CA2410797A1

CA2410797A1 - Apparatus for injecting gas into a vessel

Info

Publication number: CA2410797A1
Application number: CA002410797A
Authority: CA
Inventors: Martin Joseph Dunne; Gregory John Hardie
Original assignee: Individual
Current assignee: Technological Resources Pty Ltd
Priority date: 2001-04-11
Filing date: 2002-04-10
Publication date: 2002-10-24
Anticipated expiration: 2022-04-10
Also published as: BR0204820A; EP1377689A4; EP1377689A1; JP2004518826A; WO2002083958A1; RU2285049C2; ATE298006T1; CN1461351A; MXPA02012159A; CN1243836C; EP1377689B1; CA2410797C; KR20030011884A; KR100825940B1; JP4175896B2; DE60204675D1; BR0204820B1; DE60204675T2; AUPR436901A0

Abstract

An injection lance (26) for injecting hot gas into a vessel includes an elongate gas flow duct (31) which receives hot gas from a gas inlet structure (32) and an elongate central tubular structure (33) which extends within gas flow duct (31) from its rear end to its forward end. Adjacent the forward end of duct (31), central structure (33) carries a series of flow directing vanes (34) for imparting swirl to the hot gas flow exiting the duct. The wall of duct (31) downstream from gas inlet (32) is internally water cooled by flow of water through annular passages (43,44). The cooling water also flows through the interior of a duct tip (36) at the forward end of duct (31). The front end of central structure (33) which carries the swirl vanes (34) is internally water cooled by cooling water supplied forwardly through a central water flow passage (52) from a water inlet (53) at the rear of the lance through to a nose (35) of the central structure. The cooling water returns back through the central structure via an annular water return passage (54) to a water outlet (55) at the rear end of the lance.

Claims

1. Apparatus for injecting gas into a vessel, including:

a gas flow duct extending from a rear end to a forward end from which to discharge gas from the duct;
an elongate central tubular structure extending within the gas flow duct from its rear end to its forward end;
a plurality of flow directing vanes disposed about the central tubular structure adjacent the forward end of the duct to impart swirl to a gas flow to the forward end of a duct, the forward end of the central structure and the forward end of the duct co-acting together to form an annular nozzle for flow of gas from the duct with swirl imparted by said vanes;
cooling water passages within the central tubular structure for flow of cooling water forwardly through the central structure from its rear end to its forward end and to internally cool that forward end and thence to return back through the central structure to its rear end.

2. Apparatus as claimed in claim 1, wherein the forward end of the duct is formed as a hollow annular tip formation and the gas flow duct includes duct tip cooling water supply and return passages for supply of cooling water forwardly along the duct into the duct tip and return of that cooling water back along the duct.

3. Apparatus as claimed in claim 1 or claim 2, wherein the interior peripheral surface of the duct is lined with refractory material.

4. Apparatus as claimed in any one of the preceding claims, wherein the central tubular structure defines a central water flow passage for flow of water forwardly through that structure directly to the forward end of the central structure and an annular water flow passage disposed about the central passage for return flow of water from the forward end of the central structure back to the rear end of that structure.

5. Apparatus as claimed in claim 4, wherein the central tubular structure comprises a central tube providing the central water flow passage and a further tube disposed around the central tube to define said annular water flow passage between the tubes.

6. Apparatus as claimed in any one of the preceding claims, wherein the central structure includes a heat insulating outer shield to retard heat transfer from gas in the gas flow duct into the cooling water passages in the central structure.

7. Apparatus as claimed in claim 6, wherein the heat insulating shield includes a plurality of tubular segments of heat insulating material disposed end to end to form the heat shield as a substantially continuous tube extending from the rear end to the front end of the central structure about an annular air gap disposed immediately within the heat shield.

8. Apparatus as claimed in claim 7, wherein said air gap is formed between the tubular heat shield and the further tube defining the outer wall of the annular water return flow passage.

9. Apparatus as claimed a.n claim 7 or claim 8, wherein said tubular segments of the heat shield are supported to accommodate longitudinal expansion of each segment independently of the other such segments.

10. Apparatus as claimed in any one of the preceding claims, wherein the forward end of the central structure includes a domed nose portion provided internally with a single spiral cooling water passage to receive water from the central water flow passage in the central structure at the tip of the nose and direct that water in a single flow around and backwardly along the nose to cool the nose with a single coherent stream of cooling water.

11. Apparatus as claimed in any one of the preceding claims and provided with a gas inlet for introduction of hot gas into the rear end of the duct, the gas inlet including a refractory body defining a first tubular gas passage aligned with and extending directly to the rear end of the duct and a second tubular gas passage transverse to the first passage to receive hot gas and direct it to the first passage so that the hot gas and any particles entrained therein impinge on refractory wall of the first passage, the gas flow undergoing a change of direction in passing from the first passage to the second passage.

12. Apparatus as claimed in claim 11, wherein the first and second gas flow passages are essentially normal to one another.

13. Apparatus as claimed in claim 11 or claim 12, wherein the central tubular structure extends centrally through the first gas flow passage of the gas inlet and rearwardly beyond the gas inlet.

14. Apparatus as claimed in claim 13, wherein the rear end of the central structure is located rearwardly of the gas inlet and is provided with water couplings for the flow of cooling water to and from the central structure.

15. A metallurgical vessel fitted with apparatus for injecting a flow of gas into an upper part of the vessel under high temperature conditions, said apparatus being constructed in accordance with any one of claims 1 to 14 and being mounted in a roof of the vessel to extend downwardly through the roof with the rear end of the gas flow duct disposed above the roof and the forward end of the duct located in the upper part of the vessel.