USRE32511E - Method and apparatus for making instantaneous scarfing cuts - Google Patents

Method and apparatus for making instantaneous scarfing cuts Download PDF

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Publication number
USRE32511E
USRE32511E US06/139,450 US13945080A USRE32511E US RE32511 E USRE32511 E US RE32511E US 13945080 A US13945080 A US 13945080A US RE32511 E USRE32511 E US RE32511E
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Prior art keywords
scarfing
oxygen
path
workpiece
laser beam
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US06/139,450
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Stephen A. Engel
Ronald E. Fuhrhop
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ESAB AB
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L-Tec Co
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Priority claimed from US05/684,833 external-priority patent/US4038108A/en
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Priority to US06/139,450 priority Critical patent/USRE32511E/en
Assigned to L-TEC COMPANY, A NY LIMITED PARTNERSHIP reassignment L-TEC COMPANY, A NY LIMITED PARTNERSHIP ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: UNION CARBIDE CORPORATION A NY CORP
Assigned to SECURITY PACIFIC BUSINESS CREDIT INC., A DE CORP. reassignment SECURITY PACIFIC BUSINESS CREDIT INC., A DE CORP. SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: L-TEC COMPANY A NY LIMITED PARTNERSHIP
Assigned to L-TEC COMPANY reassignment L-TEC COMPANY ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: UNION CARBIDE CORPORATION, A CORP OF NY.
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/14Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor
    • B23K26/1423Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor the flow carrying an electric current
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36Removing material
    • B23K26/362Laser etching
    • B23K26/364Laser etching for making a groove or trench, e.g. for scribing a break initiation groove
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K7/00Cutting, scarfing, or desurfacing by applying flames
    • B23K7/06Machines, apparatus, or equipment specially designed for scarfing or desurfacing

Definitions

  • the present invention relates, in general, to thermochemical removal of metal from the surface of a workpiece, commonly called scarfing, and more particularly, to making instantaneous or flying scarfing cuts.
  • Another aspect of the invention consists of scarfing apparatus, comprising in combination:
  • laser means capable of impinging at least one laser beam on the work surface so as to produce a heated path of desired length across said surface relative to its direction of motion, by having the laser beam heat a series of points on said surface to their oxygen ignition temperature, said heated path being located proximate to the centerline projection of said scarfing oxygen stream on the work surface.
  • the preferred method of laser heating the surface of the workpiece to its oxygen ignition temperature is by traversing a continuous wave laser beam such that the beam impinges a continuum of points across the surface of the workpiece.
  • stream of scarfing oxygen as used throughout the present specification and claims is intended to mean a stream of oxygen gas directed obliquely at the surface of the workpiece of sufficient intensity to thermochemically remove a surface layer of metal, customarily to a depth of about 1 to 8 mm, and to make a scarfing cut at least 25 mm wide.
  • Streams of scarfing oxygen are preferably sheet-like, but may also be circular or of other shapes.
  • FIG. 1 is a side view illustrating a preferred embodiment of the method and apparatus of the present invention for making an instantaneous scarfing cut.
  • FIG. 2 is a front view (without the scarfing unit) of FIG. 1 illustrating a preferred arrangement for using a laser to successively heat a series of points on the surface of a workpiece to their oxygen ignition temperature.
  • FIG. 3 shows an alternative arrangement for laser heating the surface of the workpiece.
  • FIG. 4 illustrates the shape of a scarfing cut made when the arrangement shown in FIG. 3 is used to make a flying start.
  • a laser unit 1 including a focusing lens 4, is mounted on the scarfing machine frame (not shown)--it could be mounted remotely--and arranged so that the laser beam R impinges on the surface of the workpiece W at point A, the point where the scarfing cut is to begin.
  • Scarfing unit 3 is typically comprised of conventional upper and lower preheat blocks 12 and 13, respectively, which may be provided with rows of either premixed or post-mixed preheat ports 14 and 15, and suitable gas passages therein.
  • the scarfing oxygen nozzle slot 16 is formed by the lower surface 17 of upper preheat block 12 and the upper surface 18 of the lower preheat block 13. The slot-like oxygen nozzle 16 terminates with a discharge orifice 19.
  • point A may be slightly ahead of or coincide with the area enclosed by the straight line projections of surfaces 17 and 18 onto the work surface.
  • Oxygen and fuel gas are supplied to the scarfing unit 3 through feed pipes 20 and 21, respectively by means well known in the art.
  • the apparatus shown in FIG. 1 functions as follows. First, the preheat flames emanating from scarfing unit 3 are ignited by actuating the flow of fuel gas from the rows of preheat ports 14 and 15, and a low flow of oxygen gas through orifice 19. The preheat flames are indicated by lines 22. Relative motion is taking place between the scarfing apparatus and the workpiece. Just before the defective area to be scarfed on the surface of workpiece W reaches point A, the stream of oxygen from orifice 19 is turned up to the scarfing oxygen rate. Simultaneously therewith, or shortly thereafter, the laser beam R is turned on, causing point A to immediately reach oxygen ignition temperature, causing an instantaneous scarfing cut to begin at point A.
  • the laser beam is then directed across the surface of the workpiece relative to its direction of travel, causing the scarfing reaction to spread to the desired width by following the laser heated path.
  • the stream of scarfing oxygen is kept on for as long as the scarfing cut is desired.
  • the laser beam may be shut off as soon as the scarfing cut has reached its desired width.
  • Relative motion may be started after a scarfing reaction of desired width has been initiated, in those cases where a flying start is not desired.
  • a flying start is one which takes place with the workpiece moving relative to the scarfing apparatus at normal scarfing speeds.
  • FIGS. 2 and 3 illustrate two ways in which a laser may be used to heat a path of desired length on the work surface to its oxygen ignition temperature.
  • FIG. 2 is a front view of FIG. 1 with the scarfing unit not shown.
  • the laser 1 and its optical system is turned on and rotated through the angle ⁇ , causing the laser beam R to heat a continuous series of points, forming a path on the metal work surface between points A and B to be heated to their oxygen ignition temperature.
  • the beam R may be optically directed to traverse the path between points A and B.
  • FIG. 3 An alternative technique for heating a path on the work surface is illustrated in FIG. 3, where the laser beam is directed between points A and B by moving (by means not shown) reflecting mirror M and lens 4, respectively across the path of the desired scarfing cut to position M' and 4'.
  • the laser used in FIGS. 2 and 3 is preferably of the continuous wave type. However, a pulsed laser may be used, in which case a series of closely-spaced spots between points A and B are brought to their oxygen ignition temperature. The individual spots will flow together as the oxygen is turned on. Of course, other optical arrangements may be used to achieve the same result, including use of more than one laser.
  • FIG. 4 shows the shape of a scarfing cut made when a flying start is made in accordance with this invention, using a single laser and the arrangement shown in FIGS. 2 or 3.
  • the start of the cut begins at point A and continues to point B due to relative motion between the scarfing apparatus and the workpiece W.
  • Area 101 represents the scarfing cut.
  • the present invention may be used for the same purposes as disclosed in applicant's parent case, U.S. Pat. No. 4,038,108.
  • Such uses include, but are not limited to making conventional scarfing cuts with a sheet-like stream of oxygen, i.e. desurfacing the entire surface; making individual fin-free spot scarfing cuts whose width is narrower, as wide as or wider than the width of the scarfing nozzle, and making spot scarfing cuts by mounting several scarfing units together for spot scarfing in a gang-pass arrangement.

Abstract

An instantaneous scarfing cut on the surface of a metal workpiece can be made by:
(a) causing relative motion between the workpiece and a stream of scarfing oxygen gas, and simultaneously therewith
(1) impinging at least one laser beam on the work surface so as to produce a heated path of desired length across said surface relative to its direction of motion, said heated path being produced by the laser beam heating a series of points on said surface to their oxygen ignition temperature, and
(2) impinging a stream of scarfing oxygen onto said heated path, thereby causing an instantaneous scarfing cut to begin along said path, and
(b) continuing the flow of scarfing oxygen until the desired length of cut has been produced.

Description

BACKGROUND
This application is a continuation-in-part of U.S. application Ser. No. 684,833, filed May 10, 1976, now U.S. Pat. No. 4,038,108, the entire disclosure of which is incorporated herein by reference.
The present invention relates, in general, to thermochemical removal of metal from the surface of a workpiece, commonly called scarfing, and more particularly, to making instantaneous or flying scarfing cuts.
The prior art, discussed more fully in applicant's above-mentioned parent application discloses methods for making instantaneous scarfing starts which require either electric arcs and their associated complex equipment or adjuvant material, such as metal powder or hot wires. Applicant's parent application discloses methods and apparatus for making instantaneous starts by using laser beams in conjunction with a high-intensity jet of oxygen. The present invention is a modification of the invention disclosed and claimed in said parent application and distinguished therefrom in that it eliminates the use of the high intensity jet of oxygen.
OBJECTS
It is an object of this invention to provide a simple and reliable method and apparatus which is capable of making instantaneous or flying scarfing cuts on a workpiece without the use of any adjuvant powder or wire or electric arcs.
It is another object of this invention to provide a method and apparatus which is capable of making instantaneous or flying scarfing cuts without the use of a high intensity jet of oxygen to spread the starting puddle.
SUMMARY OF INVENTION
The above and other objects which will become apparent to those skilled in the art are achieved by the present invention, one aspect of which consists of a method for making an instantaneous scarfing cut on the surface of a metal workpiece, comprising the steps of:
causing relative motion between the workpiece and a stream of scarfing oxygen gas, and simultaneously therewith
(1) impinging at least one laser beam on the work surface so as to produce a heated path of desired length across said surface relative to its direction of motion, said heated path being produced by the laser beam heating a series of points on said surface to their oxygen ignition temperature, and
(2) impinging a stream of scarfing oxygen onto said heated path, thereby causing an instantaneous scarfing cut to begin along said path, and
(b) continuing the flow of scarfing oxygen until the desired length of cut has been produced.
Another aspect of the invention consists of scarfing apparatus, comprising in combination:
(a) scarfing nozzle means capable of discharging a controlled stream of scarfing oxygen onto the surface of a workpiece to be scarfed,
(b) means for producing relative motion between said nozzle means and said workpiece, and
(c) laser means capable of impinging at least one laser beam on the work surface so as to produce a heated path of desired length across said surface relative to its direction of motion, by having the laser beam heat a series of points on said surface to their oxygen ignition temperature, said heated path being located proximate to the centerline projection of said scarfing oxygen stream on the work surface.
The preferred method of laser heating the surface of the workpiece to its oxygen ignition temperature is by traversing a continuous wave laser beam such that the beam impinges a continuum of points across the surface of the workpiece.
The term "stream of scarfing oxygen" as used throughout the present specification and claims is intended to mean a stream of oxygen gas directed obliquely at the surface of the workpiece of sufficient intensity to thermochemically remove a surface layer of metal, customarily to a depth of about 1 to 8 mm, and to make a scarfing cut at least 25 mm wide. Streams of scarfing oxygen are preferably sheet-like, but may also be circular or of other shapes.
IN THE DRAWINGS
FIG. 1 is a side view illustrating a preferred embodiment of the method and apparatus of the present invention for making an instantaneous scarfing cut.
FIG. 2 is a front view (without the scarfing unit) of FIG. 1 illustrating a preferred arrangement for using a laser to successively heat a series of points on the surface of a workpiece to their oxygen ignition temperature.
FIG. 3 shows an alternative arrangement for laser heating the surface of the workpiece.
FIG. 4 illustrates the shape of a scarfing cut made when the arrangement shown in FIG. 3 is used to make a flying start.
DETAILED DESCRIPTION OF THE INVENTION
In FIG. 1, a laser unit 1, including a focusing lens 4, is mounted on the scarfing machine frame (not shown)--it could be mounted remotely--and arranged so that the laser beam R impinges on the surface of the workpiece W at point A, the point where the scarfing cut is to begin. Scarfing unit 3 is typically comprised of conventional upper and lower preheat blocks 12 and 13, respectively, which may be provided with rows of either premixed or post-mixed preheat ports 14 and 15, and suitable gas passages therein. The scarfing oxygen nozzle slot 16 is formed by the lower surface 17 of upper preheat block 12 and the upper surface 18 of the lower preheat block 13. The slot-like oxygen nozzle 16 terminates with a discharge orifice 19. In order to start the thermochemical reaction, point A may be slightly ahead of or coincide with the area enclosed by the straight line projections of surfaces 17 and 18 onto the work surface. Oxygen and fuel gas are supplied to the scarfing unit 3 through feed pipes 20 and 21, respectively by means well known in the art.
The apparatus shown in FIG. 1 functions as follows. First, the preheat flames emanating from scarfing unit 3 are ignited by actuating the flow of fuel gas from the rows of preheat ports 14 and 15, and a low flow of oxygen gas through orifice 19. The preheat flames are indicated by lines 22. Relative motion is taking place between the scarfing apparatus and the workpiece. Just before the defective area to be scarfed on the surface of workpiece W reaches point A, the stream of oxygen from orifice 19 is turned up to the scarfing oxygen rate. Simultaneously therewith, or shortly thereafter, the laser beam R is turned on, causing point A to immediately reach oxygen ignition temperature, causing an instantaneous scarfing cut to begin at point A. The laser beam is then directed across the surface of the workpiece relative to its direction of travel, causing the scarfing reaction to spread to the desired width by following the laser heated path. The stream of scarfing oxygen is kept on for as long as the scarfing cut is desired. The laser beam may be shut off as soon as the scarfing cut has reached its desired width.
Relative motion may be started after a scarfing reaction of desired width has been initiated, in those cases where a flying start is not desired. A flying start is one which takes place with the workpiece moving relative to the scarfing apparatus at normal scarfing speeds.
FIGS. 2 and 3 illustrate two ways in which a laser may be used to heat a path of desired length on the work surface to its oxygen ignition temperature. FIG. 2 is a front view of FIG. 1 with the scarfing unit not shown. The laser 1 and its optical system is turned on and rotated through the angle β, causing the laser beam R to heat a continuous series of points, forming a path on the metal work surface between points A and B to be heated to their oxygen ignition temperature. Instead of rotating the laser, the beam R may be optically directed to traverse the path between points A and B.
An alternative technique for heating a path on the work surface is illustrated in FIG. 3, where the laser beam is directed between points A and B by moving (by means not shown) reflecting mirror M and lens 4, respectively across the path of the desired scarfing cut to position M' and 4'.
The laser used in FIGS. 2 and 3 is preferably of the continuous wave type. However, a pulsed laser may be used, in which case a series of closely-spaced spots between points A and B are brought to their oxygen ignition temperature. The individual spots will flow together as the oxygen is turned on. Of course, other optical arrangements may be used to achieve the same result, including use of more than one laser.
FIG. 4 shows the shape of a scarfing cut made when a flying start is made in accordance with this invention, using a single laser and the arrangement shown in FIGS. 2 or 3. The start of the cut begins at point A and continues to point B due to relative motion between the scarfing apparatus and the workpiece W. Area 101 represents the scarfing cut.
The present invention may be used for the same purposes as disclosed in applicant's parent case, U.S. Pat. No. 4,038,108. Such uses include, but are not limited to making conventional scarfing cuts with a sheet-like stream of oxygen, i.e. desurfacing the entire surface; making individual fin-free spot scarfing cuts whose width is narrower, as wide as or wider than the width of the scarfing nozzle, and making spot scarfing cuts by mounting several scarfing units together for spot scarfing in a gang-pass arrangement.

Claims (10)

What is claimed is:
1. A method for making an instantaneous scarfing cut on the surface of a metal workpiece, comprising the steps of:
(a) causing relative motion between the workpiece and a stream of scarfing oxygen gas, and simultaneously therewith
(1) impinging at least one laser beam on the work surface so as to produce a heated path of desired length across said surface, relative to its direction of motion, said heated path being produced by the laser beam heating a series of points on said surface to their oxygen ignition temperature, and
(2) impinging a stream of scarfing oxygen onto said heated path, thereby causing an instantaneous scarfing cut to begin along said path, and
(b) continuing the flow of scarfing oxygen until the desired length of cut has been produced.
2. The method of claim 1 wherein the heated path is produced by rotating a continuous wave laser beam across the work surface.
3. The method of claim 1 wherein the heated path is produced by rotating a pulsed laser beam across the work surface.
4. The method of claim 1 wherein the stream of scarfing oxygen is sheet-like.
5. The method of claim 1 wherein the heated path is produced by moving a reflecting mirror and beam focusing lens across the work surface.
6. Scarfing apparatus comprising in combination:
(a) scarfing nozzle means capable of discharging a controlled stream of scarfing oxygen onto the surface of a workpiece to be scarfed,
(b) means for producing relative motion between said nozzle means and said workpiece, and
(c)laser means capable of impinging at least one laser beam on the work surface to produce a heated path of desired length across said surface relative to its direction of motion, by heating a series of points on said surface to their oxygen ignition temperature, said heated path being located proximate to the centerline projection of said scarfing oxygen stream on the work surface.
7. The apparatus of claim 6 wherein the laser means is a continuous wave laser.
8. The apparatus of claim 6 wherein said laser means is a pulsed laser.
9. The apparatus of claim 6 including means for rotating said laser beam along said path.
10. The apparatus of claim 6 including means for optically moving said laser beam along said path. .Iadd.11. A method for initiating a gas deseaming process on a workpiece by melting of the surface of the workpiece to ignition temperature by means of a point heat source, characterized in that the point heat source is given a motion parallel to the orifice of the planing nozzle in direct connection to this, oxidizing gas simultaneously flowing through the planing nozzle. .Iaddend.
US06/139,450 1976-05-10 1980-04-11 Method and apparatus for making instantaneous scarfing cuts Expired - Lifetime USRE32511E (en)

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Application Number Priority Date Filing Date Title
US06/139,450 USRE32511E (en) 1976-05-10 1980-04-11 Method and apparatus for making instantaneous scarfing cuts

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US05/684,833 US4038108A (en) 1976-05-10 1976-05-10 Method and apparatus for making an instantaneous thermochemical start
US06/139,450 USRE32511E (en) 1976-05-10 1980-04-11 Method and apparatus for making instantaneous scarfing cuts

Related Parent Applications (2)

Application Number Title Priority Date Filing Date
US05/684,833 Continuation-In-Part US4038108A (en) 1976-05-10 1976-05-10 Method and apparatus for making an instantaneous thermochemical start
US05/789,720 Reissue US4084988A (en) 1976-05-10 1977-04-25 Method and apparatus for making instantaneous scarfing cuts

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0471179A1 (en) * 1990-08-11 1992-02-19 Audi Ag Process for deburring metal workpiece edges

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2288027A (en) * 1940-05-31 1942-06-30 Linde Air Prod Co Method of and apparatus for initiating desurfacing operations
US3360398A (en) * 1965-03-11 1967-12-26 United Aircraft Corp Fabrication of thin film devices
US3597578A (en) * 1967-03-16 1971-08-03 Nat Res Dev Thermal cutting apparatus and method
US3656988A (en) * 1969-02-27 1972-04-18 Watch Stones Co Ltd Method for the fabrication of holes in a workpiece by means of laser-beams and apparatus for the performance of the aforesaid method
US3966504A (en) * 1973-05-21 1976-06-29 Centro-Maskin I Goteborg Ab Method and apparatus for thermochemical gas scarfing
US3966503A (en) * 1975-01-13 1976-06-29 Union Carbide Corporation Method for making instantaneous scarfing starts
JPS5319462A (en) * 1976-07-17 1978-02-22 Chuo Menki Seisakushiyo Kk Laminating apparatus for cotton belt

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2288027A (en) * 1940-05-31 1942-06-30 Linde Air Prod Co Method of and apparatus for initiating desurfacing operations
US3360398A (en) * 1965-03-11 1967-12-26 United Aircraft Corp Fabrication of thin film devices
US3597578A (en) * 1967-03-16 1971-08-03 Nat Res Dev Thermal cutting apparatus and method
US3749878A (en) * 1967-03-16 1973-07-31 Nat Res Dev Gas assisted laser cutting apparatus
US3656988A (en) * 1969-02-27 1972-04-18 Watch Stones Co Ltd Method for the fabrication of holes in a workpiece by means of laser-beams and apparatus for the performance of the aforesaid method
US3966504A (en) * 1973-05-21 1976-06-29 Centro-Maskin I Goteborg Ab Method and apparatus for thermochemical gas scarfing
US3966503A (en) * 1975-01-13 1976-06-29 Union Carbide Corporation Method for making instantaneous scarfing starts
JPS5319462A (en) * 1976-07-17 1978-02-22 Chuo Menki Seisakushiyo Kk Laminating apparatus for cotton belt

Non-Patent Citations (4)

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Title
Adams, M. J., The Use of the CO 2 Laser for Cutting and Welding, Welding Institute Research Bulletin, vol. 9, Sep. 1968. *
Adams, M. J., The Use of the CO2 Laser for Cutting and Welding, Welding Institute Research Bulletin, vol. 9, Sep. 1968.
Sullivan, A. B. J. et al.; Gas Jet Laser Cutting; British Welding Journal; Aug., 1967. *
Sullivan, A. B. J. et al.; Gas-Jet Laser Cutting; British Welding Journal; Aug., 1967.

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0471179A1 (en) * 1990-08-11 1992-02-19 Audi Ag Process for deburring metal workpiece edges

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