Nozzle for a liquid-cooled plasma burner, arrangement thereof with a nozzle cap, and liquid-cooled plasma burner comprising such an arrangement

• US 8,575,510 B2
• Filed: 03/23/2009
• Issued: 11/05/2013
• Est. Priority Date: 04/08/2008
• Status: Active Grant

• Current Assignee: Kjellberg Finsterwalde Plasma und Maschinen GmbH (Kjellberg-Stiftung)
• Original Assignee: Kjellberg Finsterwalde Plasma und Maschinen GmbH (Kjellberg-Stiftung)
• Inventors: Laurisch, Frank, Krink, Volker, Grundke, Timo, Reinke, Ralf-Peter
• Primary Examiner(s): PASCHALL, MARK H
• Application Number:
  US12/937,172
• Publication Number:
  US 20110108528A1
• Time in Patent Office: 1,688 Days
• Field of Search: 219/121.48, 219/121.49, 219/121.5, 219/121.51, 219/121.52, 219/74, 219/75, 313/231.31, 313/231.41, 313/231.51
• US Class Current: 219/121.5
• CPC Class Codes: H05H 1/28 Cooling arrangements
• CPC Class Codes: H05H 1/34 Details, e.g. electrodes, nozzles
• CPC Class Codes: H05H 1/3478 Geometrical details

Abstract

The invention relates to a liquid-cooled plasma burner, comprising a nozzle bore for the plasma gas jet to exit at a nozzle tip and a first section whose outer surface gradually tapers in the shape of a cone at an angle α in the direction of the nozzle tip, except for at least one deflection section that extends in the shape of a cone at an angle β in the direction of the nozzle tip. The invention also relates to an arrangement thereof with a nozzle cap and to a plasma burner comprising such an arrangement.

Claims

1. A nozzle for a liquid-cooled plasma burner, comprising:

a nozzle bore for a plasma gas jet to exit at a nozzle tip;

a first section, the outer surface of said first section tapering in the shape of a cone in the direction of the nozzle tip at an angle α

; and

a plurality of deflection sections arranged on said outer surface, at least two of said deflection sections extending in the shape of a cone in the direction of the nozzle tip at angles β

1, β

2 to enhance cooling and coolant flow.

2. The nozzle as claimed in claim 1 wherein the angle α

is in a range from 20°

to 120°

.

3. The nozzle as claimed in claim 2 wherein the angle β

1, β

2 is in a range from 20°

to 120°

.

4. The nozzle as claimed in claim 3 wherein said plurality of deflection sections extend in the shape of a cone at the same angle β

1 or β

2.

5. The nozzle as claimed in claim 3 wherein said plurality of deflection sections extend in the shape of a cone at different angles β

1, β

2.

6. The nozzle as claimed in claim 5 wherein the angles α

and β

1 or β

2 differ by a maximum of 30°

.

7. The nozzle as claimed in claim 5 wherein the angles α

and β

1 or β

2 are equal in size.

8. The nozzle as claimed in claim 7 wherein an angle γ

, which is formed by the outer surface of the first section, which tapers in the shape of a cone, and the outer surface of the or one of the deflection section(s), which extends in the shape of a cone, is between 60° and

160°

.

9. The nozzle as claimed in claim 8 wherein an angle δ

, which is formed by an edge of the or one of the deflection section(s), which is at the front relative to the nozzle tip, and the centre axis of the nozzle is between 75° and

105°

.

10. The nozzle as claimed in claim 9 wherein the angle δ

is 90°

.

11. The nozzle as claimed in claim 8 wherein the length or lengths (a1, a2, . . . ) of the deflection sections(s) running parallel to the centre axis of the nozzle is or are in the range from 1 to 3 mm.

12. The nozzle as claimed in claim 11 wherein the lengths (a1, a2, . . . ) of the deflection section(s) running parallel to the centre axis of the nozzle are equal in size.

13. The nozzle as claimed in claim 8 wherein the length or lengths (b1, b2, . . . ) of the deflection sections(s) running perpendicular to the centre axis of the nozzle is or are in the range from 1 to 4 mm.

14. The nozzle as claimed in claim 13 wherein the lengths (h1, b2, . . . ) of the deflection section(s) running perpendicular to the centre axis of the nozzle are equal in size.

15. The nozzle as claimed in claim 14 wherein the nozzle has a second section with a cylindrical outer surface to be received in a nozzle bracket.

16. The nozzle as claimed in claim 15 wherein the nozzle has a third section with a substantially cylindrical outer surface, which is located immediately before the nozzle bore relative to the centre axis of the nozzle.

17. The nozzle as claimed in claim 15 wherein the nozzle has a third section with a substantially cylindrical outer surface, which is located at least partially opposite the nozzle bore relative to the centre axis of the nozzle.

18. The nozzle as claimed in claim 17 wherein there is a groove for an O-ring located in the vicinity of the nozzle tip.

19. An arrangement, comprising:

a nozzle having;

a nozzle bore for a plasma gas jet to exit at a nozzle tip; and

a first section, the outer surface of said first section tapering in the shape of a cone in the direction of the nozzle tip at an angle α

, a plurality of deflection sections arranged on said outer surface, at least two of said deflection sections extending in the shape of a cone in the direction of the nozzle tip at angles β

1, β

2 to enhance cooling and coolant flow;

a nozzle cap; and

wherein the nozzle cap and the nozzle form a coolant chamber which is in fluid connection with a coolant supply line and a coolant return line, and wherein, at least in the region of the first section of the nozzle, the nozzle cap has an internal surface tapering in the shape of a cone in the direction of the nozzle tip.

20. The arrangement as claimed in claim 19 wherein the area of the circular annular surface of the coolant chamber reduces in the direction of the nozzle tip along the centre axis of the nozzle in the at least one deflection section 1.5 to 8 times more quickly than before the at least one deflection section.

21. The arrangement as claimed in claim 20 wherein the area of the circular annular surface of the coolant chamber (10) in the direction of the nozzle tip along the centre axis of the nozzle immediately after the at least one deflection section is 1.5 to 8 times larger than the smallest area of the deflection section.

22. The arrangement as claimed in claim 21 wherein the circular annular surface of the coolant chamber in the direction of the nozzle tip along the centre axis of the nozzle immediately after the at least one deflection section jumps at least to the value it has immediately before the deflection section.

23. The arrangement as claimed in claim 22 wherein the coolant supply line and the coolant return line are arranged offset to one another by 180°

.

24. A liquid-cooled plasma burner, comprising:

a coolant supply line;

a coolant return line;

a nozzle having;

a nozzle bore for a plasma gas jet to exit at a nozzle tip; and

a first section, the outer surface of said first section tapering in the shape of a cone in the direction of the nozzle tip at an angle α

, a plurality of deflection sections arranged on said outer surface, at least two of said deflection sections extending in the shape of a cone in the direction of the nozzle tip at angles β

1, β

2 to enhance cooling and coolant flow;

a nozzle cap; and

wherein the nozzle cap and the nozzle form a coolant chamber which is in fluid connection with said coolant supply line and said coolant return line, and wherein, at least in the region of the first section of the nozzle, the nozzle cap has an internal surface tapering in the shape of a cone in the direction of the nozzle tip.

25. The plasma burner as claimed in claim 24, further comprising a secondary gas supply line and a nozzle cover guard.