The present invention relates to refining discs and plate segments for refining discs, and more particularly to the shape of the bars and grooves that define the refining elements of the discs or segments. The plate segments may be used, for example, in refining machines for disperging, deflaking, and for refining all ranges of consistency (HiCo, LoCo and MC) of lignocellulosic material. Further, the invention may be applied to various refiner geometries, such as disc refiners, conical refiners, double disc refiners, double conical refiners, cylindrical refiners, and double cylindrical refiners.
Lignocellulosic material, such as wood chips, saw dust and other wood or plant fibrous material, is refined by mechanical refiners that separate fibers from the network of fibers that form the material. Disc refiners for lignocellulosic material are fitted with refining discs or disc segments that are arranged to form a disc. The discs are also referred to as “plates.” The refiner positions two opposing discs, such that one disc rotates relative to the other disc. The fibrous material to be refined flows through a center inlet of one of the discs and into a gap between the two refining discs. As one or both of the discs rotate, centrifugal forces move the material radially outward through the gap and out the radial periphery of the disc.
The opposing surfaces of the discs include annular sections having bars and grooves. The grooves provide passages through which material moves in a radial plane between the surfaces of the disc. The material also moves out of the radial plane from the grooves and over the bars. As the material moves over the bars, the material enters a refining gap between crossing bars of the opposing discs. The crossing of bars apply forces to the material in the refining gap that act to separate the fibers in the material and to cause plastic deformation in the walls of said fibers. The repeated application of forces in the refining gap refines the material into a pulp of separated and refined fibers.
As the leading edges of the bars cross, the material is “stapled” between the bars. Stapling refers to the forces applied by the leading faces and edges of opposite crossing bars to the fibrous material as the leading faces and edges overlap. As the bars cross on opposite discs cross, there is an instantaneous overlap between the leading faces of the crossing bars. This overlap forms an instantaneous crossing angle which has a vital influence on the material stapling and/or the covering capability of the leading edges of the bars.
The zero degree draft angle, narrow bars and deep grooves of conventional high performance plates may result in excessive and unsustainable stresses at the root 20 of the bars. Bar failure, e.g., shearing of bars at the root, may result, especially if the plate is formed of materials other than from the 17-4PH alloy group. Plates formed of the high strength 17-4PH alloy tend to have excessive wear and short operational lives when subjected to an abrasive refining environment. Refiner plates formed of alloys other than 17-4PH tend to have bar and groove pattern designs constrained by the brittleness of the utilized alloy material.
Because of excessive stresses on high and narrow bars, plates having conventional high performance bar and groove patterns may not be practically formed of high wear resistance stainless steel material. Stainless steel with good wear characteristics has been used to form less demanding refiner plate designs. But unsuccessful attempts have been made to develop alloys combining the toughness of the 17-4PH alloy with the wear resistance of other stainless steel alloys. Despite the efforts to find or develop suitable alloys, high performance refiner plate patterns keep break when formed of materials (other than 17-4PH) having inadequate energy absorption potential.
The greater amount of bar material in bars with large draft angles increases the moment of inertia of the bars. The added bar material and greater inertia enhances the breakage resistance of the bars. The wide draft angle also lowers the applicable bar height to bar width ratio and thus leads to lower bar edge length potential. The consequences of lower bar height to width ratios and lower edge lengths are typically: lower energy efficiency, suboptimal fiber quality development, and a reduction in hydraulic capacity due to the non-linear reduction in open area in the grooves in the course of the plate's service life caused by large draft angles. Large draft angles also reduce the “sharpness” of the leading edges of the bars which may have a negative impact on the quality consistency over the service life of the plates.
There is a long felt need for high performance refiner plates and techniques to design plates that may be formed of a wide range of metal alloys, e.g., other than the 17-4PH alloy, that are now typically used to form conventional plates only. Further, there is a long felt need for refiner plates that provide both the refining characteristics typically found only with high performance refiner plates and have a long service life through enhanced wear resistance.
A novel design technique has been developed for achieving refiner plates having bars with increased strength (such as typically found in high performance plates) and formed from high wear resistance materials. While the high wear resistance materials are commonly used in refiner plates, these features tend not to be present in conventional high performance plates formed of the 17-4PH alloy. The design techniques disclosed herein for high performance refiner plates is applicable to plates formed of alloys other than the 17-4PH alloy. By using the design techniques disclosed herein, refiner plates may be designed having high wear resistance and to be less prone to bar breakage than the conventional refiner plates described above.
The design technique treats the bars of a refiner plates as having an upper section and a lower section. The upper section of refining bars provides the refining action. The lower sections of the bars define the grooves that provide passages through which cellulosic material is transported between the refining plates. A design goal for the upper section of the bars is to provide high performance refining. A design goal for the lower sections of bars is to provide strength to the bar. The upper section of the bar should preferably mimic the bar design of high performance plates to achieve the performance of such plates, such as bars that are narrow and have zero or small draft angles. To achieve the design goal for the upper section, the region at the top and upper section of the bars may have narrow bar widths, shallow or zero draft angles and sharp upper edges, e.g. corners. To achieve the design goal for the lower region of the bars, the width of the bar may be increased, e.g., by wide draft angles and generous radii in corners at the bar roots, to avoid sharp corners at the roots of the bar. The lower section of the bars are preferably designed to provide sufficient resistance to bar breakage, such as by having rather wide thicknesses and generously curved roots at the substrate of the refiner plate.
Each bar 31, 32 has two distinct sections which are: (i) an upper refining section 42 and (ii) a lower strength section 44. The upper section 42 of the bars is between the line KS at the upper end of the bars. The lower section 44 of the bars is below the line KS. The depth of the bar on one side (adjacent groove 34) is deeper than the depth of the bar on the opposite side, which is adjacent groove 36. The upper bar section 42 is generally similar for all bars and may be rectangular in cross-section. For example, the upper section of each bar is preferably narrow, has a small draft angle, e.g., one or two degree or less, and a sharp upper edge 52. The lower section 44 of each of the bars (below line KS) are relatively wide, especially at the root 50 (adjacent the deep grooves 34), have root corner radii, e.g., 0.030 inches or greater, and have a large draft angle, e.g., five degrees or greater, on at least on one side wall that is adjacent groove 36.
The lower sections 44 of the bars define grooves that are alternating wide shallow grooves 36 and narrow, deep grooves 34. The bars shown in
The following formulas show how the design goals and techniques described above are applied to limit stress at the bar roots of a refiner plate. The following equation may be used to calculate the relative stress applied to a bar over the height of the bar:
Where M is a moment, e.g., torque, applied to a bar along a direction perpendicular to the bars vertical axis and parallel to the plate. The force (F) is treated for purposes of calculating stress on the bar as being applied to the upper edge of the bar, where the bar depth (zz) is zero. The moment (M) is a function of the force (treated as a constant) and the depth of the bar, where zz is zero at the top of the bar and maximum at the root of the bar. The parameter (y), is the middle of the bar, (along the depth of the bar) and is aligned with the bar axis. The parameter (w) is the width of the bar. The parameter I is the area moment of inertia (second moment of inertia) of the bar mass. The parameter σ is a bending stress applied to the bar by the force (F).
A comparison of standard and new bar design was made in terms of stress to prove the concept of the design goals. Two options for the bar shape were compared: (i) a regular bar shape with a 5 degree draft, and (ii) a bar shape (see
The following calculations show the viability of the bar and groove designs shown in
The parameter Wnew is used to determine the width (w) of a bar and in the above equation to determine Wnew, wherein the parameter wo is the bar width at the top of the bar. In addition, σ1 represents the stress at the root in a conventional bar design (see FIG. 2); σ2 represents the stress in the refining section of the bar design shown in
An ideal bar shape is, for purposes of this discussion, a bar having a constant stress from the top to the root of the bar, or at least from the transition (KS) to the root. An ideal bar has a curved shape for the bar sidewall(s) that increases the width of the bars such that the stress in the bar remains constant for (zz>zs). The ideal bar shape may be defined by the following formulas.
The above equation is one example of a means to determine a bar width for the lower section of an ideal bar where the stress in the bar remains constant along the depth (zz), or at least from ZS to the root of the bar. In the above example, ZS occurs at ZZ=1.4 b, where b is the width of the bar at the top of the bar. It is preferred that boundary (ZS average) on a bar between the upper section and the lower section be a distance from the top of the bar that is within 20 percent and preferably within five percent of 1.4 times the bar width. Due to manufacturing variations, particularly casting variations, the actual ZS at any specific point in a bar pattern may vary by substantially more than 20 percent. The average ZS is based on an average ZS for all bars in a refining section and after the bars have been machined following casting. Similarly, the bars shown in
The stresses for all bar designs for a distance from the top of the bar in excess of zs can be calculated as follows:
Setting all unknown constant factors to one, the relative stresses may be derived over the depth of the proposed bar designs, which are shown in the graph of
The graph of
The loss (Aloss in the equation below) in groove area can be determined as follows:
Lost Area:
By increasing the depth and width of deep, wide grooves, the area of all of the combined grooves can be adjusted to compensate for the wider lower section of bars and the alternating narrow, shallow grooves. In the example shown in
Refining feed material, e.g., wood chips and other lignocellulosic material, is processed by a refiner having a pair of opposing refiner plates mounted on discs, at least one of which discs rotates. The opposing surfaces of these plates have refining zones with grooves and bars, such as shown in
While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
This application claims the benefit of application Ser. No. 60/887,972, filed Feb. 2, 2007, which is incorporated in its entirety by reference.
Number | Name | Date | Kind |
---|---|---|---|
4712745 | Leith | Dec 1987 | A |
5181664 | Kohler | Jan 1993 | A |
5467931 | Dodd | Nov 1995 | A |
5476228 | Underberg | Dec 1995 | A |
5893525 | Gingras | Apr 1999 | A |
6032888 | Deuchars | Mar 2000 | A |
6607153 | Gingras | Aug 2003 | B1 |
6957785 | Virving | Oct 2005 | B2 |
Number | Date | Country |
---|---|---|
9522653 | Aug 1995 | WO |
9524528 | Sep 1995 | WO |
Number | Date | Country | |
---|---|---|---|
20080210795 A1 | Sep 2008 | US |
Number | Date | Country | |
---|---|---|---|
60887972 | Feb 2007 | US |