US20160016259A1 - Optimization of melt pool shape in a joining process - Google Patents
Optimization of melt pool shape in a joining process Download PDFInfo
- Publication number
- US20160016259A1 US20160016259A1 US14/336,215 US201414336215A US2016016259A1 US 20160016259 A1 US20160016259 A1 US 20160016259A1 US 201414336215 A US201414336215 A US 201414336215A US 2016016259 A1 US2016016259 A1 US 2016016259A1
- Authority
- US
- United States
- Prior art keywords
- melt pool
- energy
- amount
- done
- applying
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000000034 method Methods 0.000 title claims abstract description 65
- 230000008569 process Effects 0.000 title claims abstract description 63
- 238000005304 joining Methods 0.000 title description 5
- 238000005457 optimization Methods 0.000 title 1
- 239000000155 melt Substances 0.000 claims abstract description 167
- 239000000758 substrate Substances 0.000 claims abstract description 61
- 239000007787 solid Substances 0.000 claims abstract description 23
- 238000003466 welding Methods 0.000 claims abstract description 23
- 239000007788 liquid Substances 0.000 claims abstract description 19
- 238000007711 solidification Methods 0.000 claims description 19
- 230000008023 solidification Effects 0.000 claims description 19
- 238000010438 heat treatment Methods 0.000 claims description 16
- 239000000835 fiber Substances 0.000 claims description 12
- 238000005204 segregation Methods 0.000 claims description 12
- 230000000977 initiatory effect Effects 0.000 claims description 4
- 238000005336 cracking Methods 0.000 description 8
- 239000000463 material Substances 0.000 description 7
- 229910045601 alloy Inorganic materials 0.000 description 6
- 239000000956 alloy Substances 0.000 description 6
- 230000015572 biosynthetic process Effects 0.000 description 6
- 229910000601 superalloy Inorganic materials 0.000 description 6
- 238000001816 cooling Methods 0.000 description 5
- 230000007547 defect Effects 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 239000000470 constituent Substances 0.000 description 4
- 238000002844 melting Methods 0.000 description 4
- 230000008018 melting Effects 0.000 description 4
- 230000035515 penetration Effects 0.000 description 4
- 239000000843 powder Substances 0.000 description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 238000004891 communication Methods 0.000 description 3
- 230000004907 flux Effects 0.000 description 3
- 238000007726 management method Methods 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 230000007704 transition Effects 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 239000000654 additive Substances 0.000 description 2
- 230000000996 additive effect Effects 0.000 description 2
- 239000011324 bead Substances 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 239000012141 concentrate Substances 0.000 description 2
- 239000000356 contaminant Substances 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000011261 inert gas Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- 230000008439 repair process Effects 0.000 description 2
- 229910000995 CMSX-10 Inorganic materials 0.000 description 1
- 229910001011 CMSX-4 Inorganic materials 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- OQPDWFJSZHWILH-UHFFFAOYSA-N [Al].[Al].[Al].[Ti] Chemical compound [Al].[Al].[Al].[Ti] OQPDWFJSZHWILH-UHFFFAOYSA-N 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 229910000856 hastalloy Inorganic materials 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000000265 homogenisation Methods 0.000 description 1
- BHEPBYXIRTUNPN-UHFFFAOYSA-N hydridophosphorus(.) (triplet) Chemical compound [PH] BHEPBYXIRTUNPN-UHFFFAOYSA-N 0.000 description 1
- 229910001026 inconel Inorganic materials 0.000 description 1
- 238000010309 melting process Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000012768 molten material Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 229910001173 rene N5 Inorganic materials 0.000 description 1
- 229910001088 rené 41 Inorganic materials 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 230000000153 supplemental effect Effects 0.000 description 1
- 229910021324 titanium aluminide Inorganic materials 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/20—Bonding
- B23K26/21—Bonding by welding
- B23K26/24—Seam welding
- B23K26/26—Seam welding of rectilinear seams
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
- B23K26/06—Shaping the laser beam, e.g. by masks or multi-focusing
- B23K26/0604—Shaping the laser beam, e.g. by masks or multi-focusing by a combination of beams
- B23K26/0608—Shaping the laser beam, e.g. by masks or multi-focusing by a combination of beams in the same heat affected zone [HAZ]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
- B23K26/06—Shaping the laser beam, e.g. by masks or multi-focusing
- B23K26/067—Dividing the beam into multiple beams, e.g. multifocusing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/08—Devices involving relative movement between laser beam and workpiece
- B23K26/082—Scanning systems, i.e. devices involving movement of the laser beam relative to the laser head
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/08—Devices involving relative movement between laser beam and workpiece
- B23K26/083—Devices involving movement of the workpiece in at least one axial direction
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/08—Devices involving relative movement between laser beam and workpiece
- B23K26/0869—Devices involving movement of the laser head in at least one axial direction
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/20—Bonding
- B23K26/32—Bonding taking account of the properties of the material involved
-
- B23K26/3206—
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/70—Auxiliary operations or equipment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/18—Dissimilar materials
- B23K2103/26—Alloys of Nickel and Cobalt and Chromium
Definitions
- the present invention relates to joining processes, and more particularly to processes for shaping a melt pool during a joining process.
- Various processes are known for joining materials, which may collectively refer to the joinder of two or more substrates, as well as the repair or enhancement of one or more substrates.
- conduction welding and keyhole welding are known processes for the joining of materials.
- an entire thickness of a portion of the substrate 10 may be melted via an energy source 12 into a melt pool 14 .
- a keyhole 16 is formed through the entire thickness of the melt pool 14 of the substrate 10 .
- the melt pool 14 and associated keyhole 16 also traverse the substrate 10 in a direction of the weld 18 .
- the molten material of the melt pool 14 solidifies into a weld bead 20 behind the keyhole 16 as the keyhole advances.
- an inert gas 21 is provided around the melt pool to prevent oxidation of the substrate or other process material and (likely with supplemental gas) to suppress any plasma forming at the surface.
- the energy source 12 provides an amount of energy that is insufficient to form a keyhole 16 as was shown in FIG. 1 . Instead of forming a keyhole, heat is conducted into the substrate 10 from a surface of the substrate 10 .
- weld pool shape greatly influences susceptibility to weld cracking during the process of solidification. Solidifying grains grow normal to the solid-liquid interface (in the direction of maximum temperature gradient) and grow epitaxially with grain orientation most preferred with respect to the adjoining solid. Such shapes and grain orientations may significantly affect cracking.
- grains of parallel alignment form on each side of the pool (as viewed in 2D). Viewed in 3D, the grains also form roughly perpendicular to the sides of a cone. The grains terminate their solidification at the weld centerline (last location to solidify). Such grains also tend to be relatively large because there is no change in direction of solidification (from each linear side) and grains of preferred orientation can simply extend themselves toward the weld centerline.
- Low melting point elements e.g., sulfur and phosphorous
- similar constituents compounds such as eutectics
- Such constituents are known to aggravate solidification cracking because they may not sustain the stresses of final solidification.
- tear drop shaped weld pools 22 such constituents 32 segregate at the weld centerline 30 and are spread over relatively few and coarse grain boundaries. Such segregation expectedly leads to weld solidification cracking.
- cracking may occur as a result of tensile stress and as a result of a crack prone microstructure. It is postulated that in addition to affecting segregations that promote the latter crack prone microstructure, weld pool shape also affects stress distributions important for crack-free solidification. Stress concentrations in welds are complex and dependent on many factors, but likely the most important factor involves heat management. The restraint of the solid metal adjoining the solidifying melt is very important to such stress management. For example, a fully restrained substrate requires the solidifying melt to sustain all contraction stresses. Alternately, a non-constrained substrate accommodates shrinkage strains and is far less susceptible to cracking. Processes that are able to distribute such stresses are thus desired.
- initiation and termination of keyhole mode laser welds requires transitioning from a conduction mode to the keyhole mode to a conduction mode of welding (respectively). That is, when the laser beam is first directed to the substrate, it first produces a shallow melt pool. Translation and further energy delivery develops a through section keyhole. Such development involves turbulent motion of the melt and is prone to defect generation, e.g., porosity.
- through section penetration transitions to partial penetration and a hole surrounded by the molten metal transitions to a shallow melt pool. The molten geometric changes involved in such transitioning are prone to trapping of weld defects.
- the melt pool 14 may be characterized by a high depth to width (aspect) ratio in the substrate 10 due to the concentration of energy and speed of the welding process. Due to the high aspect ratio of the keyhole 16 and the speed of welding, voids (porosity) may form near the midpoint of a depth of the melt pool 14 remote from the melt pool surface. The voids may become trapped in the solidifying melt pool before the pores are able to travel to the melt pool surface. This effect is magnified by the presence of the tear drop shape ( FIG. 2 ), which provides less area for the defects to escape.
- conduction welding provides a melt pool that is generally more shallow and wide, but may still have a tear drop shaped melt pool as described herein.
- FIG. 1 illustrates the formation of a keyhole of a typical prior art keyhole welding process.
- FIG. 2 illustrates a top view of the tear drop shaped melt pool formed by the prior art process of FIG. 1 .
- FIG. 3A-3B illustrate a contour shaped melt pool having a solid/liquid interface in accordance with an aspect of the present invention.
- FIG. 4 illustrates a process of welding for forming a contoured melt pool in accordance with an aspect of the present invention.
- FIG. 5 illustrates the path of travel of a first energy source and a second energy source in a process in accordance with an aspect of the present invention.
- FIG. 6 illustrates a two-in-one fiber for use in an aspect of the present invention.
- FIG. 7 illustrates a melt pool formed by applying additional energy to edges of the melt pool in accordance with an aspect of the present invention.
- FIG. 8 illustrates the application of energy to form a contoured melt pool in accordance with an aspect of the present invention.
- FIGS. 9A-9D illustrate the formation of a curvilinear and curviplanar melt pool ( FIGS. 9C and 9D ) and a prior art melt pool ( FIGS. 9A-9B ) in accordance with an aspect of the present invention.
- aspects of the present invention are directed to processes and systems that strongly influence the shape of the melt pool in a joining process, such as a keyhole welding or a conduction welding process, relative to known processes.
- a process for welding comprising applying a first amount of energy and a second amount of energy to the substrate effective to provide a melt pool comprising a curvilinear and curviplanar solid/liquid interface.
- the contoured melt pool reduces segregation of artifacts and stress concentration within a depth and along a centerline of a width of the melt pool, as well as reduces a likelihood of void entrapment in the melt pool relative to a more tear drop shaped melt pool, for example.
- grains of highly varied alignment form on each side of the melt pool.
- the grains tend to curve toward the forward travel direction.
- Such grains also tend to be relatively small because there is continuous change in direction of solidification and grains of preferred orientation initiate and compete with advantage over grains of less preferred orientation.
- undesirable artifacts may spread throughout the solidifying weld and/or over many fine grain boundaries. Propensity for weld solidification cracking is thereby reduced.
- melt pool shape may not directly affect restraint of the solid metal adjoining the solidifying melt
- the melt pool shape may affect the direction and concentration of the resultant tensile stresses that typically, in conjunction with restraint, result in cracking. It is important that such stresses are not concentrated but rather distributed.
- melt pool shape control and process heat management may result in distributing such stresses.
- weld shape control processes described herein may improve the avoidance of deep penetration weld defects.
- Application of process energy in the wake of a deep penetration weld may shape the melt pool to transition from keyhole to conduction mode welding in a manner so as to minimize turbulence. Such transitioning can effectively avoid generation of inclusions and voids and/or enhance the opportunity for voidage to clear to the surface of the melt pool and to dissipate thereon.
- the substrate is heated outside of the melt pool to intentionally reduce a cooling rate or solidification rate of the melt pool and to effectively broaden the melt pool at least at a trailing edge region thereof (relative to processes without a heating outside the melt pool step).
- an inner region of the forming melt pool is heated so as to affect the shape of the melt pool.
- the widening of the melt pool at the trailing edge region creates more area for contaminants or voidage, for example, within the melt pool to be removed, as well as reduces segregation of artifacts along the centerline of the melt pool as was shown in FIG. 2 .
- the resulting solidified weld bead with reduced artifact segregation will be significantly stronger upon solidification.
- FIGS. 3A-3B there is shown a melt pool 100 on a substrate 105 which is widened relative to the teardrop shape melt pool 22 of the prior art described above (shown in dotted lines in FIG. 3 ).
- FIG. 3A shows the melt pool 100 from a top view in 2D while FIG. 3B shows the contoured shape 102 in a depth (D) of the melt pool 100 .
- a curviplanar solid/liquid interface 103 is shown between the melt pool 100 and the solid portion of the substrate 105 adjacent the melt pool 100 .
- the solid line in FIG. 3A represents the periphery 104 of the melt pool 100 having the contoured shape 102 .
- the melt pool 100 is provided with the contoured shape 102 at least at a trailing edge region 106 of the melt pool 100 .
- trailing edge region refers to the rear half of the melt pool 100 , such as any area of the melt pool 100 that is disposed between a vertical plane extending through a midpoint 108 (transverse to the direction of travel) and a rearmost point 110 of the melt pool 100 . It is appreciated however, that the area of the melt pool in front of the trailing edge region 106 (leading edge region 127 ) may also be broadened by the processes described herein.
- artifacts 114 will not segregate toward the centerline 112 as solidification occurs, but instead will be distributed more evenly about the perimeter of the melt pool 100 as shown in FIG. 3A .
- the substrate upon solidification, the substrate avoids weakening normally caused by centerline segregation of artifacts.
- Various processes are contemplated to produce a melt pool 100 on a substrate 105 having the contoured shape 102 described herein and shown in FIGS. 3A-3B .
- a number of processes will be described below; however, it is understood that the present invention is not so limited to any particular embodiment.
- the processes described herein may be utilized to join two substrates edge to edge, to repair one or more substrates, to enhance one or more substrates (by the addition of additional superalloy powder, for example, in front of the melt pool or therein), or as a way to build smaller substrates into larger assemblies.
- FIG. 4 there is shown an exemplary welding process to form a melt pool 100 with at least a trailing edge region 106 having the contoured shape 102 ( FIG. 3 ). It is appreciated that the melt pool is typically continuously advanced through the substrate 105 creating a weld seam.
- FIG. 4 thus represents the formation of a melt pool at a point in time with an area behind thereof which may have already been melted and resolidified and an area in front which has yet to be contacted by an energy source.
- a first energy source 116 provides a first amount of energy 118 to the substrate 105 .
- the first amount of energy 118 may be sufficient to form a keyhole 120 through the substrate 105 and a melt pool 100 about the keyhole 120 .
- the first amount of energy 118 solely forms a melt pool 100 but does not form a keyhole 120 as is the case in conduction welding.
- the melt pool 100 provided by the first amount of energy 118 may not have an optimal shape, e.g. has a tear drop shape 22 , such as that shown in FIG. 2 if no other actions were taken.
- a second energy source 122 may be utilized so as to deliver a second amount of energy 124 outside the width (W) of the melt pool 100 to provide the trailing edge region 106 with a contoured shape 102 as was shown in FIGS. 3A-3B .
- the first amount of energy 122 and the second amount of energy 124 may be provided from the same energy source.
- the first energy source 116 may be rapidly time shared with distinct amounts of energy momentarily directed to remote locations, such as by programmed oscillations of galvanometer driven scanning laser beam optics.
- the second amount of energy 124 is applied in a region outside a width (W) of the melt pool 100 .
- the second amount of energy 124 may be applied to regions 132 on one or more of the opposed sides of the melt pool 100 forming in the substrate 105 as will be explained in further detail below and as shown in FIG. 5 .
- the second amount of energy 124 is also applied within a width (W) of the melt pool 100 , which may also widen and shape the melt pool 100 .
- the second amount of energy 124 heats the region outside the width (W), but is insufficient in of itself to melt the substrate in the regions 132 . It is appreciated, however, that the heat from the melt pool 100 may be sufficient to melt a portion of the substrate 105 , particularly at the periphery of the melt pool 100 .
- the heating of the region outside the width (W) of the melt pool 100 increases a temperature of the substrate 105 about the melt pool 100 , and is thus effective to decrease a resolidificaiton rate of the melt pool, such as in a direction of travel of the weld.
- the cooling rate reduction about the melt pool 100 is effective to influence, e.g., broaden (relative to a process without such side heating), a shape of the trailing edge region 106 of the melt pool 100 since by decreasing the cooling rate.
- the contoured shape 102 of the melt pool 100 can be formed.
- the second amount of energy 124 is selected to heat the substrate 105 and nearby solidified deposit to a temperature that is from 1 to 300° C. below its melting temperature.
- the first and second energy sources (whether distinct or a time shared single source) 116 , 122 may be moved collectively in the direction of the weld 128 along a length of the substrate 105 .
- the substrate 105 may be moved in the direction of the weld 128 with respect to energy sources 116 , 122 which may be rendered stationary.
- first and second energy sources 116 , 122 may be moved in the same direction as one another.
- one energy source 116 may be moved in a first direction and the second energy source 122 may be moved in a distinct second direction.
- the first energy source 116 may be moved in the direction of the weld 128 while the second energy source 122 may be moved in a direction 130 transverse to the direction of the weld 128 .
- a normal speed of travel of the first energy source 116 can be maintained while the second energy source 122 may trail the first energy source 116 to heat the substrate 105 at regions, e.g., regions 132 , outside the width (W) of the melt pool 100 to control the cooling rate of the melt pool as described herein.
- the second energy source 122 may also heat an interior region of the melt pool 100 .
- the regions 132 are areas disposed on both sides 123 of the melt pool 100 , the sides being defined and extending between a leading edge and a trailing edge of the melt pool 100 .
- the size of either of the regions 132 to be heated adjacent the melt pool 100 may be any size necessary to achieve the desired result and would be readily determinable by one skilled in the art.
- the first amount of energy is applied in a direction of the weld 128 and the second amount of energy 124 is applied in a zig-zag pattern 134 as shown in FIG. 5 , but the movement of the first energy source 116 and/or the second energy source 122 may follow any other suitable pattern.
- the first amount of energy 118 has a greater power density and/or frequency than the second amount of energy 124 such that the first amount of energy 118 is effective to form the melt pool 100 while the second amount of energy 124 heats at least a region outside of a width (W) of the melt pool as was shown in FIG. 5 .
- the amount of first energy 118 applied for a longer duration or at more frequent intervals than the second amount of energy 124 to achieve the desired effect is without limitation.
- the second amount of energy 124 may be applied after initiation of the application of the first amount of energy 118 as is the case when the second energy source 122 applies the second amount of energy 124 behind a leading edge of the forming melt pool 100 .
- the first amount of energy 118 may be applied at the same time as the second amount of energy 124 or after the application of the first amount of energy 118 , for example.
- the applications of energy may be either continuous or pulsed in delivery.
- a single energy source is utilized.
- a single energy source is utilized along with a laser fiber to provide one or more energy beams on the substrate.
- a two-in-one fiber 135 may be used in combination with a single energy source, such as first energy source 116 , to provide the melt pool 100 having the contoured shape 102 . As shown in FIG.
- the two-in-one fiber 135 comprises an inner core 136 and an outer annulus 138 surrounding the inner core 136 .
- Two-in-one fibers are commercially available from Trumpf, Inc. (Plymouth Township, Mich.).
- the two-in-one fiber 135 provides a first amount of energy 118 through the inner core 136 and a second amount of energy 124 through the outer annulus 138 of the fiber 135 .
- the first amount of energy 118 may be effective to form the melt pool 100 in the substrate 105 as described herein.
- the second amount of energy 124 may contact a region, e.g., regions 132 , outside of the width (W) of the melt pool 100 so as to decrease a solidification of the melt pool 100 at least at the trailing edge region 106 thereof as described herein.
- the production of the differing first and second amounts of energy may be accomplished as described above, such as by applying the first amount of energy 118 through the core 136 at a greater intensity or for a longer duration than the second amount of energy through the annulus 138 .
- a keyhole 120 ( FIG. 4 ) and an adjacent melt pool 100 may be formed by the first amount of energy 118 traveling through the inner core 136 and the width outside of the keyhole 120 and melt pool 100 may be heated by the second amount of energy 124 traveling through the outer annulus 138 .
- a melt pool 100 that may be formed in a substrate 105 via applying the first amount of energy 118 and the second amount of energy 124 applies energy to the substrate 105 outside of the width (W) of the melt pool 100 so as to decrease a solidification of the melt pool 100 at least at the trailing edge region 106 thereof as described herein ( FIG. 5 ).
- an additional amount of energy 144 may be applied to the melt pool 100 at any location, e.g., locations 146 , within the melt pool 100 remote from the centerline 112 of the width (W) as is shown in FIG. 7 .
- the additional energy 144 is further effective to heat the melt pool at edges 148 of the sides 123 thereof and decrease a solidification rate of the melt pool 100 at least at the edges 148 .
- the edges 148 include at least edges of the trailing edge region 106 of the melt pool 100 .
- a third energy source 150 applies the additional amount of energy 144 as shown in FIG. 7 while the first energy source 116 applies the first amount of energy 118 and the second energy source 122 applies the second amount of energy 124 as explained previously ( FIG. 5 ).
- the additional energy 144 may be applied from time-shared energy from the first energy source 116 and/or the second energy source 122 .
- the additional amount of energy 144 may be applied in any suitable pattern, for example, in a zig-zag pattern transverse to the centerline 112 .
- the additional amount of energy 144 may be applied in the direction of the weld 128 ( FIG. 4 ).
- the second amount of energy 124 and additional energy 144 may be oscillated in a side-to-side motion or even into and out of the plane of processing by their respective sources in in a desired direction ( 128 and/or 130 , for example) to further refine solidifying grains and to scatter potential segregants or artifacts 114 from the centerline 112 .
- the application of additional energies to the first amount of energy 118 is believed to result in the redirection and homogenization of weld stresses that otherwise concentrate with single source, unidirectional process energy application.
- the additional application of energies as explained herein may promote a degree of post-weld stress relief heat treatment.
- a melt pool 100 having a contoured shape 102 with curvilinear and/or curviplanar solid/liquid interfaces may be formed without applying heat outside the width (W) of the melt pool 100 .
- a first energy source 118 applies energy to form at least a leading edge region of a melt pool 100 while a second energy source 122 applies energy to form a trailing edge region 106 of the melt pool as was shown and explained with respect to FIG. 5 .
- neither of the first and second energies are applied on the substrate outside the width (W) of the melt pool, but are still effective to provide the contoured shape 102 shown in FIGS. 3A-3B .
- the first amount of energy 118 and the second amount of energy 124 may each be applied in a concentric pattern as shown in FIG. 8 . Any one path in the pattern may overlap with another. In addition, though each path is shown as being substantially linear in a direction at a point in time, it appreciated that the application of energy is not so limited. Side to side movement in any direction as the associated energy source or substrate moves in a particular direction is also contemplated.
- the second amount of energy 124 is applied to a greater extent than the first amount of energy 118 . For example, the second amount of energy 124 may be applied for a longer duration, at more frequent intervals, and/or to a greater surface area relative to the first amount of energy 118 .
- curvilinear refers to a curved line and the term “curviplanar” refers to a curved plane.
- curviplanar it is also meant that there are no straight lines associated with a plane of the melt pool (below such as one might have with a cone or cylinder).
- the melt pool viewed top down on the process plane (2D) could show a solid/liquid interface line that is either straight (linear) 150 or curved (rounded, oval, or the like (curvilinear 152 )).
- the processes described herein provide a curvilinear solid/liquid interface.
- a solid/liquid interface surface may represent a plane 154 . If the plane 154 were conical 156 (as one might expect from a tear-drop shaped weld pool) (see FIG. 9C ), then it would have relatively straight sides as viewed in a transverse cross section and grains 158 would grow toward a common weld centerline . If the plane were curviplanar 160 as would be expected from an oval-shaped weld pool, for example, then its sides would be curved and grains 158 would have to have multiple orientations to grow from the solid/liquid interface as shown in FIG. 9D . Aspects of the present invention thus provide for a melt pool with a solid/interface that also has a curviplanar solid/liquid interface.
- the depth of the melt by any of the applied energies may be controlled so as to provide the desired shape within the depth of the melt pool. For example, this may be accomplished by controlling parameters of the energy application as would be understood by the skilled artisan, such as controlling pulse duration, pulse duration, frequency, and/or other any suitable parameters.
- the melt pool 100 includes only minimal, if any, planar liquid/solid interfaces. In a particular embodiment, there are no planar liquid/solid interfaces of the melt pool 100 .
- the substrate 105 may comprise any material with which would benefit from the processes described herein.
- the substrate 105 comprises a superalloy material.
- superalloy is used herein as it is commonly used in the art to refer to a highly corrosion-resistant and oxidation-resistant alloy that exhibits excellent mechanical strength and resistance to creep even at high temperatures.
- Superalloys typically include a high nickel or cobalt content.
- Exemplary superalloys include, but are not limited to alloys sold under the trademarks and brand names Hastelloy, Inconel alloys (e.g. IN 738, IN 792, IN 939), Rene alloys (e.g.
- the substrate 105 may comprise a ceramic material.
- the one or more energy sources to form the melt pool 100 and to heat the regions 132 outside the width (W) or periphery 126 of the melt pool 100 may be any suitable energy source sufficient to accomplish the corresponding objective.
- the one or more energy sources either or both of sources 116 , 122 for example, may be a laser energy source. It is appreciated that the skilled artisan would be able to identify the parameters and understand in what manner to vary the parameters so as to provide a melt pool 100 having a desired shape as described herein. Such parameters may include but are not limited to power density, pulse duration, pulse intervals, frequency, use of two-in-one fibers, the number of energy sources, use of hybrid (e.g. plasma and laser) sources, spacing between source and substrate, and the like.
- the depth of the melt pool 100 and thus the melting of the substrate 105 may be controlled as desired.
- a portion of the melt pool 100 e.g., such as the region 140 shown in FIG. 3A
- a melt pool 100 may have a curvilinear and a curviplanar solid/liquid interface so as to improve the clearance of artifacts and porosity from the melt pool 100 .
- the amount of energy applied to the substrate 105 by the one or more energy sources is applied non-uniformly in some manner or includes a power gradient.
- the energy source which forms the melt pool 100 may begin melting at a particular predetermined power density which is gradually increased over a predetermined time interval to form the keyhole and/or melt pool. This has the likelihood of reducing turbulence that typically causes defects, such as pores or other undesirable inclusions.
- contoured shape 102 of the melt pool 100 is shown as being a relatively elliptical shape from a top view, it is understood, however, that the present invention is not so limited. It is contemplated that other shapes may be formed and the melt pool 100 does not have the tear drop shape 22 so that artifacts 114 do not segregate along the centerline 30 of the melt pool 100 as was shown in FIG. 2 . Also, the melt pool shape provided herein may be any one that provides reduced stress along the centerline and provides a greater likelihood for the escape of porosity from the melt pool prior to resolidification relative to a tear drop shaped melt pool.
- one or more controllers may be provided which is in direct or wireless communication with at least the one or more energy sources.
- controller 142 is shown in communication with first energy source 116 and second energy source 122 .
- the one or more controllers may be programmed with or may have software/hardware for controlling the energy sources.
- the one or more controllers are configured to execute computer readable instructions for adjust parameters such as power density, pulse duration, frequency, and direction of travel of the energy source(s) or substrate as described above.
- one or more sensors e.g., temperature sensors, are provided to monitor the melting process.
- the one or more sensors are also in communication with the controller 142 .
- the one or more controllers 142 may comprise one or more inputs for receiving information, such as temperature on the substrate or stress distribution surrounding the process location, from the one or more of the sensors described.
- the controller 142 may comprise, for example, a special purpose computer comprising a microprocessor, a microcomputer, an industrial controller, a programmable logic controller, a discrete logic circuit or other suitable controlling device.
- the controller 142 comprises input channels, a memory, an output channel, and a computer.
- the term computer may include a processor, a microcontroller, a microcomputer, a programmable logic controller (PLC), an application specific integrated circuit, and other programmable circuits.
- the memory may include a computer-readable medium or a storage device, e.g., floppy disk, a compact disc read only memory (CD-ROM), or the like.
- the controller 142 comprises computer readable instructions for performing any aspect of the methods or for controlling any aspect of the systems described herein.
- the processes described herein may take place under appropriate flux conditions to shield the melt pool 100 from atmospheric oxygen.
- the processes described herein may be performed in the presence of a flowing stream of argon or other inert gas (shown by reference numeral 21 ) over the melt pool 100 which shields the melt pool 100 from atmospheric oxygen as was shown in FIG. 1 .
- a flux powder of a size and composition as described in U.S. Published Patent Application No. 2013/0136868 may be introduced onto the substrate and/or the melt pool to similarly shield the melt pool from atmospheric oxygen.
- the use of a flux powder has a plurality of advantages associated therewith including the formation of a layer of slag at a top surface of the melt pool which aids in carrying away contaminants from the melt pool and in itself insulating and controlling heat dissipation, thereby influencing weld pool shape and stresses.
- the additive material may be in the form of a superalloy powder, which is applied to the melt pool or ahead of the formation of the melt pool as described in U.S. 2013/0136868.
Landscapes
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- Mechanical Engineering (AREA)
- Laser Beam Processing (AREA)
Abstract
There is provided a process for welding that includes applying a first amount of energy 118 and a second amount of energy 122 to a substrate 105 effective to provide a melt pool 100 comprising a curvilinear and/or curviplanar solid/liquid interface 103 about at least a trailing edge region 106 and within a depth (D) of the melt pool 100.
Description
- The present invention relates to joining processes, and more particularly to processes for shaping a melt pool during a joining process.
- Various processes are known for joining materials, which may collectively refer to the joinder of two or more substrates, as well as the repair or enhancement of one or more substrates. For example, conduction welding and keyhole welding are known processes for the joining of materials. As shown in
FIG. 1 , in keyhole welding, an entire thickness of a portion of thesubstrate 10 may be melted via anenergy source 12 into amelt pool 14. In this way, akeyhole 16 is formed through the entire thickness of themelt pool 14 of thesubstrate 10. As the process traverses in the direction of travel of the weld, themelt pool 14 and associatedkeyhole 16 also traverse thesubstrate 10 in a direction of theweld 18. The molten material of themelt pool 14 solidifies into aweld bead 20 behind thekeyhole 16 as the keyhole advances. In the embodiment shown, aninert gas 21 is provided around the melt pool to prevent oxidation of the substrate or other process material and (likely with supplemental gas) to suppress any plasma forming at the surface. In conduction welding, theenergy source 12 provides an amount of energy that is insufficient to form akeyhole 16 as was shown inFIG. 1 . Instead of forming a keyhole, heat is conducted into thesubstrate 10 from a surface of thesubstrate 10. - A number of issues may arise during formation of the melt pool. The first involves segregations of problematic elements and constituents. The second involves concentrated tensile stress. The third involves entrapment of voids particular to keyhole welding. With respect to segregations, it is appreciated that weld pool shape greatly influences susceptibility to weld cracking during the process of solidification. Solidifying grains grow normal to the solid-liquid interface (in the direction of maximum temperature gradient) and grow epitaxially with grain orientation most preferred with respect to the adjoining solid. Such shapes and grain orientations may significantly affect cracking.
- For tear drop-shaped weld pools of linear solid liquid interface, grains of parallel alignment form on each side of the pool (as viewed in 2D). Viewed in 3D, the grains also form roughly perpendicular to the sides of a cone. The grains terminate their solidification at the weld centerline (last location to solidify). Such grains also tend to be relatively large because there is no change in direction of solidification (from each linear side) and grains of preferred orientation can simply extend themselves toward the weld centerline.
- Low melting point elements (e.g., sulfur and phosphorous) and similar constituents (compounds such as eutectics) naturally concentrate at the last point of solidification. Such constituents are known to aggravate solidification cracking because they may not sustain the stresses of final solidification. Referring to
FIG. 2 , in the case of tear drop shapedweld pools 22,such constituents 32 segregate at theweld centerline 30 and are spread over relatively few and coarse grain boundaries. Such segregation expectedly leads to weld solidification cracking. - In addition, cracking may occur as a result of tensile stress and as a result of a crack prone microstructure. It is postulated that in addition to affecting segregations that promote the latter crack prone microstructure, weld pool shape also affects stress distributions important for crack-free solidification. Stress concentrations in welds are complex and dependent on many factors, but likely the most important factor involves heat management. The restraint of the solid metal adjoining the solidifying melt is very important to such stress management. For example, a fully restrained substrate requires the solidifying melt to sustain all contraction stresses. Alternately, a non-constrained substrate accommodates shrinkage strains and is far less susceptible to cracking. Processes that are able to distribute such stresses are thus desired.
- Further, it is appreciated that initiation and termination of keyhole mode laser welds requires transitioning from a conduction mode to the keyhole mode to a conduction mode of welding (respectively). That is, when the laser beam is first directed to the substrate, it first produces a shallow melt pool. Translation and further energy delivery develops a through section keyhole. Such development involves turbulent motion of the melt and is prone to defect generation, e.g., porosity. Upon weld termination, through section penetration transitions to partial penetration and a hole surrounded by the molten metal transitions to a shallow melt pool. The molten geometric changes involved in such transitioning are prone to trapping of weld defects.
- Still further, in keyhole welding, the
melt pool 14 may be characterized by a high depth to width (aspect) ratio in thesubstrate 10 due to the concentration of energy and speed of the welding process. Due to the high aspect ratio of thekeyhole 16 and the speed of welding, voids (porosity) may form near the midpoint of a depth of themelt pool 14 remote from the melt pool surface. The voids may become trapped in the solidifying melt pool before the pores are able to travel to the melt pool surface. This effect is magnified by the presence of the tear drop shape (FIG. 2 ), which provides less area for the defects to escape. Compared to keyhole welding, conduction welding provides a melt pool that is generally more shallow and wide, but may still have a tear drop shaped melt pool as described herein. - The invention is explained in the following description in view of the drawings that show:
-
FIG. 1 illustrates the formation of a keyhole of a typical prior art keyhole welding process. -
FIG. 2 illustrates a top view of the tear drop shaped melt pool formed by the prior art process ofFIG. 1 . -
FIG. 3A-3B illustrate a contour shaped melt pool having a solid/liquid interface in accordance with an aspect of the present invention. -
FIG. 4 illustrates a process of welding for forming a contoured melt pool in accordance with an aspect of the present invention. -
FIG. 5 illustrates the path of travel of a first energy source and a second energy source in a process in accordance with an aspect of the present invention. -
FIG. 6 illustrates a two-in-one fiber for use in an aspect of the present invention. -
FIG. 7 illustrates a melt pool formed by applying additional energy to edges of the melt pool in accordance with an aspect of the present invention. -
FIG. 8 illustrates the application of energy to form a contoured melt pool in accordance with an aspect of the present invention. -
FIGS. 9A-9D illustrate the formation of a curvilinear and curviplanar melt pool (FIGS. 9C and 9D ) and a prior art melt pool (FIGS. 9A-9B ) in accordance with an aspect of the present invention. - Aspects of the present invention are directed to processes and systems that strongly influence the shape of the melt pool in a joining process, such as a keyhole welding or a conduction welding process, relative to known processes. In accordance with one aspect of the present invention, there is provided a process for welding comprising applying a first amount of energy and a second amount of energy to the substrate effective to provide a melt pool comprising a curvilinear and curviplanar solid/liquid interface. As will be described herein, the contoured melt pool reduces segregation of artifacts and stress concentration within a depth and along a centerline of a width of the melt pool, as well as reduces a likelihood of void entrapment in the melt pool relative to a more tear drop shaped melt pool, for example.
- More specifically, with a curvilinear and curviplanar solid/liquid interface, grains of highly varied alignment form on each side of the melt pool. The grains tend to curve toward the forward travel direction. Such grains also tend to be relatively small because there is continuous change in direction of solidification and grains of preferred orientation initiate and compete with advantage over grains of less preferred orientation. Further, undesirable artifacts may spread throughout the solidifying weld and/or over many fine grain boundaries. Propensity for weld solidification cracking is thereby reduced.
- In addition, it is appreciated that while melt pool shape may not directly affect restraint of the solid metal adjoining the solidifying melt, the melt pool shape may affect the direction and concentration of the resultant tensile stresses that typically, in conjunction with restraint, result in cracking. It is important that such stresses are not concentrated but rather distributed. Another key benefit of the processes described herein is that melt pool shape control and process heat management may result in distributing such stresses.
- Further, the weld shape control processes described herein may improve the avoidance of deep penetration weld defects. Application of process energy in the wake of a deep penetration weld, for example, may shape the melt pool to transition from keyhole to conduction mode welding in a manner so as to minimize turbulence. Such transitioning can effectively avoid generation of inclusions and voids and/or enhance the opportunity for voidage to clear to the surface of the melt pool and to dissipate thereon.
- In particular embodiments, the substrate is heated outside of the melt pool to intentionally reduce a cooling rate or solidification rate of the melt pool and to effectively broaden the melt pool at least at a trailing edge region thereof (relative to processes without a heating outside the melt pool step). In other embodiments, an inner region of the forming melt pool is heated so as to affect the shape of the melt pool. In either case, the widening of the melt pool at the trailing edge region creates more area for contaminants or voidage, for example, within the melt pool to be removed, as well as reduces segregation of artifacts along the centerline of the melt pool as was shown in
FIG. 2 . The resulting solidified weld bead with reduced artifact segregation will be significantly stronger upon solidification. - By way of example, with reference to
FIGS. 3A-3B , there is shown amelt pool 100 on asubstrate 105 which is widened relative to the teardropshape melt pool 22 of the prior art described above (shown in dotted lines inFIG. 3 ).FIG. 3A shows themelt pool 100 from a top view in 2D whileFIG. 3B shows thecontoured shape 102 in a depth (D) of themelt pool 100. A curviplanar solid/liquid interface 103 is shown between themelt pool 100 and the solid portion of thesubstrate 105 adjacent themelt pool 100. The solid line inFIG. 3A represents theperiphery 104 of themelt pool 100 having the contouredshape 102. In certain embodiments, themelt pool 100 is provided with thecontoured shape 102 at least at a trailingedge region 106 of themelt pool 100. As used herein, the term “trailing edge region” refers to the rear half of themelt pool 100, such as any area of themelt pool 100 that is disposed between a vertical plane extending through a midpoint 108 (transverse to the direction of travel) and arearmost point 110 of themelt pool 100. It is appreciated however, that the area of the melt pool in front of the trailing edge region 106 (leading edge region 127) may also be broadened by the processes described herein. In any case, via the increased broadened and/or contoured shape relative to prior art processes,artifacts 114 will not segregate toward thecenterline 112 as solidification occurs, but instead will be distributed more evenly about the perimeter of themelt pool 100 as shown inFIG. 3A . Thus, upon solidification, the substrate avoids weakening normally caused by centerline segregation of artifacts. - Various processes are contemplated to produce a
melt pool 100 on asubstrate 105 having the contouredshape 102 described herein and shown inFIGS. 3A-3B . A number of processes will be described below; however, it is understood that the present invention is not so limited to any particular embodiment. By way of example only, the processes described herein may be utilized to join two substrates edge to edge, to repair one or more substrates, to enhance one or more substrates (by the addition of additional superalloy powder, for example, in front of the melt pool or therein), or as a way to build smaller substrates into larger assemblies. - Referring to
FIG. 4 , there is shown an exemplary welding process to form amelt pool 100 with at least a trailingedge region 106 having the contoured shape 102 (FIG. 3 ). It is appreciated that the melt pool is typically continuously advanced through thesubstrate 105 creating a weld seam.FIG. 4 thus represents the formation of a melt pool at a point in time with an area behind thereof which may have already been melted and resolidified and an area in front which has yet to be contacted by an energy source. - In the embodiment shown, a
first energy source 116 provides a first amount ofenergy 118 to thesubstrate 105. In certain embodiments, the first amount ofenergy 118 may be sufficient to form akeyhole 120 through thesubstrate 105 and amelt pool 100 about thekeyhole 120. In other embodiments, the first amount ofenergy 118 solely forms amelt pool 100 but does not form akeyhole 120 as is the case in conduction welding. In any case, themelt pool 100 provided by the first amount ofenergy 118 may not have an optimal shape, e.g. has atear drop shape 22, such as that shown inFIG. 2 if no other actions were taken. - To provide the
melt pool 100 with thecontoured shape 102, asecond energy source 122 may be utilized so as to deliver a second amount ofenergy 124 outside the width (W) of themelt pool 100 to provide the trailingedge region 106 with acontoured shape 102 as was shown inFIGS. 3A-3B . Alternately, the first amount ofenergy 122 and the second amount ofenergy 124 may be provided from the same energy source. For example, thefirst energy source 116 may be rapidly time shared with distinct amounts of energy momentarily directed to remote locations, such as by programmed oscillations of galvanometer driven scanning laser beam optics. In an embodiment, the second amount ofenergy 124 is applied in a region outside a width (W) of themelt pool 100. For example, the second amount ofenergy 124 may be applied toregions 132 on one or more of the opposed sides of themelt pool 100 forming in thesubstrate 105 as will be explained in further detail below and as shown inFIG. 5 . In certain embodiments, the second amount ofenergy 124 is also applied within a width (W) of themelt pool 100, which may also widen and shape themelt pool 100. - In this embodiment, the second amount of
energy 124 heats the region outside the width (W), but is insufficient in of itself to melt the substrate in theregions 132. It is appreciated, however, that the heat from themelt pool 100 may be sufficient to melt a portion of thesubstrate 105, particularly at the periphery of themelt pool 100. The heating of the region outside the width (W) of themelt pool 100 increases a temperature of thesubstrate 105 about themelt pool 100, and is thus effective to decrease a resolidificaiton rate of the melt pool, such as in a direction of travel of the weld. In addition, the cooling rate reduction about themelt pool 100 is effective to influence, e.g., broaden (relative to a process without such side heating), a shape of the trailingedge region 106 of themelt pool 100 since by decreasing the cooling rate. Through control of the pattern of application of the second amount ofenergy 124, thecontoured shape 102 of themelt pool 100 can be formed. In an embodiment, the second amount ofenergy 124 is selected to heat thesubstrate 105 and nearby solidified deposit to a temperature that is from 1 to 300° C. below its melting temperature. - In an embodiment, the first and second energy sources (whether distinct or a time shared single source) 116, 122 may be moved collectively in the direction of the
weld 128 along a length of thesubstrate 105. Alternatively, thesubstrate 105 may be moved in the direction of theweld 128 with respect toenergy sources - Further, the first and
second energy sources FIG. 5 , oneenergy source 116 may be moved in a first direction and thesecond energy source 122 may be moved in a distinct second direction. For example, as shown inFIG. 5 , thefirst energy source 116 may be moved in the direction of theweld 128 while thesecond energy source 122 may be moved in adirection 130 transverse to the direction of theweld 128. In this way, a normal speed of travel of thefirst energy source 116 can be maintained while thesecond energy source 122 may trail thefirst energy source 116 to heat thesubstrate 105 at regions, e.g.,regions 132, outside the width (W) of themelt pool 100 to control the cooling rate of the melt pool as described herein. As shown, it is contemplated that thesecond energy source 122 may also heat an interior region of themelt pool 100. - In one embodiment, the
regions 132 are areas disposed on bothsides 123 of themelt pool 100, the sides being defined and extending between a leading edge and a trailing edge of themelt pool 100. The size of either of theregions 132 to be heated adjacent themelt pool 100 may be any size necessary to achieve the desired result and would be readily determinable by one skilled in the art. - In certain embodiments, the first amount of energy is applied in a direction of the
weld 128 and the second amount ofenergy 124 is applied in a zig-zag pattern 134 as shown inFIG. 5 , but the movement of thefirst energy source 116 and/or thesecond energy source 122 may follow any other suitable pattern. - In certain embodiments, to obtain the differential application of energy, the first amount of
energy 118 has a greater power density and/or frequency than the second amount ofenergy 124 such that the first amount ofenergy 118 is effective to form themelt pool 100 while the second amount ofenergy 124 heats at least a region outside of a width (W) of the melt pool as was shown inFIG. 5 . - In other embodiments, the amount of
first energy 118 applied for a longer duration or at more frequent intervals than the second amount ofenergy 124 to achieve the desired effect. It is appreciated that the order of application of the first amount ofenergy 118 and the second amount ofenergy 124 is without limitation. For example, the second amount ofenergy 124 may be applied after initiation of the application of the first amount ofenergy 118 as is the case when thesecond energy source 122 applies the second amount ofenergy 124 behind a leading edge of the formingmelt pool 100. Alternatively, the first amount ofenergy 118 may be applied at the same time as the second amount ofenergy 124 or after the application of the first amount ofenergy 118, for example. Also, the applications of energy may be either continuous or pulsed in delivery. - The above embodiment described the use of two
energy sources melt pool 100 with thecontoured shape 102. It is appreciated, however, that a fewer or greater number of energy sources may be utilized. In one embodiment, a single energy source is utilized. In a particular embodiment, a single energy source is utilized along with a laser fiber to provide one or more energy beams on the substrate. Referring toFIG. 6 , for example, a two-in-onefiber 135 may be used in combination with a single energy source, such asfirst energy source 116, to provide themelt pool 100 having the contouredshape 102. As shown inFIG. 6 , for example, the two-in-onefiber 135 comprises aninner core 136 and anouter annulus 138 surrounding theinner core 136. Two-in-one fibers are commercially available from Trumpf, Inc. (Plymouth Township, Mich.). In an embodiment, the two-in-onefiber 135 provides a first amount ofenergy 118 through theinner core 136 and a second amount ofenergy 124 through theouter annulus 138 of thefiber 135. In this way, the first amount ofenergy 118 may be effective to form themelt pool 100 in thesubstrate 105 as described herein. In addition, utilizing a single energy source, the second amount ofenergy 124 may contact a region, e.g.,regions 132, outside of the width (W) of themelt pool 100 so as to decrease a solidification of themelt pool 100 at least at the trailingedge region 106 thereof as described herein. - The production of the differing first and second amounts of energy may be accomplished as described above, such as by applying the first amount of
energy 118 through thecore 136 at a greater intensity or for a longer duration than the second amount of energy through theannulus 138. In a particular embodiment, for example, a keyhole 120 (FIG. 4 ) and anadjacent melt pool 100 may be formed by the first amount ofenergy 118 traveling through theinner core 136 and the width outside of thekeyhole 120 and meltpool 100 may be heated by the second amount ofenergy 124 traveling through theouter annulus 138. - Referring now to
FIG. 7 , there is shown amelt pool 100 that may be formed in asubstrate 105 via applying the first amount ofenergy 118 and the second amount ofenergy 124 applies energy to thesubstrate 105 outside of the width (W) of themelt pool 100 so as to decrease a solidification of themelt pool 100 at least at the trailingedge region 106 thereof as described herein (FIG. 5 ). Further, in this aspect, an additional amount ofenergy 144 may be applied to themelt pool 100 at any location, e.g.,locations 146, within themelt pool 100 remote from thecenterline 112 of the width (W) as is shown inFIG. 7 . Theadditional energy 144 is further effective to heat the melt pool atedges 148 of thesides 123 thereof and decrease a solidification rate of themelt pool 100 at least at theedges 148. In an embodiment, theedges 148 include at least edges of the trailingedge region 106 of themelt pool 100. By applying the additional heat to atleast edges 148 of the trailingedge region 106, the trailingedge region 106 is kept relatively hot, which results in the trailingedge region 106 cooling at substantially the same rate as the leading edge region of the melt pool 100 (or closer thereto than without application of the additional energy). This may result in favorably affecting a shape of the solidifying material, such as by providing a substantially symmetrical and oval shaped solidifying melt pool (2D) and a spherical, ellipsoidal, or the like surface-shaped solid/liquid interface (3D). - In an embodiment, a
third energy source 150 applies the additional amount ofenergy 144 as shown inFIG. 7 while thefirst energy source 116 applies the first amount ofenergy 118 and thesecond energy source 122 applies the second amount ofenergy 124 as explained previously (FIG. 5 ). Alternatively, theadditional energy 144 may be applied from time-shared energy from thefirst energy source 116 and/or thesecond energy source 122. The additional amount ofenergy 144 may be applied in any suitable pattern, for example, in a zig-zag pattern transverse to thecenterline 112. Alternatively, the additional amount ofenergy 144 may be applied in the direction of the weld 128 (FIG. 4 ). - In certain embodiments, the second amount of
energy 124 and additional energy 144 (if applied) may be oscillated in a side-to-side motion or even into and out of the plane of processing by their respective sources in in a desired direction (128 and/or 130, for example) to further refine solidifying grains and to scatter potential segregants orartifacts 114 from thecenterline 112. In any case, the application of additional energies to the first amount ofenergy 118 is believed to result in the redirection and homogenization of weld stresses that otherwise concentrate with single source, unidirectional process energy application. Further, the additional application of energies as explained herein may promote a degree of post-weld stress relief heat treatment. - In still another embodiment, it is contemplated that a
melt pool 100 having a contouredshape 102 with curvilinear and/or curviplanar solid/liquid interfaces may be formed without applying heat outside the width (W) of themelt pool 100. For example, afirst energy source 118 applies energy to form at least a leading edge region of amelt pool 100 while asecond energy source 122 applies energy to form a trailingedge region 106 of the melt pool as was shown and explained with respect toFIG. 5 . However, in this instance, neither of the first and second energies are applied on the substrate outside the width (W) of the melt pool, but are still effective to provide the contouredshape 102 shown inFIGS. 3A-3B . - For example, the first amount of
energy 118 and the second amount ofenergy 124 may each be applied in a concentric pattern as shown inFIG. 8 . Any one path in the pattern may overlap with another. In addition, though each path is shown as being substantially linear in a direction at a point in time, it appreciated that the application of energy is not so limited. Side to side movement in any direction as the associated energy source or substrate moves in a particular direction is also contemplated. In an embodiment, the second amount ofenergy 124 is applied to a greater extent than the first amount ofenergy 118. For example, the second amount ofenergy 124 may be applied for a longer duration, at more frequent intervals, and/or to a greater surface area relative to the first amount ofenergy 118. - As mentioned, in any of the processes described herein, it is desirable to provide a
melt pool 100 having a curvilinear and/or curviplanar solid/liquid interface. The term “curvilinear” refers to a curved line and the term “curviplanar” refers to a curved plane. By “curviplanar,” it is also meant that there are no straight lines associated with a plane of the melt pool (below such as one might have with a cone or cylinder). Thus, as shown inFIG. 9A and 9D , the melt pool viewed top down on the process plane (2D) could show a solid/liquid interface line that is either straight (linear) 150 or curved (rounded, oval, or the like (curvilinear 152)). In one aspect, the processes described herein provide a curvilinear solid/liquid interface. - Further, if the
melt pool 100 could be viewed in 3D, (e.g. by multi-positioned x-ray, etc.), then a solid/liquid interface surface may represent a plane 154. If the plane 154 were conical 156 (as one might expect from a tear-drop shaped weld pool) (seeFIG. 9C ), then it would have relatively straight sides as viewed in a transverse cross section andgrains 158 would grow toward a common weld centerline . If the plane were curviplanar 160 as would be expected from an oval-shaped weld pool, for example, then its sides would be curved andgrains 158 would have to have multiple orientations to grow from the solid/liquid interface as shown inFIG. 9D . Aspects of the present invention thus provide for a melt pool with a solid/interface that also has a curviplanar solid/liquid interface. - It is appreciated that the depth of the melt by any of the applied energies may be controlled so as to provide the desired shape within the depth of the melt pool. For example, this may be accomplished by controlling parameters of the energy application as would be understood by the skilled artisan, such as controlling pulse duration, pulse duration, frequency, and/or other any suitable parameters. In an embodiment, the
melt pool 100 includes only minimal, if any, planar liquid/solid interfaces. In a particular embodiment, there are no planar liquid/solid interfaces of themelt pool 100. - For the processes described herein, the
substrate 105 may comprise any material with which would benefit from the processes described herein. In certain embodiments, thesubstrate 105 comprises a superalloy material. The term “superalloy” is used herein as it is commonly used in the art to refer to a highly corrosion-resistant and oxidation-resistant alloy that exhibits excellent mechanical strength and resistance to creep even at high temperatures. Superalloys typically include a high nickel or cobalt content. Exemplary superalloys include, but are not limited to alloys sold under the trademarks and brand names Hastelloy, Inconel alloys (e.g. IN 738, IN 792, IN 939), Rene alloys (e.g. Rene N5, Rene 41, Rene 80,Rene 108,Rene 142, Rene 220), Haynes alloys, Mar M, CM 247, CM 247 LC, C263, 718, X-750, ECY 768, 262, X45, PWA 1483 and CMSX (e.g. CMSX-4) single crystal alloys, GTD 111, GTD 222, MGA 1400, MGA 2400,PSM 116, CMSX-8, CMSX-10, PWA 1484, IN 713C, Mar-M-200, PWA 1480, IN 100, IN 700, Udimet 600, Udimet 500 and titanium aluminide. Alternatively, thesubstrate 105 may comprise a ceramic material. - The one or more energy sources to form the
melt pool 100 and to heat theregions 132 outside the width (W) or periphery 126 of themelt pool 100 may be any suitable energy source sufficient to accomplish the corresponding objective. In an embodiment, the one or more energy sources, either or both ofsources melt pool 100 having a desired shape as described herein. Such parameters may include but are not limited to power density, pulse duration, pulse intervals, frequency, use of two-in-one fibers, the number of energy sources, use of hybrid (e.g. plasma and laser) sources, spacing between source and substrate, and the like. - In any of the embodiments described herein, it is appreciated that the depth of the
melt pool 100 and thus the melting of thesubstrate 105 may be controlled as desired. As mentioned above, it is contemplated that a portion of the melt pool 100 (e.g., such as theregion 140 shown inFIG. 3A ) may have a shorter depth from a top surface of thesubstrate 105 relative to a remainder of themelt pool 100. In this way, amelt pool 100 may have a curvilinear and a curviplanar solid/liquid interface so as to improve the clearance of artifacts and porosity from themelt pool 100. - In certain embodiments, the amount of energy applied to the
substrate 105 by the one or more energy sources is applied non-uniformly in some manner or includes a power gradient. For example, the energy source which forms themelt pool 100 may begin melting at a particular predetermined power density which is gradually increased over a predetermined time interval to form the keyhole and/or melt pool. This has the likelihood of reducing turbulence that typically causes defects, such as pores or other undesirable inclusions. - Further, although the
contoured shape 102 of themelt pool 100 is shown as being a relatively elliptical shape from a top view, it is understood, however, that the present invention is not so limited. It is contemplated that other shapes may be formed and themelt pool 100 does not have thetear drop shape 22 so thatartifacts 114 do not segregate along thecenterline 30 of themelt pool 100 as was shown inFIG. 2 . Also, the melt pool shape provided herein may be any one that provides reduced stress along the centerline and provides a greater likelihood for the escape of porosity from the melt pool prior to resolidification relative to a tear drop shaped melt pool. - To carry out the methods described herein, one or more controllers may be provided which is in direct or wireless communication with at least the one or more energy sources. For example, in
FIG. 4 ,controller 142 is shown in communication withfirst energy source 116 andsecond energy source 122. The one or more controllers may be programmed with or may have software/hardware for controlling the energy sources. As such, the one or more controllers are configured to execute computer readable instructions for adjust parameters such as power density, pulse duration, frequency, and direction of travel of the energy source(s) or substrate as described above. In certain embodiments, one or more sensors, e.g., temperature sensors, are provided to monitor the melting process. The one or more sensors are also in communication with thecontroller 142. As such, the one ormore controllers 142 may comprise one or more inputs for receiving information, such as temperature on the substrate or stress distribution surrounding the process location, from the one or more of the sensors described. - The
controller 142 may comprise, for example, a special purpose computer comprising a microprocessor, a microcomputer, an industrial controller, a programmable logic controller, a discrete logic circuit or other suitable controlling device. In one embodiment, thecontroller 142 comprises input channels, a memory, an output channel, and a computer. As used herein, the term computer may include a processor, a microcontroller, a microcomputer, a programmable logic controller (PLC), an application specific integrated circuit, and other programmable circuits. The memory may include a computer-readable medium or a storage device, e.g., floppy disk, a compact disc read only memory (CD-ROM), or the like. In an embodiment, thecontroller 142 comprises computer readable instructions for performing any aspect of the methods or for controlling any aspect of the systems described herein. - The processes described herein may take place under appropriate flux conditions to shield the
melt pool 100 from atmospheric oxygen. In certain embodiments, the processes described herein may be performed in the presence of a flowing stream of argon or other inert gas (shown by reference numeral 21) over themelt pool 100 which shields themelt pool 100 from atmospheric oxygen as was shown inFIG. 1 . - In other embodiments, a flux powder of a size and composition as described in U.S. Published Patent Application No. 2013/0136868 (, the entirety of which is hereby incorporated by reference herein) may be introduced onto the substrate and/or the melt pool to similarly shield the melt pool from atmospheric oxygen. The use of a flux powder has a plurality of advantages associated therewith including the formation of a layer of slag at a top surface of the melt pool which aids in carrying away contaminants from the melt pool and in itself insulating and controlling heat dissipation, thereby influencing weld pool shape and stresses. In addition, if any of the processes described herein are to be utilized as an additive manufacturing process, the additive material may be in the form of a superalloy powder, which is applied to the melt pool or ahead of the formation of the melt pool as described in U.S. 2013/0136868.
- While various embodiments of the present invention have been shown and described herein, it will be obvious that such embodiments are provided by way of example only. Numerous variations, changes and substitutions may be made without departing from the invention herein. Accordingly, it is intended that the invention be limited only by the spirit and scope of the appended claims.
Claims (20)
1. A process for welding comprising:
forming a melt pool having a width along a longitudinal length of a substrate;
heating the substrate outside the width of the melt pool with an amount of energy which does not melt the substrate but is effective to reduce a resolidification rate of the melt pool and reduce segregation of artifacts and stress concentration along a centerline of the width.
2. The process of claim 1 , wherein the forming is done with a first amount of energy from a first energy source, and wherein the heating is done with a second amount of energy from a distinct second energy source or time-shared energy from the first energy source.
3. The process of claim 1 , wherein the heating is done on both opposed sides of the width of the melt pool.
4. The process of claim 1 , wherein the heating is done following the initiation of the forming of the melt pool and behind a leading edge of the forming melt pool.
5. The process of claim 1 , wherein the forming is done in a direction of the weld, and wherein the heating is done in a direction transverse to the direction of the weld.
6. The process of claim 1 , wherein the forming forms a keyhole in the melt pool, and wherein the heating is done by applying heat outside the width of the melt pool behind the keyhole.
7. The process of claim 1 , wherein the heating and forming are done simultaneously via a two-in-one fiber, wherein the forming is done through a central portion of the fiber, and wherein the heating is done through an annular region about the central portion.
8. The process of claim 1 , wherein the forming and the heating are done using a laser source, and wherein the heating of the melt pool results in a melt pool having substantially a bowl shape.
9. The process of claim 1 , further comprising applying additional energy to the melt pool at a location remote from the centerline of the width, the additional energy further effective to decrease a solidification rate of the melt pool at edges of the melt pool.
10. A process for welding comprising:
forming a melt pool in a substrate via applying a first amount of energy thereto; and
applying a second amount of energy to the substrate outside a periphery of the melt pool to reduce segregation of artifacts and stress concentration along a centerline of a width of the melt pool.
11. The process of claim 10 , wherein the forming of the melt pool is done with a first amount of energy from a first energy source, and wherein the applying of a second amount of energy outside a periphery of the melt pool is done with a second amount of energy from a distinct second energy source or time-shared energy from the first energy source.
12. The process of claim 10 , wherein the applying of a second amount of energy outside a periphery of the melt pool is done following initiation of the forming of the melt pool behind a leading edge of the forming melt pool.
13. The process of claim 10 , wherein the forming of the melt pool is done in a direction of the weld, and wherein the applying of a second amount of energy outside a periphery of the melt pool is done in a direction transverse to the direction of the weld.
14. The process of claim 10 , wherein the forming a melt pool forms a keyhole in the melt pool, and wherein the applying of a second amount of energy outside a periphery of the melt pool is done by applying energy to the substrate outside the width of the melt pool behind the keyhole.
15. The process of claim 10 , wherein the forming and applying are done simultaneously via a two-in-one fiber, wherein the melt pool is formed through energy traveling through a central portion of the fiber, and wherein the applying of a second amount of energy outside a periphery of the melt is done through an annular region about the central portion.
16. The process of claim 10 , wherein the forming and the applying are done using a laser source, and wherein the heating of the melt pool results in a melt pool having substantially a bowl shape.
17. The process of claim 10 , further comprising applying additional energy to the melt pool at a location remote from the centerline of the width, the additional energy further effective to decrease a solidification rate of the melt pool at edges of the melt pool.
18. A process for welding comprising applying a first amount of energy and a second amount of energy to the substrate effective to provide a melt pool comprising a curvilinear and a curviplanar solid/liquid interface about at least a trailing edge region and within a depth of the melt pool, the applying of the first and second energies effective to reduce turbulence of the melt pool; and reduce segregation of artifacts and stress concentration within the depth and along a centerline of a width of the melt pool.
19. The process of claim 18 , wherein the applying comprises:
applying the first amount of energy to the substrate and the second amount of energy behind the first amount of energy in a direction of the weld to provide the melt pool, wherein the second amount of energy is applied to a greater extent than the first amount of energy.
20. The process of claim 18 , wherein the applying comprises:
forming a melt pool having a width along a longitudinal length of the substrate;
heating the substrate outside the width of the melt pool with an amount of energy which does not melt the substrate but is effective to reduce a resolidification rate of the melt pool and reduce segregation of artifacts and stress concentration along the centerline of the width.
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/336,215 US20160016259A1 (en) | 2014-07-21 | 2014-07-21 | Optimization of melt pool shape in a joining process |
DE112015003358.0T DE112015003358T5 (en) | 2014-07-21 | 2015-07-21 | OPTIMIZATION OF THE MELT BATHING FORM IN A JOINTING METHOD |
PCT/US2015/041291 WO2016014499A1 (en) | 2014-07-21 | 2015-07-21 | Optimization of melt pool shape in a joining process |
CN201580039767.8A CN106536120B (en) | 2014-07-21 | 2015-07-21 | Optimization of the shape of the weld pool during joining |
KR1020207008944A KR102255255B1 (en) | 2014-07-21 | 2015-07-21 | Optimization of melt pool shape in a joining process |
KR1020177004726A KR20170031238A (en) | 2014-07-21 | 2015-07-21 | Optimization of melt pool shape in a joining process |
US16/281,185 US11440138B2 (en) | 2014-07-21 | 2019-02-21 | Optimization of melt pool shape in a joining process |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/336,215 US20160016259A1 (en) | 2014-07-21 | 2014-07-21 | Optimization of melt pool shape in a joining process |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US16/281,185 Division US11440138B2 (en) | 2014-07-21 | 2019-02-21 | Optimization of melt pool shape in a joining process |
Publications (1)
Publication Number | Publication Date |
---|---|
US20160016259A1 true US20160016259A1 (en) | 2016-01-21 |
Family
ID=55073806
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US14/336,215 Abandoned US20160016259A1 (en) | 2014-07-21 | 2014-07-21 | Optimization of melt pool shape in a joining process |
US16/281,185 Active 2035-04-03 US11440138B2 (en) | 2014-07-21 | 2019-02-21 | Optimization of melt pool shape in a joining process |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US16/281,185 Active 2035-04-03 US11440138B2 (en) | 2014-07-21 | 2019-02-21 | Optimization of melt pool shape in a joining process |
Country Status (5)
Country | Link |
---|---|
US (2) | US20160016259A1 (en) |
KR (2) | KR20170031238A (en) |
CN (1) | CN106536120B (en) |
DE (1) | DE112015003358T5 (en) |
WO (1) | WO2016014499A1 (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20170197278A1 (en) * | 2016-01-13 | 2017-07-13 | Rolls-Royce Plc | Additive layer manufacturing methods |
US10179952B2 (en) * | 2013-03-08 | 2019-01-15 | Rutgers, The State University Of New Jersey | Patterned thin films by thermally induced mass displacement |
JP2020514550A (en) * | 2015-12-04 | 2020-05-21 | レイセオン カンパニー | Composition and method for melt processing aluminum alloys |
US10828837B2 (en) | 2018-12-13 | 2020-11-10 | General Electric Company | Method for melt pool monitoring using algebraic connectivity |
US10828836B2 (en) | 2018-12-13 | 2020-11-10 | General Electric Company | Method for melt pool monitoring |
US10894364B2 (en) | 2018-12-13 | 2021-01-19 | General Electric Company | Method for melt pool monitoring using geometric length |
US20210094124A1 (en) * | 2019-10-01 | 2021-04-01 | Futaba Industrial Co., Ltd. | Manufacturing method of component |
US11020907B2 (en) | 2018-12-13 | 2021-06-01 | General Electric Company | Method for melt pool monitoring using fractal dimensions |
US20210362264A1 (en) * | 2020-05-20 | 2021-11-25 | The Boeing Company | Fabrication with regulated grain formation |
US11285671B2 (en) | 2018-12-13 | 2022-03-29 | General Electric Company | Method for melt pool monitoring using Green's theorem |
US11833623B2 (en) | 2013-07-16 | 2023-12-05 | Illinois Tool Works Inc. | Additive manufacturing system for joining and surface overlay |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102020119395A1 (en) * | 2019-07-24 | 2021-01-28 | Shiloh Industries, Inc. | Sheet metal assembly with post-treated welded joint |
DE102021113430A1 (en) | 2021-05-25 | 2022-01-20 | Audi Aktiengesellschaft | Process for laser beam deep welding |
US12030251B2 (en) | 2021-08-20 | 2024-07-09 | General Electric Company | Irradiation devices with optical modulators for additively manufacturing three-dimensional objects |
US12280446B2 (en) | 2021-08-20 | 2025-04-22 | General Electric Company | Irradiation devices with optical modulators for additively manufacturing three-dimensional objects |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2283448A (en) * | 1993-10-27 | 1995-05-10 | Rolls Royce Plc | Improvements in or relating to electron beam welding |
US5461692A (en) * | 1993-11-30 | 1995-10-24 | Amoco Corporation | Multimode optical fiber coupling apparatus and method of transmitting laser radiation using same |
US20130105447A1 (en) * | 2011-10-26 | 2013-05-02 | Titanova Inc | Puddle forming and shaping with primary and secondary lasers |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3244579B2 (en) * | 1993-12-17 | 2002-01-07 | 富士通株式会社 | Optical fiber amplifier |
JP3272534B2 (en) * | 1994-03-14 | 2002-04-08 | 三菱重工業株式会社 | Laser welding method for Al alloy |
US5616261A (en) * | 1995-06-07 | 1997-04-01 | Chrysler Corporation | Laser welding system |
US6444947B1 (en) * | 1997-08-01 | 2002-09-03 | Fraunhofer-Gesellschaft Zur Forderung Der Angewandten Forschung E.V. | Method and device for laser beam welding |
US6054672A (en) * | 1998-09-15 | 2000-04-25 | Chromalloy Gas Turbine Corporation | Laser welding superalloy articles |
JP2001252780A (en) * | 2000-03-09 | 2001-09-18 | Laser Oyo Kogaku Kenkyusho:Kk | Method of joining by laser beam for cylinders of different kinds of metals |
US6479168B2 (en) * | 2001-04-03 | 2002-11-12 | The Regents Of The University Of Michigan | Alloy based laser welding |
WO2003031108A1 (en) * | 2001-10-09 | 2003-04-17 | Ecole Polytechnique Federale De Lausanne (Epfl) | Process for avoiding cracking in welding |
US7154064B2 (en) * | 2003-12-08 | 2006-12-26 | General Motors Corporation | Method of improving weld quality |
US6972390B2 (en) * | 2004-03-04 | 2005-12-06 | Honeywell International, Inc. | Multi-laser beam welding high strength superalloys |
CA2819095C (en) * | 2010-12-17 | 2018-09-04 | Magna International Inc. | Laser beam welding |
JP5658579B2 (en) * | 2011-01-28 | 2015-01-28 | 日新製鋼株式会社 | Laser welded section steel |
US20130309000A1 (en) * | 2012-05-21 | 2013-11-21 | General Electric Comapny | Hybrid laser arc welding process and apparatus |
CN103817439B (en) * | 2014-03-13 | 2017-01-11 | 机械科学研究院哈尔滨焊接研究所 | Prefabricated welding material laser welding method capable of obviously improving joint tissue and stress state |
-
2014
- 2014-07-21 US US14/336,215 patent/US20160016259A1/en not_active Abandoned
-
2015
- 2015-07-21 KR KR1020177004726A patent/KR20170031238A/en not_active Ceased
- 2015-07-21 KR KR1020207008944A patent/KR102255255B1/en active Active
- 2015-07-21 DE DE112015003358.0T patent/DE112015003358T5/en active Pending
- 2015-07-21 WO PCT/US2015/041291 patent/WO2016014499A1/en active Application Filing
- 2015-07-21 CN CN201580039767.8A patent/CN106536120B/en active Active
-
2019
- 2019-02-21 US US16/281,185 patent/US11440138B2/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2283448A (en) * | 1993-10-27 | 1995-05-10 | Rolls Royce Plc | Improvements in or relating to electron beam welding |
US5461692A (en) * | 1993-11-30 | 1995-10-24 | Amoco Corporation | Multimode optical fiber coupling apparatus and method of transmitting laser radiation using same |
US20130105447A1 (en) * | 2011-10-26 | 2013-05-02 | Titanova Inc | Puddle forming and shaping with primary and secondary lasers |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10179952B2 (en) * | 2013-03-08 | 2019-01-15 | Rutgers, The State University Of New Jersey | Patterned thin films by thermally induced mass displacement |
US12083633B2 (en) | 2013-07-16 | 2024-09-10 | Illinois Tool Works Inc. | Additive manufacturing heating control systems and methods |
US11833623B2 (en) | 2013-07-16 | 2023-12-05 | Illinois Tool Works Inc. | Additive manufacturing system for joining and surface overlay |
JP2020514550A (en) * | 2015-12-04 | 2020-05-21 | レイセオン カンパニー | Composition and method for melt processing aluminum alloys |
US20170197278A1 (en) * | 2016-01-13 | 2017-07-13 | Rolls-Royce Plc | Additive layer manufacturing methods |
US11285671B2 (en) | 2018-12-13 | 2022-03-29 | General Electric Company | Method for melt pool monitoring using Green's theorem |
US11020907B2 (en) | 2018-12-13 | 2021-06-01 | General Electric Company | Method for melt pool monitoring using fractal dimensions |
US10894364B2 (en) | 2018-12-13 | 2021-01-19 | General Electric Company | Method for melt pool monitoring using geometric length |
US11679548B2 (en) | 2018-12-13 | 2023-06-20 | General Electric Company | Method for melt pool monitoring |
US10828836B2 (en) | 2018-12-13 | 2020-11-10 | General Electric Company | Method for melt pool monitoring |
US10828837B2 (en) | 2018-12-13 | 2020-11-10 | General Electric Company | Method for melt pool monitoring using algebraic connectivity |
US20210094124A1 (en) * | 2019-10-01 | 2021-04-01 | Futaba Industrial Co., Ltd. | Manufacturing method of component |
US20210362264A1 (en) * | 2020-05-20 | 2021-11-25 | The Boeing Company | Fabrication with regulated grain formation |
US12257642B2 (en) * | 2020-05-20 | 2025-03-25 | The Boeing Company | Fabrication with regulated grain formation |
Also Published As
Publication number | Publication date |
---|---|
US11440138B2 (en) | 2022-09-13 |
CN106536120A (en) | 2017-03-22 |
KR102255255B1 (en) | 2021-05-21 |
DE112015003358T5 (en) | 2017-04-13 |
KR20200035502A (en) | 2020-04-03 |
WO2016014499A1 (en) | 2016-01-28 |
US20190176265A1 (en) | 2019-06-13 |
KR20170031238A (en) | 2017-03-20 |
CN106536120B (en) | 2022-04-26 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US11440138B2 (en) | Optimization of melt pool shape in a joining process | |
Gong et al. | Laser-arc hybrid additive manufacturing of stainless steel with beam oscillation | |
KR101715475B1 (en) | Laser welding method | |
Liu et al. | Effects of processing parameters on crystal growth and microstructure formation in laser powder deposition of single-crystal superalloy | |
KR101974252B1 (en) | Laser weld method and weld structure | |
JP5736135B2 (en) | Double laser beam welding method for first and second filler metals | |
EP0740977B1 (en) | Containerless method of producing crack free metallic articles | |
CN104284752B (en) | Repair of directionally solidified alloys | |
US10967460B2 (en) | Method for manufacturing a part by melting powder, the powder particles reaching the bath in a cold state | |
EP3112077A1 (en) | Laser welding method | |
Franco et al. | Analysis of copper sheets welded by fiber laser with beam oscillation | |
Zhan et al. | Experimental and simulation study on the microstructure of TA15 titanium alloy laser beam welded joints | |
CN1638897A (en) | Method of removing casting defects | |
JPH09110596A (en) | Method for repairing part for single crystal gas turbine engine and single crystal metal product for | |
CN105636737A (en) | Method of melting a surface by laser using programmed beam size adjustment | |
CN114799526B (en) | Narrow gap laser swing-filling wire composite welding method for ultra-high-strength steel thick plates | |
US20200353679A1 (en) | Method for irradiating a powder layer in additive production using continuously defined production parameters | |
JP2018167320A (en) | Laser build-up welding device, laser build-up welding method and weld repairing method | |
KR20190002760A (en) | Oscillating welding method | |
Arbo et al. | On weldability of aerospace grade Al-Cu-Li alloy AA2065 by wire-feed laser metal deposition | |
Taheri et al. | Features of hybrid laser-arc welding of GTD-111 superalloy compared to laser beam welding | |
US20180250742A1 (en) | Leg elimination strategy for hatch pattern | |
Ojo et al. | Loop travel-path of fibre laser welded Alclad AA2219-O alloy | |
Chen et al. | Wire arc additive manufacturing: systems, microstructure, defects, quality control, and modelling | |
Bertrand et al. | Temporal pulse shaping: a key parameter for the laser welding of dental alloys |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: SIEMENS ENERGY, INC., FLORIDA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:BRUCK, GERALD J.;KAMEL, AHMED;SIGNING DATES FROM 20140812 TO 20140912;REEL/FRAME:033746/0637 |
|
STCV | Information on status: appeal procedure |
Free format text: BOARD OF APPEALS DECISION RENDERED |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- AFTER EXAMINER'S ANSWER OR BOARD OF APPEALS DECISION |