The present disclosure relates to co-extrusion of multi-layer thin polymer films using blown film processes.
Although so-called “double bubble” and “triple bubble” blown film processes are well known techniques for use in co-extruding multi-layer thin polymer films, these methods suffer from certain limitations.
A multi-layer tubular film is co-extruded and cooled to form a first bubble, then collapsed, preheated and blown into a second bubble. The second bubble is further heated from outside to produce a decreasing temperature gradient from the outside surface of the film to the inside surface of the film. The outside surface of the film is hotter than the inside surface of the film and the inside surface of the film is hot enough for re-blowing but sufficiently cool to avoid blocking. The film is then collapsed, blown into a third bubble and cooled to produce biaxially-oriented film, which is then collapsed, blown into a fourth bubble, heated and then cooled film to relieve stress and impart desired shrink properties to the film to produce ship-stable biaxially-oriented film.
In one aspect, a method for producing a biaxially-oriented blown film comprises co-extruding a tubular film having at least three layers, cooling the tubular film to produce tubular cooled film, collapsing the tubular cooled film to produce collapsed cooled film, preheating the collapsed cooled film to produce collapsed preheated film, blowing the collapsed preheated film to produce tubular preheated film, further heating the tubular preheated film from outside of the tubular preheated film to produce further heated tubular film having a decreasing temperature gradient from an outside surface of the further heated tubular film to an inside surface of the further heated tubular film whereby the outside surface of the further heated tubular film is hotter than the inside surface of the further heated tubular film and the inside surface of the further heated tubular film is hot enough for re-blowing but sufficiently cool to avoid blocking, then collapsing, blowing and cooling the further heated tubular film to biaxially orient the further heated tubular film and produce biaxially-oriented tubular film, and collapsing, blowing, heating and then cooling the biaxially-oriented tubular film to relieve stress within the biaxially-oriented tubular film to produce ship-stable biaxially-oriented tubular film.
In some embodiments, preheating the cooled film to produce the preheated film may comprise heating the collapsed cooled film to produce the collapsed preheated film. Heating the collapsed cooled film may comprise passing the collapsed cooled film through a liquid bath that is warmer than the collapsed cooled film to produce the collapsed preheated film and/or heating the collapsed cooled film with infrared radiation to produce the collapsed preheated film.
In some embodiments, preheating the cooled film to produce the preheated film comprises blowing the collapsed cooled film to produce tubular cooled film, heating the tubular cooled film with infrared radiation while the tubular cooled film is in tubular form to produce tubular heated film, and collapsing the heated tubular film to produce collapsed preheated film. In such embodiments, the method may comprise further heating the collapsed heated film to produce the preheated film, for example by passing the collapsed heated film through a liquid bath that is warmer than the collapsed heated film to produce the preheated film and/or heating the collapsed heated film with infrared radiation to produce the preheated film.
These and other features will become more apparent from the following description in which reference is made to the appended drawings wherein:
Each of the methods comprises co-extruding a tubular film 102 having at least three layers 102A, 102B, 102C. As used in this specification, the term “multi-layer” means at least three layers. As shown in the Figures, extruders 104 extrude the multi-layer film through an annular co-extrusion die 106. The methods each further comprise rapidly cooling the tubular film to produce tubular cooled film 108 using cooling apparatus 112. The cooling apparatus 112 may comprise, for example, an outer and/or inner cooling mandrel or a water ring to provide water cooling or other liquid cooling. The cooling provided by the cooling apparatus 112 reduces crystallinity in the film. After cooling, the tubular cooled film 108 is then collapsed by nip rollers 114 to become collapsed cooled film 116.
After cooling, each of the methods comprises preheating the collapsed cooled film 116 to produce collapsed preheated film 118. The preheating may be carried out in a number of ways.
As shown in
Optionally, as shown in
Alternatively, as shown in
In each case, the collapsed preheated film 118 proceeds to nip rollers 130. Optionally, coatings or other treatments, for example UV irradiation, can be applied to the collapsed preheated film 118 before it proceeds to the nip rollers 130.
In each of the methods shown in
Next, in each of the methods shown in
In each of the methods shown in
The ship-stable biaxially-oriented tubular film 154 is then collapsed by nip rollers 156 to form collapsed ship-stable biaxially-oriented tubular film 158, which is then fed to a winder 160. Optionally, the collapsed ship-stable biaxially-oriented tubular film 158 may be further cooled, for example by chill rollers 162 or blown air, before being passed to the winder 160. Also optionally, the collapsed ship-stable biaxially-oriented tubular film 158 may by slit and unfolded before being passed to the winder 160.
As can be seen from the drawings, each of the exemplary methods includes at least four “bubbles” of film in tubular form: a first bubble between the annular co-extrusion die 106 and the nip rollers 114, a second bubble between the nip rollers 130 and the nip rollers 140, a third bubble between the nip rollers 140 and the nip rollers 144 and a fourth bubble between the nip rollers 148 and the nip rollers 156. Some embodiments may include one or more additional bubbles; for example the methods shown in
Because the diameter of the film can be adjusted between the nip rollers 130 and the nip rollers 140 and again between the nip rollers 140 and the nip rollers 144, the methods of the present disclosure allow for increased flexibility in adjusting the diameter of the blown film without having to change the sizing calibrator (e.g. inner mandrel or vacuum sizer) used for the initially extruded tubular film 102. For example, if the initially extruded tubular film 102 has a diameter of 100 mm, depending on the material it could only be re-blown to approximately 300 mm in diameter in a single step; and larger diameters would require stopping the line to change the size calibrator. By using the two stage process, that is, a first bubble between the nip rollers 130 and the nip rollers 140 and a second bubble between the nip rollers 140 and the nip rollers 144, the diameter of the film can be increased to approximately 400 mm without stopping the line to change the size calibrator.
Additionally, the use of at least four bubbles also allows the film to be exposed to moisture (e.g. in the liquid bath 120) after the first bubble, with the next bubble being used to provide heating and drying to remove moisture and obviate curling before expanding the film in the third bubble. Thus, in certain preferred embodiments at least two bubbles (the initial bubble after extrusion and a subsequent downstream bubble) are used to treat the film before expanding it.
By way of example, and without limitation, the method shown in
Certain exemplary embodiments have been described by way of example. It will be apparent to persons skilled in the art that a number of variations and modifications can be made without departing from the scope of the claims.
This application claims priority to and the benefit of U.S. Provisional Application No. 62/522,409 filed on Jun. 20, 2017, the teachings of which are hereby incorporated by reference in their entireties.
Number | Date | Country | |
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62522409 | Jun 2017 | US |