US3743814A

US3743814A - Oxygen lance

Info

Publication number: US3743814A
Application number: US00236507A
Authority: US
Inventors: G Oakes
Original assignee: Individual
Current assignee: Individual
Priority date: 1970-12-18
Filing date: 1972-03-20
Publication date: 1973-07-03
Anticipated expiration: 1990-07-03

Abstract

An oxygen lance is disclosed such as used by the steel industry in connection with introducing oxygen into open-hearth or basic oxygen furnaces containing molten steel. The oxygen lance has tubular coolant channels and an oxygen supply channel with an apertured brass casting forming the oxygen delivery tip. The tip includes a coolant chamber centrally thereof. The coolant channels of the lance are placed in communication with the coolant chamber for an improved cooling effect.

Description

July 3, 1973 United States Patent [191 Oakes U OXYGEN LANCE [76] Inventor: Grant A. Oakes, RD. N0. 4, Primary Exami"er R' Staubly Comand, Ohio 44410 Attorney-Webster B. Harpman Mar. 20, 1972 Appl. No.: 236,507

[22] Filed:

ABSTRACT Related US. Application Data An oxygen lance is disclosed such as used by the steel Division 'of Ser. No. 99,570, Dec. 118, i970, Pat. No. 3,676,634.

industry in connection with introducing oxygen into open-hearth or basic oxygen furnaces containing molten steel. The oxygen lance has tubular coolant channels and an oxygen supply channel with an a brass casting forming the oxygen delive pertured ry tip. The tip includes a coolant chamber centrally thereof. The coolant channels of the lance are placed in communication with the coolant chamber for an improved cooling effeet.

References Cited UNITED STATES PATENTS 3 Claims, 3 Drawing Figures a ga/1&7 I w Patented July 3, 1973 2 Sheets-Sheet 2 2 2 j fl B H M O 8 V e r FIG.3

OXYGEN LANCE BACKGROUND OF THE INVENTION 1. Field of the Invention This invention relates to oxygen lances of the type normally employed to introduce oxygen into openheaths of BOF furnaces in the steel industry.

2. Description of the Prior Art Prior structures of this type comprise several long pipe sections positioned one within the other and secured at one of their ends to an aperatured casting. The long pipes which are of different diameters provide axially extending passageways for the oxygen and outward and return passageways for a liquid coolant such as water. The apertures in the casting which otherwise closes the tip of the lance communicates with the oxygen supply pipe so that the oxygen is introduced through the same into the open-hearth or BOF vessel and still other apertures establish communication between the coolant channels of the pipes to introduce some cooling effect into the casting.

As heretofore used the casting erodes relatively rapidly as a result of its exposure to the heat and turbulence of the molten metal into which the oxygen is being introduced through the lance with the result that the area of the casting is reduced to a point where the coolant channels are opened whereupon the lance must be withdrawn from the furnace. Heretofore, such oxygen lances have been discarded after a relatively short life.

This invention provides for rebuilding such oxygen lances to render them more efficient in operation and capable of a longer life and to make possible continued reuse of the same through subsequent rebuilding operations.

SUMMARY OF THE INVENTION A method of rebuilding an oxygen lance having an eroded tip portion comprises cutting away a portion of the lance tip casting to form a coolant chamber capping the chamber, installing plugs of suitable material in the oxygen delivery apertures in the tip portion and rebuilding the tip portion to its original configuration by welding metal thereon and subsequently removing said plugs and reshaping said tip portion.

DESCRIPTION OF THE DRAWINGS FIG. 1 is a cross sectional side elevation with parts broken away of the delivery end portion of an oxygen lance showing the eroded tip portion and break through into the coolant channels therein.

FIG. 2 is a side elevation of the tip portion of the oxygen lance of FIG. 1 showing steps in the rebuilding thereof and FIG. 3 is a cross-sectional side elevation with parts broken away showing the same after rebuilding.

DESCRIPTION OF THE PREFERRED EMBODIMENT In its simplest form the method of rebuilding an oxygen lance disclosed herein comprises welding replacement metal in the eroded area of the tip portion of the oxygen lance.

By referring to FIG. 1 of the drawings the tip portion of an oxygen lance may be seen to comprise a casting 10 usually formed of bronze and which casting 10 is carried on the outermost or free'ends of a plurality of

tubes

11, 12 and 13 respectively.

The ends of the

tubes

11, 12 and 13 are affixed to the casting 10 as by welding. The

tubes

11, 12 and 13 are usually about feet long and their opposite ends, not shown, are engaged in a manifold through which a coolant such as water and a supply of oxygen are placed in communication with the lance.

The oxygen is delivered to the tip of the oxygen lance through the tube 11 which is welded as at 14 to an upstanding central portion 15 of the casting 10 and the oxygen flows through passageways 16 in the casting l0 and thus outwardly of the lance and into the molten metal in the open-hearth or basic oxygen furnace in which the lance is used.

The tube 13 is welded in a watertight manner to the casting 10 as by the weld 17 and water introduced into the opposite or manifold end of the tube 13 will flow downwardly and is able to enter cooling bores 18 in the casting 10 by way of tubular connections 19 which extend through the tube 12 and into the casting 10. Return coolant bores 20 establish communication between the coolant bores 18 and the area within the tube 12 and it will be observed that coolant is circulated through the central portion of the casting 10 by the plurality of radially positioned

coolant bores

18 and 20. The end of the tube 12 is engaged in annular groove 21 in the casting 10.

Still referring to FIG. 1 of the drawings it will be observed-that the end of the tube 12 is spaced with respect to the bottom of the annular groove 21 in the casting 10 by a plurality of spacing members 22 so that coolant within the tube 13 can move in under the end of the tube 12 and enter the space within the tube 12 and flow outwardly therethrough. Arrows in FIG. 1 of the drawings indicate the direction of flow of the coolant and it will be observed that the annular groove 21 in the casting 10 forms a cooling chamber within the same.

In FIG. I of the drawings the eroded end surface of the oxygen lance and specifically the lower portion of the casting 10 is indicated by the letter E and it will be observed that at the maximum point of erosion the metal of the casting 10 has been removed to a point where the lowermost areas of the

coolant bores

18 and 20 are exposed as indicated in FIG. 1 by the letter B.

- the steel industry and that when failure has occurred as at point B in FIG. 1 the lance is no longer usable.

In rebuilding the oxygen lance and more specifically the casting 10 comprising the tip thereof by the method disclosed herein, several successive steps are taken as follows and as illustrated in FIGS. 2 and 3 of the drawings.

By referring to FIG. 2 it will be seen that a portion of the casting 10 of FIG. 1 is disclosed in cross section and that shaped graphite plugs 23 have been inserted in each of the oxygen passageways 16 in the casting 10 and that the plugs 23 are of a length greater than the original length of the passageways as determined by the original end configuration of the oxygen lance and as shown for example by the broken lines in FIG. 1 of the drawings which describe the arcuate end portion 26 of the lance as it originally existed.

Still referring to FIG. 2 of the drawings, it will be seen that a chamber 24 has been formed in the casting in the area defined by the junction of the

coolant bores

18 and 20 and which area was indicated in FIG. 1 by the letter B. A cap is applied as a closure to the coolant chamber 24 by positioning the same on an annular shoulder formed therein.

The eroded area of the casting 10 is then rebuilt by the application of metal as by welding until the eroded area is completely filled. It will be observed that the metal applied in the build up step of the method of rebuilding the oxygen lance tip will be positioned around and about the graphite plugs 23 so that the oxygen passageways 16 are retained in their original form and over the cap 25 so that an effective seal is insured.

It will be further observed that the coolant chamber 24 is now considerably larger than the junction area of the

coolant bores

18 and 20 in the original form of the casting 10 and that as a result of its increased area the rebuilt casting 10 forms a more efficient tip end of the oxygen lance. The coolant chamber 24 may obviously be larger than illustrated in FIG. 2 of the drawing as it may include radial extensions between the several oxygen delivery passageways 16 and in any event, the coolant is introduced into a wider area in the rebuilt casting 10 than was possible in its original form.

It will further be observed that the coolant chamber 24 is in the area of the maximum erosion of the metal of the casting and that it is capable therefore of maintaining this portion of the casting at a lower temperature than in the original form of the casting forming the tip of the oxygen lance and that the life expectancy of the rebuilt oxygen lance and particularly the tip thereof, is thus greatly increased.

By referring now to FIG. 3 of the drawings a cross sectional side elevation of a rebuilt oxygen lance and particularly the tip thereof may be seen and it will be observed that the oxygen delivery passageway 16 extend to the end surface 27 of the rebuilt tip. A broken line 28 in the cross sectional representation of the casting 10 indicates the weld junction of the rebuilt metal with the metal of the original casting 10.

It will be observed that the rebuilt casting 10 has been restored to its original configuration as by machining and that the graphite plugs 23 as seen in FIG. 2 of the drawings which were present during the rebuilding operation have been removed. The cap 25 remains in position forming a wall of the coolant chamber 24 as heretofore described. Arc welding under inert gas may be employed.

The above described method of rebuilding the eroded tip portion of an oxygen lance will thus be seen to provide a rebuilt lance and more particularly the end casting thereof that is improved with. respect to the original form threrof and which rebuilt oxygen lance will have a substantially greater life in its reuse cycle than that of the original lance tip.

Those skilled in the art will recognize that an improved product results from the method described herein and which product may be formed as a new oxygen lance tip for first time use if so desired and which new product would incorporate the coolant chamber 24 formed in the original casting 10 of a new oxygen lance tip by forming the coolant chamber in the area of the junctions of the coolant bores therein as be drilling into the area and then capping and/or plugging the drilled opening used to form the coolant chamber.

Although but one embodiment of the present invention has been illustrated and described it will be apparent to those skilled in the art that various changes and modifications in the method and article herein disclosed may be made therein without departing from the spirit of the invention and having thus described my invention what I claim is:

1. An article usable as an end closure and tip portion of an oxygen lance having three concentrically spaced tubular members of uneven length, said article consisting of a one piece metal member of circular shape, the diameter thereof registering with the outermost one of said three tubular members, a circular upstanding boss centrally of said member and of a diameter registering with the innermost one of said three tubular members, said metal member having an annular channel therein of a diameter registering with the middle one of said three tubular members, a first series of passageways consisting of circumferentially spaced inclined bores diverging downwardly and outwardly through said upstanding boss and metal member for the passage of oxygen therethrough, said metal member having a cavity in the central portion thereof and spaced inwardly from the top and bottom surfaces thereof, a second series of passageways in said metal member consisting of bores arranged circumferentially and spaced with respect to said first series of passageways and extending from the top surface thereof between said channel and said boss and communicating with said cavity and a third series of passageways in said metal member arranged circumferentially and spaced with respect to said first and second series of passageways and extending from the sides of said boss through the same and communicating with said cavity.

2. The article set forth in claim 1 and wherein tubular extensions are positioned in said second series of passageways and extend outwardly therefrom and communicate with apertures in said middle one of said three tubular members.

3. The article set forth in claim 1 and wherein notches are formed circumferentially in the bottom of said annular channel to provide a-plurality of passageways therebeneath.

, :1: w :0: m w

Claims

3. The article set forth in claim 1 and wherein notches are formed circumferentially in the bottom of said annular channel to provide a plurality of passageways therebeneath.