Method for assembling tubular joining sleeve and a conduit lining tube by laser welding

Patent metadata

Field	Value
Publication number	US-10562235-B2
Application number	US-201615762499-A
Country	US
Kind code	B2
Filing date	Sep 21, 2016
Priority date	Sep 23, 2015
Publication date	Feb 18, 2020
Grant date	Feb 18, 2020

Abstract

The present invention relates to a method and to a device for assembling together two tubes (1, 2) comprising a tubular junction sleeve and an internal pipe liner tube made of thermoplastic materials by laser welding two contact surfaces of revolution (1-1, 2-1) pressed one against the other at the ends of the tubular sleeve of said liner tube overlapping coaxially.

First claim

The invention claimed is:

1. A method of assembling a sleeve to a liner comprising:
providing a laser device configured to emit a laser beam having a wavelength;
providing a sleeve comprising a thermoplastic material, wherein the sleeve a is transparent to the wavelength of the laser beam, and wherein the sleeve is tubular;
providing a first steel pipe comprising:
an inner surface and a first end;
a first liner which covers a lined portion of the inner surface of the first steel pipe, wherein the first liner comprises a thermoplastic material, and wherein the first liner is absorbent to the wavelength of the laser beam; and
an unlined portion adjacent the first end of the first steel pipe where the inner surface of the first steel pipe is not covered by the first liner, wherein a first end of the first liner is adjacent the unlined portion of the first steel pipe;

providing a second steel pipe comprising:
an inner surface and a second end;
a second liner which covers a lined portion of the inner surface of the second steel pipe, wherein the second liner comprises a thermoplastic material, and wherein the second liner is absorbent to the wavelength of the laser beam; and
an unlined portion adjacent the second end of the second steel pipe where the inner surface of the second steel pipe is not covered by the second liner, wherein a second end of the second liner is adjacent the unlined portion of the second steel pipe;

inserting a first end of the sleeve into the first end of the first steel pipe such that the first end of the sleeve contacts the first end of the first liner and inserting a second end of the sleeve into the second end of the second steel pipe such that the second end of the sleeve contacts the second end of the second liner, wherein the inserting steps coaxially align the sleeve, the first steel pipe and the second steel pipe relative to a common longitudinal axis;
applying pressure to an inner surface of the sleeve in a radial direction, wherein the pressure is applied at the first end of the sleeve;
emitting the laser beam from the laser device;
directing the laser beam toward the inner surface of the sleeve at the first end of the sleeve and rotating the laser beam about the common longitudinal axis through 360°;
wherein, during the step of directing the laser beam:
the laser device is arranged inside the sleeve or the first liner;
the step of applying pressure is simultaneously performed;
the laser beam passes firstly through the first end of the sleeve in order to reach a zone of contact between the first end of the sleeve and the first end of the first liner;
respective contacting surfaces of the first end of the sleeve and the first end of the first liner are pressed against each other; and
the first end of the sleeve is fused to the first end of the first liner to form a first weld zone.

2. The method according to claim 1 , wherein the first and second liners and the sleeve each have a thickness that is less than or equal to 5 mm.

3. The method according to claim 1 , wherein:
the first end of the first liner has a constant thickness and defines a cylindrical inner surface having a first diameter;
the first end of the sleeve has a constant thickness and defines a cylindrical outer surface which has a diameter equal to the first diameter;
in the step of inserting the first end of the sleeve into the first end of the first steel pipe, the first end of the sleeve is positioned in an overlapping manner with the first end of the first liner; and
the respective contacting surfaces of the first end of the sleeve and the first end of the first liner comprise the cylindrical inner surface of the first end of first liner and the cylindrical outer surface of the first end of the sleeve.

4. The method according to claim 1 , wherein:
the first end of the first liner has a thickness which is smaller than a thickness of a main portion of the first liner and defines a concave portion of an inner surface of the first end of the first liner, the concave portion having an inner diameter that is greater than an inner diameter of the main portion of the first liner;
the first end of the sleeve has a thickness which is smaller than a thickness of a main portion of the sleeve, the first end of the sleeve defining a convex portion suitable for overlapping and abutting against the concave portion of the first end of the first liner;
in the step of inserting the first end of the sleeve into the first end of the first steel pipe, the concave portion of the first end of the first liner is positioned in an overlapping and abutting manner with the convex portion of the first end of the sleeve; and
the respective contacting surfaces of the first end of the sleeve and the first end of the first liner comprise the concave portion of the first end of the first liner and the convex portion of the first end of the sleeve.

5. The method according to claim 1 , wherein the first weld zone is a continuous weld zone having a helical shape or the first weld zone comprises a plurality of adjacent circular weld zones.

6. The method according to claim 1 , wherein:
the step of directing the laser beam toward the inner surface of the sleeve is performed by:
directing the laser beam in a longitudinal direction parallel to the common longitudinal axis to a mirror in such a manner that a surface of the mirror reflects the laser beam toward the inner surface of the sleeve, the surface of the mirror being inclined at an angle of inclination relative to the common longitudinal axis, wherein the angle of inclination is from 30° to 60°, and
rotating the mirror through 360° about the common longitudinal axis.

7. The method according to claim 6 , wherein the mirror is rotated at a speed of 10 revolutions per second to 1 revolution every 10 seconds.

8. The method according to claim 6 , wherein during the step of directing the laser beam toward the inner surface of the sleeve the mirror is additionally moved in the longitudinal direction.

9. The method according to claim 8 wherein the steps of rotating the mirror and moving the mirror in the longitudinal direction are performed simultaneously such that the first weld zone is formed with a helical shape.

10. The method according to claim 6 , wherein the angle of inclination is variable and is changed during the step of directing the laser beam toward the inner surface of the sleeve.

11. The method according to claim 10 , wherein during the step of directing the laser beam toward the inner surface of the sleeve, the angle of inclination is changed after rotating the mirror about the common longitudinal axis through 360°, such that the first weld zone is a circular weld zone, and successive steps of rotating the mirror through 360° about the common longitudinal axis and subsequently changing the angle of inclination are repeated in order to make a additional circular weld zones.

12. The method according to claim 1 , wherein in the step of directing the laser beam toward the inner surface of the sleeve, the laser beam is directed perpendicular to the respective contacting surfaces, or is inclined at an angle of 0° to 30°, relative to a perpendicular to the respective contacting surfaces.

13. The method according to claim 1 , further comprising forming the first liner by performing steps of:
positioning short lengths of transparent first tubes and long lengths of absorbent second tubes in an alternating manner such that each first tube meets an adjacent second tube at a respective annular contact plane, wherein each of the first and second tubes is positioned coaxially relative to a common first liner axis,

Assignees

• Saipem Sa

Inventors

• Pionetti François-Régis
• Lirola François
• Majdoub Taoufik

Classifications

• B29C66/5344

  said single elements being substantially annular, i.e. of finite length, e.g. joining flanges to tube ends (B29C66/5346 takes precedence) · CPC title

• B29C66/14

  the joint having the same thickness as the thickness of the parts to be joined (B29C66/1142 takes precedence) · CPC title

• B29C66/81455

  being a fluid inflatable bag or bladder, a diaphragm or a vacuum bag for applying isostatic pressure (inflatable element positioned between the joining tool and a backing-up part B29C66/82421) · CPC title

• B29C66/81267

  Transparent to electromagnetic radiation, e.g. to visible light · CPC title

• B29C66/612

  Making circumferential joints · CPC title