DRAG TIP FOR A PLASMA CUTTING TORCH

• US 20090057277A1
• Filed: 09/04/2007
• Published: 03/05/2009
• Est. Priority Date: 09/04/2007
• Status: Active Grant

• Current Assignee: Victor Equipment Co. (Enovis Corp.)
• Original Assignee: Thermal Dynamics Corporation (Enovis Corp.)
• Inventors: Conway, Christopher J., Hussary, Nakhleh A., Renault, Thierry R., MacKenzie, Darrin H.
• Granted Patent: US 8,222,561 B2
• Time in Patent Office: Days
• US Class Current: 219/121.500
• CPC Class Codes: H05H 1/34 Details, e.g. electrodes, nozzles
• CPC Class Codes: H05H 1/3478 Geometrical details
• CPC Class Codes: H05H 1/3484 Convergent-divergent nozzles

Abstract

A drag tip for use in a plasma cutting torch is provided that includes an inner tip portion defining a distal end face, an inner cavity through which a plasma gas flows, and an orifice disposed between the distal end face and the inner cavity. An outer tip portion surrounds the inner tip portion and defines an inner chamber to accommodate a flow of secondary gas and also a distal end portion. The distal end face of the inner tip portion is adapted for contact with a workpiece and extends distally beyond the distal end portion of the outer tip portion, and the flow of secondary gas exits the outer tip portion proximate the distal end portion. Variations of the drag tip and methods of operation are also provided.

Claims

1. A drag tip comprising:

an inner tip portion defining;

a distal end face;

an inner cavity through which a plasma gas flows; and

an orifice disposed between the distal end face and the inner cavity,

an outer tip portion surrounding the inner tip portion and defining;

an inner chamber to accommodate a flow of secondary gas;

and

a distal end portion,

wherein the distal end face of the inner tip portion is adapted for contact with a workpiece and extends distally beyond the distal end portion of the outer tip portion, and the flow of secondary gas exits the outer tip portion proximate the distal end portion.

2. The drag tip according to claim 1, wherein the distal end face of the inner tip portion extends distally beyond the distal end portion of the outer tip portion a nominal distance of greater than or equal to about 0.010 inches.

3. The drag tip according to claim 2, wherein the distal end face of the inner tip portion extends distally beyond the distal end portion of the outer tip portion a nominal distance of about 0.020 inches.

4. The drag tip according to claim 1, wherein the distal end portion of the outer tip portion defines a distal inner wall that is angled outwardly.

5. The drag tip according to claim 1, wherein the orifice of the inner tip portion transitions to an enlarged recessed area proximate the distal end face.

6. The drag tip according to claim 1, wherein the inner tip portion and the outer tip portion define separate pieces.

7. The drag tip according to claim 6, wherein the inner tip portion defines a faceted outer wall that engages an inner wall of the outer tip portion to secure the pieces together.

8. The drag tip according to claim 1, wherein the inner tip portion and the outer tip portion define a unitary piece.

9. The drag tip according to claim 1, wherein at least one of the inner tip portion and the outer tip portion are formed from a precipitation hardened copper alloy.

10. The drag tip according to claim 1 further comprising a protective coating disposed over at least a portion of the distal end face of the inner tip portion.

11. The drag tip according to claim 10, wherein the coating is applied by a process selected from the group consisting of thermal spray, thin film, sol-gel, and thick film.

12. The drag tip according to claim 1, wherein the distal end face of the inner tip portion is water-cooled.

13. A drag tip comprising at least one outer tip portion that is offset proximally from a distal end face of the tip and a deflecting wall disposed proximate a distal end portion of the tip that directs a flow of shield gas along and away from the distal end portion of the tip.

14. The drag tip according to claim 13, wherein the deflecting wall is formed in the outer tip portion.

15. The drag tip according to claim 13, wherein the deflecting wall is formed in an inner tip portion.

16. The drag tip according to claim 13 further comprising an orifice formed through the distal end face of the tip, wherein the orifice transitions to an enlarged recessed area proximate the distal end face.

17. The drag tip according to claim 13, wherein the tip is formed from a precipitation hardened copper alloy.

18. The drag tip according to claim 13 further comprising a protective coating disposed over at least a portion of the distal end face of the tip.

19. The drag tip according to claim 18, wherein the coating is applied by a process selected from the group consisting of thermal spray, thin film, sol-gel, and thick film.

20. The drag tip according to claim 13, wherein the distal end face of the inner tip member is water-cooled.

21. A drag tip comprising:

an inner tip member defining;

a distal end face;

an inner cavity through which a plasma gas flows; and

an orifice disposed between the distal end face and the inner cavity, the orifice transitioning to an enlarged recessed area proximate the distal end face, and

an outer tip member surrounding the inner tip member;

wherein a distal end face of the inner tip member is adapted for contact with a workpiece and extends distally beyond a distal end portion of the outer tip member, and a flow of secondary gas exits the outer tip member proximate the distal end portion and is angled outwardly.

22. The drag tip according to claim 21, wherein the inner tip member defines a faceted outer wall that engages an inner wall of the outer tip member to secure the inner tip member to the outer tip member.

23. The drag tip according to claim 21 further comprising a protective coating disposed over at least a portion of the distal end face of the inner tip member.

24. A method of operating a plasma arc torch in a drag cutting mode, the method comprising directing a flow of secondary gas along a distal end portion of a drag tip, subsequently directing the flow of secondary gas away from the distal end portion of the drag tip a distance proximal from a workpiece, and directing the flow of secondary gas against the workpiece.

25. The method according to claim 24, wherein the secondary gas is provided from a plurality of gas sources having different types of gases.