Fluid cooled coherent jet lance

Metallurgical apparatus – Means for melting or vaporizing metal or treating liquefied... – By means introducing treating material

Reexamination Certificate

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Details

C266S268000

Reexamination Certificate

active

06334976

ABSTRACT:

TECHNICAL FIELD
This invention relates generally to coherent jet technology.
BACKGROUND ART
A recent significant advancement in the field of gas lancing is the development of the coherent jet technology disclosed, for example, in U.S. Pat. No. 5,814,125—Anderson et al. In the practice of this technology, a high velocity gas jet ejected from a lance is maintained coherent over a relatively long distance by the use of a flame envelope around and coaxial with the high velocity gas jet. The flame envelope is generated by combusting respective streams of fuel and oxidant which are each annular to the ejected high velocity gas jet. The resulting coherent jet can be used to deliver gas into a liquid, such as molten metal, from a relatively long distance above the surface of the liquid. One very important application of this coherent jet technology has been for providing oxygen for use in an electric arc furnace.
It is desirable to employ coherent jet technology in other steelmaking operations such as basic oxygen furnaces. The potential for using coherent jet technology in a basic oxygen furnace and other large scale applications would be enhanced if the coherent jets were made longer.
Accordingly it is an object of this invention to provide a lance which may be used to provide a coherent gas jet which may be longer than comparable heretofore known coherent jets.
SUMMARY OF THE INVENTION
The above and other objects, which will become apparent to those skilled in the art upon a reading of this disclosure, are attained by the present invention which is:
A lance for providing at-least one coherent jet comprising:
(A) a main passageway communicating with at least one nozzle for providing main gas from the lance;
(B) a first annular passageway coaxial with and radially spaced from the main passageway for flow of cooling fluid;
(C) a second annular passageway coaxial with and radially spaced from the first annular passageway for flow of first flame envelope fluid;
(D) a third annular passageway coaxial with and radially spaced from the second annular passageway for flow of second flame envelope fluid;
(E) a fourth annular passageway coaxial with and radially spaced from the third annular passageway for flow of cooling fluid; and
(F) at least one flow passage for flow of cooling fluid between the first annular passageway and the fourth annular passageway.
As used herein the term “coherent jet” means a gas jet which has a velocity profile for a considerable distance downstream of the nozzle from which it was ejected which is similar to the velocity profile which it has upon ejection from the nozzle.
As used herein the term “annular” means in the form of a ring.
As used herein the term “flame envelope” means an annular combusting stream coaxial with the main gas stream.
As used herein the term “length” when referring to a coherent gas jet means the distance from the nozzle from which the gas is ejected to the intended impact point of the coherent gas jet or to where the gas jet ceases to be coherent.
As used herein the term “axis” means the imaginary line running longitudinally through the center of a lance.


REFERENCES:
patent: 3427151 (1969-02-01), Koudelka et al.
patent: 4488682 (1984-12-01), Kobayashi et al.
patent: 4622007 (1986-11-01), Gitman
patent: 5714113 (1998-02-01), Gitman et al.
patent: 5814125 (1998-09-01), Anderson et al.
patent: 5823762 (1998-10-01), Anderson et al.
patent: 6096261 (2000-08-01), Anderson et al.
patent: 866139 (1998-09-01), None
patent: 874194 (1998-10-01), None

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