Nozzle and method of operation for a plasma arc torch

• US 5,317,126 A
• Filed: 01/14/1992
• Issued: 05/31/1994
• Est. Priority Date: 01/14/1992
• Status: Expired due to Term

• Current Assignee: Hypertherm Incorporated
• Original Assignee: Hypertherm Incorporated
• Inventors: Sanders, Nicholas A., Luo, Lifeng, Couch, Richard W. Jr., Sobr, John, Backander, Patrik
• Primary Examiner(s): Paschall, Mark H.
• Application Number:
  US07/820,278
• Time in Patent Office: 868 Days
• Field of Search: 219/121.51, 219/121.49, 219/121.52, 219/121.5, 219/74, 219/75, 219/121.39, 219/121.55
• US Class Current: 219/121.51
• CPC Class Codes: H05H 1/34 Details, e.g. electrodes, nozzles
• CPC Class Codes: H05H 1/3421 Transferred arc or pilot arc mode
• CPC Class Codes: H05H 1/3436 Hollow cathodes with internal coolant flow
• CPC Class Codes: H05H 1/3442 Cathodes with inserted tip
• CPC Class Codes: H05H 1/3457 Nozzle protection devices
• CPC Class Codes: H05H 1/3468 Vortex generators

Abstract

In a plasma arc cutting torch a flow of plasma gas is bypassed out of a plasma chamber, preferably at an annular gap between a pre-orifice in an inner nozzle piece and an exit nozzle orifice in an outer nozzle piece. A bypass channel formed between the inner and outer nozzle pieces directs the bypass flow to atmosphere. A metering valve or restricting orifice remote from the gap controls the amount of the bypass flow and delays the response of changes in the flow parameters in the plasma chamber to changes in the bypass flow. The pre-orifice and nozzle orifice are positioned and dimensioned to optimize the mass flow velocity and the strength of a vortex-type flow at the pre-orifice, thereby creating a virtual nozzle immediately below the electrode. The gas flow in the plasma chamber is highly uniform and very steady.

Claims

1. In a transferred arc plasma torch having a torch body mounting an electrode and a nozzle closely spaced from the electrode at a lower end of the torch to define a plasma chamber therebetween, said nozzle having a central orifice with an upstream entrance end adjacent the electrode and a downstream exit end adjacent and spaced from a workpiece with a high current density plasma jet exiting the torch from the central nozzle orifice and a plasma gas inlet passage formed in said torch body to direct plasma gas to the plasma chamber via a swirl ring, the improvement comprising

a plasma gas bypass channel formed in said nozzle with an inlet located downstream of the nozzle orifice entrance end and adjacent the exit end, said channel creating a bypass flow of plasma gas that increases the mass flow rate of the plasma gas through the plasma chamber and creating a highly uniform and very steady flow of the plasma gas through the plasma chamber.

2. The improvement of claim 1 wherein said bypass channel inlet is an annular gap and the bypass channel extends from said annular gap through the nozzle.

3. The improvement according to claim 2 wherein said nozzle has an inner nozzle part and an outer nozzle part surrounding the inner nozzle part and wherein said bypass channel includes an annular inlet opening between said inner and outer nozzle parts.

4. The improvement according to claim 3 wherein said bypass channel is formed by a spacing between said inner and outer nozzle parts and includes at least one vent passage formed in said nozzle downstream of said bypass channel inlet.

5. The improvement according to claim 4 wherein said bypass channel has a generally conical shape with an angle of inclination with respect to the centerline of the torch body of at least about 45°

.

6. The improvement according to claim 2 wherein the nozzle has inner and outer nozzle pieces that are mutually spaced to defied between said bypass channel and wherein said inner nozzle has a pre-orifice and said outer nozzle has a nozzle orifice aligned with said pre-orifice, said pre-orifice having a larger cross sectional opening than said nozzle orifice and creating a strong vortex flow of said plasma gas opposite said electrode that stabilizes the location of the arc on the electrode.

7. The improvement according to claim 6 wherein the height of said bypass channel between said pre-orifice and said nozzle orifice is sized to produce said bypass flow while maintaining a sufficient flow rate and vortex flow pattern to stabilize the arc at the entrance to said nozzle orifice.

8. The improvement according to claim 1 wherein said bypass channel includes a vent path to atmosphere.

9. The improvement according to claim 8 wherein said vent path includes at least one vent opening that produces flow friction but does not substantially impede flow of plasma gas therethrough.

10. The improvement according to claim 9 further comprising bypass gas flow control means operably connected in said vent path downstream of said at least one vent opening to form a choke point removed from said at least one opening.

11. The improvement according to claim 10 further comprising means operably connected to said plasma gas inlet passage to control the total flow of plasma gas to the torch.

12. The improvement according to claim 1 wherein said bypass channel comprises a set of holes formed in said nozzle extending from said central nozzle orifice to the exterior surface of said nozzle.

13. The improvement according to claim 6 wherein said bypass channel includes a set of holes formed in a nozzle wall portion extending from said pre-orifice to said nozzle orifice with said holes each in fluid communication between the interior of said nozzle and a conical channel formed in said nozzle.

14. A nozzle for a high current density plasma arc torch having a torch body, an electrode mounted in the body in a spaced relationship with respect to the nozzle to define a plasma chamber therebetween with a nozzle orifice at one end of the nozzle providing an exit for the plasma arc from the torch to a workpiece when the arc is transferred, and a plasma gas inlet passage that directs plasma gas to the plasma arc chamber at its upper end opposite the nozzle orifice, comprising

an inner nozzle body having a generally hollow, cylindrical upper portion and a downwardly converging lower portion terminating in a pre-orifice,

an outer nozzle body having a hollow generally cylindrical first portion that surrounds said inner body first portion, and a downwardly converging lower portion that surrounds said inner body lower portion in a mutually spaced relationship to define therebetween an annular bypass channel, said outer body lower portion terminating in a nozzle orifice that is aligned with and axially spaced from said pre-orifice, and,

an opening between said pre orifice and said nozzle orifice that provides a second outlet for said plasma gas from said nozzle to said bypass channel,

at least one vent opening formed in said nozzle at the end of said channel remote from said opening.

15. The nozzle of claim 14 wherein the inner surface of said inner nozzle, in combination with said electrode, defines a flow path for the plasma gas through the plasma chamber that has a progressively smaller flow radius to produce a high velocity vortex at the pre-orifice.

16. The nozzle according to claim 15 wherein said bypass channel is generally conical and has an angle of inclination with respect to the centerline of the nozzle of at least 45°

.

17. The nozzle according to claim 16 wherein the diameter of the pre-orifice is greater than the diameter of the nozzle orifice, and wherein the spacing between the pre-orifice and the nozzle orifice is a continuous gap,

18. The method of operating a high current density, transferred arc plasma cutting torch having an electrode and a nozzle mounted in a mutually closely spaced relationship at a lower end of a torch body with a plasma chamber defined between the electrode and the nozzle, a swirling flow of plasma gas to the plasma chamber at an upper end thereof, and a nozzle orifice that guides a transferred plasma arc to a workpiece from an orifice entrance end to an exit orifice end, comprising,

directing a portion of the plasma gas flow from the plasma chamber downstream of the orifice entrance end and before it exits through the nozzle orifice at the exit end to increase the mass flow rate in the plasma chamber without increasing the mass flow rate through the nozzle orifice, and

creating a highly uniform and very steady flow of the plasma gas through the plasma chamber at the same times as said directing.

19. The method of claim 18 wherein said directing occurs as close to said nozzle exit orifice end as possible to extend said high velocity flow over the electrode, including its lower end opposite said nozzle orifice.

20. The method of claim 18 further comprising creating a virtual nozzle with said vortex flow at a point between the lower end of said electrode and the nozzle orifice.

21. The method of claim 18 wherein said directing is highly uniform and stable to produce a high degree of arc stability.

22. The method of claim 18 wherein said directing includes venting said directed gas flow portion to atmosphere.

23. The method of claim 22 wherein said venting includes guiding said directed gas portion away from said nozzle orifice along a path that forms an angle of at least 45°

with the centerline of the torch.

24. The method of claim 22 wherein said venting includes controlling the flow rate of said directed flow at a point remote from said nozzle orifice to introduce a delay int he response of flow in said plasma chamber to changes in said diverted flow.

25. The method of claim 24 further comprising the step of restricting said directed flow prior to said controlling to increase the uniformity of said flow.

26. The method of claim 24 further comprising the step of controlling the total flow rate of plasma gas to said torch in coordination with said venting control to set the ratio of the directed plasma gas flow rate and the flow rate of the plasma gas through said nozzle orifice that is not so directed.