Method for the preparation of aluminized steel sheets to be welded and then press hardened

Patent metadata

Field	Value
Publication number	US-9827633-B2
Application number	US-201715615226-A
Country	US
Kind code	B2
Filing date	Jun 6, 2017
Priority date	Apr 25, 2014
Publication date	Nov 28, 2017
Grant date	Nov 28, 2017

Abstract

A method for the preparation of steel sheets for fabricating a welded steel blank is provided. The method includes procuring at least two pre-coated steel sheets, each having a pre-coating of an intermetallic alloy layer, topped by a layer of aluminum metal or aluminum alloy or aluminum-based alloy. The sheets have a principal face, an opposite principal face, and at least one secondary face. The sheets are positioned so a gap between 0.02 and 2 mm exists between the secondary faces. The secondary faces face each other. The positioning of the first and second sheets defines a median plane perpendicular to the principal faces. Layers of metal alloy are removed by melting and vaporization simultaneously on the principal faces, in a peripheral zone of the sheets, the peripheral zones being the zones of the principal faces closest in relation to the median plane.

First claim

What is claimed is:

1. A method for the preparation of sheets to be used for the fabrication of a welded steel blank, comprising the steps of:
procuring at least one pre-coated first steel sheet and one pre-coated second steel sheet, each sheet including:
a steel substrate and
a pre-coating including an intermetallic alloy layer in contact with the steel substrate, topped by a metal alloy layer of aluminum metal or aluminum alloy or aluminum-based alloy,
the first sheet comprising a principal face, an opposite principal face and at least one secondary face,
the second sheet comprising a principal face, an opposite principal face and at least one secondary face,

positioning the first and second sheets to form a gap from 0.02 and 2 mm between the secondary faces, the secondary faces facing each other, the positioning of the first and second sheets defining a median plane perpendicular to the principal faces of the first and second sheets; and
removing the metal alloy layers in first and second peripheral zones of the first and second sheets, respectively, by melting and vaporization simultaneously on the principal faces of the sheets, the peripheral zones being zones of the principal faces closest to the median plane and located one on either side of the median plane.

2. The preparation method as recited in claim 1 , wherein the simultaneous removal by melting and evaporation is carried out by a laser beam that spans the median plane.

3. The preparation method as recited in claim 1 , wherein widths of the first and second peripheral zones are from 0.25 to 2.5 mm.

4. The preparation method as recited in claim 1 , wherein widths of the first and second peripheral zones are equal.

5. The preparation method as recited in claim 1 , wherein widths of the first and second peripheral zones are different.

6. The preparation method as recited in claim 1 , wherein the step of removal by melting and vaporization is carried out on the principal faces and on the opposite principal faces simultaneously.

7. The preparation method as recited in claim 1 , wherein the intermetallic alloy layers remain in the first and second peripheral zones after the respective metal alloy layers are removed.

8. The preparation method as recited in claim 1 , wherein the steel substrates of the first and second steel sheets have different compositions of steel.

9. The preparation method as recited in claim 1 , wherein the pre-coatings on the first and second steel sheets have different thicknesses.

10. The preparation method as recited in claim 1 , wherein the metal alloy layers include, with the percentages expressed by weight, from 8 to 11% silicon, from 2 to 4% iron, and the a balance of the composition including aluminum and unavoidable impurities.

11. The preparation method as recited in claim 1 , wherein the gap is greater than 0.04 mm.

12. The preparation method as recited in any of the claim 1 , wherein the gap is greater than 0.06 m.

13. A method for fabricating a welded blank comprising the steps of:
procuring at least first and second sheets prepared by the method recited in claim 1 ; and
carrying out a welding operation of the first sheet and the second sheet in the peripheral zones, along a plane defined by the median plane, less than one minute after the removal of the metal alloy layer by melting and vaporization on the at least one first sheet and at least one second sheet.

14. The fabrication method as recited in claim 13 , wherein the welding operation is carried out by at least one laser beam.

15. The fabrication method as recited in claim 13 , wherein the welding operation is carried out simultaneously by two laser beams, one effecting a welding of the side of the principal faces, and the other effecting a welding of the side of the opposite principal faces.

16. The fabrication method as recited claim 13 wherein the removing by melting and vaporization is carried out by a laser beam, and the devices for the removal and the welding operation are combined in a single piece of equipment, a relative speed of displacement in relation to that of the at least one first sheet and that of at least one second sheet is identical.

17. The fabrication method as recited in claim 13 , wherein the welding operation is carried out using simultaneously at least one laser beam and one filler rod.

18. The fabrication method as recited in claim 13 , wherein the removing step is guided by a device that tracks the median plan and wherein coordinates (x-y) defining a location of the plane at an instant t are recorded by a controller and used to guide the welding operation that is subsequently carried out.

19. The fabrication method as recited in claim 13 , wherein the removing step is guided by a first device that tracks the median plane and the welding operation is guided by a second device that tracks the median plane and is separate from the first device.

20. The fabrication method as recited in claim 13 , wherein the first and second sheets are clamped by a clamping device during the removing step, the clamping being kept constant until the welding operation and at least during the welding operation.

21. A method for fabricating a press-hardened part from a welded blank, comprising the following steps:
procuring at least one welded blank fabricated as recited in claim 13 ;
heating the at least one welded blank to create, by alloying between the steel substrate and the pre-coating an intermetallic alloy compound, and to confer a partially or totally austenitic structure on the substrate;
hot-forming the at least one welded blank to obtain a part;
cooling the part at a rate sufficient to form at least martensite or bainite in the substrate, thus obtaining a press hardening.

22. The fabrication method as recited in claim 21 , wherein the hot forming of the at least one welded blank is carried out by a hot stamping operation.

23. A welded blank fabricated by an assembly comprising:
at least one first and second pre-coated steel sheet prepared by the method recited in claim 1 ;
at least one welded joint defining the median plane perpendicular to the principal faces of the at least one first and second sheets; and
cross sections perpendicular to the median plane wherein the first sheet has at least one first cross section on one side of the median plane and the second sheet has at least one second cross section on the other side of the median plane;
morphological characteristics of the intermetallic alloy layers of the at least one first and second sheets resulting from solidification after melting and vaporization of the pre-coating in the peripheral zones being identical in the at least one first cross section and at least one second cross section.

24. The welded blank as recited in claim 23 , wherein a sum of the widths of the peripheral zones varies by less than 10% along the welded joint.

25. The welded blank as recited in claim 23 , wherein the metal alloy layer includes, with concentrations expressed by weight, from 8 to 11% silicon and from 2 to 4% iron, the balance of the composition comprising aluminum and unavoidable impurities.

26. Use of a steel part fabricated as recited in claim 21 for the fabrication of structural, anti-intrusion or impact absorption parts in vehicles, in particular automobiles.

27. The preparation method as recited in claim 1 , wherein the step of procuring is followed

Assignees

• Arcelormittal

Inventors

• Schmit Francis
• Vierstraete Rene
• Yin Qingdong
• Ehling Wolfram

Classifications

• B23K26/361

  for deburring or mechanical trimming (B23K26/351 takes precedence) · CPC title

• B23K9/173

  and of a consumable electrode · CPC title

• B23K9/167

  and of a non-consumable electrode · CPC title

• B23K26/348

  in combination with arc heating, e.g. tungsten inert gas [TIG], metal inert gas [MIG] or plasma welding · CPC title

• B23K26/211

  with interposition of special material to facilitate connection of the parts · CPC title