METHOD FOR COAXIALLY WELDING TWO TUBES TOGETHER

Abstract

The invention provides a method for coaxially welding together two tubes. Axial ends of the tube walls of the respective tubes are machined in such a way that they have a stepped shape over at least a first part of the tube wall thicknesses. The stepped hapes complement each other. The method comprises the subsequent steps of A positioning the first tube and the second tube coaxially with respect to each other, wherein the machined axial ends contact each other at least over the first part of the first tube wall thickness and the first part of the second tube wall thickness and wherein the first stepped shape of the machined axial end of the first tube wall and the second stepped shape of the machined axial end of the second tube wall fit into each other, and wherein a seam is present between the first parts of the first tube and the second tube thicknesses, B fixating the first tube and the second tube at discrete positions over the circumference of the seam via attachment welds, C welding the first tube and the second tube to each other over the entire circumference of the first tube and the second tube, wherein the circumferential weld extends over the entire thickness of the first tube all and over the entire thickness of the second tube wall.

Claims

1. A method for coaxially welding together a first metal tube having a first tube wall and a second metal tube having a second tube wall, wherein the inner diameter of the first tube equals the inner diameter of the second tube and wherein an axial end of the first tube wall is machined in such a way that the axial end of the first tube wall, when seen in a longitudinal cross section, has a first stepped shape over at least a first part of the first tube wall thickness, the first part extending from the inner side of the first tube wall, and wherein an axial end of the second tube wall is machined in such a way that the axial end of the second tube wall, when seen in a longitudinal cross section, has a second stepped shape over at least a first part of the second tube wall thickness, the first part extending from the inner side of the second tube wall, and wherein the first stepped shape and the second stepped shape complement each other, the method comprising the subsequent steps of A positioning the first tube and the second tube coaxially with respect to each other, wherein the respective machined axial ends contact each other at least at the location of the first part of the first tube wall thickness and the first part of the second tube wall thickness, the first stepped shape of the machined axial end of the first tube wall and the second stepped shape of the machined axial end of the second tube wall fitting into each other such that, as a result of the fit of the first stepped shape and the second stepped shape a movement of the first tube and the second tube with respect to each other in the radial direction is blocked, B fixating the first tube and the second tube at a number of discrete positions at the circumference of the seam via attachment welds, C circumferentially welding the first tube and the second tube over the entire circumference of the first tube and the second tube, wherein the circumferential weld extends over the entire thickness of the first tube wall and over the entire thickness of the second tube wall.

2. Method according to claim 1, wherein the stepped shape, seen in the axial direction of the first tube, extends within a length having a magnitude of between 0.01 mm and 1.50 mm, preferably between 0.10 mm and 1.00 mm and more preferably between 0.15 mm and 0.75 mm.

3. Method according to claim 1, wherein the first part of first tube wall thickness, seen in the radial direction of the first tube, extends within a length having a magnitude of between 2.0 and 12 mm, preferably between 2.5 mm and 10 mm and further preferably between 3.0 mm and 8.0 mm.

4. Method according to claim 1, wherein the first stepped shape comprises an outer annular end face and an inner annular end face, the outer annular end face and the inner annular end face, seen in the axial direction of the first tube, being arranged at a distance of each other.

5. Method according to claim 4, wherein the outer annular end face and/or the inner annular end face extend(s) parallel to a radial plane that is oriented perpendicular to the axial direction of the first tube.

6. Method according to claim 1, wherein the first part of the first tube wall extends over the entire thickness of the first tube wall and/or wherein the first part of the second tube wall extends over the entire thickness of the second tube wall.

7. Method according to claim 1, wherein the machined end of the first tube wall, seen in radial direction, is further machined at the outer side of the first part of the first tube wall thickness over a second part of the first tube wall thickness connecting to the first part of the first tube wall, and wherein the machined end of the second tube wall, at the outer side of the first part of the second tube wall thickness, is further machined over a second part of the second tube wall thickness connecting to the first part of the second tube wall, wherein after performing step A an open seam is present between the second parts of the first tube and the second tube thicknesses.

8. Method according to claim 7, wherein the open seam is substantially V-shaped or U-shaped when seen in a longitudinal cross section.

9. Method according to claim 7, wherein when seen in the axial direction the first parts of the first tube and the second tube thicknesses are arranged within the maximum axial dimension of the open seam, preferably within the middle 50% of the maximum axial dimension of the open seam, more preferably within the middle 10% of the maximum axial dimension of the open seam.

10. Method according to claim 1, comprising the step of, before step A, milling the axial ends of the first tube wall and the second tube wall for obtaining the machined ends of the first tube wall and the second tube wall.

11. Method according to claim 1, wherein when performing step C a single welding layer is welded that extends at least entirely over the first parts of the first tube wall and the second tube wall thicknesses.

12. Method according to claim 1, wherein when performing step C at least a part of the circumferential weld which extends over the first parts of the first tube wall and the second tube wall thicknesses, is welded by TIG welding.

13. Method according to claim 12, wherein the welding supply material is supplied to the welding pool during the TIG welding as a wire in an automated manner, preferably in a preheated condition.

14. Method according to claim 1, wherein while performing step C a welding torch is positioned at a fixed position with respect to the seam between the first tube and the second tube fixated to each other during step B, and wherein the fixated first tube and second tube are rotated about their coaxial axes.

Description

[0026] FIG. 1 shows two steel tubes 1, 2 each with an (outer) diameter of 114.3 mm (4 inch). Tubes 1, 2 are positioned coaxially with respect to each other and against each other and respectively have a cylindrical tube wall 3, 4. The thicknesses of the tube walls 3, 4 are equal to each other and are indicated in FIG. 2a with the letter d. In the present embodiment, d is equal to 6.0 mm. Also the inner diameters of the tubes 1, 2 are equal to each other, like the outer diameters of tubes 1, 2. Between the tubes 1, 2 that are positioned against each other, more specifically between the axial end faces of the tube walls 3, 4 of the respective tubes 1, 2 that face each other, a seam 5 is present, more specifically a welding seam 5.

[0027] When seen in an axial longitudinal cross section as shown in FIG. 2a, the welding seam 5 has a stepped shape as the axial ends of the tube walls 3, 4 that face each other each have a stepped shape. These respective stepped shapes complement each other as a result of which the said axial ends fit into each other when the tubes 1, 2, as in FIG. 1, are coaxially positioned against each other. The tubes 1, 2 lock each other in the radial direction, such that tubes 1, 2 cannot move in the radial direction with respect to each other and hence remain coaxial to each other.

[0028] The said stepped shapes of the axial ends of the tube walls 3, 4 are obtained by a milling process. More specifically, the said stepped shapes of the axial end faces are the result of the respective axial end of tube 3 having an inner annular end face 6 and an outer annular end face 7. The end faces 6, 7 of tube wall 3 are arranged at a distance t from each other when seen in the axial direction of tube 1. In the chosen example t equals 0.25 mm. The radial dimension d1 of the inner annular end face 6 in the chosen embodiment is 4.5 mm and the radial dimension d2 of the outer annular end face 7 is 1.5 mm. In the embodiment of FIGS. 1, 2a and 2b, d equals d1+d2. The inner annular end face 6 forms a protruding part on the respective axial end of tube wall 3. In general it is advantageous when d2 is smaller than d1 such that the transfer between d1 and d2 is relatively close to the outer diameter of the tube, which is advantageous for the reliability of the weld joint to be made. On the other hand it can be disadvantageous when d2 becomes so small that the respective protruding part is vulnerable to damages. In general it is preferred to choose d2 larger than 0.5 mm or even larger than 1.0 mm.

[0029] Wall tube 4 has an inner annular end face 8 and an outer annular end face 9 which are arranged at a distance t from each other in the axial direction as well. The radial dimensions of the end faces 8, 9 are respectively equal to d1 and d2. The outer annular end face 9 is a part of the protruding part on the respective axial end of tube wall 4.

[0030] In view of the above description the stepped shapes of the axial ends of tube walls 3, 4 that face each other complement each other.

[0031] The welding of tubes 3, 4 can e.g. be effected by the TIG welding process. For welding the tubes 3, 4 to each other a common axis 10 of the tubes 1, 2 is oriented horizontally and the tubes 1, 2 are fixated to each other at a number of discrete, mutually approximately equidistant positions at the outer side of welding seam 5 via attachment welds. In this fixated situation, one of the tubes 1, 2 is clamped in a turning device that allows for a rotation of the attached tubes 1, 2 about their common axis 10. Seen in the direction parallel to axis 10, a welding torch is subsequently placed directly above welding seam 5, at a 12 o'clock orientation. Subsequently the welding process is started, wherein the welding torch remains at its position or substantially at its position, and the welding seam 5 rotates a full 360° about axis 10. The welding can be effected at a relatively high amperage, e.g. more than 300 A and at a relatively high speed of e.g. between 25 and 30 cm per minute. The welding process results in a welding layer 21 as shown in FIG. 2b. Welding layer 21 is a welding penetration and extends at both the inner side of tube walls 3, 4 as well as the outer sides thereof. Even though FIG. 2b shows the stepped shape of the axial ends of the tube wall 3, 4 for clarity purposes and for the purpose of explaining the present invention, it will be clear to a skilled person that all material of the tubes 1, 2 inside the welding layer 21 has been molten. It is advantageous to use the same welding process for welding the welding layer 21 and for welding the said attachment welds.

[0032] FIG. 3 shows two steel tubes 31, 32 coaxial with respect to each other and positioned against each other, with a welding seam 35 in between. Tubes 31, 32 have a cylindrical tube wall 33, 34 of which the respective thicknesses are equal but larger than thickness d of tubes 3, 4. In the present embodiment the thickness D of tube walls 33, 34 equal approximately 10 mm. Welding seam 35 has, at least in axial cross section, a stepped shape at the inner side of the tube walls 33, 34 which is equal to the stepped shape of welding seam 5. More specifically, D1=d1, D2=d2 and T=t. At the outer sides of tube walls 33, 34 the welding seam 35 is open and more specifically welding seam 35 is substantially U-shaped. The bottom of the U-shape is rounded with a radius R and the legs of the U-shape diverge and enclose an angle a having a magnitude of 40 degrees. The stepped shape of the inner part of the welding seam 35 is within the middle 10% of the U-shape at the outer circumference of tubes 33, 34, when seen in the axial direction.

[0033] FIG. 4b shows the cross section according to FIG. 4a in a welded state. Welding seam 35 is welded over the entire thickness D of the tube walls 33, 34 by a base welding layer 51, a welding layer 52 on top of it and a third welding layer 53 extending to both sides of the tube walls 33, 34. The welding layers 52 and 53 that are arranged on the base welding layer 51 can advantageously be welded with a different welding process, such as the MIG/MAG process, to allow the welding seam to be filled faster.