Screw elements with reduced energy input during the build-up of pressure
View Patent ↗The present invention relates to screw elements with novel, tightly intermeshing, self-cleaning, co-rotating screw profiles for multishaft screw machines with pairs of co-rotating and fully abrading screw shafts, to the use of these screw elements in multishaft screw machines and to a method of generating these screw elements.
1. Screw elements for multiscrew extruders with pairs of co-rotating screws, wherein the screws are fully wiping in pairs, and wherein each screw has one of:
a generating screw profile and a generated screw profile consisting of arcs with non-infinite radiuses, each of the generating and generated screw profiles being axisymmetric referring to one axis which passes through the point of rotation of the respective screw profile,
wherein each of the generating screw profile and the generated screw profile comprises one sealing region, one or more transition regions, one channel region, one or more tip regions, one or more flank regions, and one or more grooved regions, and each screw profile consists of a sequence of the one sealing region, one of the transition regions, the one channel region, another of the transition regions, and
further wherein
the sealing region consists of a sequence of tip region, flank region, tip region,
the channel region consists of a sequence of root region, flank region, root region, and
each transition region is one of the flank regions.
2. The screw elements according to claim 1 , wherein the sealing region is characterized in that
the flank region has an angle δ_fb 1 starting from the point of rotation of the screw profile which is greater than or equal to half the opening angle δ_gz between the two barrel intersection points (δ_fb 1 ≧arccos(0.5*a/ra)),
one tip region has an angle δ_kb 1 starting from the point of rotation of the screw profile which is smaller than or equal to the difference between the tip angle of a one-flight Erdmenger screw profile and the opening angle δ_gz between the two barrel intersection points (δ_kb 1 ≦π−4*arccos(0.5*a/ra)),
the other tip region has an angle δ_kb 2 starting from the point of rotation of the screw profile which is smaller than or equal to the difference between the tip angle of a one-flight Erdmenger screw profile and the opening angle δ_gz between the two barrel intersection points (δ_kb 2 ≦π−4*arccos(0.5*a/ra)),
and further wherein the channel region is characterized in that
the flank region has an angle δ_fb 2 starting from the point of rotation of the screw profile which is greater than or equal to half the opening angle δ_gz between the two barrel intersection points (δ_fb 2 ≧arccos(0.5*a/ra)) and the minimum distance between the flank region and the screw radius ra is larger than half the flight depth h,
one root region has an angle δ_nb 1 starting from the point of rotation of the screw profile which is smaller than or equal to the difference between the tip angle of a one-flight Erdmenger screw profile and the opening angle δ_gz between the two barrel intersection points (δ_nb 1 <π−4*arccos(0.5*a/ra)),
the other root region has an angle δ_nb 2 starting from the point of rotation of the screw profile which is smaller than or equal to the difference between the tip angle of a one-flight Erdmenger screw profile and the opening angle δ_gz between the two barrel intersection points (δ_nb 2 ≦π−4*arccos(0.5*a/ra)).
3. The screw elements according to claim 2 , wherein the two barrel intersection points are surrounded by barrel regions wherein each barrel region comprises, in each barrel bore and based on each of the two barrel intersection points, an angle of δ_gb in relation to the centre point of the barrel bores, and further wherein the sum of the angles of the tip and flank regions δ_kb 1 , δ_kb 2 and δ_fb 1 of the sealing region is in the range from 0.75*δ_gz to 2*δ_gb+δ_gz and the sum of the angles of the root and flank regions δ_nb 1 , δ_nb 2 and δ_b 2 of the channel region is in the range from 0.75*δ_gz to 2*δ_gb+δ_gz.
4. The screw elements according to claim 1 , wherein the transition region consists of a flank region.
5. The screw elements according to claim 1 , comprising screw profiles which produce a linear seal to the intermeshing zone.
6. The screw elements according to claim 1 , comprising screw profiles which produce a punctiform seal to the intermeshing zone.
7. The screw elements according to claim 1 , wherein a maximum distance between the tip regions of the sealing region of the screw profiles and the barrel is in the range of 0 to 0.05 times the centre distance.
8. The screw elements according to claim 1 , wherein the flight number z is 1.
9. The screw elements according to claim 8 , comprising 8-arc screw profiles.
10. The screw elements according to claim 1 , wherein the flight number z is 2.
11. The screw elements according to claim 1 , wherein the screw elements are designed as conveying elements or mixing elements.
12. The screw elements according to claim 1 , wherein the screw elements are designed as kneading elements.
13. The screw elements according to claim 1 , wherein the screw elements are designed as transition elements.
14. The Screw elements according to claim 2 , wherein the sum of the angles of the tip and flank regions δ_kb 1 , δ_kb 2 and δ_fb 1 of the sealing region is in the range from δ_gz to δ_gb+δ_gz and the sum of the angles of the root and flank regions δ_nb 1 , δ_nb 2 and δ_b 2 of the channel region is in the range from δ_gz to δ_gb+δ_gz.
15. The screw elements according to one of claim 2 , wherein the maximum distance between the tip regions of the sealing region of the screw profiles and the barrel is in the range of 0 to 0.025 times the centre distance.
16. The screw elements according to claim 1 , wherein the generating screw profile consists of n arcs and the generated screw profile consists of n′ arcs, wherein all of the arcs of the generating screw profile merge into each other tangentially such that a closed, convex screw profile is obtained, and wherein the number of arcs n of the generating screw profile is selected such that n is an integer greater than or equal to 1.
17. The screw elements according to claim 1 , wherein the generating and the generated screw element are single-flighted screw elements.
18. The screw elements according to claim 1 , wherein the profile of the generating and the generated screw element are each created of 16 arcs, wherein adjacent arcs in each half of the profile generated by the axis of symmetry have different radii and/or different centers.
19. The screw elements according to claim 1 , wherein the generating and the generated screw elements each have two tip regions.
20. The screw elements according to claim 1 , wherein the generating and the generated screw elements each have two root regions.
21. The screw elements according to claim 1 , wherein the profile both of the generating and the generated screw elements each comprises exactly one sealing region, exactly two transition regions, and exactly one channel region, and the sealing region is followed directly by the transition region, which is followed directly by the channel region, which is followed directly by the transition region.