Generating discrete gas jets in plasma arc torch applications

• US 7,598,473 B2
• Filed: 05/11/2006
• Issued: 10/06/2009
• Est. Priority Date: 05/11/2005
• Status: Active Grant

• Current Assignee: Hypertherm Incorporated
• Original Assignee: Hypertherm Incorporated
• Inventors: Duan, Zheng, Liebold, Stephen M., Lindsay, Jon W., Cook, David Jonathan
• Primary Examiner(s): Paschall; Mark H
• Application Number:
  US11/432,282
• Publication Number:
  US 20060289398A1
• Time in Patent Office: 1,244 Days
• Field of Search: 219/121.48, 219/121.5, 219/121.51, 219/121.52, 219/74, 219/75, 313/231.31, 313/231.41
• US Class Current: 219/121.5
• CPC Class Codes: B23K 10/00 Welding or cutting by means of a plasma
• CPC Class Codes: H05H 1/34 Details, e.g. electrodes, nozzles
• CPC Class Codes: H05H 1/3405 Arrangements for stabilising or constricting the arc, e.g. by an additional gas flow
• CPC Class Codes: H05H 1/3457 Nozzle protection devices
• CPC Class Codes: H05H 1/3468 Vortex generators
• CPC Class Codes: H05H 1/3478 Geometrical details

Abstract

The invention is generally directed to a nozzle for a plasma torch, the nozzle having a rear portion that defines at least a portion of a plasma chamber and a front portion that includes a first end and a second end. The first end is adjacent the rear portion, and the second end defines a plasma exit portion. One or more fluid passageways are disposed within the front portion and extend from the first end to the second end. The fluid passageways have passageway exit portions that provide one or more discrete jets of a secondary fluid to surround a plasma jet that is ejected from the plasma exit portion. Features of the invention include faster cutting, thicker workpiece piercing capability, reduced noise, improved arc stability, and increased consumable life, all of which improve productivity associated with plasma arc torch workpiece processing.

Claims

1. A nozzle for a transferred arc plasma cutting torch comprising, the nozzle comprising:

a rear portion defining at least a portion of a plasma chamber; and

a front portion including a first end disposed adjacent to the rear portion, a second end defining a plasma exit portion, and a plurality of gas passageways disposed within the front portion, each of the plurality of gas passageways extending from the first end to the second end and defining a gas path that provides a flow of secondary gas that exits the gas passageway via a gas passageway exit portion, each gas passageway exit portion being (a) disposed adjacent the plasma exit portion and (b) coplanar with the plasma exit portion,

the plurality of gas passageways and gas passageway exit portions, in combination, providing a plurality of discrete jets of the secondary gas which are disposed substantially parallel to a plasma jet and which reduce entrainment of an ambient fluid or the secondary gas into the plasma jet.

2. The nozzle of claim 1, wherein the plurality of gas passageways each define a gas path that generates substantially parallel flow between the secondary gas exiting the passageway exit portion and the plasma jet.

3. The nozzle of claim 1, wherein the plurality of gas passageways, in combination, generate a plurality of discrete jets that coaxially surround the plasma jet.

4. The nozzle of claim 1, wherein each of the plurality of gas passageways generates diverging angular flow of the secondary gas exiting the passageway exit portion relative to the plasma jet.

5. The nozzle of claim 1, wherein the discrete jets reduce an interaction between an ambient fluid and the plasma jet.

6. The nozzle of claim 1, wherein the plurality of fluid passageways form a radial arrangement about the plasma exit portion.

7. The nozzle of claim 1, wherein the front portion further includes a relief flat disposed along a side of each of the plurality of gas passageways to increase an amount of the secondary gas flow that enters into the plurality of gas passageways.

8. The nozzle of claim 1, wherein the plurality of gas passageways impart a swirling motion to the secondary gas.

9. The nozzle of claim 1, wherein the rear portion further includes a securing mechanism for securing the nozzle to a plasma torch body.

10. The nozzle of claim 1, wherein the front and rear portions are formed from an electrically conductive material.

11. The nozzle of claim 1, further comprising a circumscribing component defining an interior surface and an exterior surface, the circumscribing component mounted relative to the front portion such that at least a portion of the interior surface cooperates with the front portion to form the plurality of gas passageways.

12. The nozzle of claim 11, wherein the interior surface of the circumscribing component defines a portion of one or more discrete gas passageways that correspond to the plurality of gas passageways disposed on the front portion of the nozzle.

13. The nozzle of claim 1, further comprising a circumscribing component defining an interior surface and an exterior surface, the circumscribing component mounted relative to the front portion of the nozzle such that at least a portion of the interior surface cooperates with the front portion to form a secondary gas passageway.

14. The nozzle of claim 13, wherein a secondary gas flows through the secondary gas passageway independently of a plasma gas that flows through the plasma chamber and a shielding gas that flows over the exterior surface of the circumscribing component.

15. The nozzle of claim 1, wherein each of the plurality of gas passageways provide a discrete path for the secondary gas.