EP0561256A1

EP0561256A1 - Method in contact-free air-drying of a material web as well as a nozzle-blow-box and a pulp dryer that make use of the method

Info

Publication number: EP0561256A1
Application number: EP93103768A
Authority: EP
Inventors: Pertti Heikkilä; Iikka Jokioinen
Original assignee: Valmet Paper Machinery Inc
Current assignee: Valmet Technologies Oy
Priority date: 1992-03-19
Filing date: 1993-03-09
Publication date: 1993-09-22
Anticipated expiration: 2013-03-09
Also published as: KR0172974B1; BR9301228A; JPH06248593A; DE69330413T2; DE69330413D1; FI921193A0; CA2092004C; FI921193A; ATE203071T1; JP3305802B2; FI92421B; KR930019930A; ES2159510T3; CN1081485A; CA2092004A1; CN1031656C; EP0561256B1

Abstract

The invention concerns a method in air-drying of material webs, in particular of material webs of relatively high grammage, such as pulp webs. Also, the invention concerns a nozzle-blow-box and a pulp dryer that make use of the method. To the web (W) to be dried, from underneath the web, air blowings (B₂) substantially perpendicular to the web and air blowings (B₃) substantially parallel to the plane of the web (W) are applied. By means of these blowings (B₂,B₃), both heat is transferred to the web (W) and the web is supported by air free of contact, and the run of the web through the dryer is stabilized. In order to improve the transfer of heat in comparison with a plane carrier face (FIG. 7C; 31c), the air flow velocity parallel to the plane of the web (W) to be dried and air-supported in connection with the nozzle-carrier face (31) is initially (34) kept substantially invariable, whereupon the air flow velocity is lowered in the lateral areas (35;35b;35d;35e) of said carrier face (31) by employing lateral areas (35, 35b,35e) of the nozzle-carrier face (31) that become rampwise and/or stepwise lower in the air-flow direction.

Description

The invention concerns a method in air-drying of material webs, in particular of material webs of relatively high grammage, such as pulp webs, in which method, to the web to be dried, from underneath the web, air blowings substantially perpendicular to the web and air blowings substantially parallel to the plane of the web are applied, by means of which blowings both heat is transferred to the web and the web is supported by air free of contact, and the run of the web through the dryer is stabilized.
Further, the invention concerns a nozzle-blow-box of an air dryer, through which box air blowings are applied to the material web to be dried, by means of which blowings both transfer of heat is produced from the drying air to the web and contact-free air support and stabilization of the run of the web are obtained, said nozzle-blow-box comprising a box part, in which there is a nozzle-carrier face placed against the web, in the middle of which face there is a substantially V-section groove transverse to the running direction of the web, which groove is opened towards the web and in whose opposite walls there are series of nozzle holes so that, out of said series of nozzle holes, support and stabilization air blowings can be applied which are cross-wise and of opposite directions in relation to each other, and in which nozzle-carrier face, at both sides of its V-section groove, there are plane nozzle-carrier-face portions placed in the same plane with each other.
Further, the invention concerns a pulp dryer that makes use of the method of the invention and/or of the nozzle-blow-box of the invention.
In through-dryers in paper and pulp industry, blow boxes are commonly used whose nozzle-carrier face consists of a plane plate, into which blow holes have been punched. Such nozzles are placed either at one side or at both sides of the airborne web to be dried. The nozzle-carrier-face commonly includes a number of rows of holes, one row after the other in the running direction of the web. The blow air flows in the space between the web and the nozzle-carrier-face, and the blow air is collected away through suction slots placed between the nozzle boxes.
In the prior-art direct-blow nozzle boxes of air dryers for paper, board or pulp web, in which boxes the blowing of air is directed perpendicularly to the material web to be dried, a well-known problem is the lateral flow of the consumed air between the web to be dried and the nozzle-carrier-face. Above and in the following, the term "lateral flow" is understood as meaning air flows parallel to the plane of the carrier face and of the web, which flows are additionally parallel to or opposite to the running direction of the web. Since the air must escape from the treatment gap, a lateral flow cannot be avoided. Said lateral flow deteriorates the transfer of heat in the prior-art blow-nozzle boxes, and the disturbing effect is increased with an increase in the velocity of the exhaust-air flow. Further, the loss of pressure produced by the blow box is increased when the velocity increases in the lateral flow. On the other hand, in view of the runnability of the web to be dried, in the blow box, it is preferable to make use of the lateral flow by shaping the blow face and the geometry of its nozzle openings such that, on the carrier face of the blow box, a zone of negative pressure is formed, which stabilizes the run of the web and by whose means a stable and unstrained run of the web is ensured.
With respect to the prior art most closely related to the present invention, reference is made to the SE Patent No. 8,106,152 of Messrs. Fläkt AB (equiv. US Pat. 4,505,053) as well as to the International Patent Application WO 88/08950 of K. Krieger (equiv. US Pat. 5,016,363). The object of the present invention is further development of the prior-art nozzle-blow-boxes disclosed in said patents while avoiding the drawbacks which are present in them and which will be described in more detail later.
In the blow boxes described in said SE patent, triangular openings, so-called "fish eyes", have been punched into their plane nozzle-carrier-face, at which openings the front edge, i.e. the base of the triangle, has sharp edges. A sharp edge is not a major drawback as long as the amount of air discharged out of the nozzle is sufficient. At times, the amount of air received by the nozzle may be reduced considerably from the dimensioned value, for example, if the filters for drying air are blocked, in which case the web starts reaching contact with the nozzle face. It has been noticed that said sharp edges plane material out of the face of, e.g., a pulp web, in which case both the quality of the finished product is deteriorated and rubbish remains in the dryer. On the other hand, the rubbish disturbs the threading of the pulp web. Formation of a "cigar" is spoken of, for the material detached out of the face of the pulp web by planing forms a roll resembling the structure of a cigar.
The present invention is above all related to the nozzle-blow-boxes employed in pulp dryers, in which the web runs above the nozzle and carrier faces of the boxes. The function of the air blowings is both to transfer heat from the blown air to the web and to support the web free of contact. In view of the runnability of the web, it is preferable to blow part of the air parallel to the plane of the nozzle, in which case the web is stabilized at a distance of 3...6 mm from the carrier face. In such a case, however, in the prior-art nozzle-blow-boxes, the velocity of the exhaust air in the space between the web and the nozzle becomes high. This results in deterioration of the transfer of heat and in extra pressure losses. The detrimental effect of the high velocity of the exhaust air can be reduced by making the nozzles sufficiently narrow, but then the number of the nozzles becomes so high that the cost of manufacture of the dryer is increased substantially.
An object of the present invention is to provide a novel method and a novel nozzle-blow-box construction by whose means it is possible to avoid the drawbacks discussed above and to improve the transfer of heat from the drying air to the airborne web to be dried. Said improvement of the transfer of heat can be utilized most efficiently in the form of smaller size of the dryer. In this way, the cost of construction, e.g., of a pulp dryer and the cost of the machine hall can be lowered decisively.
An object of the present invention is to reduce the effect of deteriorating of the transfer of heat by the lateral flow while the run of the web is stabilized by means of said flow.
In view of achieving the objectives stated above and those that will come out later, the method of the invention is mainly characterized in that, in order to improve the transfer of heat in comparison with a plane carrier face, the air flow velocity parallel to the plane of the web to be dried and air-supported in connection with the nozzle-carrier face is initially kept substantially invariable, whereupon the air flow velocity is lowered in the lateral areas of said carrier face by employing lateral areas of the nozzle-carrier face that become rampwise and/or stepwise lower in the air-flow direction.
On the other hand, the nozzle-blow-box in accordance with the invention, is mainly characterized in that extensions of said nozzle-carrier-face portions are constituted by stepwise and/or ramp-shaped carrier-face portions placed further apart from the material web to be supported, in the area of which carrier-face portions the velocities of said support and stabilization air flows, as compared with the velocity prevailing in connection with the plane nozzle-carrier-face portions, are lowered, and that the nozzle-carrier face is provided with nozzle perforations, through which additional blowings substantially perpendicular to the plane of the material web to be supported can be applied from the nozzle-blow-box.
By means of the invention, the effect of deteriorating of the transfer of heat by the lateral flow has been minimized by lowering the lateral portions of the nozzle to a level lower than the plane middle portion, whereby the velocity of the lateral flow is lowered. Moreover, the lateral flows are preferably directed so that they do not directly collide against the air jets of the direct blowing on the plane face or on the lowered lateral portions.
The lowering of the lateral areas of the nozzle-carrier-face portions in accordance with the invention is based on the idea that a high flow velocity of the exhaust air between the web and the nozzle-carrier face deteriorates the coefficient of heat transfer. The lower the space between the web and the nozzle-carrier face, the higher becomes the velocity of the exhaust air. The velocity of the exhaust air is increased in both directions from the centre line of the nozzles towards the edges when more air is introduced. When the lateral areas of the nozzle-carrier-face are lowered in accordance with the present invention, the flow velocity in this area is lowered.
The nozzle-blow-box in accordance with the invention is a combination of a nozzle with positive/negative pressure, in which the magnitude of the lateral flow that produces the negative pressure is chosen appropriately in relation to the amount of air in the direct blowing.
It is characteristic of the hole-nozzle field in accordance with the invention in the carrier face that, with the very little nozzle-to-web distances with which the nozzles of the present invention operate, the coefficient of heat transfer is not essentially dependent on the distance, provided that the exhaust air does not disturb the air jets blown out of the nozzle holes to a significant extent. On the other hand, it is well known that, when there are several rows of nozzle holes, one row after the other, the air discharged out of the nozzles must pass towards the edges in the space between the nozzle and the web, and the higher this flow velocity is, the more does it disturb the air jets blown out of the holes and the more does it deteriorate the coefficient of heat transfer.
In a preferred embodiment of the nozzle-blow-box in accordance with the invention, from the walls of a V-section groove placed in the middle of the nozzle face, air jets are directed, crosswise in relation to one another, at continuous rounding points between the plane carrier face placed at each side of the walls of said V-section groove. As the air jets are tangential to the rounding points, they turn and become parallel to the plane portions of the carrier face by the Coanda effect. Between the web and the carrier faces, in accordance with the Bernoulli principle, a zone of negative pressure is formed, which stabilizes the web at a certain distance from the carrier face, as a rule, of an order of 3...6 mm. Also on the horizontal part of the carrier face, in the invention, attempts are made to avoid direct collisions between the jets of direct blowing and the air jets that flow in the lateral direction.
According to the invention, the lateral areas of the nozzle-carrier face of the nozzle-blow-box have been lowered so that the velocity of the lateral flow is lowered as the cross-sectional flow area becomes larger, whereby the heat-transfer effect of the blow jets coming from the holes of direct blowing placed in the lowered inclined and/or straight nozzle-carrier-face portion is improved.
The nozzle-blow-box in accordance with the invention is suitable for use for drying of the web both in one-sized/two-sided drying, in the case of low-grammage webs (< 200 g/sq.m), and both underneath and above the web. In the case of heavy webs, such as pulp webs, the nozzle-blow-boxes in accordance with the invention are best suitable for lower nozzles together with direct-blow boxes that operate as upper nozzles, or alone as lower nozzle boxes in one-sided drying.
A further advantage that is achieved by means of the geometry of the blow-carrier faces of the nozzle-blow-boxes in accordance with the invention is a smooth blow face with no sharp edges, as the air of the lateral flow is introduced out of the central V-section groove while guided by rounded faces.
Since, according to the invention, as is indicated by measurements that have been carried out and that will be described in more detail later, the transfer of heat to the web can be improved by about 5...10 %, this improvement can be taken to useful use immediately in the form of reduced size of the dryer, which lowers the cost of investment of the dryer and of the machine hall substantially, and which also, indirectly, reduces the number of production interruptions and improves the operating time ratio of the dryer. The advantages mentioned above are particularly important in the case of large and complicated pulp dryers.
In a nozzle-blow-box in accordance with the invention, when a V-section groove is used in the middle of its carrier face, through which groove the blowings parallel to the carrier face are applied crosswise, in addition to a favourable blow/heat-transfer technique, a rigid mechanical construction is obtained, in which the V-section groove rigidifies the nozzle-carrier-face efficiently without any other rigidifying structures, which would be necessary otherwise.
It is a minor drawback of the blow face of the blow box in accordance with the invention that it is somewhat more difficult to manufacture than a uniform plane face. This drawback can, however, be solved by means of development of the manufacturing technology.
In the following, the invention will be described in detail with reference to some preferred embodiments of the invention illustrated in the figures in the accompanying drawing and to test results related to said embodiments.
Figure 1 is a schematic vertical sectional view in the machine direction of a pulp dryer that makes use of the method and of a set of nozzle-blow-boxes in accordance with the invention.
Figure 2 is an axonometric view of the modular construction of a pulp dryer that makes use of the method and of a set of nozzle-blow-boxes of the invention.
Figure 3 is a schematic vertical sectional view in the machine direction of a set of nozzle-blow-boxes in accordance with the invention and of a set of boxes of direct blowing placed above said set of boxes.
Figure 4 is an axonometric illustration of a nozzle-blow-box in accordance with the invention and of the principle of its blowings.
Figure 5 is an axonometric view of the construction of an upper direct-blow box.
Figure 6 shows an embodiment of a carrier face of a nozzle-blow-box in accordance with the invention and of the blow nozzles of said carrier face in more detail, together with the most important parameters of dimensioning.
Figures 7A, 7B, 7C, 7D, and 7E illustrate different variations of different embodiments and dimensions of bevel and step formations of the nozzle-carrier faces of a nozzle-blow-box in accordance with the invention and of a nozzle-blow-box of reference.
Figure 8A shows a nozzle-blow-box as shown in Figs. 4 or 5, seen from the side of the nozzle-carrier face.
Figure 8B is an enlarged schematic vertical sectional view in the machine direction of a preferred geometry and dimensioning of the V-section groove of the nozzle.
Figure 9 illustrates different relative coefficients of heat transfer in the cases illustrated in Figs. 7A to 7E as a function of the distance of the web at a first air-blow velocity.
Figure 10 illustrates the corresponding measurement results in a way corresponding to Fig. 9, at a second, higher air-blow velocity.
Fig. 1 is a schematic vertical sectional view in the machine direction of a pulp dryer that makes use of the method and of a set of nozzle-blow-boxes in accordance with the invention. The dryer comprises a closed hood 12, in whose interior there is a set of nozzle-blow-boxes 30 in accordance with the invention and, placed facing said set of boxes, a set of boxes 40 of direct blowing, the web W to be dried being passed through the treatment gaps 25 formed by said sets of boxes as supported by air free of contact. The pulp web W_in or equivalent that is passed into the dryer is passed through the wet press 10 and over the roll 11 for regulation of the tension of the web, through an inlet opening 12a, into the hood 12, in which the web W to be dried runs as horizontal draws back and forth, being guided by guide rolls 13. The dried web W is removed through an outlet opening 12b placed in the bottom part of the hood 12, being passed by the intermediate of an alignment roll 14 through a set of drive rolls 15 further (W_out). In Fig. 1, the path of the web threading belt or rope is illustrated by the reference numeral 16 and by the dashed-dotted line.
In Fig. 1, the circulation of drying air taking place inside the hood 12 is illustrated schematically by means of arrows A₁...A₂. The arrows A₁ and the air ducts 17 placed in connection with them represent the introduction of replacement air from the heat recovery, and the arrows A₂ and the air ducts 18 placed in connection with them represent the passage of the exhaust air to the heat recovery.
Fig. 2 illustrates the modular construction of a pulp dryer that makes use of the method and of a nozzle-blow-box in accordance with the invention and whose basic principle is, e.g., similar to that illustrated in Fig. 1. The dryer-blower module comprises blower towers 21 and blowers, which are provided with blade wheels 22. The module construction comprises heating radiators 24, through which the blow air is passed into the gap between the upper nozzles and the lower nozzles, i.e. into the web gap 25. Further, the module construction includes air filters 26. At the operating side of the blower module, there is a tending bridge 28, in connection with which there are servicing gates 27 for the blower motors and servicing doors 29 for the blower modules. Fig. 2 shows the circulation of the drying air as illustrated by the arrows, and also the nozzle-blow- boxes 30,40 in accordance with the invention and the web gaps 25 between them.
With respect to Figs. 1 and 2, it is to be emphasized that, above, they have been described just as one field of application of the method and of the set of nozzle-blow- boxes 30,40 in accordance with the invention and that the method and the set of nozzle-blow- boxes 30,40 in accordance with the invention can also be applied in a great number of other environments and also in other than pulp dryers, for example in board and paper-web dryers, even though the pulp dryers are the most advantageous and primary field of application of the invention, in which several different advantages of the invention are best used for a useful purpose.
Fig. 3 is a schematic illustration of a set of nozzle-blow-boxes 30 in accordance with the invention and of an opposite set of boxes 40 of direct blowing. In the following, the shorter name "lower box" will be used for the nozzle-blow-boxes 30, because they are preferably placed underneath the horizontally running web W. Between the lower boxes 30, there are free spaces 30a, and, in a corresponding way, between the direct-blow boxes 40, there are free spaces 40a. Through the spaces 30a and 40a, the blow air is passed further through the healing radiators 24 shown in Fig. 2, being carried by the blower 22, back to the blow boxes. As is shown in Fig. 3, the web W to be dried, typically a pulp web, runs as a horizontal run through the web gap 25. The web gap 25 is defined from below by the lower boxes 30, which are placed as uniformly spaced in one horizontal plane, and from above by the direct-blow boxes 40, which are placed as uniformly spaced in a horizontal plane. On the blow boxes 30, the web W, which is usually heavy (the weight of a wet pulp web may be up to ∼2000 g/sq.m), is supported by means of the blowings B₂ and B₃. Through the nozzle holes 42 placed in the horizontal lower walls of the direct-blow boxes 40, blowings B₁ perpendicular to the plane of the web W are applied to the web W, the web W being dried from above by means of said blowings B₁.
Figs. 4, 6, and 8A and 8B illustrate the construction of the lower boxes 30 in more detall. In the middle of the carrier face 31 of the lower boxes, there is a transverse groove 32, i.e. a groove 32 passing across the width of the web W, which groove is opened towards the web W. The opening angle of the V-section groove 32 is denoted with a. Said angle a is, as a rule, in a range of a = 50°...90°, preferably a = 60°...80°. The inclined walls of the V-section groove 32, which walls are preferably plane, turn and join the horizontal plane portion 34 of the carrier face at an angle b by the intermediate of rounded portions 31b with a curve radius R. As can be seen directly from Fig. 6, between the angles a and b, there is a relationship $a + 2b = 180°$
. Both of the inclined plane faces of the V-section groove 32 have rows of blow holes 33. These blow holes 33 are placed and directed so that the air jets B₃ coming from them are tangential to the rounded portions 31b between the plane faces, said rounded portions turning the air jets B₃, by the Coanda effect, onto the plane portions 34 of the carrier face 31 and making the jets parallel to said plane portions. The blow holes 33 are placed in the opposite sides of the V-section groove 32 as fitted in such a way staggered in relation to one another (Fig. 8) that the blowings B₃ are inter-locked with one another crosswise in opposite directions. Thus, one set of the blowings B₃ is parallel to the running direction of the web W and to its plane, whereas the other set of the blowings is parallel to the plane of the web W but of a direction opposite to the running direction of the web W. In accordance with the Bernoulli principle, the blowings B₃ induce a zone of negative pressure between the web W and the carrier face 31, which zone stabilizes the web W at a certain distance H from the carrier face 31. Said distance H is, as a rule, of an order of H = 3...6 mm, in which case the air drying of the web W is, as a rule, most efficient.
In both of the lateral areas of the carrier face 31, over its length L₁ in the direction of the web, lowered lateral portions 35 are placed, whose height in relation to the web W is lower than the height of the middle-plane portions 34 of the carrier face 31. According to Fig. 6, said lateral portions 35 are inclined plane bevel parts, whose distance in relation to the plane parts 34 at the edges of the nozzle box 30 is denoted with h₂.
In the nozzle-blow-box in accordance with the invention, in the web W treatment gap 25, underneath the web W, the air velocity is first substantially invariable in connection with the plane carrier-face portions 31, whereupon the air velocity is lowered in connection with the carrier-face portions 35;35b,35d,35e stepwise or continuously when moving towards the edges of the box 30 and towards the spaces 30a in the treatment gap 25. Hereby the transfer of heat can be intensified considerably, as will come out later from the test results illustrated in Figs. 9 and 10. The intensification of the transfer of heat comes largely from the fact that, on the lowered carrier-face portions 35;35b;35d;35e, the air-flow velocity parallel to the plane of the web W is lowered considerably, which intensifies above all the heat transfer of the direct blowings B₂.
In a pulp dryer, the lower box 30 and the direct-blow box 40 as shown in Figs. 4 and 5 are placed one above the other and one facing the other, so that the faces 41 and 31 are substantially parallel to one another and, as a rule, horizontal. At the edges of the faces 41 of the direct-blow boxes 40, there may be rounded portions 43a, and at the edges of the carrier faces 31 of the lower boxes 30, there may be corresponding rounded portions 31a.
The opposite faces 31 and 41 on the lower box 30 and on the direct-blow box 40 are provided with nozzle perforations 42;36. A preferred distribution of the perforations 36 on the blow box 30 comes out from Fig. 8. Through said perforations 36;42, perpendicular blowings B₁;B₂ are directed against the web W, the drying of the web W being promoted by means of said blowings. As the air-flow velocity is lowered on the carrier-face portions 35 because of an increased cross-sectional flow area, the direct blowings B₂ will have a longer time of effect on the lower face of the web W.
Fig. 8B is a schematic illustration of a preferred embodiment of the geometry and of a dimensioning example of the V-section groove 32 described above. The geometry shown in Fig. 8B is symmetric in relation to the transverse vertical centre plane K-K. It is the starting point of the design of the V-section groove 32 that the air jets F₁ and F₂ blown from the opposite sides can be made tangential to the rounded portions 31b connected with the edges of the groove 32 so that, by the Coanda effect, said air jets turn and become parallel to the carrier face 34. The area between the groove 33 and the carrier face 34 must be expressly rounded in such a way that the air starts following the carrier face 34.
Figs. 7A...7E show some alternative embodiments of the carrier face of the blow box 30. The nozzle box 30A as shown in Fig. 7A comprises a carrier face 31, in which there are plane portions 34 at both sides of the V-section groove 32 and, after them, plane inclined bevel portions 35.
Fig. 7B shows a particularly advantageous blow box 30B, in which, at both sides of the V-section groove 32, there are plane portions 34b of the carrier face and, after them, step portions 37, which are perpendicular both to the first plane portions 34b of the carrier face and to the plane portions 35b of the carrier face that follow after the step portion 37. The initial parts 34b of the carrier face 31 are parallel to one another and in the same horizontal plane. In a corresponding way, the lateral portions of the carrier face 31 are parallel to one another and in the same horizontal plane. Fig. 7B also shows a preferred dimensioning example of the nozzle box 30B. According to Fig. 7B, the height h₂ of the step portion 37 is h₂ = 10mm. As a rule, the height of the step portion may vary in a range of h₂ = 7...15 mm.
In Fig. 7C, a nozzle box 30C is illustrated as a reference, which box has a fully plane carrier face 31c. Properly speaking, this nozzle box 30C is not in accordance with the present invention, and it is illustrated in this connection for the sake of reference only, the results of said comparison coming out from Figs. 9 and 10, which will be described in more detail later.
Fig. 7D illustrates a blow box 30D in accordance with the invention, which box has relatively long plane carrier-face portions 34d and relatively short and steep, inclined lateral portions 35d. In Fig. 7D, a preferred dimensioning example is also given.
In Fig. 7E, an alternative modification of the blow box as shown in Fig. 7B is illustrated, which modification has relatively long plane carrier-face portions 34e and step portions 37, which are followed by relatively short carrier-face portions 35e. Fig. 7E also shows an example of the construction of said blow box 30E.
Fig. 8A shows the relative locations and staggering of the nozzle holes 33 in the V-section groove 32 so that the blowings B₃ of opposite directions are blown crosswise. The perforations 36 in the nozzle-carrier face 31 are placed in four lines, one line after the other, as staggered in such a way that the blowings B₂ and B₃ neither meet each other nor disturb each other. The mutual spacing of the nozzle holes 33 is, as a rule, in a range of 20...50 mm, and, in a corresponding way, the mutual spacing of the nozzle holes 36 in the transverse direction and in the machine direction is, as a rule, in a range of 40...100 mm.
Further, as to the dimensioning of the blow boxes shown in Figs. 6 and 7, it can be stated as follows, with reference to the denotations in Fig. 6. The angle a of the V-section groove 32 in the middle of the carrier face is, as a rule, in a range of a = 50°...90°, in which case the angle b of the Coanda faces 31b is in a range of b = 45°...65°. The height h₁ of the V-section groove 32 is, as a rule, in a range of $h₁ = (2...5) x Φ$
, wherein Φ is the diameter of the nozzle holes 33 in the walls of the V-section groove 32. The diameter Φ of the nozzle holes 33 is chosen as related to the diameter of the direct-blow nozzles 36 in the carrier face so that the air quantity in the carrier-blowings B₃ blown through the nozzle holes 33 is about 30...60 %, preferably 35...45 %, of the overall air quantity of the blowings B₂ and B₃. The length L₁ of the bevelled or step-formed lateral portions 35,35b,35d,35e in the carrier face 31 is chosen so that it is (0.1...0.3) x L, preferably (0.2...0.25) x L, wherein L is the total length of the blow box 30 in the machine direction. Said length L is, as a rule, in a range of L ≈ 300...500 mm. The difference in height h₂ of the bevelled portions 35,35d or of the step-formed portions 35b and 35e is chosen in a range of h₂ = 7...15 mm, preferably h₂ ≈ 10 mm.
Figs. 9 and 10 illustrate test results obtained with nozzles as shown in Figs. 7A...7E graphically. In Figs. 9 and 10, the vertical axis represents the relative heat transfer coefficient α_R, and the horizontal axis represents the distance of the web W from the carrier face 31, expressly from its plane portion 34. In Figs. 7A...7E, the letter symbol corresponds to the curves A...E in Figs. 9 and 10.
Of the nozzle described above, versions as shown in Figs. 7A...7E were made, whose transfer of heat was examined in a static test device by blowing hot air against a plane metal face. The efficiency of the transfer of heat was obtained by measuring the rate of heating of the plate by means of temperature-measurement detectors inlaid in it. In Figs. 9 and 10, the measured relative heat-transfer coefficients α_R are seen as a function of the distance H between the web and the carrier face 31 of the nozzle box at two different blow velocities. According to the results, a lowering h₁ of the lateral portions 35;35b;35d;35e provides an increase of an order of 5...10 % in the coefficient of heat transfer as compared with a plane carrier face (Fig. 7C, carrier face 31c), when the distance H equals the normal airborne distance of a pulp web W (3...6 mm). On the contrary, at larger distances H, a lowering of the lateral portions 35 does not give any corresponding advantage. The increase was highest in the case of the nozzles at which the lateral portions 35;35b of the carrier face 31 had been lowered most, on the average (Figs. 7A and 7B). The measurement results given in Fig. 9 were obtained with a blow velocity of w_puh = 26 m/s of the blowings B₂ and B₃, and the results given in Fig. 10 were obtained with a corresponding blow velocity of w_puh = 34 m/s, while the temperature T_puh of the blow air was T_puh = 150°C. As comes out from Figs. 9 and 10, there are substantially great differences in the relative heat-transfer coefficient α_R exactly at the optimal airborne web W distances H = 3...6 mm.
The simulation and measurement method employed in the measurements of Figs. 9 and 10 has been described in more detail in the paper by P. Heikkilä and I. Jokioinen, "Airfoil Dryer Heat Transfer", published in The Helsinki Symposium on Alternate Methods of Pulp and Paper Drying in Helsinki, June 4...7(1991).
Based on the measurements described above, the most advantageous embodiment of the invention is, according to the present-day opinion and on the basis of the available measurement results, the blow-nozzle box 30A as shown in Fig. 7A. According to the measurement results of Figs. 9 and 10, a carrier face 34b,35b with a steep step formation (37), as shown in Fig. 7B, is optimal in view of the transfer of heat, but a nozzle-blow-box 30A as shown in Fig. 7A, which is provided with continuously lowering ramp-formed lateral portions 35 of the carrier face, is preferable in an overall consideration, because, in it, the risk of formation of a "cigar" is lower, for the geometry of the blow face does not include sharp angles. Thus, according to a present-day estimate, a nozzle-blow-box 30A as shown in Fig. 7A (also in respect of its dimensions) is the best embodiment of the invention in a case in which the distance, e.g., of a pulp web W from the horizontal portion 34 of the carrier face 31 is ∼ 5 mm.
In the following, the patent claims will be given, and the different details of the invention may show variation within the scope of the inventive idea defined in said claims and differ from what has been stated above for the sake of example only.
The invention concerns a method in air-drying of material webs, in particular of material webs of relatively high grammage, such as pulp webs. Also, the invention concerns a nozzle-blow-box and a pulp dryer that make use of the method. To the web (W) to be dried, from underneath the web, air blowings (B₂) substantially perpendicular to the web and air blowings (B₃) substantially parallel to the plane of the web (W) are applied. By means of these blowings (B₂,B₃), both heat is transferred to the web (W) and the web is supported by air free of contact, and the run of the web through the dryer is stabilized. In order to improve the transfer of heat in comparison with a plane carrier face (FIG. 7C; 31c), the air flow velocity parallel to the plane of the web (W) to be dried and air-supported in connection with the nozzle-carrier face (31) is initially (34) kept substantially invariable, whereupon the air flow velocity is lowered in the lateral areas (35;35b;35d;35e) of said carrier face (31) by employing lateral areas (35, 35b,35e) of the nozzle-carrier face (31) that become rampwise and/or stepwise lower in the air-flow direction.

Claims

Method in air-drying of material webs, in particular of material webs of relatively high grammage, such as pulp webs, in which method, to the web (W) to be dried, from underneath the web, air blowings (B₂) substantially perpendicular to the web and air blowings (B₃) substantially parallel to the plane of the web (W) are applied, by means of which blowings (B₂,B₃) both heat is transferred to the web (W) and the web is supported by air free of contact, and the run of the web through the dryer is stabilized, characterized in that, in order to improve the transfer of heat in comparison with a plane carrier face (FIG. 7C; 31c), the air flow velocity parallel to the plane of the web (W) to be dried and air-supported in connection with the nozzle-carrier face (31) is initially (34) kept substantially invariable, whereupon the air flow velocity is lowered in the lateral areas (35;35b;35d;35e) of said carrier face (31) by employing lateral areas (35,35b,35e) of the nozzle-carrier face (31) that become rampwise and/or stepwise lower in the air-flow direction.
Method as claimed in claim 1, characterized in that, in the method, a number of nozzle-blow-boxes (30) are employed, which are placed underneath the web (W) and whose top side forms a carrier face (31) that supports the web (W), blowings (B₃) directed parallel to the running direction of the web (W) and opposite to said running direction being blown crosswise out of a groove space (32) placed in the middle of said carrier face, and blowings (B₂) perpendicular to the web being blown against the web out of nozzle openings (36) placed in the carrier face, and the time of effect of said latter blowings upon the lower face of the web (W) being made longer by increasing the cross-sectional flow area between the web and the carrier face in the lateral areas (35;35b,35d,35e) of the web and the carrier face (31).
Method as claimed in claim 1 or 2, characterized in that, by means of said stepwise and/or ramp-shaped lateral areas (35;35b,35d,35e) of the nozzle-carrier face (31), both the transfer of heat from the drying air to the web (W) is optimized and the height (H) of airborne running of the web (W) to be dried and supported in relation to the nozzle-carrier face (31) is regulated.
Method as claimed in any of the claims 1 to 3, characterized in that the air blowings (B₃) applied from the central groove (32) in the nozzle-carrier face (31) crosswise in opposite directions are directed out of their nozzle openings (33) substantially tangentially to the curved guide faces (31b) placed at the beginning of the nozzle-carrier face (31), by means of which faces, by the Coanda effect, said blowings (B₂,F₁,F₂) are turned over a certain angle (b) to make them parallel to the plane initial parts (34) of the carrier face (31) and parallel to the plane of the web (W) that runs at their proximity.
Method as claimed in any of the claims 1 to 4, characterized in that the blow-air quantity of said stabilizing air blowings (B₃) blown crosswise along the carrier face (31) and parallel to the plane of the web (W) is 30...60 %, preferably about 35...45 % of the overall blow-air quantity of the nozzle-blow-box (30).
Method as claimed in any of the claims 1 to 5, characterized in that said crosswise blowings (B₃), which are directed as parallel to the carrier face and to the plane of the web (W) to be dried and supported, are slowed down in the lateral area of the carrier face of the nozzle box (30) over a length L₁ parallel to the run of the adjacent web (W), which length L₁ is chosen as $L₁ = (0.1...0.3) x L$
, preferably $L₁ = (0.2...0.25) x L$
, wherein L is the overall length of the carrier face (31) of the nozzle-blow-box (30), which is again chosen in a range of L = 300...500 mm.
Method as claimed in any of the claims 1 to 6, characterized in that the blow air of the nozzle-blow-box (30) is removed out of the drying and support gap (25) through spaces (30a) placed between said nozzle-blow-boxes (30).
Method as claimed in any of the claims 1 to 7, characterized in that, placed opposite to the blow boxes (30) placed underneath the web (W) to be dried and supported, upper direct-blow boxes (40) are employed, out of which blowings (B₁) substantially perpendicular to the plane of the web (W) are directed, in which case the web (W) is dried two-sidedly (Figs. 1, 2 and 3).
Nozzle-blow-box (30) of an air dryer, through which box air blowings (B₂,B₃) are applied to the material web (W) to be dried, by means of which blowings both transfer of heat is produced from the drying air to the web (W) and contact-free air support and stabilization of the run of the web are obtained, said nozzle-blow-box (30) comprising a box part, in which there is a nozzle-carrier face (31) placed against the web (W), in the middle of which face (31) there is a substantially V-section groove (32) transverse to the running direction of the web (W), which groove is opened towards the web (W) and in whose opposite walls there are series of nozzle holes (33) so that, out of said series of nozzle holes (33), support and stabilization air blowings can be applied which are crosswise and of opposite directions in relation to each other, and in which nozzle-carrier face (31), at both sides of its V-section groove (32), there are plane nozzle-carrier-face portions (34) placed in the same plane with each other, characterized in that extensions of said nozzle-carrier-face portions (34) are constituted by stepwise and/or ramp-shaped carrier-face portions (35;35b;35d,35e) placed further apart from the material web (W) to be supported, in the area of which carrier-face portions the velocities of said support and stabilization air flows, as compared with the velocity prevailing in connection with the plane nozzle-carrier-face portions (34), are lowered, and that the nozzle-carrier face (31) is provided with nozzle perforations (36), through which additional blowings (B₂) substantially perpendicular to the plane of the material web (W) to be supported can be applied from the nozzle-blow-box (30).
Nozzle-blow-box as claimed in claim 9, characterized in that extensions of both of the plane walls of said V-section groove (32) are constituted by curved Coanda guide faces (31b), which extend continuously as the plane parts (34) of the carrier face (31), that the nozzle holes (33) provided in the walls of said V-section grooves (32) are fitted in such a way that the principal direction of the air jets (B₃) discharged from them is substantially tangential to the curved Coanda guide face (31b) placed facing it.
Nozzle-blow-box as claimed in claim 9 or 10, characterized in that the angle (a) between the plane walls of said V-section groove (32) is in a range of a = 50°...90°, that the depth h₁ of said V-section groove is $h₁ = (2...5) x Φ$
, wherein Φ is the diameter of the nozzle holes in the walls of said V-section groove (32).
Nozzle-blow-box as claimed in any of the claims 9 to 11, characterized in that, with respect to their length L₁ in the direction of running of the material web (W), said stepwise and/or ramp-shaped lateral parts (35;35b;35d;35e) of the nozzle-carrier face (31) of the nozzle-blow-box have been chosen so that $L₁ = (0.1...0.3) x L$
, preferably $L₁ = (0.2...0.25) x L$
, wherein L is the overall length of the nozzle-blow-box (30) in the direction of running of the web (W), which length has been chosen in a range of L = 300...500 mm, and that the maximum difference in height (h₂) of said lateral area (35) of the carrier face, as compared with said plane part (34) of the nozzle-carrier face (31), has been chosen in a range of h₂ = 7...15 mm, preferably h₂ ≈ 10 mm.
Nozzle-blow-box as claimed in any of the claims 9 to 12, characterized in that said nozzle holes (33) in the V-section groove (32) are placed in the opposite walls of the V-section groove as staggered alternatingly and as substantially uniformly spaced, which spacing has been chosen in a range of 20...50 mm, and that the perforations (36) in said carrier faces (31) are arranged as staggered in relation to said nozzle holes (33) and placed in 3...5 transverse rows in the running direction of the web (W) and as substantially uniformly spaced both in the running direction of the web (W) and in the transverse direction, which spacing has been chosen in a range of 40...10 mm.
Pulp dryer that makes use of a method as claimed in any of the claims 1 to 8 and/or of sets of nozzle-blow-boxes (30) as claimed in any of the claims 9 to 13, characterized in that the pulp dryer comprises a number of nozzle-blow-boxes (30), which are placed at horizontal distances (30a) from one another, through which gaps (30a) the air that supports, dries and stabilizes the material web (W) is primarily removed from the treatment gaps (25), that there is a number of said nozzle-blow boxes (30) in the direction of running of the web (W) one after the other in the same horizontal plane, and that there are several lines of said nozzle-blow-boxes (30) placed one above the other, so that the pulp web (W_in-W_out) to be dried runs through the dryer as air-supported inside the hood (13) of the pulp dryer as horizontal backward and forward runs placed one above the other, the running direction of the material web (W) being reversed between said runs by means of reversing rolls (13).
Pulp dryer as claimed in claim 14, characterized in that, placed opposite to said nozzle-blow-boxes (30), above the material web (W), there are direct-blow boxes (40), substantially perpendicular blowings being applied to the web through nozzle openings or slots (42) placed in the plane face (41) of said boxes placed facing the web (W), and that, between said direct-blow boxes (40), there are intermediate spaces (40a), through which the upper blow air (B₁) is passed further.
Pulp dryer as claimed in claim 15, characterized in that said nozzle-blow-boxes (30) placed underneath the web (W) and the direct-blow boxes (40) placed opposite to them are of equal length, as compared with each other, in the running direction of the web (W) and placed one facing the other as uniformly spaced (Fig. 3).