Pinned fly ring for rotary drum washer and method of manufacture

Abstract

Disclosed is a fly ring adapted to be used in a rotary drum filtering apparatus, and a method of forming such a fly ring. The fly ring comprises a plurality of ring segments, each ring segment being laser cut. Each ring segment has a first end which overlaps a second end of an adjacent ring segment, forming a lapped joint. Each ring segment first and second end has at least two spaced apart through holes, the through holes of the first end being aligned with the through holes of the second end. A custom fastener extends through the first end and second end aligned through holes.

Claims

1. A method of manufacturing a fly ring for a rotary drum filtering apparatus, the method comprising the steps of: laser cutting a plurality of arc shaped ring segments out of a metal plate, each ring segment having an outer circumference dimension within a predetermined tight tolerance, and at least two through holes in each end of each segment, overlapping the ends of the ring segments so that all of the assembled segments form a complete ring, the ring having a predetermined outer circumference within a given tight tolerance, passing a custom fastener through each of the at least two through holes in each end of each ring segment and securing each fastener in each hole, so that the assembled segments form the ring.

2. The method of manufacturing a fly ring according to claim 1 wherein the custom fastener comprises a bolt with a head on one side of the lapped joint, and a washer and a nut on the other side of the lapped joint.

3. The method of manufacturing a fly ring according to claim 1 wherein the custom fastener has a lead in chamfer to further force alignment of the through holes.

4. The method of manufacturing a fly ring according to claim 1 wherein the custom fastener comprises a bolt having a head, a first diameter portion adjacent the head and with a first diameter, a neck portion adjacent the first diameter portion with a smaller diameter than the first diameter, and a third threaded diameter portion adjacent the neck portion, the third diameter portion having a third diameter greater than the neck portion diameter and less than the first diameter.

5. The method of manufacturing a fly ring according to claim 4 wherein the end of the first diameter portion adjacent the neck portion has a lead in chamfer, and wherein the end of the custom fastener opposite the head end has a lead in chamfer.

6. The method of manufacturing a fly ring according to claim 1 wherein the at least two through holes in each end of each segment are formed by, after the ring segments are cut by laser cutting, and the ends of the ring segments are overlapped, the holes are cut by laser cutting.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a perspective vewer of a pulp vacuum washer.

(2) FIG. 2 is a top view of a prior art concentric ring.

(3) FIG. 3 is a perspective view of the ring shown in FIG. 2.

(4) FIG. 4 is a side view of an overlapping joint of a fly ring according to this disclosure.

(5) FIG. 5 is a top view of the joint of FIG. 4.

(6) FIG. 6 is a bottom view of the overlapping joint of FIG. 4.

(7) FIG. 7A is a side view of a custom fastener used to connect the two ring segments.

(8) FIG. 7B is an end view of the custom fastener shown in FIG. 7A.

(9) FIG. 8A is an enlarged view of a pinned fly ring according to this disclosure.

(10) FIG. 8B is a side view of the ring shown in FIG. 8A.

(11) FIG. 8C is a cross-section of the overlapping joint of the ring segments shown in FIG. 8A.

(12) Before one embodiment of the disclosure is explained in detail, it is to be understood that the disclosure is not limited in its application to the details of the construction and the arrangements of components set forth in the following description or illustrated in the drawings. The disclosure is capable of other embodiments and of being practiced or being carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. Use of including and comprising and variations thereof as used herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. Use of consisting of and variations thereof as used herein is meant to encompass only the items listed thereafter and equivalents thereof. Further, it is to be understood that such terms as forward, rearward, left, right, upward, downward, side, top and bottom, etc., are words of convenience and are not to be construed as limiting terms.

DESCRIPTION OF THE EMBODIMENT

(13) Illustrated in the FIGS. 4 through 8 of the drawings is a fly ring 100 adapted to be used in a rotary drum washer, such as the one illustrated in FIG. 1, the fly ring 100 comprising a plurality of ring segments 104. In the disclosed fly ring 100, each ring segment 104 is identical to each other, but in other embodiments (not shown), each ring segment length can be different. Each ring segment 104 is laser cut, and, as illustrated in FIGS. 4, 5, 6 and 8B, has a first end 108 which overlaps a second end 112 of an adjacent ring segment, forming a lapped joint 116. As illustrated in FIGS. 8A, 8B and 8C, each ring segment first and second end has at least two spaced apart through holes 120 and 124, the through holes of the first end being aligned with the through holes of the second end. A custom fastener 130 extends through the first end and second end aligned through holes. The custom fastener 130 comprises a bolt with a head 134 on one side of the lapped joint 116, and a washer 140 and a nut 144 on the other side of the lapped joint 116.

(14) Also disclosed is a method of forming the fly ring 100 for a rotary drum washer. The method comprises the following steps. First, laser cutting the plurality of arc shaped ring segments 104 out of a metal plate, each ring segment 104 having an outer circumference dimension within a predetermined tight tolerance. At least two through holes 120 and 124 are also laser cut into each end of each segment 104.

(15) The ends of the ring segments 104 are then overlapped so that the assembled ring segments form a complete fly ring 100. Because of the tight tolerance cut dimension of the outer arc of each ring segment 104, the ring 100 has a predetermined outer circumference within a given tight tolerance.

(16) After overlapping one ring segment end over another ring segment end, the custom fastener 130 is driven through each of the at least two through holes in each end of each ring segment. The custom fastener 130 is then secured in each hole by placing the washer 140 and threading the nut 144 onto the end of the fastener 130, so that the assembled segments form the ring 100. As can be seen in FIGS. 5 and 6, the alignment of the edges of the inner circumference of the ring segments is not crucial, but the alignment of the outer circumference of the ring segments is.

(17) As illustrated in FIGS. 7A and 7B, the custom fastener 130 comprises a bolt having the head 134. The custom fastener 130 also includes a first diameter portion 150 adjacent the head 134 and with a first diameter, and a neck portion 154 adjacent the first diameter portion 150 with a smaller diameter than the first diameter. The custom fastener 130 also includes a third threaded diameter portion 158 adjacent the neck portion 154, the third diameter portion 158 having a third diameter greater than the neck portion diameter and less than the first diameter.

(18) The end of the first diameter portion adjacent the neck portion has a first lead in chamfer 160, and the end of the custom fastener opposite the head end has a lead in chamfer 164. Each of these lead in chamfers aid in securing the ring segments together by accommodating and realigning any misalignment In the through holes in the end of the rings segments.

(19) Benefits

(20) Conventional cutting of ring segments by laser cutting faded to produce rings with the precise dimensions needed to accurately form a functional drum. The disclosed process modifies conventional laser cutting to improve its precision so that the laser cut segments can be used to form a properly dimensioned drum. More particularly, in the disclosed process, the laser cutting is speed optimized to obtain the desired tolerance and finish. The speed will vary depending on the material and power of the laser. This improved laser cutting permits the precision needed to accurately cut the ring segments. The ring segments can then be joined at a lap joint to form the precise shape needed for the drum.

(21) This pinned fly ring takes advantage of this high precision laser cutting process and eliminates the need for welding, straightening, and machining while not compromising structural integrity. The new design comprises laser cut ring segments and custom designed fasteners. Unlike the traditional fly ring, the joints are lap joints with pre-laser cut holes.

(22) After the ring segments are cut using the improved laser cutting, the joints between the ring segments are overlapped. The holes cut by laser cutting are then aligned. A custom faster is then used to secure the lapped segment ends to one another. The custom fastener includes a chamfered portion which forces the aligned openings to orient themselves so the precise drum outer circumference can be achieved.

(23) The custom fastener is used to maintain the tight tolerance required between the hole and the shank of the bolt. Typical purchased fasteners do not have the high tolerance required to get the proper fit.

(24) The neck portion between the fastener head and the threaded shank is a thread run-out groove. Because it is impossible to thread completely to a shoulder, the groove provides a means to end the thread and still tighten the nut completely.

(25) The custom designed fasteners are driven into place and secured by a nut.

(26) The assembly process comprises three easy steps. 1. Position the rings. 2. Drive the custom fasteners through the holes. 3. Fasten with a nut.

(27) The new assembly process can be completed in a fraction of the time and does not require special skill (such as welding) to complete.

(28) Various other features of this disclosure are set forth in the following claims.