[0001 ] The present invention relates to nozzles for casti ng metal beams, such as H-beams and the like. The nozzle of the present invention allows a better control of the metal flow into a mould, yielding metal beams with low defects.

Background for the invention

[0002] In metal forming processes, metal melt is transferred from one metallurgical vessel to another, to a mould or to a tool. For example, as shown in Figure 1 a ladle (1 1 ) is filled with metal melt out of a furnace and transferred to a tund ish (1 0). The metal melt can then be cast through a pouring nozzle (1 ) from the tundish to a mould for forming slabs, billets, beams or ingots. Flow of metal melt out of a metallurgic vessel is d riven by gravity through a nozzle system (1 , 1 1 1 ) located at the bottom of said vessel. In particular, the tundish (1 0) is provided at its bottom floor (1 0a) with a nozzle (1 ) bringing in fluid communication the interior of the tundish with the mould. Some installations make without a tundish and connect the lad le directly to the mould.

[0003] In some cases, two nozzles are used for a single mould in order to ensure optimal filling of the mould and thermal profile of the metal flowing into the mould. This solution may be used for simple rectangu lar profiles, such as in US3931 850, but it is usually used for moulding complex shaped metal parts, such as H-shaped beams or similar. For example, JPH091 22855 discloses a H-beam mould fed by two nozzles located at the intersections between each flange with web of the H-beam (note that the "flange? refer to the two lateral elements of the "H" and the " web' refers to the middle element connecting both flanges ; H- beams are also often referred to as I-beams, the two terms being used herein as synonyms). Using two nozzles for a single mould yields several d rawbacks. First, the production costs are increased since two nozzles are required , instead of a single one. Second, the flow rates of the two nozzles must be well coord inated d uring casting, lest the overall metal feeding flow becomes uneven. This is not easy to achieve. [0004] H-beam casting installations have been proposed comprising a single nozzle per mould, thus solving the drawbacks discussed above associated with the use of two nozzles as described, for example; in JPS58224050, JPH 1 1 51 44, and JPH051 46858. In each of the foregoing documents, a single nozzle comprising an end outlet as well as front ports opening at the peripheral wall of the nozzle is positioned at the intersection between one flange only and the web of the H-mould. Because of its offset position with respect to the mould such nozzles have a more complex front ports design which openings are not distributed around the perimeter of the nozzle symmetrically with respect to a vertical plane as it would be the case in nozzles positioned symmetrically with respect to a mould. They comprise at least a first front port extending substantially parallel to the web, and opening towards the opposite flange of the H-mould. In order to ensure proper filling of the corners of the flange located on the nozzle side, the foregoing nozzles also comprise two front ports forming a Y with the first front port. The front ports usually extend downwards.

[0005] The size of the nozzle is limited by the clearance available at the intersection of the flange with the web of the H-mould, keeping in mind that contact between the nozzle and the mould walls should be avoided, lest solidified metal bridges would form between the nozzle and the cold mould walls. This has consequences on the flow rate achievable by such nozzles, which size of the peripheral wall is limited, thus limiting the size of the axial bore and front ports too. JPH091 22855 proposes a pair of nozzles having a trianglular cross- sectional shape, with rounded corners, in order to optimize the clearance available at the intersection points between each flange and the web of the H-mould. Said nozzles are provided with an end outlet only, also triangular in shape, and comprise no front ports.

[0006] The flow profile and thermal profile of the molten metal filling the mould are of course of prime importance to ensure the production of flawless beams. Both flow and thermal profiles in H-beam moulds are very sensitive to the design of such single nozzles and, in particular, to the number, location, and design of the front ports. For example it is important to ensure a filling of the mould which is stable in time, that avoids as far as possible metal jets hitting a mould wall with excessive momentum, which creates uncontrolled turbulences and rapidly erodes the mould thus decreasing service life thereof. When vortices and turbulences are formed, cooling of the beam becomes more difficult to control and flaws appear.

[0007] It is an object of the present invention to provide a nozzle suitable for filling complex shaped moulds such as H-beams, T-beams, L-beams, C-beams, and the like, yield ing enhanced control of the metal jets penetrating into such mould, resulting in smoother flow and thermal profiles and , ultimately, in metal beams with very low flaw concentrations. This and other advantages of the present invention are presented in the following sections.

Summary of the invention

[0008] The present invention is defined i n the appended independent claims. Preferred embodiments are defined in the dependent claims. In particular, the present invention concerns a submerged nozzle for casting steel comprising : an inlet portion, located at a first end of the nozzle and comprising an inlet orifice;

an elongated portion defined by an outer peripheral wall and extend ing along a first longitudinal axis (XI ) from said inlet portion, or adjacent thereto, to, an outlet portion, located adjacent to and including a second end of the nozzle, opposite the first end, said outlet portion being defined by an outer peripheral wall and comprising a first outlet front port opening on said outer peripheral wall, a bore extending parallel to the first longitudinal axis (XI ) opening at said inlet orifice and extending along the elongated portion of the nozzle and at least partly in the outlet portion of the nozzle whence it opens to the atmosphere at least through said first front port, which extends along a front port direction (Yl ) transverse to said first longitud inal axis (XI ) from a front port inlet joining the bore to a front port outlet opening at the outer peripheral wall of the outlet portion of the nozzle,

wherein a planar cut of the nozzle outlet portion along a plane normal to the first direction (XI ) comprises:

o the outline of the outer peripheral wall of the outlet portion of the nozzle defined by the wall perimeter and the wall centroid of the area defined by said wall perimeter

o a first transverse axis (Y) passing by the bore centroid (50x) and extending along a d irection parallel to the orthogonal projection of the front port direction (Yl ) onto the plane of the cut; wherein,

• the nozzle comprises no front port extending along a direction opposite to the direction of the first front port with respect to the longitudinal axis and belonging to the plane defined by the longitudinal axis (XI ) and the front port direction (Yl ), and in that, in said planar cut:

• the distance (LI ) from the wall centroid to the outer peripheral wall measured along the first transverse axis (Y) on the side of the front port is greater than the same distance (L2) measured on the side opposite the front port; LI > L2.

[0009] The expression "opening to the atmosphere" means opening to the atmosphere surrounding the exterior of the nozzle. If the nozzle front port is inserted in the cavity of a mould, the "atmosphere" refers to the space defined by the cavity of the mould surrounding said nozzle front port. A "front port is used herein in its commonly accepted definition of a port channel in fluid communication with, and extending transverse from the axial bore and comprising an outlet opening at least partially at the nozzle peripheral wall. It includes ports opening partly at the second end of the nozzle, if they also open at the peripheral wall, such as the lower front port in Figure 3.

[001 0] The "centroid" of a plane figure or two-dimensional shape is defined as the arithmetic mean ("average") position of all the points in the shape. In other words, it is the point at which a cardboard cut-out of the region could be perfectly balanced on the tip of a pencil (assuming uniform density and a uniform gravitational field). In geometry the term " barycentef of a two-dimensional figure is a synonym for "centroid, and in physics, the " barycentef and "centroid form a single point for shapes of uniform density only.

[001 1 ] Such geometry allows a substantially deeper penetration of a nozzle in the web direction of a complex shaped mould, such as a H-mould when said nozzle is positioned at the crossing point between a flange and the web of the mould. At the same time, it allows an elongation of the front port channel, which allows a more stable metal flow and a dissipation of momentum thereof as hitherto possible with traditional nozzles having concentric bore and peripheral wall. [001 2] The planar cut further comprises the outline of the bore, defined by the bore perimeter and by the bore centroid of the area defined by said bore perimeter. The bore centroid is preferably located at a d istance to the outer peripheral wall on the side of the front port measured along the first transverse axis (Y) which is greater or equal to LI . [001 3] In order to further promote penetration of the nozzle in the web portion of a mould, it is preferred that the distance (H I ) from wall to wall of the nozzle measured along a direction normal to the axis (Y) at a d istance L/2 from the wall centroid (l x) on the side of the front port (35) is less than the d imension (H2) measured in the same direction at a distance L/2 from the wall centroid (l x) on the side opposite the front port (35); H I < H2. Actually, the wall perimeter is preferably either egg-shaped, with a positive curvature over the whole length of the wall perimeter or, alternatively, is preferably pear-shaped, with the curvature changing sign local ly. The nozzle may have a prismatic geometry throughout the whole length of the elongated and outlet portions (1 B, 1 C), such that LI > L2 over the whole length of the nozzle. Alternatively, LI may be substantially equal to L2 in an upstream portion of the nozzle, excluding the outlet portion, and the outer peripheral wal l changing geometry in a downstream portion of the nozzle, includ ing the outlet portion, such that LI > L2. Depending on the design of the nozzle, the latter embodiment may be useful for reducing the amount of refractory material required.

[001 4] It is preferred that the outlet portion further comprises an end outlet opening at the second end of the nozzle. It is further preferred that the outlet portion further comprises at least one secondary front port extending transversally to both longitud inal axis (XI ) and front port axis, from the bore to the peripheral wall of the outlet portion. It is more preferred that at least two such secondary front ports be provided, forming with the first front port a Y-shape. Better dissipation of the metal flow momentum is obtained when the outlet portion further comprises a second front port extending along an axis comprised within the half- plane defined by the longitudinal axis (XI ) and the front port axis. Such second front port is located either above or below the first front port. [001 5] The first front port may extend normal to the longitudinal axis (XI ) or downwards. In other words, the centroid of the front port outlet can be at the same distance from the nozzle second end as, or closer thereto than the centroid of the front port inlet.

[001 6] The present invention also concerns a casting installation for casting metal beams comprising

(a) A metallurgical vessel provided with at least one submerged nozzle as defined above with the inlet orifice thereof being in fluid communication with the interior of the metallurgical vessel ; and wherein the bore with the first front port extend out of said metallu rgical vessel and penetrating in,

(b) A beam blank mould defining a cross-section divided in at least a first elongated portion extending along a fi rst mould direction and at least a second elongated portion, extending along a second mould d irection transverse to the first mould direction.

Characterized in that, said first mould direction is comprised within the plane defined by the first longitudinal axis (XI ) and the front port direction (Yl ) and is preferably normal to the first longitudinal axis, XI .

[001 7] The blank beam mould in the casting installation of the present invention may have a T-cross-section, an L-cross-section, an X-cross-section, a C-cross-section, or a H-cross- section. The blank beam mould preferably has a H-cross-section with the web of the H being defined by the first elongated portion, and the two lateral flanges being defined by the second elongated portion and a thi rd elongated portion, both substantially normal to the second elongated portion, and wherein said submerged nozzle is positioned at the area intersecting a flange and the web of the H-beam cross-section. The casting installation of the present invention preferably comprises a single submerged nozzle per blank beam mould.

Brief description of the Figures

[001 8] For a fuller understand ing of the nature of the present invention, reference is made to the following detailed description taken in conjunction with the accompanying drawings in which : Figure 1 : represents a general view of a casting installation for casting a metal beam.

Figure 2 : shows an example of nozzle accord ing to the present invention inserted in a H- mould.

Figure 3 : shows an embod iment of nozzle accord ing to the present invention. Figure 4: shows cross-sectional views of the nozzle portion of nozzles accord ing to the present invention.

Figure 5 : shows embodiments of the outlet portion of nozzles accord ing to (a) prior art and (b)-(g) the present invention.

Figure 6: compares the front port length of a nozzle of the prior art with nozzles according to the present invention.

Figure 7: illustrates how to determine experimental ly the position of the wall centroid.

Detailed description of the invention

[001 9] As i llustrated in Figure 3, a nozzle accord ing to the present invention can be d ivided i nto three main portions: · an inlet portion (1 A), located at a first end of the nozzle and comprising an inlet orifice (1 8);

• an elongated portion (I B) defined by an outer peripheral wal l and extending along a first longitudinal axis (XI ) from said inlet portion (1 A), or adjacent thereto, to,

· an outlet portion (1 C), located adjacent to and includ ing a second end of the nozzle, opposite the first end, said outlet portion being defined by an outer peripheral wall and comprising a first outlet front port (35) opening on said outer peri pheral wall.

[0020] The nozzle further comprises a bore (50) extending parallel to the first longitudinal axis (XI ) opening at said inlet orifice (1 8) and extending along the elongated portion (1 B) of the nozzle and at least partly in the outlet portion (1 C) of the nozzle whence it opens to the atmosphere at least through said first front port (35), which extends along a front port direction (Yl ), transverse to said first longitud inal axis (XI ) from a front port inlet (35 i) joining the bore (50) to a front port outlet (35o) opening at the outer peripheral wall of the outlet portion of the nozzle.

[0021 ] Because a nozzle according to the present invention is particularly suitable for casting complex shapes, like H-beams, using a single nozzle per mould, which is located offset with respect to the plane of symmetry of the mould normal to the web, typically at the intersection of a flange (1 OOf) and the web (1 OOw) of the mould (1 00), the metal should not flow out of the nozzle front ports symmetrically with respect to a vertical plane passing by the longitudinal axis, XI . In particular, the first front port (35) is designed to extend, when in use, in a direction parallel to the mould web, and oriented away from the flange at which intersection with the web said nozzle is located. Because of the proximity of the outer wall (l OOf-out) of the mould flange located "behind" the nozzle front port (35) (cf. Figure 6(d) & (e)), a nozzle according to the present invention comprises no front port extending along a direction opposite to the direction of the first front port (35) with respect to the longitudinal axis and belonging to the plane defined by the longitudinal axis (XI ) and the front port direction, Yl .

[0022] In a planar cut of the nozzle outlet portion (1 C) along a plane normal to the first direction (XI ) passing through the front port inlet (35 i), the following features can be identified:

o the outline of the outer peripheral wall of the outlet portion (1 C) of the nozzle defined by the wall perimeter (1 P) and the wall centroid (1 x) of the area defined by said wall perimeter

o a first transverse axis (Y) passing by the bore centroid (50x) and extending along a direction parallel to the orthogonal projection of the front port direction (Yl ) onto the plane of the cut. [0023] It is essential that the distance (LI ) from the wall centroid (l x) to the outer peripheral wall measured along the first transverse axis (Y) on the side of the front port (35) is greater than the same distance (L2) measured on the side opposite the front port (35); LI > L2. LI is preferably at least 5% greater than L2, more preferably at least 1 0% greater than L2, most preferably at least 20% or even at least 40% greater than L2, wherein the percentage is calculated as (LI - L2) / L2 x 1 00. This geometry implies a thinning of the cross-sectional shape of the nozzle in the direction of the front port (35), such that it can better fit into the somewhat restricted area defined by the intersection between a first and a second elongated mould portions defining a beam profile having, e.g., a H-, L-, T-cross-section, or the like. The "thinning" of the nozzle cross-section at the level of the first front nozzle can also be expressed by defining the distance (H I ) from wall to wall of the nozzle measured along a direction normal to the axis (Y) at a distance L2 /2 from the wall centroid (l x) on the side of the front port (35), which must be less than the wall to wall distance (H2) measured in the same direction at a distance L2 /2 from the wall centroid (l x) on the side opposite the front port (35); HI < H2. Figure 4 shows the dimensions (LI ) H I and L2, H2 in nozzle cross- sections according to two embodiments of the present invention, (a) an egg-shaped cross- section and (b) a pear-shaped cross-section.

[0024] In an egg-shaped cross-section, the curvature of the wall perimeter is positive over the whole length of the perimeter, which characterizes a convex shape. An egg-shaped cross-section as meant in the present invention comprises a "fat" end and a "lean" end and should not be confused with an elliptical cross-section, having two identical ends and which does not fall within the scope of the present invention. Indeed, the centroid of an ellipse is located at the intersection between major and minor diameters thereof, so that LI = L2 and HI = H2 in an ellipse. The wall perimeter of nozzles according to the present invention comprises at most one axis of symmetry, but never two as is the case of ellipses. The cross- sectional shape of nozzles according to the present invention having a convex cross- sectional perimeter is not restricted to egg-shapes and could be devoid of any axis of symmetry. However, an egg-shape or oval-shape (from ovum in Latin) symmetrical with respect to the first transverse axis (Y) is preferred.

[0025] Alternatively, the wall perimeter may comprise convex and concave portions, the latter being characterized by a negative curvature. A preferred embodiment of this type is a pear-shaped cross-section, symmetrical with respect to the first transverse axis, Y of the type illustrated in Figures 4(b), 5(c), and 6(a), (d), (e). A pear like shape is characterized by a "fat" convex end separated from a "lean" convex end by a concave portion. A pear-like cross-section fits quite well at the intersection zone between a flange and the web of a H- beam mould, as illustrated in Figure 6(d). Figure 6(e) shows a slight variation to a pear- shaped outer peripheral wall wherein two opposite circular segments of different diameters are joined by straight lines. The front port opens at the circular segment of smaller diameter.

[0026] It is clear that the wall perimeter may comprise straight sections, which are only singular embodiments of convex or concave curvatures, with an infinite radius and a zero- curvature. An example of such cross-sectional shape is illustrated in Figure 5(e), which looks like a thin egg or a fat pear.

[0027] As illustrated in Figure 6(d), providing a nozzle characterized by LI > L2 allows a deeper penetration of the first front port (35) in the web of e.g., a H-beam blank mould while maintaining the same clearance, δ, between nozzle and mould walls as compared with a traditional mould having equal LI and L2. Figure 6(e) shows a further embodiment of an outer peripheral wall giving enhanced clearance between the mould walls and the nozzle peripheral wall.

[0028] The peripheral wall may be characterized by LI > L2 only in the outlet portion (1 C), or over it may extend over part or the whole length of the nozzle. In the former case, LI may be equal to L2 in a portion of the nozzle upstream from the outlet portion (1 C) (the terms "upstreani' and " downstream" refer to the flow direction through the nozzle when in use, said flow starting from the nozzle inlet (1 8) and ending at the front port outlet (35o)). Any length of the elongated portion (I B) of the nozzle may be characterized by LI > L2 without departing from the scope of the present invention, as long as the portion of the nozzle which is inserted in the mould can fit in the corresponding space.

[0029] Since LI and L2 are measured with respect to the wall centroid (l x) it is important to define said centroid properly. As discussed above, the "centroid (l x) of an area is herein used in its traditional geometrical definition of the arithmetic mean ("average") position of all the points in the area, which is equivalent to the barycenter of the area having homogeneous density (i.e., ignoring that the refractory density is higher than the bore density). For simple figures such as circles or ellipses, having two axes of symmetry the position of the centroid is easy to determine. For less regular geometries, however, having one or no axis of symmetry as is the case with the wall peri meter of nozzles accord ing to the present invention, it is not always straightforward to calculate or determine geometrically the position of the centroid. Figure 7 illustrates how to experimentally determine the position of the centroid of any two dimensional shape. The outline of the peripheral wall is cut out from cardboard. To ensure uniform density of the lamina, the bore position should not be cut out of the cardboard representing the shape of the peripheral wall . In Figure 7, the outline of the peripheral wall of the nozzle discussed in Figures 4(b) and 6(d) is represented, with the position of the circular bore indicated with a dashed circle (not cut out, though). The cardboard lamina is then held by a pin (= white circle) i nserted at a first point near the lamina perimeter, in such a way that it can freely rotate around the pin ; and a plumb line is dropped from the pin (cf. Figure 7(a)). The position of the plumb line is marked on the body (cf. dashed line in Figure 7(b)). The experiment is repeated with the pin inserted at a different point of the lamina (cf. Figure 7(b)). The intersection of the two lines is the wall centroid (l x) (cf. black circle in Figure 7(b)). This empirical method allows the determination of the centroid of any surface in a simple and reliable way.

[0030] Besides the outer peripheral wall outline and the first transverse axis (Y) the planar cut further comprises the outline of the bore (50), defined by the bore perimeter (50P) and by the bore centroid (50x) of the area defined by said bore perimeter. The bore centroid (50x) is located at a distance, L' l to the outer peripheral wall on the side of the front port (35) measured along the first transverse axis (Y) which is preferably greater or equal to LI (L' l > LI ). The wall centroid (l x) and the bore centroid (50x) may be located at the same point (i.e., L' l = LI ), preferably on the first transverse axis, Y. In this case, a nozzle according to the present invention characterized by LI > L2 has the advantage that the first front port (35) can be longer than in a traditional nozzle with LI = L2. The first front port length, UNV, can be even further prolonged if the centroid (50x) of the bore on such cut plane is offset with respect to the wall centroid (l x) such that the first transverse axis (Y) starting from said bore centroid (50x), passes through the wall centroid (l x) and extends until it reaches the wall perimeter (I P) (i.e., L' l > LI ). This is illustrated in Figures 6(a)-(d), comparing the length, UNV, of the first front port in nozzles accord ing to the present invention (cf. lower halves of Figures 6(a)-(d)) compared with the length, LPA, of a traditionally "co-axial" nozzle (cf. upper halves of Figures 6(a)-(d)). The cross-section of Figure 6(a) corresponds, e.g., to the nozzle illustrated in Figure 5 (c), the one of Figure 6(b) corresponds to a nozzle as illustrated in any of Figures 5 (b)&(d), and the cross-section of Figure 6(c) corresponds to a nozzle as illustrated, e.g., in Figure 5 (g) with a thinning of the bore (50) in the outlet portion (1 C) of the nozzle. One unique advantage of nozzles according to the present invention is that the length, UNV, of the first front port (35) can be extended substantially while keeping the necessary clearing, δ, with the mould walls.

[0031 ] Extending the length of the first front port (35) has multiple advantages. First, it creates a substantially more stable metal melt flow out of the first front nozzle, jetting out at a relatively long distance along the mould web section and creating substantially less turbulences than shorter front ports. Second, as illustrated in Figure 6(d), the front port outlet (35o) of a nozzle according to the present invention (lower half) extends deeper into the mould web section than a traditional "co-axial" nozzle (upper half), thus reducing the distance the metal jet must cover to fill the mould properly. Third, a longer front port (35) reduces the momentum of the metal flow, thus decreasing the impact force of the jet against the outer flange wall (1 OOf-out) of the mould flange opposite the nozzle. This is important, since the impacting flow creates turbulences and rapidly erodes the flange outer wall of the mould. Finite element modelling (FEM) or computational fluid dynamics (CFD) show that high sub-meniscus velocities in the mould increase the risk of mould level fluctuations and of flow detachment at the level of the radii between web and flange opposite to the nozzle. The lowest sub-meniscus velocities were obtained with nozzles according to the present invention, due to enhanced momentum dissipation along the longer first front port (35).

[0032] The front port direction (Yl ) along which extends the first front port (35) may be normal to the first long itudinal axis, XI . This would correspond to a horizontal front port (35) as illustrated in Figure 5(d), wherein the term "horizontal" is used with respect to the position of the nozzle in use. Alternatively, the front port direction (Yl ) may be transverse but not normal to the first longitudinal axis, XI . In particular, the first front port (35) may extend downwards (with respect to the position of the nozzle in use) such that the centroid of the front port outlet (35o) is closer to the nozzle second end than the centroid of the front port inlet (35 i). If the first front port (35) is inclined (i.e., if the front port direction (Yl ), is not normal to the longitudinal axis, XI , it is possible that the front port outlet (35o) be out of the cut plane. This is the case, e.g., in Figure 5(b), (c), (e)-(g), wherein the cuts B-B are made on two parallel planes for sake of clarity, such as to show the whole length of the first front port (35) from inlet (35 i) to outlet (35o).

[0033] For a proper filling of complex shaped moulds, a single front port may not be sufficient. A nozzle according to the present invention may therefore further comprise an end outlet (37) opening at the second end of the nozzle (cf. Figures 3 and 5(b), (c) & (f))- An end outlet (37) is formed by a channel in fluid communication with the longitudinal bore and opening exclusively at the second end of the nozzle. If a channel opening extends partly at the second end and partly at the peripheral wall of the nozzle, it is referred to as a front port (cf. e.g., Figure 3). It may also comprise at least one secondary front port (39a, 39b) extending transversally to the longitudinal axis (XI ) and front port direction (Yl ), from the bore (50) to the peripheral wall of the outlet portion (1 C). For a H-mould as illustrated in Figures 1 and 2 , the nozzle preferably comprises two secondary front ports (39a, 39b) forming with the first front port (35) a Y centred on the bore such that the flange adjacent the nozzle may be filled with metal melt as illustrated in Figures 3 and 5(f)-

[0034] Further dissipation of the flow momentum and enhanced flow stability may be obtained by providing the nozzle with a second front port (36) extending along an axis comprised within the half-plane defined by the first longitudinal axis (XI ) and the first transverse axis, Y. In other words, as illustrated in Figure 5(c), a second front port (36) can be located above or below the first front port (the terms "above" and "below" being used herein with respect to the nozzle position in use). The second front port (36) can be parallel or not to the first front port (35). In a variation of the present embodiment, the first and second front ports (35, 36) may be connected by a thinner channel as illustrated in Figure 3, conferring a dog-bone shape to the front ports outlets.

[0035] A nozzle according to the present invention is advantageous in use with an installation for casting metal beams as illustrated in Figure 1 and comprising: (a) A metallurgical vessel (1 0, 1 1 ) provided with at least one submerged nozzle (1 ) according to the present invention with the inlet orifice (1 8) thereof being in fluid communication with the interior of the metallurgical vessel ; and wherein the bore (50) with the first front port (35) extends out of said metallurgical vessel and penetrating partially in,

(b) A beam blank mould (1 00) defining a cross-section divided in at least a first elongated portion extending along a first mould direction and at least a second elongated portion, extending along a second mould d irection transverse to the first mould direction. wherein, said first mould direction is comprised within the plane defined by the first longitudinal axis (XI ) and the front port direction (Yl ) and is preferably normal to the first longitud inal axis, XI .

[0036] The blank beam mould can have a T-, an L-, an X-, a C-, a H- or similar cross- section. In case of a H- or a C-cross-section, the web of the H or C being defined by the first elongated portion, and the two lateral flanges of the H or C bei ng defined by the second elongated portion and a third elongated portion, both substantially normal to the first elongated portion. One single such submerged nozzle for each mould is sufficient and is preferably positioned at the area i ntersecting the web and a flange of the H- or C-beam cross-section. Similarly, in case of T-, L-, or X-cross-sections, a single nozzle can be used for each mould, and is preferably positioned at the intersecting area between the first and second elongated portions of the mould.

[0037] A nozzle accord ing to the present i nvention permits a better control of the metal jet flowing out thereof into complex shaped moulds for producing beams and the like. With the greater length, UNV, of the first front port (35) than hitherto possible. This has the advantages of enhanced flow momentum d issipation as well as higher stability and lower velocity of the outpouring metal jet. This in turn prevents flow disruption at the rad ii of complex shaped moulds, as well as decreasing the formation of vortices and dead zone, responsible for many defects i n cast beams. A nozzle according to the present invention also permits to increase the clearance between the outer peripheral wall of the outlet portion and the mould wal ls, thus red ucing the risk of solidified metal bridges between the nozzle and the mould walls.