Drag tip for a plasma cutting torch

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 disposed between the inner tip portion and the outer tip portion and inside the outer tip portion 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:

a distal end face; and

at least one outer tip portion including an inner surface and a distal end portion, the distal end portion being offset proximally from the distal end face and including a deflecting wall,

wherein the deflecting wall is disposed proximate the distal end portion of the at least one outer tip portion and angled outwardly from the inner surface for directing a flow of shield gas along and away from the distal end face.

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 to define an inner chamber between the inner tip member and the outer tip member and inside the outer 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 flows through the inner chamber and 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 plasma arc torch including a drag tip having a distal end face and a distal portion that is offset proximally from the distal end face, the method comprising:

directing a flow of secondary gas inside the drag tip and along the distal end portion of the 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.