Method and apparatus for extrusion processing of high fiber content foods

Abstract

An extruder (20) is specifically designed for the production of animal feed products (e.g., aquatic feeds) containing substantial quantities of low-cost fibrous materials, such as rice byproducts, at high production rates. The extruder (20) includes an elongated barrel (22) with a screw assembly (24) within the barrel and an endmost extrusion die assembly (34). The screw assembly (24) includes an inlet screw assembly (42) and a processing screw assembly (44). The assembly (44) includes screw components (50-56) of differential pitch to present a long pitch inlet section (64) and a tight pitch discharge section (68). Materials passing through the screw assembly (24) are successively subjected to high levels of steam injection (STE) followed by high levels of friction and shear (SME), so that the STE/SME ratio is at least about 6/1.

Claims

1. A single screw extruder processing screw assembly comprising a plurality of screw components in end-to-end alignment with each screw component including an elongated shaft and outwardly extending helical flighting along the length of said shaft, said flighting being of the same hand and presenting an inlet portion, an intermediate portion, and a discharge portion, the pitch x diameter values of said inlet, intermediate, and discharge portions being different, and including at least one flow-restricting element between the discharge portion of one of said components, and the inlet portion of the next adjacent component, said inlet portion having a length L.sub.1, a fighting diameter D.sub.1, and a pitch P.sub.1, said intermediate portion comprising first and second sub-portions, said first sub-portion having a length L.sub.2, a flighting diameter D.sub.2, and a pitch P.sub.2, said second sub-portion having a length L.sub.3, a fighting diameter D.sub.3, and a pitch P.sub.3, and said discharge portion having a length L.sub.4, a flighting diameter D.sub.4, and a pitch P.sub.4, said inlet portion having an L.sub.1/D.sub.1 ratio of from about 0.8-2 and a pitch P.sub.1D.sub.1 of from about 1.5-2.8, said first sub-portion having an L.sub.2/D.sub.2 ratio of from about 0.1-0.7 and a pitch P.sub.2D.sub.2 of from about 1.0-2.0, said second sub-portion having an L.sub.3/D.sub.3 ratio of from about 0.05-0.9 and a pitch P.sub.3D.sub.3 of from about 0.5-2.0, said discharge portion having an L.sub.4/D.sub.4 ratio of from about 0.1-0.9 and a pitch P.sub.4D.sub.4 of from about 0.1-0.9, the length L.sub.1 being greater than the individual lengths L.sub.2, L.sub.3, and L.sub.4, and also greater than the combined length of L.sub.2 and L.sub.3.

2. The assembly of claim 1, said inlet portion having a wrap W.sub.1 of from about 180-450, said first sub-portion having a wrap W.sub.2 of from about 45-180 said second sub-portion having a wrap W.sub.3 of from about 90-360, and said discharge portion having a wrap W.sub.4 of from about 180-450.

3. The assembly of claim 1, said inlet portion having a fighting surface S.sub.1 of from about 1245-2105 sq.Math.cm, said first sub-portion having a fighting surface S.sub.2 of from about 318-537 sq.Math.cm, said second sub-portion having a flighting surface S.sub.3 of from about 501-846 sq.Math.cm, and said discharge portion having a fighting surface S.sub.4 of from about 650-1098 sq.Math.cm.

4. The assembly of claim 1, said inlet portion having a free volume V.sub.1 of from about 6870-11610 cc, said first sub-portion having a free volume V.sub.2 of from about 1500-2536 cc, said second sub-portion having a free volume V.sub.3 of from about 2160-3173 cc, and said discharge portion having a free volume V.sub.4 of from about 1563-2642 cc.

5. The assembly of claim 1, the pitch P.sub.1 of said inlet portion throughout the axial length thereof being greater than the pitch P.sub.4 of said discharge portion.

6. The assembly of claim 1, said L.sub.1/D.sub.1 being greater than any of said L.sub.2/D.sub.2, L.sub.3/D.sub.3, or L.sub.4/D.sub.4.

7. The assembly of claim 1, said P.sub.1D.sub.1 being greater than any of said P.sub.2D.sub.2, P.sub.3D.sub.3, or P.sub.4D.sub.4.

8. The assembly of claim 1, said W.sub.4 being greater than any of said W.sub.1, W.sub.2, or W.sub.3.

9. The assembly of claim 1, said S.sub.1 being greater than any of said S.sub.2, S.sub.3, or S.sub.4.

10. The assembly of claim 1, said V.sub.1 being greater than any of said V.sub.2, V.sub.3, or V.sub.4.

11. The assembly of claim 1, said D.sub.1, D.sub.2, D.sub.3, and D.sub.4 being equal.

12. A single screw extruder comprising: an elongated barrel having an inlet adjacent one end thereof and a restricted opening die assembly adjacent the opposite end thereof; a single axially rotatable processing screw assembly located within said barrel between said inlet and said die assembly, said assembly comprising a plurality of screw components in end-to-end alignment with each screw component including an elongated shaft and outwardly extending helical fighting along the length of said shaft, said flighting being of the same hand and presenting an inlet portion, an intermediate portion, and a discharge portion, the pitch x diameter values of said inlet, intermediate, and discharge portions being different, and including at least one flow-restricting element between the discharge portion of one of said components, and the inlet portion of the next adjacent component, said inlet portion having a length L.sub.1, a fighting diameter D.sub.1, and a pitch P.sub.1, said intermediate portion comprising first and second sub-portions, said first sub-portion having a length L.sub.2, a fighting diameter D.sub.2, and a pitch P.sub.2, said second sub-portion having a length L.sub.3, a fighting diameter D.sub.3, and a pitch P.sub.3, and said discharge portion having a length L.sub.4, a flighting diameter D.sub.4, and a pitch P.sub.4, said inlet portion having an L.sub.1/D.sub.1 ratio of from about 0.8-2 and a pitch P.sub.1D.sub.1 of from about 1.5-2.8, said first sub-portion having an L.sub.2/D.sub.2 ratio of from about 0.1-0.7 and a pitch P.sub.2D.sub.2 of from about 1.0-2.0, said second sub-portion having an L.sub.3/D.sub.3 ratio of from about 0.05-0.9 and a pitch P.sub.3D.sub.3 of from about 0.5-2.0, said discharge portion having an L.sub.4/D.sub.4 ratio of from about 0.1-0.9 and a pitch P.sub.4D.sub.4 of from about 0.1-0.9, the length L.sub.1 being greater than the individual lengths L.sub.2, L.sub.3, and L.sub.4, and also greater than the combined length of L.sub.2 and L.sub.3.

13. The extruder of claim 12, said inlet portion having a wrap W.sub.1 of from about 180-450, said first sub-portion having a wrap W.sub.2 of from about 45-180 said second sub-portion having a wrap W.sub.3 of from about 90-360, and said discharge portion having a wrap W.sub.4 of from about 180-450.

14. The extruder of claim 12, said inlet portion having a fighting surface S.sub.1 of from about 1245-2105 sq.Math.cm, said first sub-portion having a flighting surface S.sub.2 of from about 318-537 sq.Math.cm, said second sub-portion having a fighting surface S.sub.3 of from about 501-846 sq.Math.cm, and said discharge portion having a fighting surface S.sub.4 of from about 650-1098 sq.Math.cm.

15. The extruder of claim 12, said inlet portion having a free volume V.sub.1 of from about 6870-11610 cc, said first sub-portion having a free volume V.sub.2 of from about 1500-2536 cc, said second sub-portion having a free volume V.sub.3 of from about 2160-3173 cc, and said discharge portion having a free volume V.sub.4 of from about 1563-2642 cc.

16. The extruder of claim 12, the pitch P.sub.1 of said inlet portion throughout the axial length thereof being greater than the pitch P.sub.4 of said discharge portion.

17. The extruder of claim 12, said L.sub.1/D.sub.1 being greater than any of said L.sub.2/D.sub.2, L.sub.3/D.sub.3, or L.sub.4/D.sub.4.

18. The extruder of claim 12, said P.sub.1D.sub.1 being greater than any of said P.sub.2D.sub.2, P.sub.3D.sub.3, or P.sub.4D.sub.4.

19. The extruder of claim 12, said W.sub.4 being greater than any of said W.sub.1, W.sub.2, or W.sub.3.

20. The extruder of claim 12, said S.sub.1 being greater than any of said S.sub.2, S.sub.3, or S.sub.4.

21. The extruder of claim 12, said V.sub.1 being greater than any of said V.sub.2, V.sub.3, or V.sub.4.

22. The extruder of claim 12, said D.sub.1, D.sub.2, D.sub.3, and D.sub.4 being equal.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a perspective view of the improved extruder in accordance with the invention, illustrated with valve-type steam injectors;

(2) FIG. 2 is a vertical sectional view of an extruder similar to that of FIG. 1, but showing the use of conventional tubular steam injectors;

(3) FIG. 3 is a sectional view of the outlet die end of the extruder depicted in FIGS. 1-2, and showing the orientation of steam injectors;

(4) FIG. 4 is a vertical sectional view of the mid-section of the extruder barrel, and illustrating the preferred rotary ball valve steam injectors;

(5) FIG. 5 is an elevational view of the preferred extruder screw assembly of the invention;

(6) FIG. 6 is an exploded view of the screw assembly illustrating the respective components and the drive connection thereof;

(7) FIG. 7 is a perspective view of one of the hexagonal couplers used in the preferred screw assembly;

(8) FIG. 8 is a perspective view of a manually adjustable mid-barrel valve forming a part of the preferred screw assembly;

(9) FIG. 9 is a perspective view of a mid-barrel valve mounting spacer used with the valve illustrated in FIG. 8; and

(10) FIG. 10 is an enlarged elevational view of the preferred screw component of the invention, illustrating various geometrical features of the component.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

(11) Turning now to the drawings, a single screw extruder 20 is illustrated in FIGS. 1 and 2, and generally includes an elongated barrel 22 with an elongated, axially rotatable screw 24 situated within the barrel 22. The barrel 22 has a plurality of tubular sections or heads 26, including an inlet head 26a, bolted together in an end-to-end relationship to present an internal bore 28 extending the full length of the barrel. In the depicted embodiment, each of the heads 26 save for inlet head 26a is equipped with an inner, helically ribbed sleeve 27.

(12) The inlet head 26a includes an upright, tubular material inlet 32 for feeding material into the barrel 22 for processing. The opposite end of the barrel 22 is equipped with a die assembly 34 presenting restrictive orifice outlets 34a for the material being processed (see FIG. 3). The barrel 22 is also equipped with a series of obliquely oriented steam injection ports 36 along the length thereof, together with a pair of manually operable back pressure valve assemblies 38, all of which are important for purposes to be explained. The screw 24 is operatively coupled with a schematically illustrated bearing assembly 40 and with a conventional drive motor (not shown). In general, comestible materials to be processed are passed into barrel 22 via inlet 32, and are subjected to increasing levels of temperature, pressure, and shear during passage through the barrel; the products are then forced through the orifices of die assembly 34 in order to form the product.

(13) The screw 24 generally has an inlet screw assembly 42 and a processing screw assembly 44. As illustrated, the inlet screw assembly 42 is located within inlet head 26a and the next adjacent head 26 (FIG. 2), whereas the processing screw assembly 44 extends from the forward end of assembly 42 to die assembly 34. The purpose of assembly 42 is to quickly convey material from inlet 32 toward and into the assembly 44, where the bulk of the processing of material occurs.

(14) The assembly 42 includes a short, relatively tight pitch screw element 46 directly beneath inlet 32, and a longer pitch element 48 leading towards the inlet end of assembly 44. A careful study of FIG. 2 will confirm that the inlet screw assembly 42 is identical with the later-described screw components forming a part of the processing screw assembly 44, except that the assembly 42 is reversed, as compared with these screw components.

(15) The processing screw assembly 44 includes a total of four identical screw components 50, 52, 54, and 56 located in end-to-end alignment, as best illustrated in FIGS. 2 and 5. The screw component 50 is an entrance component, the components 52 and 54 are middle components, and component 56 is the exit component.

(16) As indicated, the components 50-56 are identical, and are best described with reference to FIG. 10 where the entrance component 50 is illustrated. Specifically, the component 50 includes an elongated shaft 58 with outwardly extending helical flighting 60 along the length of the shaft, which presents an outer peripheral surface 62. The surface defines the flighting diameter D of the component. The configuration of the flighting 60 effectively creates three sections along the length of the component 50, namely an inlet section 64, an intermediate section 66, and a discharge section 68. The intermediate section 66 is in turn divided into a first subsection 70 and a second subsection 72. Each of the sections 64 and 68-72 presents an axial length L, a flighting pitch length, and a flighting wrap about the shaft 58.

(17) Referring first to the inlet section 64, it will be seen that there is a length L.sub.1 equal to 13.81275 inches or 1.625D, with a pitch of 18.417 inches or 2.17D, a flighting wrap of 270, a flighting surface area of 1619 sq cm, and a free volume of 8931 cc. The subsection 70 has a length L.sub.2 of 3.187 inches or 0.375D, a pitch of 12.750 inches or 1.5D, a flighting wrap of 90, a flighting surface area of 413 sq cm, and a free volume of 1950 cc. Subsection 72 has a length L.sub.3 of 4.25 inches or 0.5D, a pitch of 8.5 inches or 1D, a flighting wrap of 180, a flighting surface area of 651 sq cm, and a free volume of 2441 cc. Finally, the discharge section 68 has a length L.sub.4 of 4.25 inches or 0.5D, a pitch of 4.25 inches or 0.5D, a flighting wrap of 360 a flighting surface area of 845 sq cm, and a free volume of 2013 cc. Considering the entire screw component 50, the total flighting surface area of 3528 sq cm, and the total free volume is 18,883 cc. The screw diameter D is 8.5 inches, giving a total length/diameter ratio (L/D) of 3. Importantly, it will be seen that the length L.sub.1 is greater than the individual lengths L.sub.2, L.sub.3, and L.sub.4, and is moreover greater than the combined length of the intermediate section 66, namely L.sub.2+L.sub.3. In the depicted exemplary embodiment, the overall length of the component 50 is 25.5 inches, or 3D.

(18) The foregoing dimensions and features represent the presently most preferred screw component design. Of course, these are subject to variations depending upon the type of feed ingredients being processed, the desired throughput, and other factors. To this end, the following Table 1 sets forth broad and preferred ranges for these dimensions and features, some of which are set forth in terms of D, as indicated in FIG. 10. It will also be appreciated that variation in one of the dimensions, for example, may require corresponding changes in other dimensions or features, in order to provide an optimized screw component; however, these variations may be determined through routine testing.

(19) TABLE-US-00001 TABLE 1 Section No. Inlet 64 Subsection 70 Subsection 72 Discharge 68 Length/Diameter Broad 0.8-2 0.1-0.7 0.05-0.9 0.1-0.9 (L/D) Preferred 1.2-1.8 0.2-0.6 0.3-0.7 0.3-0.7 Pitch (xD) Broad 1.5-2.8 1.0-2.0 0.5-2.0 0.1-0.9 Preferred 1.8-2.5 1.2-1.8 0.8-1.4 0.3-0.7 Wrap () Broad 180-450 45-180 90-360 180-450 Preferred 200-360 60-120 150-240 240-400 Flighting Surface Broad 1245-2105 318-537 501-846 650-1098 Area (sq. cm) Preferred 1407-1861 359-475 566-749 735-972 Free Volume (cc) Broad 6870-11610 1500-2536 2160-3173 1563-2642 Preferred 7766-10270 1697-2244 2123-2807 1767-2337

(20) The screw 24 is preferably fabricated using a drive shaft 74 operably coupled to the assembly 40 and having a hex drive component 76 and a forwardly extending, smooth shaft 76a, which extends the full length of the screw 24. A hex coupler 78 is mounted on shaft 76a and is drivingly secured to the component 76, and has forwardly extending drive lugs 80. The lugs 80 drivingly interfit with the short pitch screw element 46, which likewise includes drive lugs 82. The remaining parts of the assembly 24 are similarly mounted on the shaft 76a and connected and interfitted end-to-end, so that all of the parts are ultimately driven via hex drive component 76. The outer end of the screw 24 has a retainer bolt assembly 77, which is secured to the butt end of the shaft 76a to complete the screw construction. It has been found that this screw construction is adequate for the extruder 20 and is less expensive than using a central splined shaft with complementally formed screw parts.

(21) As illustrated in FIGS. 5 and 6, a back pressure valve spacer mount 84 is interposed between the forward end of longer pitch screw element 48 and the inlet end of screw component 50; similarly, an identical spacer mount 86 is interposed between the discharge end of screw component 52 and the inlet end of screw component 54. Also, a frustoconical shear lock 88 is connected between the discharge end of screw component 50 and the inlet end of screw component 52. An identical shear lock 90 is interposed between the discharge end of screw component 54 and the inlet end of screw component 56.

(22) Each of the mounts 84, 86 supports a conventional back pressure valve assembly 38 (FIGS. 8-9). The assembly 38 includes a central opening 92 designed to fit over the mount 84 and a pair of stationary plates 94 having a series of circularly arranged and aligned apertures 96 formed therein. The assembly 38 also includes an inner rotatable plate 98 between the plates 94 likewise having through apertures 100. The plate 98 is rotatable via hand crank assembly 102 in order to selectively move the plate 98 relative to the plate 94, thereby permitting adjustment of the effective through passages provided by the openings 96, 100.

(23) As indicated previously, the barrel 24 has a plurality of obliquely oriented ports 36. These are strategically arranged so that steam is injected into the barrel at the regions of the inlet sections 64 of the screw components 50-56. Tubular injection inserts 103 may be located within the ports 36, which are connected with external water/steam lines (not shown). If desired, ball valve-operated injected assemblies 104 may be operably coupled with some or all of the ports. Each assembly 104 (FIG. 4) includes a selectively actuatable valve body 106 having an internal mechanical drive (not shown) with an outwardly extending, axially rotatable stem 108. The stem 108 is connected to a spherical valve ball 110 having a central passageway 112. The ball 110 is located within a tubular segment 114, which is received within an outer valve sleeve 116. Selective rotation of the ball 110 serves to open and close the valve 104 as desired. In preferred practice, the valve assembly 104 is an automated valve, which can be controlled as a part of an overall digital control system for the extruder 20. Further details regarding the valve 104 can be found in application for U.S. letters patent Ser. No. 13/937,573, filed Jul. 9, 2013, and incorporated by reference herein in its entirety.

(24) Operation

(25) The extruder 20 is specifically designed for the production of animal feeds, and especially aqua feeds, containing high quantities of fibrous ingredients. These feed formulations would also typically include sources of animal or marine protein (e.g., fish meal), vegetable proteins (e.g., soy meal), starch less than 30%, with a minimum of 10% (e.g., grains such as wheat or corn), oil or fat, and minor ingredients such as vitamin/mineral premixes.

(26) Suitable fibrous ingredients include rice byproducts (e.g., hulls and bran), wheat bran, wheat middlings, distillers' dried grains, and byproducts from the oil seed industry including cottonseed cake, copra meal, groundnut meal, palm kernel meal, citrus pulp, sugar beet pulp, bagasse, linseed meal, sunflower meal, soy hulls, feather meal, guar meal, banana meal, rapeseed meal, canola meal, and mustard seed meal, and mixtures thereof.

(27) The initial ingredients are passed in serial order through a preconditioner and then through the extruder 20. In the preconditioner, the feed ingredients are moisturized and at least partially cooked before extrusion. The preconditioner may be any one of a number of devices, such as Wenger preconditioners commercialized under the designations DDC or HIP. The DDC preconditioners are the type disclosed in U.S. Pat. No. 4,752,139, whereas the HIP preconditioners are disclosed in U.S. Pat. No. 7,674,492. Both of these patents are incorporated herein in their entireties. Generally, the preconditioner is operated so as to achieve a temperature of from about 60-100 C., with a residence time of from about 15 seconds-3 minutes, and more preferably from about 2-3 minutes to obtain the maximum amount of hydration of the feed ingredients and preliminary cooking thereof.

(28) The operating conditions of the extruder 20 are also variable, but, as a general proposition, the temperatures within barrel 22 range from about 25-180 C., more preferably from about 40-120 C., with generally higher temperatures as the material proceeds from inlet 32 through die assembly 34. Internal barrel pressures are typically within the range of 200-900 psi, more preferably from about 300-600 psi. Material residence times in the extruder range from about 8-40 seconds, more preferably from about 10-15 seconds.

(29) As the preconditioned starting materials pass into the barrel 22, they are first rapidly conveyed by the inlet screw assembly 42 towards the processing screw assembly 44. During such transfer, the materials pass through the first valve barrel 38. The material then is advanced along the length of the first component 50 by the inlet section 64 thereof towards and into the intermediate section 66. During this passage, steam is injected into the material, this being facilitated because of the free volume of the inlet section and the fact that it is not full of feed material ingredients. Furthermore, the material is rolled over the tips of the flighting (leakage flow) to facilitate mixing of the ingredients. Stated otherwise, in the inlet section, thermal energy input is maximized and the materials are subjected to distributive mixing to ensure that the injected steam is properly absorbed. During passage of the material through the intermediate zone 66, the material is compacted leading to the discharge section 68, where the barrel is full of material to increase friction and shear, thus maximizing SME. This process is repeated within the components 52, 54, and 56, whereupon the material is extruded through die assembly 34. It will also be noted that restrictive elements, namely the shear locks 88 and 90, and barrel valve 38, are positioned between adjacent screw components, in order to provide still further SME input.

(30) In one series of tests, the preferred extruder 20 was tested versus a conventional Wenger X165 single screw extruder heretofore used for the production of aquatic feeds. The same preconditioner was used in each test. The same feed ingredients were also used in each case, where the amount of fibrous ingredients exceeded 20% by weight. The following Table 2 sets for the results of these runs, wherein Runs 1-3 were carried out using the extruder of the invention, and Run 4 was carried out using the conventional extruder.

(31) TABLE-US-00002 TABLE 2 Run No. 1 2 3 4 Dry Feed Rate (kg/hr) 2000 2000 4554 4500 Steam/Water to 10/13 10/13 11/22 8/12.5 Preconditioner (%) Steam/Water to Extruder 8/5 5/5 4.8/3.1 5/2 (%) SME (kWhr/t) 13 14 18.1 38.3 STE (kWhr/t) 141 118 126 102 STE/SME Ratio 10.8/1 8.4/1 14.4/1 2.7/1 Product Density (g/l) 350 341 402 Product Moisture (%) 25.8 25.9 31.6
As is evident from the foregoing data, the present invention provides much higher STE/SME ratios, preferably at least about 6/1, and more preferably from about 7-15/1. At the same time, the products produced using he extrusion equipment of the invention were of high quality and fully commercially acceptable.