PREFORM FOR A BLOW MOLDING OPERATION
20190001548 ยท 2019-01-03
Inventors
Cpc classification
B29C49/02
PERFORMING OPERATIONS; TRANSPORTING
B65B3/022
PERFORMING OPERATIONS; TRANSPORTING
B29C49/22
PERFORMING OPERATIONS; TRANSPORTING
B29C2949/3064
PERFORMING OPERATIONS; TRANSPORTING
B29C2049/4664
PERFORMING OPERATIONS; TRANSPORTING
B29C2949/3004
PERFORMING OPERATIONS; TRANSPORTING
B29C2949/3026
PERFORMING OPERATIONS; TRANSPORTING
B29C49/46
PERFORMING OPERATIONS; TRANSPORTING
B29C2049/78645
PERFORMING OPERATIONS; TRANSPORTING
B29B11/14
PERFORMING OPERATIONS; TRANSPORTING
B29C2049/222
PERFORMING OPERATIONS; TRANSPORTING
B29C2049/7862
PERFORMING OPERATIONS; TRANSPORTING
B29C2049/023
PERFORMING OPERATIONS; TRANSPORTING
B29C49/071
PERFORMING OPERATIONS; TRANSPORTING
B29C2949/20
PERFORMING OPERATIONS; TRANSPORTING
B29C49/42414
PERFORMING OPERATIONS; TRANSPORTING
International classification
B29C49/78
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method and a preform for blow molding to form a plastic container are disclosed, the preform having a coating formed on an inner surface thereof. The coating reduces a loss of heat energy from the heated preform during expansion thereof to ensure the preform maintains a temperature at or above the phase change/solidification temperature of the material forming the preform.
Claims
1. A preform for blow molding to form a plastic container comprising: a neck portion forming an opening providing fluid communication with an interior of the preform; a body portion having a closed end cap, the neck portion and the body portion forming an inner surface; and a coating formed on the inner surface of the body portion of the preform, the coating having a thermal conductivity less than a thermal conductivity of a material forming the preform.
2. The preform of claim 1, wherein the coating is a sacrificial coating.
3. The preform of claim 1, wherein the coating has a substantially uniform thickness.
4. The preform of claim 1, wherein the coating has a varied thickness.
5. The preform of claim 1, wherein the coating is formed on the inner surface in a non-continuous pattern
6. The preform of claim 1, wherein the coating is frangible.
7. The preform of claim 1, wherein the coating is dissolvable in a liquid.
8. The preform of claim 1, wherein the coating is adapted to maintain its thermal properties during the stretching operation.
9. The preform of claim 8, wherein the coating is a gel.
10. The preform of claim 8, wherein the coating is a high-viscosity liquid.
11. The preform of claim 8, wherein the coating is at least one of a jelly, silicone, paraffin wax, polypropylene, or a combination of the foregoing.
12. A method of simultaneously forming and filling a container comprising: disposing a heated preform having a coating on an inner surface thereof in a mold cavity, the coating having a thermal conductivity less than a thermal conductivity of a material forming the preform; delivering a liquid into the preform thereby expanding the preform and the coating toward an interior surface of the mold cavity to form a resulting container, wherein the coating reduces a loss of heat energy from the heated preform during the delivering step; and wherein the liquid remains within the container as an end product.
13. The method of claim 12, wherein the coating reduces a loss of heat energy from the heated preform during the delivering step to ensure the preform maintains a temperature at or above the phase change/solidification temperature of the material forming the preform.
14. The method of claim 12, wherein the coating dissolves in the liquid during the expanding of the preform.
15. The method of claim 14, wherein the coating is a constituent of the end product.
16. The method of claim 15, wherein the coating is at least one of a colorant, sugar, a surfactant, an odorizing agent.
17. The method of claim 12, wherein the coating evaporates during the delivering step.
18. The method of claim 12, wherein the coating is a sacrificial coating.
19. A method of simultaneously forming and filling a container comprising: disposing a heated preform having a sacrificial coating on an inner surface thereof in a mold cavity, the coating having a thermal conductivity less than a thermal conductivity of a material forming the preform; delivering a liquid into the preform thereby expanding the preform and the coating toward an interior surface of the mold cavity to form a resulting container, wherein the coating dissolves into the liquid or evaporates to reduce a loss of heat energy from the heated preform during the delivering step to ensure the preform maintains a temperature at or above the phase change/solidification temperature of the material forming the preform; and wherein the liquid remains within the container as an end product.
20. The method of claim 19, wherein the coating is a constituent of the end product.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0010] The above, as well as other advantages of the present invention, will become readily apparent to those skilled in the art from the following detailed description of a preferred embodiment when considered in the light of the accompanying drawings in which:
[0011]
[0012]
[0013]
[0014]
[0015]
DETAILED DESCRIPTION OF EXEMPLARY EMBODIMENTS OF THE INVENTION
[0016] The following detailed description and appended drawings describe and illustrate various exemplary embodiments of the invention. The description and drawings serve to enable one skilled in the art to make and use the invention, and are not intended to limit the scope of the invention in any manner. In respect of the methods disclosed, the steps presented are exemplary in nature, and thus, the order of the steps is not necessary or critical. Furthermore, disclosed methods provide for a coating to be placed on an article, specifically a preform, which is later blown into a bottle. Such methods are, in many instances, preferable to placing coatings on the bottles themselves. Preforms are smaller in size and of a more regular shape than the containers blown therefrom, making it simpler to obtain an even and regular coating. Furthermore, bottles and containers of varying shapes and sizes can be made from preforms of similar size and shape. Thus, the same equipment and processing can be used to coat preforms to form several different types of containers. The blow molding process may take place soon after molding and coating, or preforms may be made and stored for later blow molding. If the preforms are stored prior to blow molding operation, their smaller size allows them to take up less space in storage.
[0017] Referring to
[0018] A cross-sectional view of the preform 10 is shown in
[0019]
[0020] The coating 26 may be formed on the inner surface 28 of the preform 10 by any appropriate method such as spray coating, flow coating, or other manual or automated methods of disposing a gel or liquid onto the inner surface. Once applied, the coating 26 may be processed further, as desired. For example, the coating 26 may be cured, dried, or cooled, as necessary, or excess material forming the coating 26 may be removed from the preform 10.
[0021] Once the preform 10 has the coating 26 formed on the inner surface 28 thereof is provided, the preform 10 may be processed to form a resulting container. At the outset the preform 10 is heated to a temperature above its phase change/solidification temperature. For a preform 10 formed from PET, the preform is raised to a temperature of from between about 190 F. to about 250 F. (approximately 88 C. to 121 C.) in an oven and then placed into a mold cavity (not shown). The heated preform 10 is then disposed in a mold cavity (not shown). Halves of the mold cavity close around the heated preform 10 with the neck portion 12 disposed thereabove, and the body portion 14 disposed therein. A blow nozzle (not shown) is then disposed adjacent to or abutting the preform 10 and the blow nozzle may form a seal at the neck portion 12 of the preform 10. The mold cavity may be heated, for example to a temperature between approximately 250 F. to 350 F. (approximately 93 C. to 177 C.), in order to impart increased crystallinity levels within the resulting container. In another example, the mold cavity may be provided at ambient or cold temperatures between approximately 32 F. to 90 F. (approximately 0 C. to 32 C.), as desired.
[0022] A stretch rod (not shown) may extend into the preform 10 to initiate mechanical stretching. At this time, the coating 26 may also stretch or may begin to fracture, as desired. The coating 26 is adapted to maintain its thermal properties during the stretching operation. The stretch rod continues to stretch the preform 10 and the coating 26 thereby thinning the sidewalls of the body portion 14 and the coating 26. At this time, a pressure source, such as a piston-like device (pneumatic, mechanical and/hydraulic pressure) or a servo system, may begin to initiate the rapid transfer of a desired quantity of liquid to an interior of the preform 10. The liquid causes the preform 10 and the coating 26 to expand toward an interior surface of the mold cavity. Residual air may be vented through the stretch rod, as desired.
[0023] During the expansion of the preform 10 caused by the liquid, the coating 26 acts to reduce a loss of heat energy from the preform 10 to the liquid, the residual air, and/or the mold cavity that is contacted by the expanding preform 10. The loss of heat energy is reduced because the coating 26 has a lower thermal conductivity than the material forming the preform 10. In reducing heat energy losses from the preform 10, the coating 26 facilitates the maintenance of the thermal properties of the heated preform 10 during an expansion and filling thereof to ensure that the preform 10 maintains a temperature at or above the phase change/solidification temperature of the material forming the preform 10 (e.g., about 63 C. for PET) until the resulting container is formed. By ensuring that the preform 10 maintains a temperature at or above the phase change/solidification temperature of the material forming the preform 10 during the blowing operation, the appearance and performance of the resulting container is improved. The precise mechanism by which the coating 26 may reduce the loss of heat energy from the preform 10, but the mechanism may be by the coating 26 dissolving into the liquid, evaporating, or any other chemical or mechanical mechanism. In this way, the coating 26 is, at least partially, a sacrificial coating. As described hereinabove, the coating 26 may be a constituent of the end product that resides in the resulting container once mixed with, dissolved into, or chemically reacted with the liquid used to form the container.
[0024] Once the container is formed, the stretch rod may be withdrawn from the mold cavity while continuing to vent residual air. The stretch rod may be designed to displace a predetermined volume of the liquid when the stretch rod is withdrawn from the mold cavity, thereby allowed for a desired fill level of the liquid within the resulting container and/or a desired headspace. Generally, the desired fill level and/or headspace will correspond to a height at or near the level of the support ring 18 of the resulting container.
[0025]
[0026]
[0027] From the foregoing description, one ordinarily skilled in the art can easily ascertain the essential characteristics of this invention and, without departing from the spirit and scope thereof, can make various changes and modifications to the invention to adapt it to various usages and conditions.