| 摘要 |
1,119,552. Tubular films. GENERAL ENG. CO. (RADCLIFFE) Ltd. 9 June, 1966 [15 June, 1965], No. 25190/65. Heading B5B. An apparatus for the manufacture of tubular plastic film by extrusion comprises a toroidalshaped former 11a, (Fig. 2), means for introducing cool air within the extruded tube 36 on one side of the former so as to create a flowing air cushion between the former and the extruded tube (inlet 20 and annulus between tubes 16 and 27, apertures 19) means for extracting air from within the extruded tube on the other side of said former (apertures 29, annular space between tube 27 or 21 and tube 28 and exhaust connection 30) and mechanical draw-off means (Fig. 1), (rolls 13, 14 for pulling said extruded tube over said air cushion to expand and stretch it), a second toroidal-shaped former 12a (Fig. 2) spaced away from the first and means for introducing cool air to the extruded tube so as to create a flowing air cushion on the surface of said second former (tube 28, annulus 33 and apertures 34). As shown, the common exhaust (29) is desirably located between the two formers 11a, 12a, with a separate cool air supply for each air cushion at their other sides. As shown, the formers are inflatable, suitably by air, but alternatively by liquid which could circulate therein to give added cooling; alternatively a mechanically expandable former may be used. The embodiment of Fig. 3 shows an extension for the cool air supply to the second former (by means of an extension of tube 28) arranged to direct air into the far end of the extruded tube and an exhaust 37 for a controlled portion of said air on that side of the second former. On starting, air supplies to cooling ring 35 (Fig. 1), inlet 20 and tube 28 (Fig. 2) are shut off and pipes 24 and 25 are shut off so that the toroidal members 11a and 12a are deflated (dotted lines, Fig. 2). Outlet 30 is also closed. The tube extruded from diehead 18 passes between air ring 35 and toroidal member 11a and over the further toroidal member 12a and hence via the nip roll assembly 3, 14 to the take-up mechanism. The inlet to tube 28 is then opened to allow air to pass therethrough and up into the upper chamber 32 and out through annulus 33 and apertures 34. Inlet 20 is opened to allow air to pass up the annulus between tubes 16 and 27, and then out through apertures 19. A controlled quantity of air is then admitted into each of pipes 24 and 25 so causing toroidal members 11a and 12a to inflate, and the air supply to cooling ring 35 is then brought into operation, whilst at the same time the exhaust to connection 30 is opened so removing hot air from within the extruded tube between the toroidal members. The extruded tube then flows over the expanded toroidal members 11a, 12a, floating on a cushion of air supplied from each of apertures 19 and 34. At this stage the supply of air to cooling ring 35 may be increased to emit large quantities of cooling air without distorting the extruded tube 36 since the latter is inwardly supported by the two air cushions on the toroidal member. The rate of flow of air to apertures 19 and 34 and annulus 33 can also be increased, together with an increase in the capacity of the exhaust. The diameter of extruded tube 36 may be readily controlled by admitting or releasing a small quantity of air from either or each of the toroidal members. In operation of the embodiment of Fig. 3, air emitted at the upper end of the tube 28 causes more rapid removal of air from the upper end of the extruded tube above the second toroidal member 12a. Some of the air provides the air cushion by passing as before downwardly over toroidal member 12a to reach exhaust holes 29, (Fig. 2) while the remainder of the air passes directly through the holes 37 (Fig. 3) to the exhaust connection 30 shown in Fig. 2. |
