The present invention relates to injection molding machinery. More specifically, the present invention relates to check valves used in the barrels of an injection unit.
Some examples of known molding systems are: (i) the HyPET™ Molding System, (ii) the Quadloc™ Molding System, (iii) the Hylectric™ Molding System, and (iv) the HyMet™ Molding System, all manufactured by Husky Injection Molding Systems, Ltd.
The injection molding process typically comprises preparing a polymeric (or sometimes metal) material in an injection unit of an injection unit for melting, injecting the now-melted material under pressure into a closed and clamped mold, solidifying the material in its molded shape, opening the mold and ejecting the part before beginning the next cycle. The molding material typically is supplied to the injection unit from a hopper in the form of pellets or powder. The injection unit transforms the solid material into a molten material (sometimes called a “melt”), typically using a feed screw, which is then injected into a hot runner or other molding system under pressure from the feed screw or a plunger unit. A shut off valve assembly is often provided to stop and start the flow of molten material from the barrel to the molding system.
Many screws mount ring check valves at their distal end to prevent melt from flowing back during injection. A typical prior-art ring check valve is shown in
As is known to those of skill in the art, ring check valves have simple flow paths (in comparison to other types of check valves), resulting in lower shear rates and fewer hang-up spots for the melt. However, wear of the tip retainer and the ring is a common problem in prior art ring check valves. During recovery, the tip retainer rotates with the screw and the ring freely floats in the barrel. Relative movement of the contact surfaces of both the tip retainer and the ring, loaded with recovery pressure and viscous drag forces, causes the wear failure of these components. The problem is especially severe for high performance machines, which recover using high screw RPMs.
Some prior art ring check valves have used carbide inserts on the tip retainer to increase service life of the wearing components. Unfortunately, because of the small bearing area between wear surfaces, the problem has not been eliminated and failures of this design due to wear still occur.
According to a first aspect of the invention, there is provided a check valve for a screw. The check valve has a retainer tip that is operable to be attached to a distal end of a screw shaft, the retainer tip operable to retain a ring assembly. The ring assembly is coaxially mounted around the retainer tip, the ring assembly and the retainer tip operable to cooperatively move between an open position which permits melt to flow through the check valve and a closed position which prevents backflow of the melt. Contact surfaces between the ring assembly and the retainer tip while the ring assembly is in the open position are located proximate to the longitudinal axis of the screw.
According to another aspect of the invention, there is provided a check valve for a screw. The check valve has a retainer tip that is operable to be attached to a distal end of a screw shaft, the retainer tip operable to retain a ring assembly. The ring assembly is coaxially mounted around the retainer tip, the ring assembly and the retainer tip operable to cooperatively move between an open position which permits melt to flow through the check valve and a closed position which prevents backflow of the melt, The ring assembly includes inward-facing flutes that extend towards the retainer tip.
The invention and its embodiments will be more fully appreciated by reference to the following detailed description of illustrative (non-limiting) embodiments in accordance with the present invention when taken in conjunction with the accompanying drawings, in which:
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Resin material (typically thermoset or thermoplastic pellets) is fed from a hopper 32, through a feed throat 34 into melt channel 30. The rotational movement of screw 24 plasticizes the material prior to it exiting through nozzle 28. In some embodiments, screw 24 may include a plurality of specialized zones (not shown). For example, a first zone might include screw flights adapted for conveying solid material from the hopper 32, a latter zone for shearing and plasticizing the material, and a final zone for mixing the now-molten material prior to exiting through nozzle 28. Screw 24 may also include weirs or channels to separate out unmelted material from the melted material for further processing. Other adaptations will occur to those of skill in the art.
In addition to rotating, screw 24 is, in some embodiments, operable to reciprocate back and forth to express the melted material out through nozzle 28 and pack the material within a mold (not shown). A ring-check valve 36 is provided near the tip of screw 24 to prevent the reentry of the melted material during the forward motion of the screw 24 during its injection phase. The rotational movements of screw 24 is provided by a motor 44, which may be an electric motor, a hydraulic motor, or a combination thereof (the embodiment depicted in
Heater bands 46 are provided along a portion of the length of extrusion barrel 22 (though away from the feed throat 34) to assist in the melting of the material (in addition to the heat generated by the shearing action of screw 24) and then maintain the temperature of the molten material as it approaches the nozzle 28. In some embodiments, heater bands 46 are covered with an insulating barrel cover to minimize heat loss). Thermocouples are provided along the extrusion barrel 22 to provide an indication of the melted material's temperature.
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Retainer tip 48 includes a shaft 52 and a tip portion 60 at a distal or forward end of shaft 52. In the presently-illustrated embodiment, shaft 52 has a wider portion 54 and a thinner portion 56, with a step 58 between wider portion 54 and thinner portion 56. However, a shaft having either a constant diameter or other variations in diameter could also be used. In some embodiments, the opposing end of shaft 52 defines an interface 62 adapted to be removably mated with a complementary-interface on the end of screw 24 (
Tip portion 60 is generally conically shaped, and has a greater diameter than shaft 52 so that it provides a ledge extending beyond the wider portion 54 of shaft 52 that defines a front seat 64 for preventing removal of ring assembly 50 in a forward direction. Tip portion 60 is smaller in diameter than ring assembly 50, and is also smaller than typical prior art retainer tips (such as the one shown in
Retainer tip 48 further includes a rear seat 68 extending outwards from shaft 52 and located between tip portion 60 and interface 62. Rear seat 68 is sized as to provide a smaller diameter than extrusion barrel 22 so that it provides a clear flow path for melt travelling through extrusion barrel 22 when ring check vale 36 is in the open position. In the presently-illustrated embodiment, rear seat 68 includes a seating portion 82 for seating ring assembly 50 and a sloped portion 86 that extends within the ring assembly 50 and helps smooth the melt flow. Rear seat 68 can also include a forward wall 88 that abuts against step 58 on shaft 52 to help prevent forward travel of the rear seat 68.
Ring assembly 50 is floatably and concentrically mounted around shaft 52 between front seat 64 and rear seat 68. Ring assembly 50 includes a ring 72 that is sized as to abut against the inside of extrusion barrel 22 (
The space between ring 72 and the inner ring 80 provides a throughput region 88. As flutes 76 generally do not see excessive wearing, they can be comparatively thin relative to prior art flutes which are located on the screw, helping to increase the cross-sectional area of throughput region 88. Tip portion 60 is sized as to minimally occlude throughput region 88 by not extending past inner ring 80.
Operation of ring check valve 36 is similar to that of prior-art designs. During the recovery phase, melt pressure forces the screw 24 (including the attached retainer tip 48 and ring assembly 50) in a rearward direction, moving ring check valve 36 into its open position, allowing the melt to flow under the ring 72 (which remains substantially in place against the interior surface of extrusion barrel 22), and through throughput regions 88 towards the end of the extrusion barrel 22. During the recovery phase, the front surface of inner ring 80 provides a contact surface which abuts against an opposing contact surface on the tip portion 60, namely front seat 64. Relative (i.e., rotational) movement between contact surfaces on the retainer tip 48 and ring assembly 50 occurs proximate to the axis of screw 24, which is closer to the axis of screw 24 than in prior-art check valves, and at a lower speed, thereby reducing wear damage to ring check valve 36. In addition, inner ring 80 provides a comparatively large contact surface for front seat 64, further reducing wear. During the injection phase, the screw 24 moves forward, bringing the seating portion 82 of rear seat 68 into contact with the rearward edge 74 of ring 72, and thereby sealing off the melt path for the remainder of the injection stroke.
To reduce the amount of melt that is trapped between opposing surfaces of retainer tip 48 and inner surface 90 on inner ring 80, at least one channel 92, and optionally, multiple channels 92 (
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The description of the non-limiting embodiments provides examples of the present invention, and these examples do not limit the scope of the present invention. It is understood that the scope of the present invention is limited by the claims. The concepts described above may be adapted for specific conditions and/or functions, and may be further extended to a variety of other applications that are within the scope of the present invention. Having thus described the non-limiting embodiments, it will be apparent that modifications and enhancements are possible without departing from the concepts as described. Therefore, what is to be protected by way of letters patent are limited only by the scope of the following claims.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/CA10/00255 | 3/3/2010 | WO | 00 | 9/16/2011 |
Number | Date | Country | |
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61168647 | Apr 2009 | US |