Hybrid welding apparatus and method for spatially offset components.

专利摘要:
Hybrid welding methods include directing a laser beam from a laser to a first component that is vertically offset to a second component, and directing a welding arc from an arc welding apparatus to a weld joint between the first component and the second component to interconnect the first and second components to weld.
公开号:CH708916B1
申请号:CH01786/14
申请日:2014-11-18
公开日:2019-06-28
发明作者:Lin Dechao；Cui Yan；Lee Tollison Brian；Chandrudu Kottilingam Srikanth
申请人:Gen Electric；
IPC主号:

专利说明:

description
Background of the Invention The subject matter disclosed herein relates to welding and, more particularly, to hybrid welding for staggered components.
Welding can be used for a variety of manufacturing or repair processes in many different industrial facilities. For example, For example, welds may be used to join multiple components together, repair cracks, crevices or defects in used components, build material into used or new components, or otherwise weld or bond one or more components as required for a particular application can. However, the ability or speed with which a welding operation can be accomplished may be limited by a number of factors, including the thickness and orientation of the components being welded and the performance of the welding apparatus.
Hybrid welding can combine the use of both laser welding and arc welding to possibly weld at a fast rate while still achieving full penetration. However, as components become thicker, full penetration may still require an increase in laser power. The configuration of the laser welding device and the arc welding device can be adapted to influence the welding result. For example, For example, hybrid welding may involve the use of a leading laser welder followed by a wire-feed arc welder to provide relatively smooth welds. However, such configurations may also be limited in the relative orientation of the substrate component (s). For example, For example, components that are vertically offset more than about 1.016 mm (0.04 inches) from each other may require additional shots to ensure full penetration welds (welded seams) for both components. However, these additional shots may also depend on adaptive welding controls that vary welding parameters during a process to achieve consistent results.
Accordingly, alternative hybrid welding apparatus, systems and methods would be welcomed in the art.
Summary of the Invention The invention relates to a hybrid welding process. The hybrid welding method includes directing a laser beam from a laser at a first component that is vertically offset to a second component, and directing a welding arc from an arc welding apparatus to a weld joint between the first component and the second component around the first and second components to weld together.
In one embodiment of the hybrid welding process, the laser beam preferably does not overlap with the weld joint.
In the hybrid welding process of any of the above-mentioned types, the first component may be offset from the second component by at least about 0.508 mm (0.02 inches) to about 3.175 mm (0.125 inches).
In the hybrid welding method of any kind mentioned above, the first component to the second component may also be offset horizontally.
In particular, the first component may be horizontally offset from the second component by at least about 0.508 mm (0.02 inches) to about 1.143 mm (0.045 inches).
In the hybrid welding method of any kind mentioned above, the laser beam may have a substantially constant power over the entire welding point.
Additionally or alternatively, the laser may have a power of less than or equal to about 8 kW.
The invention further relates to a hybrid welding device. The hybrid welding apparatus includes a laser that produces a laser beam that is directed at a first component that is vertically offset from a second component, and an arc welder that generates a welding arc that is directed at a weld joint between the first component and the second component is.
In the hybrid welding apparatus as mentioned above, the laser beam preferably does not overlap the weld joint.
In the hybrid welding apparatus of any of the aforementioned types, the first component may be vertically offset from the second component by at least about 0.508mm (0.02 inches) to about 3.175mm (0.125 inches).
In the hybrid welding apparatus or any kind mentioned above, the first component to the second component may also be offset horizontally.
In particular, the first component may be horizontally offset from the second component by at least about 0.508mm (0.02 inches) to about 1.143mm (0.045 inches).
In the hybrid welding apparatus of any kind mentioned above, the laser beam may have a substantially constant power over the entire welding site.
Additionally or alternatively, the laser may have a power of less than or equal to about 8 kW.
These and other features achieved by the embodiments discussed herein will be better understood in view of the following detailed description taken in conjunction with the drawings.
Brief Description of the Drawings The embodiments shown in the drawings are illustrative and exemplary in nature and are not intended to limit the invention as defined by the claims. The following detailed description of the illustrative embodiments may be understood when read in conjunction with the following drawings in which like structure is given like reference numerals and in which:
1 is a perspective view of a schematic representation of a hybrid welding system according to one or more embodiments illustrated or described herein;
FIG. 2 illustrates a hybrid welding process according to one or more embodiments illustrated or described herein; FIG. and
3 is a cross-sectional view of a welded seam produced by the hybrid welding system according to one or more embodiments illustrated or described herein.
DETAILED DESCRIPTION OF THE INVENTION Hereinafter, one or more specific embodiments of the present invention will be described. In an effort to provide a consistent description of these embodiments, not all features of an actual implementation may be described in the description. It will be understood that in the development of any such actual implementation, as in any engineering or design project, numerous implementation-specific decisions must be made in order to achieve specific goals of the developers, such as adhering to system-related and business-related constraints of an implementation may vary to another. In addition, it will be understood that such a development effort may be complex and time consuming, but nonetheless would be a routine design, manufacturing, and manufacturing endeavor for those skilled in the art having the benefit of this disclosure.
When elements of various embodiments of the present invention are introduced, the articles "a," "an," "the" and "the" mean that one or more of the elements are present. The expressions "comprising", "containing" and "having" are meant in the inclusive sense and mean that other elements besides the listed elements may be present.
A staggered component hybrid welding system as disclosed herein generally includes a hybrid welding apparatus and two spatially offset components having a weld joint therebetween. The hybrid welding apparatus generally includes a laser and an arc welder. The laser directs a laser beam at a first component which is at least vertically offset from the second component. The arc welder directs a welding arc toward the weld joint between the first component and the second component. Directing the laser at the first component, as opposed to the weld joint itself, can provide a full penetration weld (inter-welded seam) between the spatially offset components with less joint preparation and / or without the need for adaptive control. Hybrid welding apparatus and methods for spatially offset components will now be described in greater detail herein.
Referring now to Fig. 1, a hybrid welding apparatus 20 and two spatially offset components 62 and 64 are shown schematically.
The first component 62 and the second component 64 may have any two materials which are to be welded together and which are spatially offset from each other. As used herein, "spatially offset" refers to a separation in a vertical direction y and / or a horizontal direction x (where the direction of welding z is perpendicular to the plane having the vertical direction y and the horizontal direction x). The first and second components 62 and 64 may comprise two separate and distinct parts (eg, tubes that are joined together) or may have two distinct regions of a single part passing through a gap to be welded (eg, a crack in a tube ), are separated from each other.
The first component 62 has a vertical offset 61 to the second component 64. For example, For example, the first component 62 may be vertically offset 61 from the second component 64 by at least about 0.508 mm (0.02 inches). In some embodiments, the first component 62 may be vertically offset 61 from the second component 64 by at least about 1.27 mm (0.05 inches). In still other embodiments, the first component 62 may be vertically offset 61 from the second component 64 by up to and including 3.175 mm (0.125 inches).
The first and second components 62 and 64 have a vertical offset 61 for a variety of reasons. For example, For example, if the first and second components 62 and 64 have different diameter tubes that abut one another, can have workpieces of different thicknesses, such that the thicker component is vertically larger than the other, may have non-uniform edges extending in the vertical direction y rise and fall as the weld joint 54 progresses in the direction of welding z, or otherwise may be oriented in a configuration that results in a vertical offset 61, as discussed herein.
In some embodiments, the first component 62 may additionally include a horizontal offset 63 to the second component 64. For example, For example, the first component 62 may be horizontally offset 63 from the second component 64 by at least about 0.254 mm (0.01 inch). In some embodiments, the first component 62 may be horizontally offset 63 from the second component 64 by at least about 0.508mm (0.02 inches). In still some embodiments, the first component 62 may be horizontally offset 63 from the second component 64 by up to and including 1.143 mm (0.045 inches).
Similar to the vertical offset 61, the horizontal offset 63 can be due to a variety of reasons. For example, For example, one or both of the components 62 and 64 may have nonuniform edges that diverge in the horizontal direction x as the weld joint progresses in the welding direction z, or otherwise may be aligned in a configuration that provides a horizontal offset 63 as explained herein.
The spatial offset (i.e., the vertical offset 61 and possibly the horizontal offset 63) between the first component 62 and the second component 64 may be for the entire length of the weld joint 54 or for one or more portions of the weld joint 54. If e.g. the first component 62 and the second component 64 have relatively non-uniform edges (such as when clean cut tubes of different diameters are merged), the at least vertical offset 61 may be present and possibly relatively uniform over approximately the entire length of the weld joint 54. Alternatively, where the first component 62 and / or the second component 64 have non-uniform edges or are aligned at small angles to each other, the vertical offset 61 and possibly the horizontal offset 63 along the longitudinal extent of the weld joint 54 in the welding direction z vary. For example, For example, the vertical offset 61 may increase and decrease with respect to the position along the welding direction z, and may even exist only for parts thereof.
The components 62 and 64 to be welded may be selected from materials such as ferrous and non-ferrous materials. Examples of ferrous and non-ferrous materials include, but are not limited to superalloys, low carbon steel, high strength steel, stainless steel, titanium, aluminum, and combinations thereof.
The hybrid welding apparatus 20 has a laser 30 and an arc welding apparatus 40.
The laser 30 may include any laser system that can generate a laser beam 31 and direct it to one of the components 62 and 64. For example, For example, in some embodiments, the laser 30 is selected from an Nd: YAG laser, a CO2 laser, a fiber laser, or a disk laser. In some embodiments, the laser 30 is a high power density laser.
The laser 30 generates a laser beam 32. The laser beam 32 is directed toward one of the first component and the second component 64. In particular, the laser beam 32 may be directed toward either the higher offset component 62 (as illustrated) or the lower displacement component 64. In addition, the laser beam 32 may be at various angles relative to the weld joint 54, such as an angle of 0 degrees (ie perpendicular to the weld joint 54 as illustrated) or from about plus 30 degrees to about minus 30 degrees relative to the 0 degree reference be directed. By providing a laser beam 32 on only a single one of the vertically offset components 62 and 64 (as opposed to the weld joint 54 itself), the laser beam 32 can support complete penetration of the weld joint 54 without requiring adaptive control while the laser beam 32 Welding point in the direction of welding z progresses.
The laser head 31 of the laser 30 may be separated from one of the upper surfaces 83 and 85 of the first and second components 62 and 64 by a height 22. In some embodiments, the height 22 may be based on the operating requirements of the laser head 31. In some embodiments, the height 22 between the laser head 31 and a single one of the top surfaces 83 and 85 of the first and second components 62 and 64 remains fixed while the weld passes in the direction of welding z. In other embodiments, the height 22 varies between the laser head 31 and one of the upper surfaces 83 and 85 of the first and second components 62 and 64 as the weld progresses in the welding direction z (eg, due to a moving laser head and / or an uneven surface 83 or 85).
In some embodiments, such as that illustrated in FIG. 1, the laser beam 32 has a focal point 34 that is focused on one of the surfaces 83 and 85 of the components 62 and 64. In such embodiments, the focal distance (ie, the length of the laser beam 32 between the laser head 31 and the focal point 34 is equal to the height 22 between the laser head 31 and one of the upper surfaces 83 and 85 of the components 62 and 64. Such embodiments may provide the greatest laser power by focusing all or a majority of the laser energy on a smaller surface area and achieving greater penetration capability, in particular, such embodiments may include a laser 30 of relatively lower power (eg, less than or equal to about 4 kW; for example, for Sch white components up to about 6.35 mm thick) by focusing all or most of their energy on one of the surfaces 83 and 85, rather than spreading them over a larger area, for thicker components can be a higher laser power, such as up to or above 20 kW may be required.
Still referring to FIG. 1, the hybrid welding apparatus 20 further includes the arc welder 40 in addition to the laser 30. In one embodiment, the arc welder 40 is selected from welders having non-consumable electrodes 44 such as, but not limited to, a gas metal arc welder (GMAW) (eg, a metal inert gas (MIG) welder). flux center arc welding apparatus (FCAW) and welders having wire-feed non-consumable electrodes such as, but not limited to, a wire-fed gas tungsten arc welder (GTAW) and a wire-fed plasma arc welder (PAW) ,
The arc welder 40 generates a welding arc 42 which progresses in the welding direction. In some embodiments, the laser beam 32 may be generated simultaneously and directly adjacent to the welding arc 42 to increase the combination of energy from the two sources. In some embodiments, the laser beam 32 has no overlap with the weld joint 54. By reducing or eliminating the overlap, the weld joint 54 may have more uniform properties.
In some embodiments, the laser 30 and the arc welder 40 are mounted at separate locations. In other embodiments, such as illustrated in FIG. 1, the laser 30 and the arc welder 40 are mounted on a single bracket 90. In addition, in some embodiments, the laser beam 32 may have a substantially constant welding performance throughout the weld. For example, if the laser beam 32 does not overlap with the weld joint 54, the laser beam 32 need not be adaptively controlled to still produce uniform seams.
Referring additionally to FIG. 2, a method 100 of welding for spatially offset components 62 and 64 is illustrated. The method 100 includes directing a laser beam 32 from a laser 30 to a first component 62 that is vertically offset 61 to a second component 64 at step 110, as disclosed herein. The method 100 further includes directing a welding arc 42 from an arc welder 40 to a weld joint 54 between the first component 62 and the second component 64 to weld the first and second components 62 and 64 together at step 120, as further shown disclosed herein. It should be appreciated that steps 110 and 120 may begin, stop, and occur together, or in any relative order, to achieve a sufficient weld 54.
Example Two toroidal components were placed side by side to perform welding using a hybrid welding system as disclosed herein. Each of the components had a 6.35 mm (0.25 inch) thick piece of 304L stainless steel with the first component offset vertically by about 3.175 mm (0.125 inches) and horizontally offset by about 1.143 mm (0.045) inches.
The laser produced a laser beam of 8 kW power, and the arc welder had a GMAW device which produced a weld at a wire feed rate of 350 imp with a voltage setting at 26.5V. The laser beam and the arc of welding progressed in the direction of welding at a speed of 152 inches (60 inches) per minute (ipm). A microscopic analysis (shown in Fig. 3) verified that a welded-through seam (with full penetration) had been achieved.
It should now be appreciated that directing a laser at a first component, as opposed to a weld joint itself, results in a welded seam between spatially offset components with less initial preparation of the joint and / or without the need for adaptive control can. Such hybrid welding apparatus and methods can thereby provide more efficient welding of spatially offset components.
While the invention has been described in detail in connection with only a limited number of embodiments, it should be readily understood that the invention is not limited to such disclosed embodiments. Rather, the invention may be modified to incorporate any number of variations, modifications, substitutions, or equivalent arrangements not heretofore described, which, however, are within the spirit and scope of the invention. In addition, it should be understood that while various embodiments of the invention have been described, aspects of the invention may only include some of the described embodiments. Accordingly, the invention should not be construed as being limited by the foregoing description, but is limited only by the scope of the appended claims.
A hybrid welding method comprising directing a laser beam from a laser to a first component that is vertically offset to a second component, and directing a welding arc from an arc welding apparatus to a weld joint between the first component and the second component to form the first and second components to weld the second component together.
Parts List 10 Hybrid Welding System 20 Hybrid Welding Device 22 Height 30 Laser 31 Laser Head 32 Laser Beam 34 Focus Point 40 Arc Welding Device 42 Welding Arc 44 Fusible Wire Electrode 54 Weld Joint (S) 61 Vertical Offset 62 First Component 63 Horizontal Offset 64 Second Component 83, 85 Surfaces (Components) 90 Holder 100 Procedure 110 Step (Laser) 120 Step (Welding arc) X Horizontal direction Y Vertical direction z Welding direction

权利要求:
Claims (8)
[1]
claims
A hybrid welding method, comprising: directing a laser beam from a laser to a first component that is vertically offset to a second component; and directing a welding arc from an arc welder to a weld joint between the first component and the second component to weld the first and second components together.
[2]
2. A hybrid welding method according to claim 1, wherein the laser beam does not overlap with the weld joint.
[3]
A hybrid welding method according to claim 1 or 2, wherein the first component is vertically offset from the second component by 0.508 mm to 3.175 mm.
[4]
A hybrid welding method according to any one of the preceding claims, wherein the first component to the second component is also horizontally offset.
[5]
The hybrid welding method of claim 4, wherein the first component is horizontally offset from the second component by 0.508 mm to 1.143 mm.
[6]
A hybrid welding method according to any one of the preceding claims, wherein the laser beam has a substantially constant power over the entire weld.
[7]
A hybrid welding method according to any one of the preceding claims, wherein the laser has a power of less than or equal to 8 kW.
[8]
A hybrid welding apparatus comprising: a laser generating a laser beam directed to a first component vertically offset from a second component; and an arc welding apparatus that generates a welding arc directed to a weld joint between the first component and the second component.

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法律状态:
2015-06-30| PK| Correction|Free format text: BERICHTIGUNG ERFINDER |

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2015-07-31| PK| Correction|Free format text: BERICHTIGUNG ERFINDER |

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2017-03-15| NV| New agent|Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH |

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2019-05-31| NV| New agent|Representative=s name: FREIGUTPARTNERS IP LAW FIRM DR. ROLF DITTMANN, CH |

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2021-06-30| PL| Patent ceased|

优先权:

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申请号 | 申请日 | 专利标题

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US14/087,332|US10981248B2|2013-11-22|2013-11-22|Hybrid welding apparatuses, systems and methods for spatially offset components|

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