WO2000073033A2

WO2000073033A2 - Mixing machines

Info

Publication number: WO2000073033A2
Application number: PCT/GB2000/002057
Authority: WO
Inventors: Jonathan Bridge Fletcher; Peter R. Wood
Original assignee: Carter Bros (Rochdale) Ltd.
Priority date: 1999-05-28
Filing date: 2000-05-26
Publication date: 2000-12-07
Also published as: EP1185404A2; AU5089700A; WO2000073033A3; GB9912379D0

Abstract

A mixing machine has a mixing chamber in which there are disposed at least two rotors arranged for rotation in opposite directions about respective rotational axes. The rotors have a helical projection and are rotatable so as to present a leading face of the projection to the material being mixed. The leading face has a discontinuous profile along the axial direction of the rotor so as to define first and second portions. A majority of the leading face (17) of the first portion (12) is concave and a majority of the leading face (19) of the second portion (13) is convex. The circumferential length of a tip (W1, W2) surface of the projection increases in the axial length of the rotor. A clearance defined between the tip of the projection and a facing wall of the mixing chamber decreases in size in the direction of rotation of the rotor. The rotor profiles are designed to provide zones which act on a material to be mixed in different ways so as to improve overall mixing quality and efficiency.

Description

MIXING MACHINES

The present invention relates to mixing machines of the kind that are used to mix batches of polymeric compound.

Mixing machines of the kind defined above are typically heavy duty machines used in the mixing of rubber, plastics or other viscoelastic materials exhibiting high viscosity during mixing that may need to be mixed with fillers, oils, colorants and chemical modifiers.

Such mixers comprise two counter-rotating rotors disposed in parallel in a mixing chamber. A pneumatic or hydraulic ram or pusher, the bottom face of which generally forms a top wall of the mixing chamber, forces the material to be mixed towards the mixing chamber and the rotors. The material in the chamber is subjected by contact with the rotors and/or the chamber wall, to a distributive action and to a milling or shearing action which commonly generates heat. The mixed compound is removed from the mixing chamber via a discharge door that is disposed at the bottom of the chamber.

Most mixing machines of this type are based on one of two basic designs. The first and most common is the tangential rotor mixer which was first disclosed in US patent no. 1200070 of October 1916. In such a mixer the rotors are designed to be non-intermeshing so that the loci described by the peripheries of the rotors do not intersect. The compound material to be mixed is compressed and sheared against the internal face of the wall of the mixing chamber in the early part of the mixing cycle whilst the temperature of the compound is still low. This action breaks down and disperses the raw ingredients of the mix but as the temperature increases later in the cycle the viscosity of the mix decreases resulting in less shear and dispersive action but more distributive action. In most machines of this type the rotors are non- synchronous and have a helical profile.

The second type of design is the intermeshing rotor mixer that was disclosed in US patent No. 2015618 dated 1935. In such mixers the loci described by the peripheries of the rotors during rotation intersect. The rotors generally have outwardly extending projections (such as wings or nogs) and rotate synchronously to ensure that there is no contact between projections on the respective rotors. The projections are generally of a helical configuration and are designed to ensure good distribution of the materials to be mixed early in the mixing cycle. As the temperature increases and the viscosity decreases the mix starts to flow across the projections and dispersion of the materials is effected.

The benefits of each type of mixing machine are well recognised and understood by those skilled in the field. Since there are different phases in a mixing cycle the design of any mixing machine is always a compromise of features to ensure that the discharged mix is of an acceptable standard. Attempts have been made to combine the advantages of each of the two machine types, generally by incorporating features of the tangential machine into the intermeshing type. Such designs have often included the reduction of the leading angle of the helical wing of the intermeshing rotor to force material to flow over the wing earlier in the mixing cycle and to attempt to incorporate the compression or rolling action of the tangential rotor machine into the intermeshing rotor machine.

It is an object of the present invention to mitigate the aforesaid disadvantages of existing mixing technology and to provide for an improved mixing machine.

According to a first aspect of the present invention there is provided a mixing machine comprising a mixing chamber in which there are disposed at least two rotors arranged for rotation in opposite directions about respective rotational axes, at least one of the rotors having a projection that extends along at least a part of the axial length of the rotor and the rotors being rotatable so as to present a leading face of the projection to the material being mixed, wherein the leading face has a discontinuity in its profile along the axial direction of the rotor so as to define first and second portions, a majority of the leading face of the first portion being concave and a majority of the leading face of the second portion being convex.

The invention thus exploits the advantages of both conventional tangential (in which the leading face of a wing is convex) and intermeshing (in which the leading face of a wing is concave) rotors. Each projection may have a tip that defines a surface facing a substantially complementary wall of the mixing chamber, there being a clearance between the surface and the wall.

Preferably both rotors have such a projection and the loci defined by the periphery of the rotors during rotation intersect one another.

The ratio of the axial length of the first portion to the total length of the rotor may be anywhere in the range 0.1 to 0.9 but is preferably 0.6 to 0.8.

The surface of the tip of the first portion preferably increases in circumferential length in the axial direction of the rotor. The ratio of the circumferential length at each end of the first portion may be in the range 1.1 to 10 but is preferably 1.5 to 3.

The circumferential length of the tip of the second portion of the projection is preferably consistent in the axial direction of the rotor and may be between 3% and 50% of the maximum circumferential length of the tip of the first portion but is preferably between 3% and 15%.

The height of the second portion of the projection above the rotor may be lower than or equal to the height of the first portion of the projection. The height of the second portion may be between 25% and 100% of the height of the first portion but is preferably in the range 70% to 90%.

The clearance defined between tip surface and the mixing chamber wall may decrease in the direction of rotation of the rotor by virtue, for example, of the surface being tapered.

According to a second aspect of the present invention there is provided a mixing machine comprising a mixing chamber in which there are disposed at least two rotors arranged for rotation in opposite directions about respective rotational axes, at least one of the rotors having a projection that extends axially along the rotor and has a tip defining a circumferential surface whose circumferential length increases in the axial direction of the rotor.

According to a third aspect of the present invention there is provided a mixing machine comprising a mixing chamber in which there are disposed at least two rotors arranged for rotation in opposite directions about respective rotational axes, wherein at least one of the rotors has a projection that extends axially along the rotor, the projection having a tip defining a circumferential surface that forms at least 5% of the circumference of the rotor and is tapered so that the clearance defined between the tip surface and a wall of the mixing chamber decreases in the direction of rotation of the rotor.

A specific embodiment of the present invention will now be described, by way of example only, with reference to the accompanying drawings in which:

Figure 1 is a schematic representation of a section through a mixing chamber of a mixing machine of the present invention;

Figure 2 is a plan view of the unwrapped envelope of a rotor of the mixing machine of figure 1;

Figure 3 is an end view of the rotor in the direction of arrow X of figure 2; Figure 4 is an end view of the rotor in the direction of arrow Y of figure 2; and Figure 5 is a cross section through a leading face of a main wing of the rotor of figure 2.

Referring now to the drawings, the exemplary mixing machine is a high- powered, heavy duty machine that is intended for the mixing of rubber and polymeric compounds. The machine has a housing 1 having an internal wall la that defines a mixing chamber 2 in which two parallel contra-rotating rotors 3, 4 are disposed. A hydraulically or pneumatically operated ram 5 closes the chamber 2 and, in use, serves to force material towards the rotors 3, 4.

Each rotor 3, 4 is generally cylindrical and has a plurality of helical wings 6, 7,

8 that project radially outward towards the wall la of the mixing chamber 2. The wings 6, 7, 8 of one rotor 3, 4 are arranged in such a way that they project into spaces

9 defined between the wings 6, 7, 8 of the adjacent rotor 3, 4 and are disposed such that the loci described by the periphery of the wings 6, 7, 8 of one rotor 3, 4 intersect that of the other during rotation. At the nip defined between the intermeshing surfaces of the two rotors 3, 4 and between the surfaces of each rotor 3. 4 and the chamber wall la there is a small clearance 10 through which materials may pass during mixing. The wings 6, 7, 8 have profiles that have been carefully designed to provide for zones that act on the mix in different ways. A main wing 7 extends helically from a first end of each rotor 3, 4 to the other end and has a discontinuity 1 1 dividing its profile into first and second axial portions 12, 13. The first portion 12 has an axial length indicated by 1₂ and a tip 14 that, after a lead-in formation 15. increases in circumferential length from dimension w, to dimension w₂. The second portion 13 has an axial length indicated by 1, and a tip 16 with constant circumferential length indicated by w

The first portion 12 of the main wing 7 has a leading face 1 7 whose shape is consistent along its axial length. In cross-section a predominant portion of the leading face 17 extending between the base of the wing 7 and a position near the edge 18 defined at the intersection of the leading face 17 and the tip 14, is concave (represented by 17a in figure 5) with the remainder being planar (indicated by 17b in figure 5) and extending substantially in a radial direction. In contrast, the leading face 19 of the second portion 13 of the main wing 7 has a convex profile. Thus the configuration of the first portion 12 of the wing 7 resembles that of an intermeshing mixer, whereas the profile of the second portion 13 resembles that of a tangential rotor.

The relationship between the dimensions for a particular pair of rotors may be

dependent on the particular compound that is to be mixed. The ratio could have

a value of anywhere in the range 0.1 to 0.9 but it is more likely to fall in the range 0.6

VV2 to 0.8. Similarly the ratio — may be in the range 1.1 to 10 but is preferably in the

range 1.5 to 3. The ratio of the circumferential length of the second portion 13 of the

main wing 7 to that of the adjacent first portion, i.e. — , will varv depending on the ϊl'2 compound to be mixed but may be in the range 0.03 to 0.5 with a preferred figure of between 0.03 and 0.15.

The dimension w, of the wing tip is at least 5% of the circumference of the rotor. The height h of the second portion of the main wing 7 may be anywhere in the range 25% to 100% of the height of the first portion 12 of the main wing 7 although a preferred figure is likely to be in the range 70% to 90% of that height.

In certain embodiments of the machine the surface of the wing tip 14 of the first portion 12 may be tapered so that the clearance between the tip 14 and the chamber wall la decreases in the direction of rotation of the rotor 3,4. The angle of incline of the taper is relatively small subtending an angle of between 1 second and 10 degrees to a conventional rotor concentric surface. The taper is indicated by the change in height t in figure 3.

In use, material to be mixed is introduced into a hopper (not shown) whilst the ram 5 is raised so as to permit the materials to pass into the mixing chamber 2. The ram 5 is then operated to move the material towards the rotors 3,4. After the material has been mixed by the rotors and dispersed it is discharged from an outlet door (not shown) at the bottom of the mixing chamber 2.

At the beginning of the mixing cycle the material is drawn into the nip between the rotors 3,4 and the leading face 17 of the first portion 12 of the main wing 7 ensures rapid ingestion. Initially, the ingested material is relatively hard and flows along the concave leading face 17 of the first portion 12 of the main wing 7 until it encounters the convex leading face 18 of the second portion 13. At this point the material is worked between the second portion 13 of the wing 7 and the wall la of the mixing chamber 2 where it encounters a rolling and compressive action which provides a more rapid increase in temperature and reduction in viscosity of the material than occurs along the first portion 12. This temperature increase and viscosity reduction enables the material to flow more easily across the tip 14 of the first portion 12 of the main wing 7 where it is worked between the rotors 3,4 and between the rotors 3, 4 and the wall la of the mixing chamber 1 where it is subjected to significant dispersion and shear stress. Material is still caused to flow axially along the concave leading face 17 of the first portion 12 of the main wing 7 and will be subject to some temperature increase and viscosity reduction as it flows along this face. That material which flows over the tip of the wing 7 will move circumferentially across tip 14 (and tip 16) of wing 7. To maintain constant shear and flow across tip 14 of the first portion 12 of the main wing 7 with this reducing material viscosity, the circumferential width increases from w, at the end of the rotor 3, 4 to w₂ at the end adjacent to the discontinuity.

The profile of the second portion 13 of the wing 7 is akin to that of a tangential rotor and serves to provide a rapid increase in temperature of the material so that it is able to flow over the wing tip 14 surface of the first portion 17 much earlier in the mixing cycle.

The taper t on wing tip surface 14 presents a constant compression and shear force to the material in a circumferential direction as the increase in temperature and reduction in viscosity occurs in the material as it passes across face 14 of the first portion 12 of the main projection 7. Without this taper, the reduction in viscosity caused by temperature generated in the material would result in a reducing shear on the material as it passes across the projection.

The subordinate wings 6 and 8 are provided to direct material away from the ends of the chamber and back into the main mixing flow so as to prevent material from apply pressure to dust covers and bearings located at the rotor ends. In existing machines it has been known for material to egress from the machine at these points. The wings 6, 8 also provide a small contribution to the kneading action of the rotor.

By providing rotors with wings having profiles that define separate mixing zones which act on the material to be mixed in different ways the quality and efficiency of the mixing action is improved.

It will be appreciated that numerous modifications to the above described design may be made without departing from the scope of the invention as defined in the appended claims. For example, the leading face of the second portion of the main wing may not be convex along its entire length but may have, for example, a relatively small planar portion. In addition, the taper t is considered a feature that may be used on any form of rotor wing provided the circumferential length of the projection is at least 5% of the rotational circumference of the rotor. Moreover, the increase in circumferential length of the rotor may be used on rotors that do not have the discontinuity or the tapered wing tip.

Claims

1. A mixing machine comprising a mixing chamber in which there are disposed at least two rotors arranged for rotation in opposite directions about respective rotational axes, at least one of the rotors having an axially extending projection and being rotatable so as to present a leading face of the projection to the material being mixed, wherein the leading face has a discontinuity in its profile along the axial direction of the rotor so as to define first and second portions, a majority of the leading face of the first portion being concave and a majority of the leading face of the second portion being convex.

2. A mixing machine according to claim 1 , wherein each projection has a tip that defines a surface facing a substantially complementary wall of the mixing chamber, there being a clearance between the surface and the wall.

3. A mixing machine according to claim 2, wherein both rotors have such a projection and the loci defined by the periphery of the rotors during rotation intersect one another.

4. A mixing machine according to claim 2 or 3, wherein the surface of the tip of the first portion increases in circumferential length in the axial direction of the rotor.

5. A mixing machine according to claim 4. wherein the ratio of the circumferential lengths at each end of the first portion is in the range 1.1 to 10.

6. A mixing machine according to claim 4, where ratio of the circumferential lengths at each end of the first portion is in the range 1.5 to 3.

. A mixing machine according to any one of claims 2 to 6, wherein the ratio of the axial length of the first portion to the total length of the rotor is in the range 0.1 to 0.9.

8. A mixing machine according to any one of claims 2 to 6, wherein the ratio of the axial length of the first portion to the total length of the rotor is in the range 0.6 to 0.8.

9. A mixing machine according to any one of claims 2 to 8, wherein the circumferential length of the tip of second portion of the projection is consistent in the axial direction of the rotor and is between 3% and 50% of the maximum circumferential length of the tip of the first portion.

10. A mixing machine according to any one of claims 2 to 8, wherein the circumferential length of the tip of second portion of the projection is consistent in the axial direction of the rotor and is between 3% and 15% of the maximum circumferential length of the tip of the first portion.

1 1. A mixing machine according to any preceding claim, wherein the height of the second portion of the projection above the rotor is lower than or equal to the height of the first portion of the projection.

12. A mixing machine according to claim 11, wherein the height of the second portion is between 25% and 100% of the height of the first portion.

13. A mixing machine according to claim 1 1, wherein the height of the second portion is between 70% to 90% of the height of the first portion.

4. A mixing machine according to any one of claims 2 to 13, wherein the clearance defined between the tip surface and the mixing chamber wall decreases in the direction of rotation of the rotor.

15. A mixing machine comprising a mixing chamber in which there are disposed at least two rotors arranged for rotation in opposite directions about respective rotational axes, at least one of the rotors having a projection that extends axially along the rotor and has a tip defining a circumferential surface whose circumferential length increases along the axial direction.

16. A mixing machine comprising a mixing chamber in which there are disposed at least two rotors arranged for rotation in opposite directions about respective rotational axes, at least one of the rotors having a projection that extends axially along the rotor and has a tip defining a circumferential surface that forms at least 5% of the circumference of the rotor and is tapered so that the clearance defined between the tip surface and the mixing chamber wall decreases in the direction of rotation of the rotor.

17. A mixing machine substantially as hereinbefore described with reference to the accompanying drawings.