Method for producing containers filled with a liquid filling material from blanks made of a thermoplastic material and nozzle for use in such a method
A method for producing containers filled with a liquid filling material from blanks made of a thermoplastic material and to a nozzle for use in the method. In the method, each blank is at least thermally conditioned and is then shaped to form the container in a mold during a shaping phase, by axial and radial stretching, as a result of liquid filling material being introduced under pressure into the blank through a nozzle. The axial stretching is initiated by the pulsed injection of filling material into the blank.
1. A method for producing containers filled with a liquid filling material from blanks made of a thermoplastic material, comprising the steps of: thermally conditioning a respective blank; and shaping the blank in a mold during a shaping phase to form and fill the container by introducing liquid filling material under pressure through a nozzle into the blank to axially and radially stretch the blank, the axial stretching being initiated by a pulsed injection of filling material into the blank in a targeted manner against a base of the blank, the blank being stretched only by the liquid filling material.
2. The method according to claim 1 , including supplying the filling material in an axial direction of the blank.
3. The method according to claim 1 , including supplying the filling material to the blank at a speed of 30 to 100 m/s.
4. The method according to claim 3 , including supplying the filling material at 70 to 90 m/s.
5. The method according to claim 1 , including supplying the filling material with a jet diameter from 3 to 20 mm.
6. The method according to claim 5 , including supplying the filling material with a jet diameter from 5 to 14 mm.
7. The method according to claim 6 , including supplying the filling material with a jet diameter of 10 mm.
8. The method according to claim 1 , wherein the filling material striking in pulsed injection in the blank exerts a force from 350 to 650N.
9. The method according to claim 8 , wherein the filling material exerts a force from 400 to 600N.
10. The method according to claim 1 , including changing a supply speed of the filling material during filling and shaping.
11. The method according to claim 10 , including reducing the supply speed of the filling material during filling and shaping.
12. The method according to claim 1 , including changing a jet diameter of the filling material during filling and shaping.
13. The method according to claim 1 , including guiding the axial stretching at least temporarily by a guiding device that engages externally with the blank.
14. The method according to claim 13 , including arranging the guiding device to partially enclose the blank or to interlock with. the blank.
15. The method according to claim 13 , wherein the guiding device limits axial stretching speed at least temporarily.
16. The method according to claim 1 , including moving the nozzle axially during shaping.
17. The method according to claim 1 , including detecting a position of the base of the blank at least temporarily during shaping using ultrasound or by detecting a thermal profile.
18. The method according to claim 17 , including controlling distance between the nozzle and the base of the blank.
19. The method according to claim 16 , including measuring pressure of the filling material or pressure in an exhaust air duct or a return flow line and regulating the movement of the nozzle during shaping by the measured values.
20. The method according to claim 1 , including controlling the temperature of the filling material.
21. The method according to claim 20 , including controlling the temperature of the filling material by heating the filling material.
22. The method according to claim 1 , including maintaining a position of the nozzle so that the nozzle does not move laterally at least temporarily during shaping by filling material jets leaving the nozzle in a radial direction.
23. The method according to claim 1 , wherein a cross-sectional surface of a head of the nozzle corresponds substantially to an inner cross-sectional surface of the blank.
24. A nozzle for use in a method according to claim 1 , the nozzle comprising: an opening for a filling jet; and
further openings for auxiliary jets that run substantially at a right angle to the filling jet.
25. A nozzle according to claim 24 , wherein the openings for the auxiliary jets are dimensioned so as to substantially offset forces resulting from the auxiliary jets.