US 5,032,078 AGrant
Assembly of Injection Molding Manifold, Nozzles and Mold
Issue Date:1991-07-16
•35 Claims
•8 Drawing Sheets
Abstract
A heated manifold, for use in the distribution of heated plastic resins to the various cavities of injection molds for thermoplastic materials. The parts of the manifold interlock with each other and contain the high pressures generated by the injection molding presses. The components of the manifold are fitted with seals of metals dissimilar to the manifold, and with a higher coefficient of expansion than the manifold material. The system includes heated bushings which channel the plastic materials to the individual cavities and are fitted with a removable tip which can be adjusted to change the overall length of the bushing.
Metadata
Inventor
- Salvatore Benenati
Application Information
Application Number:US 3797392
Filing Date:1989-07-12
Priority Date:1988-07-11
Art Unit:135
Classifications
IPC:
B29C 4522
Field of Search:
425264547;548;549;570;571;572;581;588;573;DIG. 58;567328.8;328.14;176 F;297.2;328.15
Patent Drawings (8 sheets)
Description
Brief Description of the Drawings
The foregoing and other objects and aspects of the invention will be better appreciated from the following detailed description of two illustrative embodiments of various aspects of the invention, reference being made in the description to the accompanying drawings. In the drawings:
FIG. 1 is a top plan view of typical molding apparatus incorporating a novel manifold;
FIG. 2 an exploded perspective of the manifold in FIG. 1 drawn to larger scale, portions of this manifold being omitted for clarity;
FIG. 2A is a portion of FIG. 2, omitting the nozzles and heater covers or FIG. 2;
FIGS. 3 and 3A are front and left-side elevations, respectively, of the molding apparatus of FIG. 1, drawn to larger scale, this apparatus being shown partially in cross-section as seen from the plane III--III and from the plane IIIA--IIIA, respectively, in FIG. 1;
FIG. 4 is a fragmentary perspective of a stock member used as components of the manifold of FIGS. 1-3;
FIG. 5 is a fragmentary cross-section of a joint in the manifold of FIGS. 1-3, formed largely of stock components like that in FIG. 4, as seen at the plane V--V of FIG. 2;
FIG. 5A is a somewhat simplified exploded perspective of the manifold joint represented in FIG. 5;
FIG. 6 is a fragmentary cross-section of another form of joint in a manifold formed largely of stock components like that in FIG. 4, as viewed at the plane VI--VI in FIG. 11;
FIG. 6A is a somewhat simplified exploded perspective of the manifold joint represented in FIG. 6;
FIG. 7 is a longitudinal cross-section of a modified bushing useful in FIGS. 5, 5A, 6 and 6A;
FIGS. 8 and 9 are fragmentary cross-sections of the molding apparatus of FIG. 1, drawn to much larger scale, as seen at the plane VIII--VIII and the plane IX--IX, respectively, in FIG. 1;
FIG. 10 is a fragmentary perspective of a component used in the manifold of FIG. 2;
FIG. 11 is a diagrammatic representation of a more complex manifold than in FIG. 2, embodying the same system of construction;
FIG. 12 is a fragmentary perspective, partly in cross-section, of a modification of the manifold in FIG. 2;
FIG. 13 is a fragmentary perspective, partly in cross-section, of portions of the manifold of FIG. 12 but drawn to larger scale;
FIGS. 14 and 15 are fragmentary cross-sections of the manifold of FIG. 12 as seen at the planes XIV--XIV and XV--XV, respectively, in FIG. 12, but drawn to larger scale; and
FIG. 16 is a fragmentary cross-section of a portion of the manifold of FIG. 12 as seen at the plane XVI--XVI in FIG. 14.
FIG. 17 is a perspective view, partly exploded, of another modification of the manifold of FIGS. 1-11 and of FIGS. 12-16;
FIG. 18 is a fragmentary perspective view of the manifold of FIG. 17, partly exploded and partly in cross-section at the vertical plane 18--18 in FIG. 17 but drawn to larger scale;
FIG. 19 is a fragmentary medial cross-section of the manifold of FIG. 17 at the vertical plane 19--19 in FIG. 17, to the same scale as FIG. 18;
FIG. 20 is a perspective view of a component, i.e., a saddle, of the manifold of FIGS. 17-19;
FIGS. 21 and 22 are cross-sections of the saddle of FIGS. 19 and 20 at the planes 21--21 and 22--22 in FIG. 20;
FIG. 23 is a medial cross-section of the manifold of FIG. 17 at the vertical plane 23--23 of FIG. 17;
FIG. 24 is a fragmentary cross-section of the manifold of FIG. 17 at the vertical plane 24--24 in FIG. 17;
FIG. 25 is a fragmentary cross-section of the manifold of FIG. 17 at the vertical plane 25--25 in FIG. 17;
FIG. 26 is a perspective view of a component of the manifold of FIG. 17, said component also appearing in FIG. 25; and
FIG. 27 is a perspective view of another component of the manifold of FIG. 17, this component also appearing in FIG. 23.
Referring now to FIGS. 1-11 of the drawings which show an illustrative embodiment of certain aspects of the invention, a manifold 1 is clamped against four nozzles 2 between a multicavity mold 6, 7 (FIGS. 3, 3A, 8 and 9) and a back plate 25. The manifold basically includes a main member 11 and two cross members 14 extending from supply nozzle 4 (GIGS. 3 and 3A) to four nozzles or feed bushings 2. Plastic resin is introduced by a supply nozzle 4 (FIGS. 3 and 3A) at high pressure, such as 2,000 pounds per square inch. The resin is molten, and it travels through the heated manifold and nozzles 2, to fill the cavities. The resin in the cavities is solidified and the molded parts are ejected when the parts 6 and 7 of the mold are separated. Spacing bars 25A at opposite sides of the assembly are interposed between back plate 25 and mold part 6, and screws 25B tighten the back plate against the manifold. Spacers 25A are not so wide as to prevent the manifold and the nozzles from being forcefully clamped together between the back plate and the mold.
The manifold shown is constructed using three members M (FIGS. 2 and 4) of essentially square identical cross-section. These members M can be routinely prefabricated to accurate dimensional standards and later cut to the required lengths and modified to make manifolds of various dimensions and configurations. These members M (FIG. 4) have a pair of semi-circular grooves 8 running symmetrically along the entire length of each of two opposite sides. Each member M also has a relatively small-diameter longitudinal bore, a resin passage. Bore 9 runs along the entire length of member M and is centered in its cross-section. Member 11 and both members 14 of the manifold in FIGS. 1-11 are made of modified stock members M. Member 11 may be called the main conduit for the resin and members 14 may be called branch conduits, in this manifold.
When manufacturing a manifold of the form in FIGS. 1-11, notch or slot 10 is machined to a depth of approximately three-fourths of the height of member 11 across the width of this member at a suitable distance from its end (FIG. 5A). The width of this slot 10 equals the width of member 14 which is the same as the width of member 11. An enlarged bore 9b is formed in each end of the stock member M used for making member 11, ending at an internal annular shoulder or abutment 9c surrounding bore 9. A bushing 12 is inserted in bore 9b; one end of bushing 12 bears against shoulder 9c and its opposite end is machined to be flush with surface 10a of slot 10 at ambient temperature. The bore in bushing 12 is the same diameter as bore 9, and these bores are coaxial.
The depth of slot 10 is such that the entire end surface of bushing 12 is exposed at surface 10a. A transverse slot 13 of one-fourth of the height of member M is cut in each member 14. A transverse bore 9a is machined in each member 14, to intersect with its bore 9, the axes of bores 9 and 9a being in a common plane.
A member 14 is pressed into a respective slot 10 near each end of member 11, forming intersections as represented in FIG. 5. The axis of bore 9 in member 11 and of the coaxial bore in each bushing 12 is in a common plane that also contains the axes of bores 9 and 9a of member 14. A clamp 15 is fixed to member 11 by screws 16, across member 14. Transverse rib 15a of each clamp 15 has a tight fit in a groove 10b of member 11 (FIG. 5A) and another transverse rib 15a of each clamp 15 fits tightly against the related end of member 11. Clamps 15 complement the strength of members 11 and 14 at their joints, to prevent distortion, as insurance for securely retaining member 14 against the end of bushing 12 (FIG. 5) where bore 9a meets the bore in bushing 12. Members 11 and 14 are coplanar at their top and bottom.
Heaters 17 extend along grooves 8 at the top and bottom of assembled members 11 and 14 (FIG. 2A). Grooves 8 are extended by machining extensions of grooves 8 around the axes of nozzles and at the intersections of member 11 and members 14. Cover plates 36 (FIGS. 2, 8, 9 and 10) are assembled to the top and bottom of members 11 and 14 along virtually the whole length of each heater 17. Each cover plate 36 has a pair of longitudinal formations 37 (FIG. 10) that provide grooves of semicircular cross-section. These formations are received in grooves 8 of members 11 and 14. Cover plates 36 are stock components as of aluminum extrusions, cut to the lengths required. Heaters 17 have cylindrical outer surfaces that have a good fit in grooves 8 and 37 so that heat is efficiently and uniformly transferred to members 11 and 14. This fit may be modified, as may be required when one member of a joint is allowed to slide slightly in the other member of that joint, as is discussed below. Cover plates 36 are fixed to members 11 and 14 by clamps 18 one of which is shown in FIG. 2. Screw 19 of clamp 18 tightens the heater cover plates against opposite sides of each of members 11 and 14.
Bores 22 of the same diameter as bore 9 are drilled near the ends of members 14, for communicating with nozzles 2. The ends of members 14 are fitted with plugs 20 as shown in FIG. 8 and secured in place by set screws 21. This arrangement avoids pockets in the manifold where small volumes of resin might otherwise be trapped and deteriorate.
Each heated nozzle 2 containing heater 40 abuts member 14, and itself has an enlarged diameter portion 2d that, is seated in bore 23 of mold plate 6. A centering ceramic washer 23a is brazed to nozzle 2 and confined radially and axially (as shown) between the bore 23 and nozzle 2. Washer 23a itself provides heat insulation between the nozzle and mold plate 6, and it serves as a spacer to provide a heat-insulating sheath of air along the nozzle, between the nozzle and the mold plate. Another ceramic washer 32 has a brazed joint 2c to nozzle 2 near its tip, supplementing washer 23a in providing heat insulation for the nozzle.
Bushing 12a is fitted in an enlarged bore at the upper end of each nozzle, in alignment with the nozzle's bore 2a. One end of bushing 12a abuts an annular shoulder 2b of the nozzle and the opposite end of bushing 12b is flush with the flat top surface of nozzle 2 at ambient temperature and abuts the lateral surface of member 14 around bore 22.
A short cylindrical spacer 3 is fixed to member 14 along the axis of each nozzle 2. These spacers provide heat-insulating space between back plate 25 and the manifold, and they enable back plate 25 and mold plate 6 to clamp each nozzle against its portion of a member 14.
Plastic resin from a high-pressure supply is injected into the described manifold via socket or bushing 27 at a central location of the manifold, shown in FIG. 9. Bushing 27 with its internal electric heating element 41 is secured by screws 28 to main conduit member 11 of the manifold. Bore 9d is drilled into member 11 to intersect with its bore 9 and member 11 is counterbored to form a surrounding step 29. The opposite ends of bushing 12b abut step 29 and the flat surface of bushing 27 that bears against member 11. A tubular extension 27a of injection bushing 27 may extend inside bushing 12b to step 29. Tubular dowel 31 between manifold member 11 and mold part 6 resists the force of the injection nozzle 4, preventing that force from distorting member 11.
Each of the bushings 12, 12a and 12b is of a metal that has a higher linear thermal coefficient of expansion than the associated part or parts that extend between the abutment ends of the bushing. For example, these bushings may be of brass, phosphor-bronze or beryllium copper in contrast to steel used for member 11 (FIGS. 5A and 9) and for nozzle 2 (FIG. 8). These bushings 12, 12a, 12b may have a liner 39 of hardened or wear-resistant material (FIG. 7) where the resin is abrasive or corrosive. The condition of these bushings abutting against the associated parts of the manifold as described above, being flush with the external surface of its containing member, is a condition that prevails when the manifold is being made and its parts are cool i.e., at ambient or room temperature. When the manifold is heated for conveying melted resin to the cavities, the bushings tend to elongate more than the distance between the abutments at the ends of the bushing. Consequently, looseness and minor imperfections at the abutment areas of the bushing's ends tend to become sealed due to the enormous force resulting from thermal elongation of the bushing.
Bushings 12, 12a and 12b (and bushings 12c of FIG. 6, discussed below) are of significant length, and are thus not to be confused with mere washers. As a rough rule, the length of a bushing should be such that, as the temperature rises from ambient temperature to its operating temperature--typically 350.degree. F. the bushing's length should increase about 0,002 inch as the result of the difference in linear thermal coefficients of expansion between the material of the bushing and the material that contains the bushing.
In each example of the thermally expanding bushing (FIG. 5A, 8 and 9), one end of the bushing abuts an internal shoulder in a component that completely contains the bushing, and the opposite end is flush with a finished surface of its containing member. In each instance, it is possible to reverse the structure, transferring the bushing to the opposite member; or one bushing might be contained partly in each of the members providing abutments for the ends of the bushing. However, having the bushing contained entirely in one member has the distinctive advantage that the external surface of the containing member and the external end of the contained bushing can be routinely and economically machined to be flush with each other at ambient temperature.
Each nozzle is securely positioned by the manifold's clamping structure so that it provides a carefully controlled orifice 38 (FIG. 8) for resin to fill a mold cavity 5. The resin passage extends from bore 2a in the nozzle via passages 43 in tip 35 to orifice 38. The nozzle 2 has a small-diameter threaded end portion 34 and a threaded tip 35 on portion 34; and washers 36* and 37* that serve a shims to locate the very end of tip 35 at an optimal position relative to orifice 38. The body of nozzle 2 has an abutment surface surrounding threaded portion 34, and portion 34 has an abutment surface at its end. These abutment surfaces are related so that companion abutment surfaces of nozzle tip 35 would engage them if there were no interposed shim washers. Accordingly, when a washer 36* and a washer 37* of equal thickness are inserted as shown, and tip 35 is tightened onto the threaded end portion 34 of the nozzle, the very end of tip 35 is moved close to the orifice. This construction allows for varied thickness of shims to be used as a means for adjusting the nozzle tip precisely in relation to the orifice 38. Tip 35 i s a heated portion of the nozzle, and because it is spaced from its containing cavity 44 of mold part 6, it becomes encased in resin. That resin extends to ceramic washer 32, and serves as a heat insulator to maintain in fluid condition the resin in the path from tip 35 to orifice 38.
The manifold of FIGS. 1-10 conveys fluid resin to four cavities of a multi-cavity mold. FIG. 11 illustrates an extension of such a manifold to serve sixteen cavities. In FIG. 11, branch conduits 14a serve pairs of nozzles 2 and a subsidiary conduit 11a serves a pair of branch conduits, all as in FIGS. 1-10. Additionally, each of two supply conduits 14b supplies fluid resin to two subsidiary supply conduits 11a. Finally, main conduit 11b couples injection bushing 27 to two supply conduits 14b.
The manifold of FIG. 11--including the nozzles and the conduit for providing fluid resin to the nozzles--involves various relationships that are essentially the same as those of the apparatus in FIGS. 1-10. However, the manifold of FIG. 11 includes a joint which is shown in FIGS. 6 and 6A that is a modification of the joint in FIGS. 5 and 5A in the manifold of FIGS. 1-10. Thus, the joint in FIG. 11 as seen at the plane VI--VI may include may include one branch conduit member 14b for supplying two oppositely directed passages of a subsidiary conduit member 11a.
In FIG. 6A, member 11a--made using a stock member M--has a slot or notch 10' cut three-fourths of its thickness so that its bore 9 is interrupted at each of two flat surfaces 10a' that bound slot 10'. A slot 13' one-quarter of its thickness is cut in member 14b near each of its ends. A transverse bore 9d is drilled all across member 14b so that, when parts 11a and 14b are pressed together to form a joint, the axes of bores 9 in members 11a and 14b, and of bore 9d will all lie in a common plane. Counter-bores from opposite sides of member 14b coaxial with bore 9d will form internal annular steps or shoulders 9e in member 14b opposite sides of bore 9 in member 14b. Two bushings 12c are set into the counterbores in member 14b, one end of each bushing bearing against its internal step 9e and the opposite end of each bushing 12c being flush with a respective flat surface of member 14b.
When members 11a and 14b are pressed into assembly with each other, the external end of each bushing 12c bears against a respective surface 10a'. Accordingly, seals are formed between thermally elongated bushings 12c and those surfaces 10a' when the manifold reaches its operating temperature.
Bore 9 in member 14b forms an intersection having a supply passage to the intersection and two branch passages into the portions of bore 9 in member 11a at opposite sides of member 14b. Bore 9 in member 11a extends to the end of member 14b at the right in FIG. 6A. That passage might be used in a manifold having an intersection in the form of (+), using three branch passages extending from the intersection. However, the end of bore 9 in member 14b is not used as a passage, so a plug (see plug 20, FIG. 8) and a set screw 21' are used to close the end of bore 9 in member 14b (FIG. 6A).
In the construction of FIG. 6, as in FIG. 5, a clamp 15 is used to strengthen the joint.
Referring to FIG. 11, it may be considered that each nozzle 2 remains at a fixed location as the manifold temperature rises from ambient to its operating temperature. During this temperature rise, member 14b becomes elongated due to its elevated temperature. This elongation might tend to force members 11a at the ends of member 14b to flex outward. However, the slot 13' in member 14b (FIG. 6A) may be made a bit wider than member 11b, to allow for the thermal elongation of member 14b. Some small amount of sliding of member 14b in each member 11a may occur as the manifold becomes hot. As this occurs, the outer end of each bushing 12c would slide along its respective surface 10a'. The amount of sliding is small, smaller than the wall thickness of bushings 12c. Accordingly, the seal formed where each bushing 12c bears against a surface 10a' is maintained during the heating of the manifold.
The same provision for limited sliding may be introduced at each of the joints in the manifold of FIG. 11 between each supply conduit and the branch conduit joined to it. As a manifold becomes heated, some flexing of each elongated branch member may occur if there is no provision for sliding, and the manifold members may also slide over the surfaces of the nozzles where they abut one another. However, the construction that provides for sliding at the joints has the value of mitigating or avoiding the possibility of heat-induced distortion. One groove 8 in member 11a at the intersection should be enlarged to allow heater 17 to shift as the manifold is heated; heat-transfer paste should be used where heater 17 fits loosely in the enlarged groove.
FIGS. 12-15 represent another form of conduit for the high-pressure fluid resin. It is to be understood that this conduit is to be clamped between the back plate 25, the nozzles 2 and the mold 6, 7 as described above.
The manifold of FIGS. 12 to 16 comprises plural straight tubes 50. These tubes have an ample wall thickness to contain the high pressure of the resin that is injected and conveyed to the mold cavities. Fittings are used at each bend or intersection in the manifold's passages, so that straight tubes can be used at all other parts of the manifold.
An injection fitting 48 bears injection bushing 60 corresponding to bushing 27, except that bushing 60 is threaded onto fitting 48 with an interposed sealing washer 61. The inlet passage 60a in bushing 60 extends via bore 48a to a transverse bore 48b in fitting 48. A roughly cubic enlargement 48c (FIG. 12) at the midsection of fitting 48 has oppositely directed shallow bores coaxially aligned with bore 48b. The ends of tubes 50 are received in these shallow bores. Bores 48a, 48b and the bores in tubes 50 form continuous branching passages. Tubes 50 and fitting 48 are brazed together and sealed to be leak-proof. Fitting 48 extends down and against mold plate 6 opposite to injection bushing 60, so as to perform the function of tubular support 31 in FIG. 9. The cross-section of bushing 48 is limited (as shown) for restricting transfer of heat from the manifold to the mold plate 6.
Surrounding fitting 48 above and below enlargement 48c and tubes 50 are a pair of sandwich plates 52, conforming closely to the exterior of fitting 48 and tubes 50.
At the right in FIGS. 12 and 14 is another fitting 47 having a bore 47a aligned with the passage in tube 50 and two oppositely directed bores 47b that are aligned with the bores in opposite tubes 49. Tubes 49 and tube 50 are brazed to fitting 47, forming a "T" in the manifold's passages. Multiple grooves 59 surround each of the three intersecting bores in "T" fitting 47. Only a thin wall 47c remains at the bottom of each groove 59. Each of the three branches of fitting 47 is essentially square; it has a circular cavity that receives the end of a respective tube 49, 50; and the fitting is brazed, leak-proof, to each of the three tubes.
Additional fittings 46 are brazed to the remote ends of tubes 49, in cylindrical cavities formed in generally cubic enlargements 46a of the fittings 46. A passage 46b having a right-angle bend (FIG. 15) is aligned with the passage in tube 49 and with the passage in nozzle 2.
Fitting 46 is clamped between the back plate (not shown) of the apparatus and mold plate 6. Nozzle 2 is of the same construction as in FIG. 8 and cooperates with mold part 6 in the manner described above in connection with FIG. 8. Nozzle 2 contains a bushing 12a' that has a relatively large thermal coefficient of expansion and forms a dependable seal against fitting 46, behaving in all respects the same as bushing 12a in FIG. 8.
As seen in FIGS. 14 and 16, fitting 47 is snugly contained within two sandwich members 51. To like effect, the cubic enlargement of each fitting 46 is snugly contained between two sandwich members 53 which are complementary to the fitting.
Additionally, each length of tube 49, 50 is snugly received in complementary grooves in sandwich members 58. Clamps 18 (FIG. 2) are used in the apparatus of FIGS. 12-16 for holding cover plates 36, 55, 56 and 57 and the paired sandwich plates securely together
As indicated in FIG. 13, each sandwich member 51, 52, 53 and 58 has a groove 54 for receiving heater 17 and the formation 37 of cover plate 36 (FIG. 10). Accordingly, there are paired grooves at opposite sides of sandwich members 58, i.e. at the generally flat top and bottom surfaces of members 58 that extend along tubes 49 and 50. Cover plates 36, 55, 56 and 57 over heaters 17 fit intimately against the tubes and fittings of the manifold, providing uniform and efficient heat transfer.
When fittings 46 are clamped between nozzles 2 and the back plate (not shown) of the molding apparatus, and the manifold temperature is raised from ambient to its operating temperature, tubes 50 become elongated and forcibly displace fittings 47 outward and away from injection bushing 60. This force might tend to cause tubes 49 to become bowed. But those tubes are tightly clamped in the complementary grooves of their sandwich plates. The thinned cross-section of metal 47c at the bottom of grooves 59 accommodates the elongation of tubes 50 and the resulting outward displacement (and return) of fittings 47 in relation to an imaginary straight line from one fitting 46 through fitting 47 to the opposite fitting 46 at each end of the manifold.
As a variant of both of the manifolds described above and shown in FIGS. 1-11 and FIGS. 12-16 of the drawings, it is contemplated that a pair of structural members (not shown) may be arranged parallel to passage member 11 in FIG. 2 or parallel to the main passage provided in FIG. 12 by tubes 50, each of those added members interconnecting a pair of nozzles 2 mechanically and each of those added members being heated in the same manner as the resin-conveying members of the mold. In such an arrangement, the problem of heat-induced distortion of the manifold would fade; instead, the portions of the manifold engaging the nozzles would be forced to slide a bit in relation to the nozzles during heating and cooling of the manifold.
A further manifold is shown in FIGS. 17-27, having several features in common with t he manifolds of FIGS. 1-11 and 12-15 and embodying additional novel features. It is understood that, without duplicating FIGS. 1, 3 and 3A, the manifold of FIGS. 17-27--in the assembled apparatus--is clamped between a back plate 25 and a multicavity mold 6, 7 in exactly the same manner as is shown in FIGS. 1, 3 and 4 for the manifold of FIG. 2 and related FIGS. In like sense, while the manifold shown in FIG. 17 includes only a fragment of one nozzle 2--the same as nozzle 2 in FIGS. 2 and 8--the manifold of FIG. 17 is normally equipped with four nozzles 2.
As with the first two manifolds described above, machine nozzle bushing 68 (FIGS. 17 and 23) provides a port through which plastic resin is injected into the manifold from a high pressure supply. Parts 68 and 70 are screwed into opposite sides of main block 69 (FIGS. 23 and 27). Part 70 is a thrust-resisting heat-insulating spacer (like spacer 3) that bears on a multicavity mold such as mold 6, 7 to resist the pressure exerted against bushing 68. Tubular metal member 65 extends horizontally through metal main block 69 between parts 68 and 70. Member 65 has a cylindrical outer surface, and metal saddles 77 are placed opposite each other, interposed between tubular member 65 and parts 68 and 70, respectively.
As seen in FIGS. 20-22, each saddle 77 has a flat circular face 77a, a hole 77b centered in circular face 77a, and a surface 77c whose cylindrical curvature is the same as the external surface of tubular member 65. The lateral surface 77d of saddle 77 is cylindrical, having a diameter such that the saddle slides in the threaded bores that receive parts 68 and 70, and surface 77c fits the exterior of member 65.
Components 68, 69 and 70, and two saddles 77 are assembled as shown in FIG. 23. Parts 68 and 70 have smooth flat ends that fit against the flat surfaces 78a of the respective saddles. When parts 68 and 70 are tightened, forcing saddles 77 against opposite sides of tubular member 65, the fit of the parts is such that resin-impervious seals are formed between the upper saddle 77 and tubular member 65 and between the upper saddle and bushing 68. Like seals are also formed (inconsequentially) by the lower saddle 77 to spacer 70 and to tubular member 65. When the parts are assembled as described and tightened, a hole 65a is drilled in alignment with passage 68a, so that resin injected at bushing 68 enters axial bore 65b of tubular member 65.
Tubular member 65 is embranced by a pair of mutually interlocking conduit covers 73 (FIG. 18) at the left and right of main block 69 (FIG. 23). These covers should have excellent thermal conductivity and they should have a good fit against the external cylindrical surface of tubular member 65 to promote excellent heat transfer from covers 73 to member 65. In the form of FIG. 18, both covers 73 have the same cross-section that includes a semi-cylindrical trough 73a which matches the cylindrical exterior of tubular member 65. Both covers 73 have L-shaped rails 73b and formations complementary to the rails including grooves 73c. The dimensions of rails 73b and their shape and location in relation to grooves 73c are such that troughs 73a have excellent firm thermal contact to tubular member 65. Covers 73 are of aluminum in this example, thus providing excellent thermal conductivity, and they are extrusions, thus being low in cost and high precise. Because of the precision, the troughs 73a have continuous contact with member 65, and the precise and consistent dimensions result in members 73 being held snugly in assembly to each other and against tubular member 65.
One procedure of assembling conduit covers 73 to member 65 is as follows. With block 69 already in place on member 65, one member 73 is placed against tubular member 65 and the other member 73 of the pair is slid along member 65 so that the L-shaped rail of the moving member telescopes into the complementary groove in member 73 that was initially applied to member 65; and the L-shaped rail of the initially placed member 73 is received in the complementary groove 73c of the moving member 73. The cross-section of the L-shaped rails is sufficiently limited so that they can yield, in being forcibly assembled to a tubular member.
Covers 73, as well as main block 69 and the other blocks that comprise the manifold, have heater channels that receive continuous flexible rod-like electrical heating elements 74 at the top and bottom of the manifold. The bottom of each channel is concave and semi-cylindrical, having the same curvature as the cylindrical heating elements 74; and a cover or retainer 75 fits in each channel, having a concave semi-cylindrical recess 75a (FIG. 18) that matches the curvature of the heating elements 74. Heater retainers 75 in the present example are aluminum extrusions that have a precise snug fit in the heater receiving grooves. This is a configuration that promotes excellent heat transfer from the heating element 74 to the main block 69. The same configuration is provided at each of the other heater-bearing members of the manifold.
Members 73 have grooves or undercuts 79 in their heater channels, slightly below the surface (e.g. surface 73d, FIG. 18) cut by the heater-receiving channel. A hammer and a round-end punch is used to press member 75 firmly against heater 74 and, in the same operation, to deform the metal of element 75 so that it flows locally into grooves 79. This operation is repeated from point to point all along the heaters. The result is an inexpensive and secure assembly that provides virtually ideal heat transfer from the heater to the manifold structure.
At the right in FIGS. 17 and 23, there is a metal "T" block 71 that unifies tubular member 65 to two oppositely extending tubular members 66 (FIG. 24). A bore in block 71 has a close fit against tubular member 71 for efficient transfer of heat, from heaters 74 to the portion of tubular member 65 that is contained in block 71. A bore in block 71 at right angles to member 65 is internally threaded to receive threaded tubular members 66. Paired saddles 77 are interposed between the ends of members 66 and tubular member 65. Transverse bores 65c in member 65 extend passage 65a into members 66. When the assembly of FIG. 24 is tightened, the main conduit 65b of the manifold extends into two branch conduits 66a. The end of member 65 at the right in FIG. 23 is suitably blocked, as by the threaded plug shown.
What has been said above concerning "T" block 71 and its tubular members 66, etc. applies equally to "cross" block 72 at the left in FIGS. 17 and 23. These blocks differ only with respect to the details of their grooves that receive segments of heaters 74.
The tubular member 66 extend to four gate blocks 67 (FIGS. 17). A respective tubular member 66 (FIGS. 19, 25 and 26) extends through gate block 67 from a block 71 or 72 via a pair of conduit covers 73. At its end, bore 66a is shut by a plug 80 and a set screw. Heat insulating spacer 70 is threaded into the top of block 67 and gate coupling 76 is threaded into the bottom of block 67. These threaded parts have flat ends that bear against saddles 77 at opposite sides of tubular member 66. The flat ends of parts 70 and 76 form seals against the flat faces of the saddle and the opposite concave semi-cylindrical surfaces 77c of saddles 77 form seals to tubular member 66, preventing the escape of high-pressure heated resin. These assembled parts provide a portion of the manifold conduit between passage 66a and nozzle 2, including bores 66b and 76a in parts 66 and 76, respectively. Heater grooves 78 (FIG. 26) are provided in the top and bottom of block 67, to receive segments of heaters 74, fixed in place by heater covers 75. The elongated heaters 74, grooves 78 and covers 75 in FIG. 26 have a U-shaped configuration. In general, the heating members, the grooves that receive them, and the heater covers have straight portions and portions that have a lengthwise curved configuration (see FIG. 17) as may be required for heating the resin-conveying passages of the manifold.
A nozzle 2 with its thermally responsive bushing 12a bears against a flat surface of gate coupling 76 and forms a seal against escape of high-pressure resin. In this respect, gate coupling 76 forms part of the manifold that can slide relative to the upper end of nozzle 2, as discussed above, in relation to the manifold of FIGS. 1-11.
Spacers 70 and nozzles 2 grip the manifold, when assembled to a back plate (e.g. back plate 25) and a multicavity mold (e.g. mold 6, 7). Depending on many conditions, there may be a significant increase of length of the manifold from block 71 to block 72 when the apparatus is being heated in preparing it for operation, manifold temperature rising from ambient to its operating temperature. Similarly, the length of the manifold may elongate on start-up, along each conduit formed by aligned tubular members 66, from one gate block 67 to the opposite-end gate block 67. When such elongations occur, the ends of tubular member 65 can be forced to slide in blocks 71 and 72, and correspondingly the remote ends of members 66 can be forced to slide relative to the assembly at each gate block 67. Such sliding is limited and does not obstruct the resin passage in the manifold at blocks 67, 71 and 72; an the integrity of the leak-proof resin-containing passage of the manifold is maintained despite such relative sliding that may occur.
The tubular members 65 and 66 in an example are of steel which has a lower thermal coefficient of expansion than conduit covers 73 which, in an example, are made of aluminum. Gaps G are provided throughout between conduit covers 73 and the adjacent blocks to allow for different expansions.
Blocks 68, 69, 71 and 72 in an example are of steel while saddles 77 in an example are of brass or bronze. Accordingly, the seals provided by saddles 77 become tighter and more secure as the manifold temperature rises from ambient to its operating condition.
The manifold of FIGS. 17-27 is remarkably flexible, in that it is constructed of standardized components that may be used (with only slight modifications of members 65, 66 and 73) to make a wide range of manifolds, as suggested by FIG. 11. Tubular members 65 and 66, conduit covers 73, and heater covers 75 can all be produced with uniformity and high precision by extrusion, and precise saddles 77 can be produced economically by die-casting. Standardized blocks 67, 69, 71 and 72 all have a smooth bore and a transverse threaded bore. These blocks do not require exacting precision; they can be mass-produced readily. The entire manifold is constructed of components that can be routinely and economically produced with high accuracy where accuracy is required, and the components can be readily adapted of ruse with molds of widely varying sizes and having widely varied numbers and arrangements of mold inlet ports. The heater are routinely assembled to the manifold structure, and the transfer of heat to the resin conduits is highly efficient, inherently tending to provide uniform resin temperature throughout the manifold.
The presently preferred embodiments of the invention in its various aspects which are described in detail above may be modified and adapted to various forms of molding apparatus by those skilled in the art. Consequently, the invention should be construed broadly in accordance with its true spirit and scope.
Claims
What is claimed is:
1. A manifold for injection molding apparatus including at least first and second elongated members, each of said first and second members having: a cross-section that is generally uniform along the length of such member, that cross-section being defined in part by mutually opposite first and second side surfaces of such member, a longitudinal passage therein for conveying fluid resin, and a slotted portion in which a slot is formed, the slot being defined by slot surfaces that intersect said mutually opposite side surfaces of the member in which the slot is formed, said slot surfaces including mutually opposite slot surfaces, the slotted portion of said first member being complementary to the slotted portion of said second member, said first and second members being assembled to each other with the slotted portion of said first member being received in the slotted portion of said second member so that each of said mutually opposite slot surfaces of said first member abuts a respective side surface of said second member and each of said mutually opposite slot surfaces of the second member abuts a respective side surface of said first member, and manifold including a connecting passage in said second member connecting the longitudinal passage therein to the longitudinal passage in said first elongated member, said connecting passage of said second member and said longitudinal passage of said first member forming a portion of a passage of the manifold extending through said first side surface of said second member and one of said mutually opposite slot surface of said first member, and electrical means for heating said elongated members extending along and in heat transfer relation to said elongated members.
2. A manifold as in claim 1 wherein the cross-section of said members are essentially the same as each other size and shape.
3. A manifold as in claim 1 wherein both of said longitudinal passages and said connecting passage in said second member have axes in a common plane, the connecting passage in the second member being contained in the slotted portion of the second member.
4. A manifold as in claim 1 wherein one of the passages of the manifold is provided, in part, by a bushing contained in said first member, said bushing having mutually opposite first and second ends, said first member having an internal step surrounding the longitudinal bore in said first member, said step constituting a first abutment for said first end of said bushing, the second end of said bushing being opposite to a portion of one side surface of said second member, said one side surface serving as as second abutment, the second abutment being disposed at the second end of the bushing when the manifold is cool, the thermal coefficient of expansion of said bushing being substantially greater than that of said first member so that the ends of the bushing are caused to bear forcefully against said abutments at an elevated temperature of the manifold during operation thereof.
5. A manifold as in claim 1 wherein said connecting passage in said second member is longitudinally aligned with the bore in said first member at one end of said first member.
6. A manifold as in claim 1 wherein said connecting passage in said second member includes portions extending oppositely from said longitudinal bore of said second member, said longitudinal bore of said first member having portions longitudinally aligned with and extending oppositely from said oppositely extending portions of said connecting passage.
7. A manifold as in claim 1, including a second passage extending opposite to said connecting passage and extending through said second side surface of said second member, said first and second side surfaces of said second member being slidable along said mutually opposite slot surfaces of the first member in response to thermally induced longitudinal changes of said second member and the slot width of the slotted portion of the second member that receives the slotted portion of the first member being sufficiently wider than the first member to accommodate said thermally induced longitudinal changes in the second member.
8. A manifold as in claim 7, including two bushings each of which has opposite first and second ends, said bushings having bores that constitute at least respective parts of said connecting passage and said second passage, said second member having internal bearing shoulders for respective first ends of said bushings and the second ends of the bushings bearing, respectively, against said slot surfaces of said first member.
9. A manifold as in claim 1, wherein said first and second assembled members are disposed between a pair of parallel planes and wherein both of said members have lateral surfaces in one of said planes, said electrical heating means including an elongated heating element extending along both of the lateral surfaces of said members in said one plane.
10. A manifold as in claim 9, further including coplanar cover plates extending along said first and second members.
11. Injection molding apparatus including multiple heated nozzles for injecting fluid resin into cavities of a mold and a unitary conduit having passages including bends and intersections, said passages extending from a fluid resin injection location to said nozzzles, and means for securing said nozzles against said conduit with passages of the conduit directed into the nozzles, said conduit including multiple straight metal tubes having ends and providing passages constituting portions of the conduit's passages, pairs of metal members forming sandwiches containing said tubes and having grooves complementary to and in heat-transmitting engagement with said tubes, electric heating elements extending along opposite sides of said pairs of grooved metal members, and fittings having fused joints to the ends of said tubes and having passage portions therein constituting said bends and junctions of the passages of said conduit.
12. Injection molding apparatus as in claim 11, wherein said securing means comprises a mold against which said nozzles are clamped, one of the fittings of said conduit providing a fluid resin injection port, one end of said one fitting bearing against said mold for providing reaction to that force of apparatus which injects fluid resin into said port.
13. Injection molding apparatus as in claim 11 including for each of said fittings a pair of mutually opposite heat-transmitting members having complementary formations in heat-transmitting engagement with each respective fitting, said heating elements including portions disposed against opposite sides of the pairs of heat-transmitting members of said fittings.
14. Injection molding apparatus as in claim 11 including metal heater cover secured to said grooved metal members, respectively, each said heater cover and the grooved metal member to which such heater cover is secured having formations complementary to opposite sides of, and thereby containing, a portion of a respective one of said heating elements.
15. Injection molding apparatus as in claim 11 wherein said conduit and each said nozzle which are secured together constitute, for each nozzle, a pair of first and second parts having mutually engaging surfaces, said apparatus having, for each of sid pairs of parts, a bushing having mutually opposite first and second ends and having a bore that provides a passage portion from the conduit into a respective one of said nozzles, said bushing being contained in said first part of a respective pair of parts, said first part also providing an internal abutment for said first end of the bushing, the second end of the bushing being at said surface of said second part for providing a second abutment for said second end of the bushing when the apparatus is below its operating temperature, the bushing having a greater thermal coefficient of expansion than that of the part which contains the bushing so that, as the apparatus becomes heated, the bushing ends are forced against said abutments for assuring sealing engagement.
16. Injection molding apparatus as in claim 11 wherein at least two of said straight tubes extend at an angle to one of said fittings and have fixed joints thereto, at least one portion of the fitting having a bore therein forming an extension of the passage in one of the tubes, said one portion of the fitting including thick-wall sections and thin extensible wall sections encircling said portion of the fitting and arranged in alternation therealong for adapting the fitting to yield in response to angular deformation forces imposed on said fitting by the tubes joined thereto.
17. A manifold for injection molding apparatus, including first and second elongated metal members having respective first and second longitudinal bores that extend in intersecting directions approximately at right angles to each other, said bores constituting passages for molding resin, said member shaving electric heating means for maintaining fluid the resin in the passages, said first member having a third bore that has mutually opposite first and second ends, said first end of the third bore extending into the first member's longitudinal bore, the second end of said third bore forming an end opening in a first longitudinal side surface of said first member, said first, second and third bores having coplanar axes, said second member having a first surface transverse to the longitudinal bore in said second member so that the longitudinal bore of the second member forms an opening in said first transverse surface, said third bore being essentially aligned longitudinally with the longitudinal bore in said second member, and means for holding said first and second members assembled to each other.
18. A manifold as in claim 17, including a bushing having mutually opposite first and second ends and having a bore that constitutes part of said longitudinal bore in said second member, said second member having a wall that contains and extends continuously along said bushing from said first end to said second end thereof, said wall having an internal shoulder against which said first end of the bushing bears and the second end of the bushing bearing forcefully against said first side surface of the first member around the opening of the third bore therein at an operating temperature of the manifold, the thermal coefficient of expansion of the bushing being significantly higher than that of said second member.
19. A manifold as in claim 17, including a bushing having mutually opposite first and second ends and having a bore that constitutes at least part of said third bore in said first member, said first member having a wall that contains and extends continuously along said bushing from said first end to said second end thereof, said wall comprising an internal shoulder against which said first end of the bushing bears forcefully at an elevated operating temperature of the manifold, the second end of said bushing bearing against sid first transverse surface of said second member, said bushing having a thermal coefficient of expansion significantly higher than that of said first member.
20. A manifold as in claim 17, wherein said first elongated member has a fourth bore in longitudinal alignment with said third bore, said fourth bore having mutually opposite first and second ends, said first end of said fourth bore opening into the longitudinal bore in said first member and the second end of said fourth bore forming an end opening in a second longitudinal side surface of said first member opposite to said first side surface thereof, said second member having a second surface transverse to said longitudinal bore of said second member so that the longitudinal bore in the second member forms an opening in said second transverse surface, said fourth bore being essentially aligned endwise with the longitudinal bore in said second member, the longitudinal bore in said second member thus having portions that extend from said third and fourth bores in opposite directions, and said first and second transverse surfaces being parallel to each other and opposed to said opposite side surfaces of said first member.
21. A manifold as in claim 20, including two bushings disposed in said first member, and each of said bushings having mutually opposite first and second ends, said bushings having bores constituting at least respective parts of said third and fourth bores, said first member having a wall for each bushing which wall contains and extends continuously along each said bushing from said first end to said second end thereof, each said wall comprising an annular shoulder, said first end of each of said bushings abutting a respective one of said annular shoulders, and the second ends of said bushings extending to said first and second transverse surfaces of said second member, respectively, and forming seals thereto, each said bushing having a thermal coefficient of expansion that is significantly higher than that of said first member.
22. A manifold for injection molding apparatus, including at least first and second elongated members that have respective longitudinal bores that form conduits for fluid resin, and means providing a passage interconnecting said bores, said first and second members extending along intersecting directions and having mutually opposed first and second surfaces, respectively, penetrated by said passage, a bushing contained in one of said members forming at least part of sid interconnecting passage means, said bushing having mutually opposite first and second ends and having a bore that constitutes at least part of the interconnecting passage means, said first member having a wall enclosing said bushing continuously from said first end to said second end of said bushing and having a shoulder against which said first end of the bushing bears, said second end of the bushing extending to said first surface of said first member and abutting said second surface of said second member at ambient temperature, means for heating said members for rendering the resin therein fluid, means for fixing said mutually opposed surfaces against relative displacement toward or away from each other while accommodating sliding of said opposed surfaces relatively along each other due to heat-induced longitudinal changes in at least one of said members, said bushing having a substantially higher thermal coefficient of expansion than said member in which it is contained.
23. Injection molding apparatus including a back plate, a multicavity mold, multiple heated nozzles for injecting fluid resin into the mold, and a manifold having an injection port and having means providing elongated passage portions from said injection port to respective manifold end portions, a cylindrical bushing for each of said nozzles, each bushing having a bore for guiding fluid resin from a respective end portion of the manifold into a respective nozzle, each nozzle including a metal wall providing a nozzle-end abutment surface and a cylindrical cavity having a recessed shoulder, each sid cavity containing a respective one of said bushings, said metal wall being solid and continuous between said recessed shoulder and said nozzle-end abutment surface, said back plate and said mold comprising means for clamping each respective nozzle including its metal wall against a respective manifold end portion, a first end of each said bushing bearing against a respective recessed shoulder and a second opposite end of the bushing being flush with said nozzle-end abutment surface at ambient temperature, said bushing having a thermal coefficient of expansion greater than that of said metal wall so that, when the temperature of said wall rises, one end of each bushing is driven forcefully against a respective manifold end portion.
24. Injection molding apparatus as in claim 23 wherein said nozzle-end abutment surface and the manifold end portion to which the nozzle-end abutment surface is clamped are slidable in relation to each other to accommodate thermally induced displacements of the manifold end portions transverse to their respective nozzles.
25. Injection molding apparatus as in claim 23, wherein said second end of the bushing and the nozzle-end abutment surface are made flush by inserting the bushing into the nozzle with said end of the bushing bearing against the recessed annular shoulder of the nozzle and, at ambient temperature, producing the flush relationship in a machining operation.
26. Injection molding apparatus as in claim 23, wherein the nozzle-end abutment surface and the surface of the manifold end portion engaged thereby are flat for enabling said flat surfaces to slide relative to each other, due to differential thermal expansions of the apparatus, said bushing providing assurance of maintaining a sealed passage from the manifold to its respective nozzle despite thermally induced sliding of the nozzle and the manifold end portion relative to each other.
27. Injection molding apparatus including multiple nozzles for injecting fluid resin into cavities of a mold, means providing an inlet port for fluid resin, and manifold means for providing passages for fluid resin from the inlet port to the nozzles, said passage providing means including lengths of straight tubular members, means joining said tubular members to form bends and branches in the passages, and means for heating said straight tubular members said heating means including pairs of mutually opposed metal conduit covers embracing straight portions of said tubular members so as to be in effective heat-transfer relation thereto, and electrical heating elements embedded in said conduit covers.
28. Injection molding apparatus as in claim 27, wherein said conduit covers have telescopically engageable formations for holding each pair of said conduit covers in assembly with each other and with a said tubular member.
29. Injection molding apparatus as in claim 2, wherein the conduit covers of each pair include first and second conduit covers, the cross-section of the first conduit cover of each pair being the same as the cross-section of the second conduit cover of that pair of conduit covers, each conduit cover having a channel for receiving the straight tubular member and having a rail and a groove parallel to the channel, the rail of the first conduit cover of each pair of conduit covers being received in the groove of the second conduit cover of that pair of conduit covers.
30. Injection molding apparatus including multiple nozzles, an inlet port at which fluid resin is to be injected, and electrically heated manifold means for providing passages for the resin from the inlet port to the nozzles, said manifold means including a first tubular member having a longitudinal passage and a second member having a second-member passage-providing bore, and means for connecting said first tubular member to said second member, said connecting means including a block having a first bore containing a portion of said first tubular member, and said block having a threaded bore intersecting said first bore, said second member having an external thread coaxial with said second-member passage-providing bore, said second member being threaded into said threaded bore, said first tubular member extending across said threaded bore and having a first transverse bore intersecting said longitudinal passage and being substantially aligned with said second-member passage-providing bore, and first means forming a seal between that external portion of said first tubular member which surrounds said first transverse bore and an end surface of said second member surrounding said second-member passage-providing bore.
31. Injection molding apparatus as in claim 30, wherein said first tubular member has a cylindrical longitudinal surface, and wherein said seal forming means includes a saddle in seal-forming engagement with an end of said second member around said second member passage-forming bore, said saddle also having a cylindrically concave surface in seal-forming engagement with said cylindrical longitudinal surface of said first tubular member around said first transverse bore when said second member is tightened in the threaded bore of said block.
32. Injection molding apparatus as in claim 30 wherein said threaded bore extends through said block, said apparatus further including a third member having a third-member passage-providing bore and having an external thread that is coaxial with said third-member passage-providing bore and that is threaded into said threaded bore, said first tubular member having second transverse bore intersecting said longitudinal passage of said first tubular member and in substantial alignment with said third-member passage-providing bore, and second means forming a seal between that external portion of the first tubular member which surrounds said second transverse bore and an end surface of said third member surrounding said third-member passage-providing bore.
33. Injection molding apparatus as in claim 32 wherein the first tubular member has a cylindrical longitudinal surface and wherein said fist and second seal forming means include a pair of saddles having respective cylindrical concave surfaces in seal-forming engagement with opposite sides of said first tubular member around said first and second transverse bores, said saddles being in seal-forming engagement with respective end surfaces of said second and third members around the respective passage-providing bores in said second and third members, respectively.
34. A manifold for injection molding apparatus including first and second elongated members each having a longitudinal bore therein and each having mutually opposite side surfaces, said first member having a slotted portion comprising a slot formed by slot surfaces that intersect the mutually opposite side surfaces of the first member, and said slot surfaces including mutually opposite slot surfaces, said longitudinal bore of said first member being interrupted between said mutually opposite slot surfaces, said second member having first and second transverse passages that extend in opposite directions from the longitudinal bore of said second member to the mutually opposite side surfaces, respectively, of said second member, said first and second members being assembled to each other so that said mutually opposite side surfaces of said second member are received between said mutually opposite slot surfaces and so that said first and second transverse passages are aligned with said longitudinal bore of said first member, and electric means for heating said elongated members extending along an in heat transfer relation to said elongated members.
35. A manifold as in claim 34, further including first and second bushings contained in said second member so as to form respective parts of said first and second transverse passages, each of said bushings having opposite first and second ends, said second member having internal stops engaged by said first end, respectively, of said bushings, the second ends of the bushings extending substantially to said mutually opposite slot surfaces, respectively, at ambient temperature, said bushings having a thermal coefficient of expansion that is substantially greater than that of said second member in which the bushings are contained so that the bushings bear forcefully against said mutually opposite slot surfaces, respectively, at an elevated temperature prevailing when the manifold is in operation.
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