Joining method

• US 4,606,778 A
• Filed: 10/26/1984
• Issued: 08/19/1986
• Est. Priority Date: 11/03/1983
• Status: Expired due to Fees

• Current Assignee: BBC AG Brown Boveri & CIE
• Original Assignee: BBC AG Brown Boveri & CIE
• Inventors: Jahnke, Bernd
• Primary Examiner(s): Brody, Christopher W.
• Application Number:
  US06/665,293
• Time in Patent Office: 662 Days
• Field of Search: 148/127, 148/131, 148/11.5 N, 148/11.5 Q, 148/12 R, 148/12.1, 148/14, 228/193-195, 29/156.8 H
• US Class Current: 148/527
• CPC Class Codes: B23K 20/16 with interposition of special material to facilitate connection of the parts, e.g. material for absorbing or producing gas
• CPC Class Codes: B23K 35/004 at least one of the workpieces being of a metal of the iron group
• CPC Class Codes: B23P 15/04 turbine or like blades from several pieces
• CPC Class Codes: F01D 5/187 Convection cooling

Abstract

The invention relates to a joining method for the production of a component from two or more constructional elements which are manufactured from a highly distortion-resistant metallic material, in particular a material based on nickel or iron. The constructional elements and the interlayer are manufactured from an oxide dispersion-hardened material, and are joined together with insertion of the interlayer to give the component. The interlayer is in an unrecrystallized fine-grained plastic state before the joining process, and undergoes recrystallization, as a result of heat treatment, only after the joining process, which is carried out at a temperature of 800 to 1,100 degrees centigrade and under a pressure of 1 to 200 Mpa.

Claims

1. A joining method for producing a component from two or more constructional elements made of a metallic material, in particular of an oxide dispersion-hardened alloy based on nickel or iron, which comprises;

heat-treating the constructional elements before being joined to produce a coarse-grained oriented structure, inserting a metallic interlayer between the constructional elements which were heat-treated to produce a coarse-grained oriented structure to form a joining zone of interlayer with surfaces of the two constructional elements, said metallic interlayer manufactured from the same oxide disperison-hardened alloy as the constructional elements and having during joining the same extrusion direction as the constructional elements, and further having a plastic fine-grained recrystallizable structure, joining the assembly of heat-treated constructional elements having a coarse-grained, oriented structure with the inserted interlayer having a plastic fine-grained recrystallizable structure by heating at a temperature between 800°

-1100°

C. and a pressure of 1 through 200 Pa to effect deformation with a fine-grained growth of the interlayer below 1 μ

m, and subjecting the resultant component formed from the constructional elements to a heat treatment to effect oriented recrystallization over the joining zone.

2. A method as claimed in claim 1, wherein said resultant component is cooled and subsequently subjected to said heat treatment to effect oriented recrystallization.

3. A method as claimed in claim 1, wherein the dimension of the interlayer is chosen sufficiently large for it to have, before recrystallization, a thickness of at least 1 to 2 grain diameters of the recrystallized material in the transverse direction.

4. A method as claimed in claim 2, wherein the surfaces of the constructional elements to be joined are polished before inserting the interlayer between the constructional elements.

5. A method as claimed in claim 1, wherein the surfaces of the constructional elements to be joined are provided with a rough saw tooth-like structure.

6. A method as claimed in claim 1, wherein after complete contact between the surfaces to be joined has been achieved, the component is cooled and then heated to at least the recrystallization temperature to cause recrystallization to take place over the joining zone.

7. A method as claimed in claim 6, wherein the component is heated to the solution annealing temperature of the intermediate layer.

8. A method as claimed in claim 3, wherein after complete contact between the surfaces to be joined has been achieved, the component is cooled and then heated to at least the recrystallization temperature to cause recrystallization to take place over the joining zone.

9. A method as claimed in claim 4, wherein after complete contact between the surfaces to be joined has been achieved, the component is cooled and then heated to at least the recrystallization temperature to cause recrystallization to take place over the joining zone.

10. A method as claimed in claim 5, wherein after complete contact between the surfaces to be joined has been achieved, the component is heated rapidly from the joining temperature to at least the recrystallization temperature to cause recrystallization to take place over the joining zone.

11. A method as claimed in claim 9, wherein the component is heated to the solution annealing temperature of the intermediate layer.

12. A method as claimed in claim 10, wherein the component is heated to the solution annealing temperature of the intermediate layer.

13. A method as claimed in claim 11, wherein the component is kept at the solution annealing temperature until the recrystallization over a weld seam at the joint reaches a desired strength of the metallized material in the joining zones.

14. A method as claimed in claim 12, wherein the component is kept at the solution annealing temperature until the recrystallization over a weld seam at the joint reaches a desired strength of the metallized material in the joining zones.

15. A method as claimed in claim 1, wherein the component is subjected to zone annealing to achieve recrystallization of the interlayer, and the zone annealing is carried out under a steep temperature gradient.