Brazed electrode for plasma cutting torch

Patent metadata

Field	Value
Publication number	US-11554449-B2
Application number	US-201916704062-A
Country	US
Kind code	B2
Filing date	Dec 5, 2019
Priority date	Feb 24, 2017
Publication date	Jan 17, 2023
Grant date	Jan 17, 2023

Abstract

A silver-copper cutting electrode assembly, and method of manufacture is provided with optimized attributes to allow for improved durability, integrity and manufacturability. An electrode has a silver tip portion which is brazed to a copper body portion where the silver portion and joint have a particular structural relationship.

First claim

What is claimed is:

1. A method of manufacturing a composite plasma cutting electrode, comprising:
providing a body portion made from a first material having a wall portion defining a cavity and a distal end having an distal end face and a first shoulder engagement portion which extends upstream from said distal end face, where said first shoulder engagement portion comprises first and second surfaces;
providing a tip portion made from a second material, said tip portion having a further distal end face and a tip cavity in said further distal end face with an emissive insert disposed in said tip cavity, an upstream end face, and a second shoulder engagement portion extending downstream from said upstream end face, and having a first and second surface,
inserting said tip portion into said distal end of said body portion such that said upstream end face of said tip portion makes direct physical contact with said first surface of said first shoulder engagement portion, where said second surface of said first shoulder engagement portion is adjacent to said second surface of said second shoulder engagement portion such that a first gap exists between said respective second surfaces, and where said first surface of said second shoulder engagement portion is adjacent to said distal end face of said body portion such that a second gap exists between said first surface of said second shoulder engagement portion and said distal end face of said body portion, wherein the body portion and the tip portion do not contact each other between said respective second surfaces forming the first gap or between the first surface of the second shoulder engagement portion and the distal end face of the body portion forming the second gap; and
brazing said tip portion to said body portion to join said body portion and said tip portion using a brazing material, wherein each of said first and second gaps are filled with said brazing material.

2. The method of claim 1 , wherein said second gap is in a range of 0.001 to 0.006 in.

3. The method of claim 2 , wherein said first gap is in a range of 0.002 to 0.0035 in.

4. The method of claim 1 , wherein said wall portion has a first thickness which is upstream of said first shoulder engagement portion and a second thickness which is downstream of said first surface of said first shoulder engagement portion, wherein said first thickness is greater than said second thickness.

5. The method of claim 1 , wherein a wall thickness of said first shoulder engagement portion is different from a wall thickness of said second shoulder engagement portion.

6. The method of claim 1 , wherein said first material is copper, said second material is silver and said brazing material contains silver.

7. The method of claim 1 , wherein said composite plasma cutting electrode has an overall length L, and said tip portion has a length SL, where SL is in the range of 10 to 20% of L.

8. The method of claim 1 , wherein said composite plasma cutting electrode has an overall length L, and said tip portion has a length SL, where SL is in the range of 12 to 17% of L.

9. The method of claim 1 , further comprising a step of machining said composite plasma cutting electrode to final dimensions after performing said step of brazing.

10. A method of manufacturing a composite plasma cutting electrode, comprising:
providing a body portion made from a first material having a wall portion defining a cavity and a distal end having an distal end face and a first shoulder engagement portion which extends upstream from said distal end face, where said first shoulder engagement portion comprises first and second surfaces;
providing a tip portion made from a second material, said tip portion having a further distal end face and a tip cavity in said further distal end face with an emissive insert disposed in said tip cavity, an upstream end face, and a second shoulder engagement portion extending downstream from said upstream end face, and having a first and second surface,
inserting said tip portion into said distal end of said body portion such that said upstream end face of said tip portion makes direct physical contact with said first surface of said first shoulder engagement portion, where said second surface of said first shoulder engagement portion is adjacent to said second surface of said second shoulder engagement portion such that a first gap exists between said respective second surfaces, and where said first surface of said second shoulder engagement portion is adjacent to said distal end face of said body portion such that a second gap exists between said first surface of said second shoulder engagement portion and said distal end face of said body portion, wherein the body portion and the tip portion do not contact each other between said respective second surfaces forming the first gap or between the first surface of the second shoulder engagement portion and the distal end face of the body portion forming the second gap; and
brazing said tip portion to said body portion to join said body portion and said tip portion using a brazing material, wherein each of said first and second gaps are filled with said brazing material, and said second gap is larger than said first gap.

11. The method of claim 10 , wherein said second gap is in a range of 0.001 to 0.006 in.

12. The method of claim 11 , wherein said first gap is in a range of 0.002 to 0.0035 in.

13. The method of claim 10 , wherein said wall portion has a first thickness which is upstream of said first shoulder engagement portion and a second thickness which is downstream of said first surface of said first shoulder engagement portion, wherein said first thickness is greater than said second thickness.

14. The method of claim 10 , wherein a wall thickness of said first shoulder engagement portion is different than a wall thickness of said second shoulder engagement portion.

15. The method of claim 10 , wherein said first material is copper, said second material is silver and said brazing material contains silver.

16. The method of claim 10 , wherein said composite plasma cutting electrode has an overall length L, and said tip portion has a length SL, wherein SL is in the range of 10 to 20% of L.

17. The method of claim 10 , wherein said composite plasma cutting electrode has an overall length L, and said tip portion has a length SL, wherein SL is in the range of 12 to 17% of L.

18. The method of claim 10 , further comprising a step of machining said composite plasma cutting electrode to final dimensions after performing said step of brazing.

Assignees

• Lincoln Global Inc

Inventors

• Namburu Praveen K
• Matthews William T

Classifications

• H05H1/34

  Details, e.g. electrodes, nozzles · CPC title

• B23K35/40

  Making wire or rods for soldering or welding · CPC title

• B23K35/22 Primary

  characterised by the composition or nature of the material · CPC title

• B23K35/0216

  Rods, electrodes or wires · CPC title

• B23K35/0211

  for use in cutting (B23K35/0205 takes precedence) · CPC title