The present invention concerns a protection tile for scroll flight wear protection.
For this type of centrifuge scroll, there is generally a tile protection avoiding flight wear and allowing for durable conveyance when the product to be transported is particularly abrasive.
These protection elements are usually fabricated using carbon tungsten or ceramics, with a coefficient of thermal expansion which can defer significantly from steel which is generally the element of the flight. Assembly of these elements is particularly delicate and several patents proposing solutions concerning rivets, glue or weld, have already been published.
One solution known from U.S. Pat. No. 4,328,925 shows the assembly via a support with grooved dove tail locking system in which an abrasive resistant element is inserted on one side and constitutes a complimentary form. The position is held via glue or deformation of tab or blocking via a plate screwed onto the support. This solution does not insure ortho-radial support of element resistant to abrasion, sufficient enough for friction of product being displaced. These elements can slip and become dislodged.
The solution in European Patent No. 0 081 938 shows an assembly using an abrasive resistant element fixed on the scroll flight using conical rivets. This solution is difficult and costly to implement due to the necessity of drilling the flights.
U.S. Pat. No. 5,429,581 shows an assembly using an abrasive resistant element with male form lodging via an axial slippage into a complimentary housing located on the scroll flight. Even though this solution satisfactory allows for bearing radial, ortho-radial and axial loads, using this method is also difficult and costly to implement due to the requirements of machining for lodgment on the flights. Maintaining tiles in lodging is insured via glue or plates, cone and screws. Multiplication of these maintaining parts can be costly.
In U.S. Pat. No. 6,206,818 an assembly solution is shown using a support with dove tail locking system grooves in which abrasion resistant element is placed present in complimentary form. This element is inserted via side entry slippage or, if space between male and female forms permits, frontal entry. Fixation of the abrasive resistant element is achieved by glue injection into the existing gaps of the support. A hole in the rear of the support and grooves over two parts allow for glue spreading over all empty spaces. This gluing is possible after welding the support on a conveyor flight, which avoids possible alteration of glue due to high temperature welds. Precise positioning of supports before weld is needed to insure final continuity of the wear resistant elements. This requires using special tools as per U.S. Pat. No. 6,230,960 which can cause a long and costly assembling.
DE 3435960 A1 shows a wear tile being one part where an additional ring is mounted in a circumferential opening at the tip of the screw blade. With this opening the screw blade is weakened and thus with high axial forces the tip of the screw blade may break.
JP 2012-551 A1 shows a protecting tile consisting of two parts. However the support is welded to the tip of the screw blade and the wear plate inserted into the support. The wear plate is fixed to the support by means of a cotter, which is inserted from the side. This however can only be done while manufacturing the apparatus. As soon as there are the protection tiles side by side, the cotter cannot be moved.
JP H03-130218 U shows a protection tile where the support is welded to the screw flight. It has a nut where a wear plate is inserted. This wear plate is then fixed by an elastic sealing. However such sealing ring would fall in aggressive (e.g. acid) environment.
U.S. Pat. No. 4,416,656 shows a wear tile consisting of a support and a wear resistant member which is secured with an additional rivet or shank, which is deformed to secure the connection.
DE 3140364 A1 describes a system where the wear resistant member is mounted directly to the screw flight. To keep the members in position pins are mounted at the upper end of the screw flight, which may weaken the flight. Further the wear resistant member must be designed new for each different width and diameter of the flight and thus cannot be used on other machines.
Considering the inconveniences of the prior art, the present invention defines a new protection tile capable of resisting different mechanical and tribological stresses which will be applied, with a simple, rapid tile assembly along the entire scroll flight.
Thus the invention is mainly characterized in that the support and wear-resistant insert are connected to each other by a mechanical locking system, whereby the support fixation on the flight ensures the locking of the insert by purely mechanical clamping, in that the support has at least one opening where the insert fits in, and preferably the insert has the same number of finger-like extensions to fit in each of the openings of the support. These protection tiles are generally fixed on the flight of a centrifuge scroll or any other mechanical element allowing for product displacement with friction of said product. With such system no additional material as glue or braze is necessary to fix the insert to the support.
An advantageous protection tile has shown that the support has at least one groove-like surface where the insert has a complementary form to fit in.
The invention further concerns a conveyor with a scroll, e.g. screw press, centrifuge, decanter and is characterized by a number of protection tiles mounted onto the scroll at its circumference where the support and wear-resistant insert are connected to each other by a mechanical locking system, whereby the support fixation on the flight insures the locking of the insert by purely mechanical clamping. Due to this purely mechanical clamping, the material used for tile insert can be any type and the invention eliminates any weld, braze, glue issues usually encountered between the support and the wear resistant insert. The use of a surface of the flight to complete a dovetail locking system is particularly advantageous as this simplifies at the same time the assembly and the locking of the tile and avoids a preliminary assembly of the support and the insert. Tile protection is then very quick to implement, with firstly an easy and simple insert fit into the support and secondly a usual support fixation on the flight of the scroll.
Invention defines a tile with a weldable support and a wear-resistant insert. The material used for tile support is generally stainless steel. All other types of steel, stainless or otherwise, may be used if weld adherent. To offer an efficient wear-resistant feature the insert may be made of special steel, tungsten carbide or other carbide or ceramic.
The invention is now described in accordance with the attached drawings, where
A centrifuge using the invention is illustrated in
As illustrated in
The support 6 according to the invention shown in
The insert 41 according to the invention shown in
The assembly of protection tile 4 onto the conveyor scroll 3 is achieved via the following steps. As shown in
Under these conditions, one can see that surfaces 36 and 7A are in contact, insuring adequate resting face for insert 41 on support 6 and allowing the protection tile to support axial load exerted by the product on the friction surface 27.
The width of finger 46 is slightly less than the width of the opening 23. Existing gaps between surfaces 43 and 26 and surfaces 42 and 25 are limited but sufficient to allow for assembly described above. Friction of the product to be transported, on surface 27 generates ortho-radial forces on insert 41. Contact between surfaces 43 and 26 or between surfaces 42 and 25, depending on scroll rotation direction, allows insert 41 to support these forces.
Finally, the dove tail locking system and especially the contact between male corner 40 of the insert 41 and female corner 10 of the support 6, allows the insert 41 to support centrifugation forces.
It can thus be appreciated that the wear-resistant tile for attachment to a scroll flight of a rotor, comprises a support part 6 attachable to the scroll flight, having a front face 7A, 7B and a back face 13, 14, and a profiled opening 23 passing entirely through the front and back faces. An insert 41 has one, lower profiled portion 46 fit within and retained only mechanically to the support part by mating of the profiles through the opening of the support part, and another portion 27 defining a primary wear-resistant surface. As shown in
Preferably, as shown in
The downwardly facing undercut at 10, 11, and 12 in a region between the back face and the front face of the support part, mates with the upwardly oriented projection 40 at the back of the central portion 66 of the insert, which has a profile that is complementary to the undercut of the support part. When the insert fits within and is retained mechanically to the support part, such that the support part at the back face and the lower portion of the insert at the back face are coplanar, the projection on the insert interlocks with the undercut on the support part.
During operation, the product to be transported could possibly pass through spaces between support 6 and insert 41 without causing harm to tile resistance. If this intrusion of product cannot be tolerated, an appropriate resin can be used to fill the gaps.
In another embodiment than the one shown in
In another embodiment than the one shown in
In another embodiment than the one shown in
The invention is not limited to the embodiments in the drawings but as explained above in the range of the following claims.
Filing Document | Filing Date | Country | Kind |
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PCT/EP2013/001436 | 5/15/2013 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
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WO2014/183772 | 11/20/2014 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
4328925 | Shapiro | May 1982 | A |
4416656 | Shapiro | Nov 1983 | A |
5429581 | Michaud | Jul 1995 | A |
6206818 | Deschamps | Mar 2001 | B1 |
20100016140 | Dietschreit | Jan 2010 | A1 |
20160107172 | Lamy | Apr 2016 | A1 |
Number | Date | Country |
---|---|---|
0081938 | Nov 1982 | EP |
2048728 | Dec 1980 | GB |
2273253 | Jun 1994 | GB |
03127643 | May 1991 | JP |
2754055 | May 1998 | JP |
3443147 | Sep 2003 | JP |
Number | Date | Country | |
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20160107172 A1 | Apr 2016 | US |