Screw element for same-sense rotating multi-screw extruders
View Patent ↗A screw element includes an outer radius R a and a core radius R i for multiscrew extruders with co-rotating and intermeshing screw shafts. The screw element has in axial cross section through its longitudinal axis a profile which has at each of the two axial end faces (i.e. a front end face and a rear end face) only one screw flight corresponding to a conventional single-start screw element for intermeshing screw shafts. In this case, the width (flight land angle φ) of the screw flight and conversely, in a corresponding way, the width (flight land angle φ) of the screw flight are formed in a special way and a shearing flight with a constant shearing flight radius R s , which is greater than R i , and less than R a , is provided.
1. A screw element for multiscrew extruders with co-rotating and intermeshing screw shafts, said screw element having an outer radius and a core radius and being rotatable about a longitudinal axis in a direction of rotation, the outer radius being greater than the core radius, the screw element further having an axial length and front and rear end faces at axial ends thereof, a profile of said screw element in axial cross-section at each of said front and rear end faces has only one screw flight, the screw flight at each of said front and rear end faces having left and right edges defining a flight surface therebetween comprising a section of a cylindrical surface having the outer radius, the profile of said screw element at each of said front and rear end faces having a circular root with the core radius and left and right flanks which join the root to the left and right flight edges, respectively, wherein
said flight surface at said front end face comprises a circumferential width that, proceeding from the front end face for a partial length of said axial length along said longitudinal axis, decreases to zero, one of said left and right edges of said flight surface at said front end face meeting a first common edge at said partial length, said first common edge proceeding to said rear end face, wherein a distance of said first common edge from said longitudinal axis first decreases and then increases proceeding from the end of said partial length to said rear end face along said longitudinal axis, said first common edge ending at one of the left and right flight edges of the flight surface at the rear end face that faces the direction of rotation,
said flight surface at said rear end face comprises a circumferential width that, proceeding from the rear end face for the partial length along said longitudinal axis, decreases to zero, one of said left and right edges of said flight surface at said rear end face meeting a second common edge at said partial length, said second common edge proceeding to said front end face, wherein a distance of said second common edge from said longitudinal axis first decreases and then increases proceeding from the end of said partial length to said front end face along said longitudinal axis, said first common edge ending at one of the left and right flight edges of the flight surface at the front end face that faces the direction of rotation, and
said screw element further defines a shearing flight having a constant shear radius that is greater than the core radius and less than the outer radius, said shear flight proceeding helically in the direction of rotation from one of said right and left flanks at said front end face that faces the direction of rotation to one of the right and left flanks at the rear end face that faces away from the direction of rotation, said shearing flight comprising a middle section and two end sections along an axial length thereof, said middle section having a substantially constant flight width, said end sections comprise transitional sections having a widths which decrease to zero at the front and rear end faces.
2. The screw element of claim 1 , wherein the profile of said screw element is designed for close meshing with another screw element.
3. A screw element in claim 2 , wherein an additional pitch is superposed on the screw element by cross-sectional twisting over at least a portion of said axial length.
4. The screw element of claim 3 , wherein the additional pitch is produced by twisting the cross-section of screw element relative to said front end face in the direction of rotation.
5. The screw element of claim 4 , wherein the additional pitch is superposed over the entire axial length of said screw element.
6. The screw element of claim 4 , wherein different additional pitches are superposed on a plurality of axial portions of said axial length.
7. The screw element of claim 3 , wherein the additional pitch is produced by twisting the cross-section of screw element relative to said front end face in a direction opposing the direction of rotation.
8. The screw element of claim 7 , wherein the additional pitch is superposed over the entire axial length of said screw element.
9. The screw element of claim 7 , wherein different additional pitches are superposed on a plurality of axial portions of said axial length.
10. The screw element of claim 1 , wherein the screw element is for a twin screw extruder.