초록 ▼

A multilayer plastic container comprises a layer of a polypropylene and an intermediate layer directly adjacent the layer of polypropylene wherein at least one of the polypropylene and intermediate layers comprises an adhesive such as maleic anhydride incorporated therein to adhere the layer of poly

A multilayer plastic container comprises a layer of a polypropylene and an intermediate layer directly adjacent the layer of polypropylene wherein at least one of the polypropylene and intermediate layers comprises an adhesive such as maleic anhydride incorporated therein to adhere the layer of polypropylene to the layer of EVOH.

대표청구항 ▼

1. A method of manufacturing a container, the method comprising: (a) providing a preform comprised of at least 90% polypropylene and having a finish and a preform blow section, the preform blow section having a neck extending from the finish, a sidewall extending from the neck and a base closing the

1. A method of manufacturing a container, the method comprising: (a) providing a preform comprised of at least 90% polypropylene and having a finish and a preform blow section, the preform blow section having a neck extending from the finish, a sidewall extending from the neck and a base closing the blow section, the base having a portion of increased thickness defining a thickness greater than all other portions of the blow section, the base being located inward of the sidewall;(b) inducing radial stretching of the preform blow section to produce an average radial stretch ratio of less than approximately 4.5:1;(c) inducing axial stretching of the preform blow section to produce an average axial stretch ratio of less than approximately 1.6:1; and(d) conforming the preform to a mold having at least a neck, a sidewall extending from the neck and a base;wherein the portion of increased thickness does not contact the sidewall of the mold during the axial or radial stretching of the preform. 2. The method of claim 1 wherein the radial stretching induces strain hardening of at least portions of the preform. 3. The method of claim 1 wherein the preform further comprises an oxygen barrier layer. 4. The method of claim 1 wherein the portion of increased thickness of the base is strain hardened. 5. The method of claim 1 wherein the radial stretching produces an average radial stretch ratio of greater than approximately 1.5:1. 6. A method of manufacturing a container comprising at least 90% polypropylene, the method comprising: (a) providing a preform having a finish and a preform blow section, the preform blow section having a neck extending from the finish, a sidewall extending from the neck and a base closing the blow section, the base having a portion of increased thickness defining a thickness greater than all other portions of the blow section, the base being located inward of the sidewall;(b) heating the preform;(c) inducing radial stretching of the preform to produce an average radial stretch ratio of less than approximately 4.5:1; and(d) inducing axial stretching of the preform to produce an average axial stretch ratio of less than approximately 1.6:1. 7. The method of claim 6, wherein the radial stretching produces an average radial stretch ratio of greater than 1.5:1. 8. The method of claim 6 wherein the axial and/or radial stretching induce strain hardening. 9. The method of claim 6 wherein the axial and/or radial stretching induce strain hardening in at least portions of the base of the blown preform. 10. The method of claim 6 wherein the preform further comprises an oxygen barrier layer. 11. A method of manufacturing a container, the method comprising: (a) providing a preform having a first layer comprising polypropylene and an adhesive in an amount of up to approximately 0.20% by weight, and a second layer comprising a barrier material, the adhesive bonding the first layer bonded directly to the second layer, the preform having a finish and a preform blow section, the preform blow section having a neck extending from the finish, a sidewall extending from the neck and a base closing the blow section, the base having a portion of increased thickness defining a thickness greater than all other portions of the blow section, the base being located inward of the sidewall and the portion of increased thickness does not cover a longitudinal axis of the preform;(b) heating the preform;(c) inducing radial and axial stretching of the preform to conform the preform to a mold. 12. The method of claim 11 wherein the radial stretching produces an average radial stretch ratio of less than approximately 4.5:1. 13. The method of claim 12 wherein the radial stretching produces an average radial stretch ratio of greater than 1.5:1. 14. The method of claim 11 wherein the axial stretching produces an average axial stretch ratio of less than approximately 1.6:1. 15. The method of claim 11 wherein the axial and/or radial stretching induce strain hardening. 16. The method of claim 11 the step of providing a preform comprising providing a preform wherein the portion of increased thickness does not contact a sidewall of the mold during the axial or radial stretching of the preform. 17. The method of claim 16 further comprising the step of conforming the preform to a mold having at least a neck, a sidewall extending from the neck and a base, wherein the portion of increased thickness does not contact the sidewall of the mold during the axial or radial stretching of the preform. 18. The method of claim 11 wherein the first layer comprises up to approximately 0.03% by weight of adhesive.