Air cooled plasma torch and components thereof

Patent metadata

Field	Value
Publication number	US-9572242-B2
Application number	US-201414281818-A
Country	US
Kind code	B2
Filing date	May 19, 2014
Priority date	May 19, 2014
Publication date	Feb 14, 2017
Grant date	Feb 14, 2017

Abstract

Embodiments of the present invention are directed to an air cooled, retract-start plasma cutting torch having improved performance. The torch comprises any one, or a combination of an improved nozzle, electrode, shield cap and swirl ring, where these components have improved geometries and physical properties which optimize plasma jet performance during cutting.

First claim

I claim:

1. An air cooled plasma cutting torch, said torch comprising:
an electrode having a hafnium insert from which a plasma jet is originated for cutting a workpiece;
a nozzle having a cylindrical portion and a truncated cone portion downstream of said cylindrical portion, said truncated cone portion directly transitions to a distal end surface and said truncated cone portion has a throat through which said plasma jet is passed during cutting, where said cylindrical portion forms a cavity into which at least some of said electrode is positioned and a gap is formed between said electrode and said cylindrical portion, and where said truncated cone portion has an angled outer surface which is angled relative to a centerline of said nozzle by an angle in the range of 30 to 60 degrees, and where said throat couples said cavity with said distal end surface; and
a shield cap having a cylindrical portion and a truncated cone portion which has an end surface, where said shield cap truncated cone portion has a hole through said end surface through which said plasma jet passes during cutting and said truncated cone portion directly transitions to said end surface; where said shield cap cylindrical portion forms a cavity into which at least some of said nozzle cylindrical portion is inserted and a gap is formed between said nozzle and said shield cap, where said shield cap truncated cone portion has an inner angled surface which is angled relative to a centerline of said shield cap by an angle which is larger than said angle of said angled outer surface of said nozzle, such that a gap between said inner angled surface and said angled outer surface decreases in a downstream direction,
wherein said throat has a length from an inlet to said throat to an outlet of said throat, and where a ratio of said length to a diameter of said throat is in the range of 3 to 4.5, where said diameter is the smallest diameter of said throat.

2. The air cooled plasma cutting torch of claim 1 , wherein said angle of said nozzle is in the range of 40 to 50 degrees.

3. The air cooled plasma cutting torch of claim 1 , wherein said ratio is in the range of 3 to 4.

4. The air cooled plasma cutting torch of claim 1 , wherein a maximum voltage drop along a length of said throat is 20 volts regardless of an operational current from a power supply to said air cooled plasma cutting torch, where said length is a length from an inlet of said throat to and exit of said throat.

5. The air cooled plasma cutting torch of claim 4 , wherein said voltage drop is in the range of 5 to 15 volts.

6. The air cooled plasma cutting torch of claim 4 , wherein said voltage drop is less than 5 volts.

7. The air cooled plasma cutting torch of claim 4 , wherein said current operational range is 40 to 100 amps.

8. The air cooled plasma cutting torch of claim 1 , wherein said throat has an inlet with a first diameter and an exit with a second diameter and a ratio between said first diameter to said second diameter is in the range of 1.5 to 4.

9. The air cooled plasma cutting torch of claim 1 , wherein said hole has a diameter which is in the range of 1.25 to 4.1 times the smallest diameter of said throat.

10. The air cooled plasma cutting torch of claim 9 , wherein said ratio is in the range of 1.75 to 2.5.

11. The air cooled plasma cutting torch of claim 1 , wherein said hole has a diameter which is greater than a diameter of said throat at an exit of said throat.

12. The air cooled plasma cutting torch of claim 1 , wherein said inner angled surface has an angle in the range of 35 to 70 degrees.

13. The air cooled plasma cutting torch of claim 1 , wherein said inner angled surface is in the range of 45 to 60 degrees.

14. The air cooled plasma cutting torch of claim 1 , wherein a largest distance of said gap between said inner angled surface and said outer angled surface is in the range of 0.03 to 0.05 inches.

15. The air cooled plasma cutting torch of claim 1 , wherein a width of said gap between said inner angled surface and said outer angled surface decreases by 30 to 60% from a widest portion of said gap to a narrowest portion of said gap.

16. The air cooled plasma cutting torch of claim 1 , wherein said nozzle has a thermal heat band at said truncated cone portion during sustained use of said air cooled plasma cutting torch at 100 amps which does not extend onto said cylindrical portion of said nozzle, wherein in the heat band the average temperature of the nozzle is 350 degrees.

17. An air cooled plasma cutting torch, said torch comprising:
an electrode having a hafnium insert from which a plasma jet is originated for cutting a workpiece;
a nozzle having a cylindrical portion and a truncated cone portion downstream of said cylindrical portion, said truncated cone portion directly transitions to a distal end surface and said truncated cone portion has a throat through which said plasma jet is passed during cutting, where said cylindrical portion forms a cavity into which at least some of said electrode is positioned and a gap is formed between said electrode and said cylindrical portion, and where said truncated cone portion has an angled outer surface which is angled relative to a centerline of said nozzle by an angle in the range of 30 to 60 degrees, and where said throat couples said cavity with said distal end surface; and
a shield cap having a cylindrical portion and a truncated cone portion which has an end surface, where said shield cap truncated cone portion has a hole through said end surface through which said plasma jet passes during cutting and said truncated cone portion directly transitions to said end surface; where said shield cap cylindrical portion forms a cavity into which at least some of said nozzle cylindrical portion is inserted and a gap is formed between said nozzle and said shield cap, where said shield cap truncated cone portion has an inner angled surface which is angled relative to a centerline of said shield cap by an angle which is larger than said angle of said angled outer surface of said nozzle, such that a gap between said inner angled surface and said angled outer surface decreases in a downstream direction,
wherein said throat has a length from an inlet to said throat to an outlet of said throat, and where a ratio of said length to a diameter of said throat is in the range of 3 to 4.5, where said diameter is the smallest diameter of said throat,
wherein said hole has a diameter which is in the range of 1.25 to 4.1 times the smallest diameter of said throat,
wherein said inner angled surface has an angle in the range of 35 to 70 degrees, and wherein a largest distance of said gap between said inner angled surface and said outer angled surface is in the range of 0.03 to 0.05 inches.

18. An air cooled plasma cutting torch, said torch comprising:
an electrode having a hafnium insert from which a plasma jet is originated for cutting a workpiece;
a nozzle having a cylindrical portion and a truncated cone portion downstream of said cylindrical portion, said truncated cone portion directly transitions to a distal end surface and said truncated cone portion has a throat through which said plasma jet is passed during cutting, where said cylindrical portion forms a cavity into which at least some of said electrode is positioned and a gap is formed between said electrode and said cylindrical portion, and where said truncated cone portion has an angled outer surface which is angled relative to a centerline of said nozzle by an angle in the range of 30 to 60 degrees, and where said throat couples

Assignees

• Lincoln Global Inc

Inventors

• Namburu Praveen K

Classifications

• H05H1/34 Primary

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

• H05H2001/3457

  Electricity · mapped topic

• H05H2001/3478

  Electricity · mapped topic

• H05H1/3478

  Geometrical details · CPC title

• H05H1/3457

  Nozzle protection devices · CPC title