Cooling tube assembly for cooling of the interior of a container

1. A cooling tube assembly comprising:

a cylindrical cooling tube extending from a first end to a second end, the cooling tube having an inner surface, an outer surface, an inner diameter, and an outer diameter, the cooling tube including a first plurality of throughbores and a second plurality of throughbores located axially between the first plurality of throughbores and the second end of the cooling tube, each of the second plurality of throughbores being circumferentially offset from each of the first plurality of throughbores;

a nozzle extending from a first end to a second end, the first end of the nozzle being located inside the cooling tube with the first plurality of throughbores being located axially between the second end of the cooling tube and the first end of the nozzle;

wherein the nozzle includes a first portion with an outer diameter less than the inner diameter of the cooling tube and a second portion with an outer diameter greater than the inner diameter of the cooling tube;

wherein the nozzle includes a bore extending from the first end to the second end, the bore having a first cross-sectional area in a first portion extending from the first end to a junction; and

wherein each individual one of the first plurality of throughbores has a cross-sectional area; and

wherein the cross-sectional area of each individual one of the first plurality of throughbores is between 5% and 15% of the first cross-sectional area of the bore of the nozzle.

2. The cooling tube of claim 1 , wherein the cross-sectional area of each individual one of the first plurality of throughbores is between 8% and 12% of the first cross-sectional area of the bore of the nozzle.

3. The cooling tube of claim 1 , wherein the first plurality of throughbores are evenly spaced around the circumference of the cooling tube.

4. The cooling tube assembly of claim 1 , wherein each of the second plurality of throughbores has a cross-sectional area; and

wherein the second plurality of throughbores are evenly spaced around the circumference of the cooling tube.

5. The cooling tube assembly of claim 4 , further comprising a third plurality of throughbores each having a cross-sectional area and being located between the second plurality of throughbores and the second end of the cooling tube.

6. The cooling tube assembly of claim 5 , wherein the sum of the cross-sectional areas of all of the first, second, and third pluralities of throughbores is between 100% and 300% of the first cross-sectional area of the first portion of the bore.

7. The cooling tube assembly of claim 1 , wherein the cross-sectional area of the bore increases from the junction to the second end.

8. The cooling tube assembly of claim 1 , wherein the bore of the nozzle extends along a central axis;

wherein the outer surface of the nozzle includes a first portion extending from the first end to a junction; and

wherein the first portion forms an angle of between 5° and 15° with the central axis.

9. The cooling tube assembly of claim 1 , wherein the outer surface of the nozzle includes a first portion, wherein the first portion forms an angle of 10° with the central axis.

10. The cooling tube assembly of claim 1 , wherein the nozzle is configured to pass air at a pressure of 1.5 bar through the nozzle from the first end to the second end at a rate of between 50 standard cubic feet per minute and 60 standard cubic feet per minute.

11. The cooling tube assembly of claim 10 , wherein the nozzle is configured to pass air at a pressure of 1.5 bar through the nozzle from the first end to the second end at a rate of 56 standard cubic feet per minute.

12. A cooling tube assembly comprising:

a cylindrical cooling tube extending from a first end to a second end, the cooling tube having an inner surface, an outer surface, an inner diameter, and an outer diameter, the cooling tube including a first plurality of throughbores and a second plurality of throughbores located axially between the first plurality of throughbores and the second end of the cooling tube, each of the second plurality of throughbores being circumferentially offset from each of the first plurality of throughbores;

a nozzle extending from a first end to a second end, the first end of the nozzle being located inside the cooling tube with the first plurality of throughbores being located axially between the second end of the cooling tube and the first end of the nozzle;

wherein the nozzle includes a first portion with an outer diameter less than the inner diameter of the cooling tube and a second portion with an outer diameter greater than the inner diameter of the cooling tube;

wherein the nozzle includes a bore extending from the first end to the second end, the bore having a first cross-sectional area in a first portion extending from the first end to a junction;

wherein each of the second plurality of throughbores has a cross-sectional area, and wherein the second plurality of throughbores are evenly spaced around the circumference of the cooling tube;

further comprising a third plurality of throughbores each having a cross-sectional area and being located between the second plurality of throughbores and the second end of the cooling tube; and

wherein the sum of the cross-sectional area of all of the first, second and third pluralities of throughbores is 216% of the first cross-sectional area of the first portion of the bore.

13. A cooling tube assembly comprising:

a cylindrical cooling tube extending from a first end to a second end, the cooling tube having an inner surface, an outer surface, an inner diameter, and an outer diameter, the cooling tube including a first plurality of throughbores and a second plurality of throughbores located axially between the first plurality of throughbores and the second end of the cooling tube, each of the second plurality of throughbores being circumferentially offset from each of the first plurality of throughbores;

a nozzle extending from a first end to a second end, the first end of the nozzle being located inside the cooling tube with the first plurality of throughbores being located axially between the second end of the cooling tube and the first end of the nozzle; and

wherein a center of each of the first plurality of throughbores are spaced 45° from a center of each of the ones of the first plurality of throughbores on either side relative to a center axis of the cooling tube.

14. A cooling tube assembly comprising:

a cylindrical cooling tube extending from a first end to a second end, the cooling tube having an inner surface, an outer surface, an inner diameter, and an outer diameter, the cooling tube including a first plurality of throughbores and a second plurality of throughbores located axially between the first plurality of throughbores and the second end of the cooling tube, each of the second plurality of throughbores being circumferentially offset from each of the first plurality of throughbores;

a nozzle extending from a first end to a second end, the first end of the nozzle being located inside the cooling tube with the first plurality of throughbores being located axially between the second end of the cooling tube and the first end of the nozzle; and

wherein a center of each of the second plurality of throughbores are spaced 45° from a center of each of the ones of the second plurality of throughbores on either side relative to a center axis of the cooling tube.

15. A cooling tube assembly comprising:

a cylindrical cooling tube extending from a first end to a second end, the cooling tube having an inner surface, an outer surface, an inner diameter, and an outer diameter, the cooling tube including a first plurality of throughbores and a second plurality of throughbores located axially between the first plurality of throughbores and the second end of the cooling tube, each of the second plurality of throughbores being circumferentially offset from each of the first plurality of throughbores;

a nozzle extending from a first end to a second end, the first end of the nozzle being located inside the cooling tube with the first plurality of throughbores being located axially between the second end of the cooling tube and the first end of the nozzle, wherein the nozzle includes a first portion with an outer diameter less than the inner diameter of the cooling tube and a second portion with an outer diameter greater than the inner diameter of the cooling tube, wherein the outer diameter of the second portion defines a maximum outer diameter of the nozzle, and wherein the second portion terminates at a seat interposed between the first and second ends, the seat seating against an axial face of the cooling tube at the second end of the cooling tube; and

wherein a center of each of the first plurality of throughbores are circumferentially offset by 22.5° from a center of each of the second plurality of throughbores closest proximate on either side relative to a center axis of the cooling tube.

16. The cooling tube assembly of claim 15 , wherein each of the third plurality of throughbores is circumferentially aligned with one of the first plurality of throughbores relative to a center axis of the cooling tube.