting to the end portion of a pipe. A carriage is secured to the track for orbital translation about the pipe end portion. The torch assembly is coupled to the carriage for rotation of the torch assembly about the pipe end portion. A controller is provided for process control of the torch assembly so as to provide for a hot wire process over an angular translation about the pipe P, the angular translation defining an angle of about 180 degrees. Embodiments of the present invention can also include a control system providing for a hot wire process over an angular translation about the pipe P, the angular translation defining an angle in the range of 180 to 360 degrees.
Another embodiment provides a torch assembly for orbital hot wire processing about a pipe end. The torch assembly includes a laser optics subassembly for providing a laser beam to the pipe surface and a contact tube subassembly for delivering a filler wire W to the pipe surface proximate the laser beam. The laser optics subassembly has a distal end from which the focused laser beam emits and the contact tube assembly includes a distal end from which the filler wire extends. The distal ends of the laser optics subassembly and contact tube assembly defining a minimum clearance distance C therebetween.
These and other features of the claimed invention, as well as details of illustrated embodiments thereof, will be more fully understood from the following description and drawings.
The above and/or other aspects of the invention will be more apparent by describing in detail exemplary embodiments of the invention with reference to the accompanying drawings, in which:
Exemplary embodiments of the invention will now be described below by reference to the attached Figures. The described exemplary embodiments are intended to assist the understanding of the invention, and are not intended to limit the scope of the invention in any way. Like reference numerals refer to like elements throughout.
The torch assembly 110 is coupled to an orbital subsystem for circumferentially translating the torch assembly 110 about the pipe end portion. More specifically, the orbital subsystem includes a track 120 that extends circumferentially about the track 120. The track 120 is located along the axial length of the pipe P so as to locate the torch assembly 110 at the end of the pipe. Secured to the track 120 is a carriage 130 secured for orbital translation about the pipe P. An exemplary track and self-propelled carriage is shown and described in U.S. Pat. No. 5,227,601, which is incorporated by reference in its entirety.
The carriage 130 is shown in one aspect as including a wire feeder 140 that rotates about the pipe P with the torch assembly 110 to feed filler wire to the contact tube 110b. An exemplary wire feeder mounted to an orbital carriage is also shown and described in U.S. Pat. No. 5,227,601. Another exemplary orbital carriage and track arrangements is provided in the Helix T55 Orbital Welder from The Lincoln Electric Company of Cleveland, Ohio. The wire feeder 140, in one aspect, includes a hub (not shown) for supporting the spool of filler wire W and a feed mechanism (not shown) to pull and feed the wire W to the contact tube 110b. An exemplary wire feeder 140 includes a motor that is configured for hot wire process control by a system controller in a manner described below. Alternatively, the wire feeder 140 may be a non-rotating feeder and separate from the carriage 130. The separate wire feeder is located and configured to provide payout of the wire from the feeder 140 does not interfere with the orbital translation of the torch assembly 110 as described in greater detail below.
The torch assembly 110 is adjustably coupled to the carriage 130 for locating the torch assembly 110 relative to the track carriage 130. For example, the system 100 includes a mechanism for adjusting the axial location of the torch assembly 110 along the pipe axis X-X relative to the carriage 130 and more particular relative to the end of the pipe P. As seen for example in
The system 100 in one aspect may be configured for radial adjustment of the torch assembly 110 relative to the outer surface of the pipe P. For example, the system may include a second adjustment mechanism such as an adjustable bracket 152 configured for radially locating the torch assembly 110 along the radial axis Z-Z along which a laser beam extends and relative to the outer surface of the pipe P.
The laser optics assembly in one embodiment is a substantially a cylindrical member having a distal end 114a from which a collimated and focused laser beam exits and a proximal end 114b coupled to a laser beam delivery device such as for example, a fiber optic cable 111, as seen for example in
In addition to or in the alternative, the lenses are minimized and their spacing zz minimized so as to minimize the clearance distance C and further minimize the overall size of the laser optics subassembly 110a. With the size of the laser optics subassembly reduced the radial extension H over the torch assembly 110 may also be minimized. Reduction of the torch assembly 110 can reduce the drive and gearing requirements of the carriage 130 and track 120. Further in addition to or in the alternative, the housing of the laser optics subassembly 110a may be constructed to properly heat shield and protect the internal components of the subassembly to mitigate the impact of the heating process on the subassembly 110a such that the clearance distance C can be minimized.
In another aspect, the heat and inadvertent arcing from the filler wire W can be minimized or reduced to mitigate the impact of the heating process on the laser optics subassembly 110a such that the clearance distance C can be minimized. In one particular embodiment, the power supply 115 heating the filler wire W may be processed control to reduce the heat, arcing and/or inadvertent spattering so as to mitigate the impact of the process on the laser optics subassembly 110a. Described in greater detail below is an exemplary embodiment of a control system for the hot wire process and system 100.
The clearance distance C and/or size of the torch assembly 110 may be a function of the diameter of the track to which the torch assembly 110 is coupled. More specifically, the diameter of the track 120 may be defined by the nominal size of the pipe P to be processed. Referring to
In operation, the carriage 130 and track 120 translates the torch assembly 110a an angular distance θ to clad the outer surface of the pipe P. In one aspect, the drive of the carriage may be configured to translate clock-wise or counter-clock-wise about the pipe P. In some embodiments, the carriage performs cladding for a pass in the clockwise direction, and then upon completion of that pass moves the head assembly along the pipe P by one bead width and then performs the next pass in a counter-clockwise direction. Thus, the carriage (and any cabling, etc.) unwinds itself with respect to the pipe P. In some exemplary embodiments, the transition from one pass to the next occurs at a different angular position during the cladding operation to ensure that not adjacent transitions are at the same angular position on the surface of the pipe. For example, for a first pass the cladding switches from the first pass to a second pass at an angular position of 180 degrees, then switches between the second and third passes at 0 degrees, then switches from the third and fourth passes at 185 degrees, and switches between the fourth and fifth passes at 5 degrees. In exemplary embodiments of the present invention, there are at least 2 angular degrees between any adjacent passes.
The contact tube subassembly 110b and filler wire W may therefore lead or follow the laser beam of the laser optics subassembly 110a about the outer surface of the pipe P. Alternatively or in addition to, the torch assembly 110 may include a second contact tube subassembly 110′b, as seen in
Referring to
Shown in
In addition to the control arrangements to carry out an orbital hot wire welding operation, the wire feed and cabling connected to the rotating torch assembly 110 should be configured so as not to interfere with the rotating components of the system. For example, the power supply cable 117 to the contact tube assembly 110b should be configured so as to avoid entanglement with the orbital welding equipment. Moreover, the laser optics subassembly 110a in one embodiment has a fiber optic cable 111 coupled to it for delivery of the laser beam from the laser source. The fiber optic cable 111 should be arranged so as avoid entanglement with the orbital welding equipment. In addition, the fiber optic cable 111 should be configured so as not to degrade the laser signal to the optics. Shown in
It should be noted that in many of the embodiments discussed above—which are intended to be exemplary in nature—the pipe remains stationary while the carriage assembly is rotated. Of course, in other exemplary embodiments, the pipe P can be rotated. Further, embodiments of the present invention are not limited to embodiments which clad the outer diameters of pipes, but can also be utilized to clad the inner diameters of pipes.
It should also be noted that even though the above description has utilized discussion of a typical round consumable or wire, embodiments of the present invention can also be used with a strip type consumable (having a generally rectangular cross-section) which can utilize linear or scanned optics to aid in the creation of the puddle, as described herein.
While the invention has been described with reference to certain embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from its scope. Therefore, it is intended that the invention not be limited to the particular embodiments disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.
The present application is a continuation-in-part of U.S. patent application Ser. No. 13/212,025, filed on Aug. 17, 2011, which is a continuation-in-part of U.S. patent application Ser. No. 12/352,667, filed on Jan. 13, 2009, both of which are incorporated herein by reference in their entirety.
Number | Date | Country | |
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Parent | 13212025 | Aug 2011 | US |
Child | 13757162 | US | |
Parent | 12352667 | Jan 2009 | US |
Child | 13212025 | US |