Self-cleaning plasticizing venting and extruding apparatus by co-rotating non-twin multi-screws and method thereof

Information

  • Patent Grant
  • 9174380
  • Patent Number
    9,174,380
  • Date Filed
    Thursday, June 9, 2011
    12 years ago
  • Date Issued
    Tuesday, November 3, 2015
    8 years ago
Abstract
A self-cleaning plasticizing venting and extruding apparatus by co-rotating non-twin multi-screws and a method thereof are provided, said apparatus comprises a screw mechanism, barrel, feeding port, venting port, discharging port, and driving mechanism. Said screw mechanism comprises non-uniform central screw and lateral screws, the axis of the central screw coincides with the barrel, and the lateral screws are provided on both sides of the central screw and engaged with the central screw; the contour lines of the threads of said central screw and said lateral screws are tangent to the inner wall of the barrel; and said driving mechanism is connected to the central screw and lateral screws. Each screw-uses an asymmetrical flow channel shape, so the flow space is asymmetric, and the compounding intensity and effectiveness enhanced. The dispersion and mixing effects are excellent, generating a self-cleaning effect. The system is suitable for high yield nano-material processing.
Description
CROSS-REFERENCE TO RELATED APPLICATIONS

The present application is a U.S. National Stage entry under 35 U.S.C. §371 of International Application No. PCT/CN2011/075550, filed on Jun. 9, 2011, designating the United States of America and published in Chinese on Dec. 15, 2011, which in turn claims priority to Chinese Application No. 201010201316.9, filed on Jun. 12, 2010 and Chinese Application No. 201110149868.4, filed on Jun. 7, 2011, each of which is hereby incorporated by reference in its entirety.


TECHNICAL FIELD

The present invention relates to a processing technique for plasticizing, venting and extruding polymeric materials, particularly to a self-cleaning plasticizing venting and extruding apparatus by co-rotating non-twin multi-screws and method thereof.


BACKGROUND ART

The co-rotating twin-screw extruders have been widely applied in the fields such as filling, modifying, blending, and reactive extruding polymeric materials, etc. The principle is that: the structures of the two screws are identical, when assembled, there is a certain phase angle between them, the centerline distance is related to the number of screw tips and the peak angle, and the rotation speeds of the two screws are the same during the processing process. To achieve the self-cleaning effect during the processing process, from the viewpoint of relative movement, the two screws keep constant in the phase therebetween, contact and make a translational movement each other. Although this structure can preliminarily solve the problems such as the poor mixing property, the poor self-cleaning property, and the poor venting effect, etc., during the material processing process, there are still the following defects: (1) as the shapes of the two screws are the same, there are consistency (symmetry) therebetween, so that there is a consistency in the geometrical space through which the fluids pass during they proceeding along the two screws, there is an absence in the conversion between the geometric shapes of the spaces for processing the fluids, the reorientation effect of the interface during the shearing process is attenuated, and the mixing effect is limited, especially, that most of the fluid mixing in the core region of the screw channels is still laminar mixing, and the interface is increased linearly with time; and (2) the studies have shown that the co-rotating twin screws can only make an effective mixing effect on the surface layer fluid near the wall region, especially in the engaging region, the effect is extraordinarily obvious, in general, and there is still an extremely large possibility for improvement in the fluid mixing in the core regions.


For this, as required, there is a need for providing an extruding process with a self-cleaning effect, and a well-mixing effect.


CONTENTS OF THE INVENTION

The primary purpose of the present invention is to overcome the defects and deficiencies in the prior art, to provide a self-cleaning plasticizing venting and extruding apparatus by co-rotating non-twin multi-screws having good plasticizing and mixing effects and having a self-cleaning effect during the polymeric materials processing process.


Another purpose of the present invention is to provide a self-cleaning plasticizing venting and extruding method by co-rotating non-twin multi-screws carried out by the above-mentioned apparatus.


The purposes of the present invention are carried out by the following technical solutions: a self-cleaning plasticizing venting and extruding apparatus by co-rotating non-twin multi-screws, comprising a screw mechanism, a barrel, a feeding port, a venting port, a discharging port, and a driving mechanism, wherein said driving mechanism is provided at the ends of the barrel respectively, and is connected to the screw mechanism; said screw mechanism is provided inside the barrel, and placed horizontally, and the inner section of the barrel is divided into a solid transporting zone, a melting zone, a venting zone and a compounding and extruding zone; said feeding port is provided above the barrel of the solid transporting zone, said venting port is provided above the barrel of the venting zone, both the feeding port and the venting port are communicated with the barrel; said discharging port is provided at the end of the barrel, said screw mechanism comprises non-uniform shaped central screw and lateral screws, the axis of the central screw is coincided with that of the barrel, the lateral screws are engaged with the central screw, and the contour lines of the threads of the central screw and the lateral screws are all tangent to the inner wall of the barrel; and said driving mechanism is connected to the central screw and the lateral screws respectively.


Said driving mechanism comprises a main electric motor and a toothed gearing mechanism which are interconnected with each other, and said toothed gearing mechanism is connected to the central screw and the lateral screws respectively. The peak angle of the screw ridge of said central screw is in a range of 0-180° (ie., the peak angle of the ridge of the screw in the cross-section of the vertical axis is in a range of 0-180°).


The rotation speeds of the central screw and the lateral screws can be the same, or different.


As a preferred embodiment, said lateral screws are two screws, left screw and right screw, which are provided on both sides of the central screw respectively, and both engaged with the central screw; the inner cavity of said barrel is consisted of three cylinder grooves which are communicated, each of the cylinder grooves are fitted with the left screw, the central screw and the right screw respectively; and the central axis distance from the cylinder grooves on both sides to the cylinder groove at the central position is equal to the centerline distance from the central screw to the left screw, and the right screw.


The phase angle difference between the positions of said left screw and said right screw is 0°, 90°, or 180°.


With the center points of the cylinder grooves of the barrel corresponding to the central screw and each of the lateral screws respectively as poles, and the rays elicited horizontally rightwards from the poles as polar axes, the shape curve of the cross-section of said central screw meets that:








when






0
°



θ


25
°


,



ρ


(
θ
)


=


(




0.32256
+

0.00392

θ

+

0.000309497






θ
2


-













2.57326
×

10

-
5




θ
3


+

9.28644
×

10

-
7




θ
4


+







1.8713
×

10

-
8




θ
5


-

8.12786
×

10

-
10




θ
6


-









9.61005
×

10

-
12




θ
7








)



D
0



;














when






25
°



θ


63
°


,



ρ


(
θ
)


=

0.5






D
0



;















when






63
°



θ


123
°


,











ρ


(
θ
)


=


(




0.5
+

0.000823


(

θ
-
63

)


-

0.00134



(

θ
-
63

)

2


+







8.00734
×

10

-
5





(

θ
-
63

)

3


-

2.14653
×

10

-
6











(

θ
-
63

)

4

+

2.76223
×

10

-
8





(

θ
-
63

)

5


-






1.37762
×

10

-
10





(

θ
-
63

)

6





)



D
0



;















when






123
°



θ


147
°


,











ρ


(
θ
)


=


(




0.25291
-

0.00207


(

θ
-
123

)


+







0.000573645



(

θ
-
123

)

2


-

8.45874
×

10

-
5











(

θ
-
123

)

3

+

6.53416
×

10

-
6





(

θ
-
123

)

4


-







2.56256
×

10

-
7





(

θ
-
123

)

5


+

4.47098
×









10

-
9





(

θ
-
123

)

6


-

2.03618
×

10

-
11





(

θ
-
123

)

7






)



D
0



;















when






147
°



θ


205
°


,











ρ


(
θ
)


=


(




0.25374
+

0.000730048






(

θ
-
147

)


-







0.000156535







(

θ
-
147

)

2


+

3.73081
×

10

-
5











(

θ
-
147

)

3

-

3.07839
×

10

-
6





(

θ
-
147

)

4


+







1.32913
×

10

-
7





(

θ
-
147

)

5


-

3.10949
×

10

-
9











(

θ
-
147

)

6

+

3.74465
×

10

-
11





(

θ
-
147

)

7


-






1.81606
×

10

-
13





(

θ
-
147

)

8





)



D
0



;















when






205
°



θ


243
°


,



ρ


(
θ
)


=

0.5


D
0



;















when






243
°



θ


307
°


,







ρ


(
θ
)


=


(




0.5
+

0.00369


(

θ
-
243

)


-

0.00226



(

θ
-
243

)

2


+







0.000184965



(

θ
-
243

)

3


-

794221
×

10

-
6





(

θ
-
243

)

4


+







2.00615
×

10

-
7





(

θ
-
243

)

5


-

2.9807
×

10

-
9





(

θ
-
243

)

6


+







2.4097
×

10

-
11





(

θ
-
243

)

7


-

8.17763
×

10

-
14





(

θ
-
243

)

8






)



D
0



;















when






307
°



θ


323
°


,







ρ


(
θ
)


=


(




0.2568
-

0.00882


(

θ
-
307

)


+

0.00414



(

θ
-
307

)

2


-







0.000908651



(

θ
-
307

)

3


+

0.000100777



(

θ
-
307

)

4


-







5.50309
×

10

-
6





(

θ
-
307

)

5


+

1.20454
×

10

-
7





(

θ
-
307

)

6


-






1.95559
×

10

-
10





(

θ
-
307

)

7





)



D
0



;















when






323
°



θ


360
°


,










°


ρ



(
θ
)


=


(




0.25618
+

0.00082668


(

θ
-
323

)


-
0.000319894








(

θ
-
323

)

2

+

4.17742
×

10

-
5





(

θ
-
323

)

3


-

2.08266
×









10

-
6





(

θ
-
323

)

4


+

4.80871
×

10

-
8





(

θ
-
323

)

5


-

4.18424
×








10

-
10





(

θ
-
323

)

6





)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape of the cross-section of said left screw is the same as the curve shape formed after the cross-section of the right screw is rotated counterclockwise by 180° along the center point of the cylinder groove of the barrel corresponding to the central screw; the shape curve of the cross-section of said right screw meets that:













when






0
°



θ


80
°


,











ρ


(
θ
)


=


(




0.28446
+

0.00173

θ

-

4.07776
×

10

-
6




θ
2


+







4.49932
×

10

-
7




θ
3


-

3.26681
×

10

-
2




θ
4






)



D
0



;















when






80
°



θ


100
°


,







ρ


(
θ
)


=


(




0.49331
+

0.00156


(

θ
-
80

)


+

3.82324
×

10

-
6





(

θ
-
80

)

2


-







4.32369
×

10

-
5





(

θ
-
80

)

3


+

5.05212
×

10

-
6





(

θ
-
80

)

4


-







2.3955
×

10

-
7





(

θ
-
80

)

5


+

4.02621
×

10

-
3





(

θ
-
80

)

6






)



D
0



;















when






100
°



θ


229
°


,











ρ


(
θ
)


=


(




0.49336
-

0.00325


(

θ
-
100

)


-

4.70431
×









10

-
6





(

θ
-
100

)

2


+

2.18207
×

10

-
7





(

θ
-
100

)

3


-






7.76735
×

10

-
10





(

θ
-
100

)

4





)



D
0



;















when






229
°



θ


305
°


,



ρ


(
θ
)


=

0.25


D
0



;















when






305
°



θ


360
°


,







ρ


(
θ
)


=


(




0.25
-

8.84562
×

10

-
6




(

θ
-
305

)


+

2.30409
×









10

-
6





(

θ
-
305

)

2


-

8.10513
×

10

-
7





(

θ
-
305

)

3


+







2.00086
×

10

-
3





(

θ
-
305

)

4


-

1.56195
×

10

-
10





(

θ
-
305

)

5






)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


or,


the shape curve of the cross-section of said central screw meets that:













when






0
°



θ


23
°


,











ρ


(
θ
)


=


(




0.39546
+

0.00436





θ

-

0.000328898






θ
2


+







0.00049615






θ
1


-

2.50164
×

10

-
1




θ
4


+

5.0823
×









10

-
11




θ
2


-

4.85534
×

10

-
10




θ
1






)



D
0



;















when






23
°



θ


145
°


,











ρ


(
θ
)


=


(




0.48059
+

0.000898536






(

θ
-
23

)


-







0.000962297



(

θ
-
23

)

2


+

5.01749
×

10

-
3











(

θ
-
23

)

1

-

1.28633
×

10

-
1





(

θ
-
23

)

4


+







1.88747
×

10

-
11





(

θ
-
23

)

3


-

1.6028
×









10

-
10





(

θ
-
23

)

1


+

7.32557
×

10

-
11





(

θ
-
23

)

7


-






1.39342
×

10

-
15





(

θ
-
23

)

11





)



D
0



;















when






145
°



θ


202
°


,






ρ


(
θ
)


=


(




0.35035
-

0.000044154


(

θ
-
145

)


+

6.21993
×









10

-
5





(

θ
-
145

)

2


-

8.31288
×

10

-
1





(

θ
-
145

)

1


+

6.56112
×









10

-
7





(

θ
-
145

)

4


-

2.23522
×

10

-
11





(

θ
-
145

)

3


+

3.57533
×









10

-
10





(

θ
-
145

)

1


-

2.18353
×

10

-
12





(

θ
-
145

)

7






)



D
0

















when






202
°



θ


225
°


,











ρ


(
θ
)


=


(




0.48074
-

0.00133


(

θ
-
202

)


+
0.000542495








(

θ
-
202

)

2

-

0.00148596



(

θ
-
202

)

1


+

8.56691
×









10

-
1





(

θ
-
202

)

4


-

1.51835
×

10

-
7





(

θ
-
202

)

3






)



D
0



;















when






225
°



θ


325
°


,







ρ


(
θ
)


=


(




0.34927
-

0.00583


(

θ
-
225

)


+
0.000183457








(

θ
-
225

)

2

-

5.41662
×

10

-
1





(

θ
-
225

)

1


+

1.25448
×









10

-
7





(

θ
-
225

)

4


-

1.7397
×

10

-
5





(

θ
-
225

)

3


+

1.27967
×









10

-
11





(

θ
-
225

)

1


-

3.77702
×

10

-
14





(

θ
-
225

)

7






)



D
0



;















when






325
°



θ


351
°


,











ρ


(
θ
)


=


(




0.35169
-

0.000591024


(

θ
-
325

)


+







0.000116942







(

θ
-
325

)

2


-

8.07623
×









10

-
1





(

θ
-
325

)

1


+

3.51208
×

10

-
7





(

θ
-
325

)

4


-






5.2224
×

10

-
9





(

θ
-
325

)

3





)



D
0



;















when






351
°



θ


360
°


,











ρ


(
θ
)


=


(




0.37187
+

0.00178


(

θ
-
315

)


+
0.000238541








(

θ
-
351

)

2

-

1.61095
×

10

-
5





(

θ
-
351

)

1






)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape of the cross-section of said left screw is the same as the curve shape formed after the cross-section of the right screw is rotated counterclockwise by 180° along the center point of the cylinder groove of the barrel corresponding to the central screw; the shape curve of the cross-section of said right screw meets that:













when






0
°




θ
°



13
°


,











ρ


(
θ
)


=


(




0.49645
+

0.00025651





2

θ

+

0.00014972





5


θ
2


-







2.18392
×

10

-
5




θ
3


+

6.8663
×

10

-
7




θ
4






)



D
0



;















when






13
°



θ


119
°


,







ρ


(
θ
)


=


(




0.49672
+

0.0016


(

θ
-
13

)


-

0.00016043





9



(

θ
-
13

)

2


+







3.66195
×

10

-
6





(

θ
-
13

)

3


-

4.18633
×

10

-
8





(

θ
-
13

)

4


+







2.44243
×

10

-
10





(

θ
-
13

)

5


-

5.70929
×

10

-
13





(

θ
-
13

)

6






)



D
0



;















when






119
°



θ


360
°


,











ρ


(
θ
)


=


(




0.39857
-

0.00147


(

θ
-
119

)


-

2.94068
×

10

-
5











(

θ
-
119

)

2

+

6.44036
×

10

-
7





(

θ
-
119

)

3


-

4.79428
×









10

-
9





(

θ
-
119

)

4


+

1.70193
×

10

-
11





(

θ
-
119

)

5


-






2.30605
×

10

-
14





(

θ
-
119

)

6





)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


or, the shape curve of the cross-section of said central screw meets that:








when






0
°



θ


27
°


,



ρ


(
θ
)


=


(




0.28995
+

0.0029





θ

+

0.00010458





6


θ
2


+







1.35828
×

10

-
6




θ
3


-

6.80098
×

10

-
8




θ
4


+






3.45975
×

10

-
9




θ
5





)



D
0



;














when






27
°



θ


36
°


,











ρ


(
θ
)


=


(




0.4847
+

0.01065


(

θ
-
27

)


-

0.00186



(

θ
-
27

)

2


+







5.1776
×

10

-
6





(

θ
-
27

)

3


+

1.23985
×

10

-
6





(

θ
-
27

)

4






)



D
0



;















when






36
°



θ


60
°


,











ρ


(
θ
)


=


(




0.4418
-

0.01131


(

θ
-
36

)


+

0.00029056





3



(

θ
-
36

)

2


-







3.02877
×

10

-
6





(

θ
-
36

)

3


-

2.6637
×

10

-
8





(

θ
-
36

)

4






)



D
0



;















when






60
°



θ


120
°


,











ρ


(
θ
)


=


(




0.287
-

0.0025


(

θ
-
60

)


+

4.57118
×

10

-
5











(

θ
-
60

)

2

-

1.90487
×

10

-
7





(

θ
-
60

)

3


+

2.28021
×








10

-
9





(

θ
-
60

)

4





)



D
0



;















when






120
°



θ


147
°


,







ρ


(
θ
)


=


(




0.28995
+

0.0029


(

θ
-
120

)


+

0.00010458





6



(

θ
-
120

)

2


+







1.35828
×

10

-
6





(

θ
-
120

)

3


-

6.80098
×

10

-
8





(

θ
-
120

)

4


+






3.45975
×

10

-
9





(

θ
-
120

)

5





)



D
0



;















when






147
°



θ


156
°


,







ρ


(
θ
)


=


(




0.4847
+

0.01065


(

θ
-
147

)


-

0.00186



(

θ
-
147

)

2


+

5.1776
×









10

-
6





(

θ
-
147

)

3


+

1.23985
×

10

-
6





(

θ
-
147

)

4






)



D
0



;















when






156
°



θ


180
°


,







ρ


(
θ
)


=


(




0.4418
-

0.001131


(

θ
-
156

)


+

0.00029056





3



(

θ
-
156

)

2


-







3.02877
×

10

-
6





(

θ
-
156

)

3


-

2.66377
×

10

-
8





(

θ
-
156

)

4






)



D
0



;















when






180
°



θ


240
°


,







ρ


(
θ
)


=


(




0.287
-

0.0025


(

θ
-
180

)


+

4.57118
×

10

-
5





(

θ
-
180

)

2


-







1.90487
×

10

-
7





(

θ
-
180

)

3


+

2.28021
×

10

-
9





(

θ
-
180

)

4






)



D
0



;















when






240
°



θ


267
°


,







ρ


(
θ
)


=


(




0.28995
+

0.0029


(

θ
-
240

)


+

0.00010458





6



(

θ
-
240

)

2


+







1.35828
×

10

-
6





(

θ
-
240

)

3


-

6.80098
×

10

-
8





(

θ
-
240

)

4


+






3.45975
×

10

-
9





(

θ
-
240

)

5





)



D
0



;















when






267
°



θ


270
°


,







ρ


(
θ
)


=


(




0.4847
+

0.01065


(

θ
-
267

)


-

0.00186



(

θ
-
267

)

2


+







5.1776
×

10

-
6





(

θ
-
267

)

3


+

1.23985
×

10

-
6





(

θ
-
267

)

4






)



D
0



;















when






270
°



θ


300
°


,







ρ


(
θ
)


=


(




0.4418
-

0.01131


(

θ
-
270

)


+

0.00029056





3



(

θ
-
270

)

2


-







3.02877
×

10

-
6





(

θ
-
270

)

3


-

2.66377
×

10

-
8





(

θ
-
270

)

4






)



D
0



;















when






300
°



θ


360
°


,







ρ


(
θ
)


=


(




0.287
-

0.0025


(

θ
-
180

)


+

4.57118
×

10

-
5





(

θ
-
180

)

2


-







1.90487
×

10

-
7





(

θ
-
180

)

3


+

2.28021
×

10

-
9





(

θ
-
180

)

4






)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape of the cross-section of said left screw is the same as the curve shape of the cross-section of said right screw; and the shape curve of the cross-section of said right screw meets that:













when






0
°



θ


85
°


,







ρ


(
θ
)


=


(




0.32013
+

0.00068520





5

θ

+

0.00011173






θ
2


-







5.88903
×

10

-
6



+

1.80316
×

10

-
7




θ
4


-

3.03623
×

10

-
9




θ
5


+







2.64496
×

10

-
11




θ
6


-

9.32845
×

10

-
14




θ
7






)



D
0



;















when






85
°



θ


95
°


,







ρ


(
θ
)


=


(




0.494681
+

0.00179


(

θ
-
85

)


-

0.00047927





3



(

θ
-
85

)

2


+







0.00010662



(

θ
-
85

)

3


-

1.63619
×

10

-
5





(

θ
-
85

)

4


+







1.24974
×

10

-
6





(

θ
-
85

)

5


-

3.77964
×

10

-
8





(

θ
-
85

)

6






)



D
0



;















when






95
°



θ


180
°


,







ρ


(
θ
)


=


(




0.494832
-

0.00076124





6


(

θ
-
95

)


-

0.00012610





1



(

θ
-
95

)

2


+







4.25652
×

10

-
6





(

θ
-
95

)

3


-

7.13683
×

10

-
8





(

θ
-
95

)

4


+

5.9942
×









10

-
10





(

θ
-
95

)

5


-

1.98695
×

10

-
12





(

θ
-
95

)

6






)



D
0



;















when






180
°



θ


360
°


,







ρ


(
θ
)


=


(




0.31789
-

0.00133


(

θ
-
180

)


-

8.60877
×

10

-
6





(

θ
-
180

)

2


+







5.0898
×

10

-
7





(

θ
-
180

)

3


-

7.16212
×

10

-
9





(

θ
-
180

)

4


+







5.3005
×

10

-
11





(

θ
-
180

)

5


-

2.05365
×

10

-
13





(

θ
-
180

)

6


+







3.64972
×

10

-
16





(

θ
-
180

)

7


-

1.76708
×

10

-
19





(

θ
-
180

)

8






)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


or,


the shape curve of the cross-section of said central screw meets that:













when






0
°



θ


50
°


,



ρ


(
θ
)


=

0.5






D
0



;















when






50
°



θ


90
°


,







ρ


(
θ
)


=


(




0.5
-

0.00309


(

θ
-
50

)


+

0.00016833





1



(

θ
-
50

)

2


-

8.44083
×









10

-
6





(

θ
-
50

)

3


+

2.19035
×

10

-
7





(

θ
-
50

)

4


-

2.06434
×

10

-
9





(

θ
-
50

)

5






)



D
0



;















when






90
°



θ


101
°


,



ρ


(
θ
)


=

0.455






D
0



;















when






101
°



θ


181
°


,







ρ


(
θ
)


=


(




0.455
-

0.00143


(

θ
-
101

)


-

0.000793059



(

θ
-
101

)

2


+







6.51522
×

10

-
5





(

θ
-
101

)

3


-

2.66487
×

10

-
6





(

θ
-
101

)

4


+







6.20495
×

10

-
8





(

θ
-
101

)

5


-

8.26745
×

10

-
10





(

θ
-
101

)

6


+







5.86449
×

10

-
12





(

θ
-
101

)

7


-

1.71691
×

10

-
14





(

θ
-
101

)

8






)



D
0



;















when






181
°



θ


193
°


,



ρ


(
θ
)


=

0.25






D
0



;















when






193
°



θ


244
°


,







ρ


(
θ
)


=


(




0.25
+

0.000361178


(

θ
-
193

)


-

0.000107545



(

θ
-
193

)

2


+







0.00002068



(

θ
-
193

)

3


-

1.60164
×

10

-
6





(

θ
-
193

)

4


+

6.82867
×









10

-
8





(

θ
-
193

)

5


-

1.63573
×

10

-
9





(

θ
-
193

)

6


+

2.06803
×

10

-
11











(

θ
-
193

)

7

-

1.07375
×

10

-
13





(

θ
-
193

)

8






)



D
0



;















when






244
°



θ


353
°


,







ρ


(
θ
)


=


(




0.31875
-

0.00104


(

θ
-
244

)


-

3.31524
×

10

-
5





(

θ
-
244

)

2


+







4.32237
×

10

-
6





(

θ
-
244

)

3


-

1.67168
×

10

-
7





(

θ
-
244

)

4


+







3.54572
×

10

-
9





(

θ
-
244

)

5


-

4.16652
×

10

-
11





(

θ
-
244

)

6


+







2.55218
×

10

-
13





(

θ
-
244

)

7


-

6.34643
×

10

-
16





(

θ
-
244

)

8






)



D
0



;















when






353
°



θ


360
°


,



ρ


(
θ
)


=

0.5






D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape of the cross-section of said left screw is the same as the curve shape of the cross-section of said right screw; the shape curve of the cross-section of said right screw meets that:













when






0
°



θ


12
°


,



ρ


(
θ
)


=

0.5






D
0



;















when






12
°



θ


93
°


,







ρ


(
θ
)


=


(




0.5
-

0.00165


(

θ
-
12

)


-

0.00013491





5



(

θ
-
12

)

2


+







0.00001181





4



(

θ
-
12

)

3


-

4.87051
×

10

-
7





(

θ
-
12

)

4


+

1.1766
×









10

-
8





(

θ
-
12

)

5


-

1.64659
×

10

-
10





(

θ
-
12

)

2


+

1.23355
×

10

-
12











(

θ
-
12

)

7

-

3.82327
×

10

-
15





(

θ
-
12

)

8






)



D
0



;















when






93
°



θ


173
°


,







ρ


(
θ
)


=


(




0.44967
-

0.0012


(

θ
-
93

)


-

0.000680386







(

θ
-
93

)

2


+

5.15007
×









10

-
5





(

θ
-
93

)

3


-

1.99396
×

10

-
6





(

θ
-
93

)

4


+

4.48589
×

10

-
8











(

θ
-
93

)

5

-

5.85347
×

10

-
10





(

θ
-
93

)

6


+

4.10152
×

10

-
12





(

θ
-
93

)

7


-






1.19263
×

10

-
14





(

θ
-
93

)

8





)



D
0



;















when






173
°



θ


230
°


,



ρ


(
θ
)


=

0.25






D
0



;















when






230
°



θ


272
°


,







ρ


(
θ
)


=


(




0.25
+

0.00057523





2


(

θ
-
230

)


-

0.00013443





3



(

θ
-
230

)

2


+







2.28201
×

10

-
5





(

θ
-
230

)

3


-

1.7105
×

10

-
6





(

θ
-
230

)

4


+







7.3701
×

10

-
8





(

θ
-
230

)

5


-

1.86726
×

10

-
9





(

θ
-
230

)

6


+







2.61628
×

10

-
11





(

θ
-
230

)

7


-

1.5782
×

10

-
13





(

θ
-
230

)

8






)



D
0



;















when






272
°



θ


283
°


,



ρ


(
θ
)


=

0.295






D
0



;















when






283
°



θ


360
°


,







ρ


(
θ
)


=


(




0.295
+

0.00013272





1


(

θ
-
293

)


+

4.58737
×

10

-
5





(

θ
-
283

)

2


-







3.34926
×

10

-
6





(

θ
-
283

)

3


+

2.15388
×

10

-
7





(

θ
-
283

)

4


-







6.89212
×

10

-
9





(

θ
-
283

)

5


+

1.18802
×

10

-
10





(

θ
-
283

)

6


-

1.04706
×









10

-
12





(

θ
-
283

)

7


+

3.70486
×

10

-
15





(

θ
-
283

)

8






)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw.


As another preferred solution, said lateral screw is only one screw, which is provided on the side of the central screw, and engaged with the central screw; the inner cavity of said barrel is consisted of two cylinder grooves which are communicated, each of the cylinder grooves is fitted with the lateral screw, and the central screw respectively; the central axis distance between the two cylinder grooves is equal to the centerline distance between the central screw and the lateral screw.


With the center points of the cylinder grooves of the barrel corresponding to the central screw and the lateral screw respectively as poles, and the rays elicited horizontally rightwards from the poles as polar axes,


the shape curve of the cross-section of said central screw is symmetric with respective to the ray of θ=120° and the ray of θ=240°, and the polar angle is within 0°≦θ≦120°, the corresponding curve meets that:













when





0


θ


2
°


,



ρ


(
θ
)


=

0.5






D
0



;















when






2
°



θ


58
°


,







ρ


(
θ
)


=


(




0.5
-

0.00243


(

θ
-
2

)


+

0.00106



(

θ
-
2

)

2


-

1.67316
×

10

-
4





(

θ
-
2

)

3


+







1.08849
×

10

-
5





(

θ
-
2

)

4


-

3.74006
×

10

-
7





(

θ
-
2

)

5


+

7.15583
×

10

-
9











(

θ
-
2

)

6

-

7.21345
×

10

-
11





(

θ
-
2

)

7


+

2.98968
×

10

-
13





(

θ
-
2

)

8






)



D
0



;















when






58
°



θ


62
°


,



ρ


(
θ
)


=

0.4






D
0



;















when






62
°



θ


118
°


,







ρ


(
θ
)


=


(




0.4
-

7.16547
×

10

-
4




(

θ
-
62

)


+

3.66366
×

10

-
4





(

θ
-
62

)

2


-







5.72993
×

10

-
5





(

θ
-
62

)

3


+

4.76052
×

10

-
6





(

θ
-
62

)

4


-







2.09619
×

10

-
7





(

θ
-
62

)

5


+

5.0282
×

10

-
9





(

θ
-
62

)

6


-







6.18021
×

10

-
11





(

θ
-
62

)

7


+

3.03396
×

10

-
13





(

θ
-
62

)

8






)



D
0



;















when






118
°



θ


120
°


,


ρ


(
θ
)


=

0.5






D
0








wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross section of said lateral screw is symmetric with respective to the ray of θ=0θ and the ray of θ=180° (ie., the positive direction of the X axis in the orthogonal coordinate system), and the polar angle is within 0°≦θ≦180°, the corresponding curve meets that:













when





0

°


θ


3

°


,



ρ


(
θ
)


=

0.4






D
0



;















when





3

°


θ


87

°


,











ρ


(
θ
)


=


(




0.40053
+

1.91042
×

10

-
4




(

θ
-
3

)


-







5.44854
×

10

-
5





(

θ
-
3

)

2


+

5.78786
×

10

-
6





(

θ
-
3

)

3


-







2.60181
×

10

-
7





(

θ
-
3

)

4


+

6.77081
×

10

-
9





(

θ
-
3

)

5


-







1.00659
×

10

-
10





(

θ
-
3

)

6


+

7.9546
×

10

-
13





(

θ
-
3

)

7


-






2.59711
×

10

-
15





(

θ
-
3

)

8





)



D
0



;















when





87

°


θ


93

°


,



ρ


(
θ
)


=

0.5






D
0



;















when





93

°


θ


177

°


,







ρ


(
θ
)


=


(




0.5
+

5.59592
×

10

-
4




(

θ
-
93

)


-







3.44997
×

10

-
4





(

θ
-
93

)

2


+

1.95669
×

10

-
5





(

θ
-
93

)

3


-







6.22514
×

10

-
7





(

θ
-
93

)

4


+

1.2176
×

10

-
8





(

θ
-
93

)

5


-







1.43316
×

10

-
10





(

θ
-
93

)

6


+

9.29081
×

10

-
13





(

θ
-
93

)

7


-






2.54457
×

10

-
15





(

θ
-
93

)

8





)



D
0



;















when





177

°


θ


180

°


,


ρ


(
θ
)


=

0.4






D
0








wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


or,


the shape curve of the cross-section of said central screw is symmetric with respective to the ray of θ=0° and the ray of θ=180°, and the polar angle is within 0°≦θ≦180°, the corresponding curve meets that:













when





0

°


θ


15

°


,



ρ


(
θ
)


=

0.5






D
0



;















when





15

°


θ


69.5

°


,







ρ


(
θ
)


=


(




0.5
-

0.00188


(

θ
-
15

)


-







8.21227
×

10

-
4





(

θ
-
15

)

2


+

8.53313
×

10

-
5





(

θ
-
15

)

3


-







4.61141
×

10

-
6





(

θ
-
15

)

4


+

1.48589
×

10

-
7





(

θ
-
15

)

5


-







2.82368
×

10

-
9





(

θ
-
15

)

6


+

2.90967
×

10

-
11





(

θ
-
15

)

7


-






1.25091
×

10

-
13





(

θ
-
15

)

8





)



D
0



;















when





69.5

°


θ


110.5

°


,



ρ


(
θ
)


=

0.35714






D
0



;















when





110.5

°


θ


165

°


,







ρ


(
θ
)


=


(




0.35714
+

3.98268
×

10

-
4




(

θ
-
110.5

)


-







1.91593
×

10

-
4





(

θ
-
110.5

)

2


+

3.54059
×

10

-
5





(

θ
-
110.5

)

3


-







2.64776
×

10

-
6





(

θ
-
110.5

)

4


+

1.08848
×

10

-
7





(

θ
-
110.5

)

5


-







2.49656
×

10

-
9





(

θ
-
110.5

)

6


+

3.00627
×

10

-
11





(

θ
-
110.5

)

7


-






1.48135
×

10

-
13





(

θ
-
110.5

)

8





)



D
0



;















when





165

°


θ


180

°


,



ρ


(
θ
)


=

0.5






D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross-section of said lateral screw is symmetric with respective to the ray of θ=0° and the ray of θ=180°, and the polar angle is within 0°≦θ≦180°, the corresponding curve meets that:













when





0

°


θ


41

°


,



ρ


(
θ
)


=

0.5






D
0



;















when





41

°


θ


150

°


,







ρ


(
θ
)


=


(




0.5
+

5.80648
×

10

-
4




(

θ
-
41

)


-







1.0674
×

10

-
4





(

θ
-
41

)

2


-

4.94415
×

10

-
7





(

θ
-
41

)

3









1.14699
×

10

-
7





(

θ
-
41

)

4


-

2.86057
×

10

-
9





(

θ
-
41

)

5









3.31268
×

10

-
11





(

θ
-
41

)

6


-

1.89458
×

10

-
13





(

θ
-
41

)

7








4.31702
×

10

-
16





(

θ
-
41

)

8





)



D
0



;















when





150

°


θ


180

°


,



ρ


(
θ
)


=

0.35714






D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


or,


the shape curve of the cross-section of said central screw is symmetric with respective to the ray of θ=120° and the ray of θ=240°, and the polar angle is within 0°≦θ≦120°, the corresponding curve meets that:













when





0

°


θ


10

°


,



ρ


(
θ
)


=

0.5






D
0



;















when





10

°


θ


58

°


,







ρ


(
θ
)


=


(




0.5
-

0.00831


(

θ
-
10

)


+







2.69315
×

10

-
4





(

θ
-
10

)

2


-

2.05095
×

10

-
5





(

θ
-
10

)

3


+







1.59416
×

10

-
6





(

θ
-
10

)

4


-

6.95534
×

10

-
8





(

θ
-
10

)

5


+







1.65362
×

10

-
9





(

θ
-
10

)

6


-

2.02237
×

10

-
11





(

θ
-
10

)

7


+






9.97816
×

10

-
14





(

θ
-
10

)

8





)



D
0



;















when





58

°


θ


62

°


,


ρ


(
θ
)


=

0.357143






D
0

















when





62

°


θ


110

°


,







ρ


(
θ
)


=


(




0.35714
-

4.90697
×

10

-
5




(

θ
-
62

)


+

1.02434
×

10

-
5





(

θ
-
62

)

2









1.22629
×

10

-
6





(

θ
-
62

)

3


1.76059
×

10

-
7





(

θ
-
62

)

4


-







1.56233
×

10

-
8





(

θ
-
62

)

5


+

5.21936
×

10

-
10





(

θ
-
62

)

6


-







7.85637
×

10

-
12





(

θ
-
62

)

7


+

4.47471
×

10

-
14





(

θ
-
62

)

8






)



D
0



;















when





110

°


θ


120

°


,



ρ


(
θ
)


=

0.5






D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross-section of said lateral screw is symmetric with respective to the ray of θ=0° and the ray of θ=180°, and the polar angle is within 0°≦θ≦180°, the corresponding curve meets that:













when





0

°


θ


30

°


,



ρ


(
θ
)


=

0.35714






D
0



;















when





30

°


θ


174

°


,







ρ


(
θ
)


=


(




0.35714
-

1.2981
×

10

-
4




(

θ
-
30

)


+

4.15281
×

10

-
5





(

θ
-
30

)

2


-







2.15177
×

10

-
6





(

θ
-
30

)

3


+

6.69687
×

10

-
8





(

θ
-
30

)

4


-







1.10347
×

10

-
9





(

θ
-
30

)

5


+

9.90148
×

10

-
12





(

θ
-
30

)

6


-







4.55739
×

10

-
14





(

θ
-
30

)

7


+

8.37526
×

10

-
17





(

θ
-
30

)

8






)



D
0



;















when





174

°


θ


180

°


,



ρ


(
θ
)


=

0.5






D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


or,


the shape curve of the cross-section of said central screw is symmetric with respective to the ray of θ=0°, the ray of θ=90°, and the ray of θ=270°, and the polar angle is within 0°≦θ≦90°, the corresponding curve meets that:













when





0

°


θ


3

°


,



ρ


(
θ
)


=

0.5






D
0



;















when





3

°


θ


87

°


,







ρ


(
θ
)


=


(




0.5
-

0.00776


(

θ
-
3

)


+







3.35014
×

10

-
5





(

θ
-
3

)

2


+

8.68488
×

10

-
6





(

θ
-
3

)

3


-







3.48947
×

10

-
7





(

θ
-
3

)

4


+

6.34905
×

10

-
9





(

θ
-
3

)

5


-







5.62555
×

10
11




(

θ
-
3

)

6


+

1.98268
×

10

-
13





(

θ
-
3

)

7






)



D
0



;















when





87

°


θ


90

°


,



ρ


(
θ
)


=

0.5






D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross-section of said lateral screw is symmetric with respective to the ray of θ=0° and the ray of θ=180°, and the polar angle is within 0°≦θ≦180°, the corresponding curve meets that:













when





0

°


θ


12

°


,



ρ


(
θ
)


=

0.35714






D
0



;















when





12

°


θ


180

°


,







ρ


(
θ
)


=


(




0.35714
+

1.16393
×

10

-
4




(

θ
-
12

)


+







1.09189
×

10

-
6





(

θ
-
12

)

2


+

1.02469
×

10

-
7





(

θ
-
12

)

3


-







7.39494
×

10

-
10





(

θ
-
12

)

4


-

2.22006
×

10

-
12





(

θ
-
12

)

5









5.1641
×

10

-
14





(

θ
-
12

)

6


-

1.7693
×

10

-
16





(

θ
-
12

)

7






)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


or,


the shape curve of the cross-section of said central screw is symmetric with respective to the ray of θ=0°, the ray of θ=72°, the ray of θ=144°, the ray of θ=216°, and the ray of θ=288°, and the polar angle is within 0°≦θ≦72°, the corresponding curve meets that:













when





0

°


θ


4

°


,



ρ


(
θ
)


=

0.5






D
0



;















when





4

°


θ


34

°


,







ρ


(
θ
)


=


(




0.5
-

0.02464


(

θ
-
4

)


+







0.00617



(

θ
-
4

)

2


-

9.00044
×

10

-
4





(

θ
-
4

)

3


+







7.03593
×

10

-
5





(

θ
-
4

)

4


-

2.98822
×

10

-
6





(

θ
-
4

)

5


+







6.51822
×

10

-
8





(

θ
-
4

)

6


-

5.71897
×

10

-
10





(

θ
-
4

)

7






)



D
0



;















when





34

°


θ


38

°


,



ρ


(
θ
)


=

0.4






D
0



;















when





38

°


θ


68

°


,







ρ


(
θ
)


=


(




0.4
+

2.66133
×

10

-
4




(

θ
-
38

)


-







4.49843
×

10

-
5





(

θ
-
38

)

2


+

3.42164
×

10

-
5





(

θ
-
38

)

3


-







4.56139
×

10

-
6





(

θ
-
38

)

4


+

3.02712
×

10

-
7





(

θ
-
38

)

5


-







9.6014
×

10

-
9





(

θ
-
38

)

6


+

1.16449
×

10

-
10





(

θ
-
38

)

7






)



D
0



;















when





68

°


θ


72

°


,



ρ


(
θ
)


=

0.5






D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross-section of said lateral screw is symmetric with respective to the ray of θ=0° and the ray of θ=180°, and the polar angle is within 0°≦θ≦180°, the corresponding curve meets that:













when





0

°


θ


20

°


,



ρ


(
θ
)


=

0.4






D
0



;















when





20

°


θ


170

°


,







ρ


(
θ
)


=


(




0.4
+

4.16738
×

10

-
4




(

θ
-
20

)


-







1.72721
×

10

-
5





(

θ
-
20

)

2


+

7.47552
×

10

-
7





(

θ
-
20

)

3


-







1.38142
×

10

-
8





(

θ
-
20

)

4


+

1.46263
×

10

-
10





(

θ
-
20

)

5


-







9.05881
×

10

-
13





(

θ
-
20

)

6


+

3.10626
×

10

-
15





(

θ
-
20

)

7


-






4.67939
×

10

-
18





(

θ
-
20

)

8





)



D
0



;















when





170

°


θ


180

°


,



ρ


(
θ
)


=

0.5






D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw.


The working principle of the above-mentioned apparatus is that: the main electric motor drives the toothed gearing mechanism, the toothed gearing mechanism drives the central screw and the two lateral screws to co-rotate around the respective axes, the rotation speeds of the central screw and the two lateral screws are the same or different, and the rotation speeds of the two lateral screws are the same. The materials enter the barrel from the feeding port, and move towards the discharging port direction under the forced transportation of the screw mechanism, at this time the solids are subjected to an asymmetric effect generated by a periodical plasticizing and extruding space generated by the rotations of the central screw and the lateral screws and an interwiping effect between the central screw and the two lateral screws, so that the heat exchanging efficiencies between the melts and the surface of the solid materials are increased, the solid materials themselves are also participated into the stirring process, and dispersed into the melts to carry out a strong convection, so as to generate dispersion and melting, and becoming melts; the melts enter the venting zone, the space consists of the central screw and the lateral screws and the inner cavity of the barrel is suddenly enlarged, the materials are continuously stirred by the rotation of the central screw and the two lateral screws so that the gases are discharged from the venting port; the melts enter the compounding and extruding zone, the melts proceed under the periodical asymmetric space effect generated by the rotation of the central screw and the two lateral screws, the interfaces are facilitated to reorientate and regenerate continuously, the materials are compounded and plasticized, and a self-cleaning effect is achieved by the interwiping effect between the central screw and the two lateral screws, so that the melts are stably extruded from the discharging port.


The self-cleaning plasticizing venting and extruding method by co-rotating non-twin multi-screws carried out by the above-mentioned apparatus, particularly, comprises the steps of:


(1) after the materials enter the barrel from the feeding port, the central screw and the lateral screws co-rotate along the axis of the respective screws under the drive of the driving mechanism; when the materials enter the solid transporting zone, the feed materials transportation is carried out under the co-effects of the axial transporting forces from the central screw and the lateral screws and the friction forces from the central screw and the lateral screws, so that the materials are forced to move towards the discharging port direction, at the same time the gases in the materials are discharged from the feeding port as the materials are heated;


(2) when the materials move to the melting zone, the central screw and the lateral screws rotate in a relatively engaging way so as to generate a periodical transport space for transporting the materials; the materials are melt under the co-effects of the friction heat generated by the high speed rotation of each of the screws and at the same time the external heat on the barrel; and the melting process is accelerated under the interwiping effect between the central screw and the lateral screws and the asymmetrical effect of the transport space, so that the materials become melts;


(3) when the melts enter the venting zone, the space consisted of the central screw and the lateral screws and the inner cavity of the barrel is suddenly enlarged, the materials are continuously stirred by the rotation of the central screw and the lateral screws, so that the gases are discharged from the venting port, and the melts move further towards the discharging port direction; and


(4) when the melts enter the compounding and extruding zone, the melts proceed under the periodical space effect generated by the rotation of the central screw and the lateral screws, the interfaces are facilitated to reorientate and regenerate continuously by the interwiping effect between the central screw and the lateral screws and the asymmetrical effect of the transport space, the materials are compounded and plasticized, at the same time a self-cleaning effect are achieved by the interwiping effect between each of the screws, so that the melts are stably extruded from the discharging port.


The rotation speeds of said two lateral screws are the same, and the rotation speed ratio between each of the lateral screws and the central screw is 0.1-6.0.


The present invention has the following advantages and beneficial effects as follow as compared with the prior art:


1. the present invention uses a central screw and two identical-shaped lateral screws to increase the solid transporting efficiency, so that it can increase the extruding yield in a higher extent, and is suitable for a large-scale production;


2. the shapes of the central screw and the lateral screws in the present invention are different, and the positions of the two lateral screws can be provided with a certain phase angle difference, so that there is an asymmetric (unconsistency) in the flow space for the materials, the compounding and heat transferring processes are enhanced, so that the heat and mechanical courses for carrying out the plasticization are greatly abbreviated, the energy consumption is low, and the effects for saving energy and reducing consumption are significant;


3. the present invention uses an interwiping effect between the central screw and the two lateral screws to carry out a self-cleaning effect during the processing process, and the residence time during the processing process has a narrow distribution, so as to improve the processing efficiency and effectiveness;


4. each of the screws in the present invention uses a non-uniform geometrical shape, under the geometrical shape effect and the interwiping effect between each of the screws, the mixing and compounding intensity and effect are overall enhanced, and the dispersing distribution and mixing effects are extremely excellent, so that it is especially suitable for processing nano-materials in high yield; and


5. the materials are transported by the cooperative rotation between the central screw and the two lateral screws in the present invention, so that an uniform interface extension can be achieved, an uniform material transportation can be achieved, and the uniformity for controlling the phase structures is good.





DESCRIPTION OF ACCOMPANYING DRAWINGS


FIG. 1 is a structural schematic diagram of embodiment 1 in the present invention.



FIG. 2 is an enlarged structural schematic diagram of embodiment 1 cutting along A-A shown in FIG. 1.



FIG. 3 is an enlarged structural schematic diagram of embodiment 2 cutting along A-A shown in FIG. 1.



FIG. 4 is an enlarged structural schematic diagram of embodiment 3 cutting along A-A shown in FIG. 1.



FIG. 5 is an enlarged structural schematic diagram of embodiment 4 cutting along A-A shown in FIG. 1.



FIG. 6 is a schematic diagram of the cross-section shape of each of the screws in embodiment 7.



FIG. 7 is a schematic diagram of the cross-section shape of each of the screws in embodiment 8.



FIG. 8 is a schematic diagram of the cross-section shape of each of the screws in embodiment 9.



FIG. 9 is a schematic diagram of the cross-section shape of each of the screws in embodiment 10.



FIG. 10 is a schematic diagram of the cross-section shape of each of the screws in embodiment 11.





PARTICULAR EMBODIMENTS

The present invention is further described in detail below by incorporating the embodiments and drawings, but the embodiments of the present invention are not limited thereto.


Embodiment 1

As shown in FIG. 1, the self-cleaning plasticizing venting and extruding apparatus by co-rotating non-twin multi-screws comprises a screw mechanism, a barrel 1, a feeding port 2, a venting port 4, a discharging port 5, and a driving mechanism, wherein said driving mechanism is provided at the ends of the barrel 1 respectively, and is connected to the screw mechanism; said screw mechanism is provided inside the barrel 1, and placed horizontally, and the inner section of the barrel 1 are divided into a solid transporting zone 9, a melting zone 10, a venting zone 11 and a compounding and extruding zone 12; said feeding port 2 is provided above the barrel 1 of the solid transporting zone 9, said venting port 4 is provided above the barrel 1 of the venting zone 11, both the feeding port 2 and the venting port 4 are communicated with the barrel 1; said discharging port 5 is provided at the end of the barrel 1, said screw mechanism comprises a central screw 6 and two uniform shaped lateral screws, the axis of the central screw 6 is coincided with that of the barrel 1, the two lateral screws are left screw 3 and right screw 13 respectively, provided on both sides of the central screw 6 respectively, and engaged with the central screw 6; and the contour lines of the threads of said central screw 6 and said lateral screws are tangent to the inner wall of the barrel 1; said driving mechanism is connected to the central screw 6 and the lateral screws respectively.


Said driving mechanism comprises a main electric motor 8 and a toothed gearing mechanism 7 which are interconnected with each other, said toothed gearing mechanism 7 is connected to the central screw 6 and the two lateral screws respectively.


The inner cavity of said barrel 1 is consisted of three cylinder grooves which have the same inner diameter and are communicated with each other, each of the cylinder grooves is fitted with the left screw 3, the central screw 6 and the right screw 13 respectively; the central axis distances from the cylinder grooves on both sides to the cylinder groove at the central position are equal to the centerline distances from the central screw 6 to the left screw 3 and the right screw 13.


The peak angle of the screw ridge of said central screw 6 is 38°.


As shown in FIG. 2, the phase angle difference between the positions of said left screw 3 and right screw 13 is 180°, ie., the cross-section shape of said left screw 3 is the same as the curve shape formed after the cross-section of the right screw 13 is rotated counterclockwise by 180° along the center point of the cylinder groove of the barrel corresponding to the central screw (ie., the shape of the cross-section of said left screw is the same as the curve shape of the cross-section formed after the right screw is rotated counterclockwise by 180° along the center point of the cylinder groove of the barrel corresponding to the central screw);


with the center points of the cylinder grooves of the barrel corresponding to the central screw 6 and each of the lateral screws respectively as poles, and the rays elicited horizontally rightwards from the poles (ie., in the orthogonal coordinate system, the rays in the positive direction of X axis of the connecting line through the center points of the cylinder grooves of the barrel) as polar axes, the shape curve of the cross-section of said central screw 6 meets that:













when





0

°


θ


25

°


,







ρ


(
θ
)


=


(




0.32256
+

0.00392





θ

+

0.00030949





7


θ
2


-

2.57326
×

10

-
5




θ
2


+







9.28644
×

10

-
7




θ
4


+

1.8713
×

10

-
11




θ
3


-

8.12786
×

10

-
10




θ
1


-






9.61005
×

10

-
12




θ
7





)



D
0



;















when





25

°


θ


63

°


,



ρ


(
θ
)


=

0.5






D
0



;















when





63

°


θ


123

°


,







ρ


(
θ
)


=


(




0.5
+

0.000823585


(

θ
-
63

)


-

0.00134



(

θ
-
63

)

2


+







8.00734
×

10

-
2





(

θ
-
63

)

2


-

2.14653
×

10

-
1





(

θ
-
63

)

4


+







2.76223
×

10

-
11





(

θ
-
63

)

2


-

1.37762
×

10

-
10





(

θ
-
63

)

1






)



D
0



;















when





123

°


θ


147

°


,







ρ


(
θ
)


=


(




0.25391
-

0.00207


(

θ
-
123

)


+

0.000573645



(

θ
-
123

)

2


-







8.45874
×

10

-
3





(

θ
-
123

)

2


+

6.53416
×

10

-
1





(

θ
-
123

)

4


-







2.56256
×

10

-
7





(

θ
-
123

)

3


+

4.47098
×

10

-
5





(

θ
-
123

)

1


-






2.03618
×

10

-
11





(

θ
-
123

)

7





)



D
0



;















when





147

°


θ


205

°


,







ρ


(
θ
)


=


(




0.25374
+

0.000730048


(

θ
-
147

)


-

0.000156535



(

θ
-
147

)

2


+







3.73081
×

10

-
5





(

θ
-
147

)

3


-

3.07839
×

10

-
6





(

θ
-
147

)

4


+







1.32913
×

10

-
7





(

θ
-
147

)

5


-

3.10949
×

10

-
9





(

θ
-
147

)

6


+







3.74465
×

10

-
11





(

θ
-
147

)

7


-

1.81606
×

10

-
13





(

θ
-
147

)

8






)



D
0



;















when





205

°


θ


243

°


,



ρ


(
θ
)


=

0.5






D
0



;















when





243

°


θ


307

°


,







ρ


(
θ
)


=


(




0.5
+

0.00369


(

θ
-
243

)


-

0.00226



(

θ
-
243

)

2


+







0.00018496





5



(

θ
-
243

)

3


-

7.94221
×

10

-
6





(

θ
-
243

)

4


+







2.00615
×

10

-
7





(

θ
-
243

)

5


-

2.9807
×

10

-
9





(

θ
-
243

)

6


+







2.4097
×

10

-
11





(

θ
-
243

)

7


-

8.17763
×

10

-
14





(

θ
-
243

)

8






)



D
0



;















when





307

°


θ


323

°


,







ρ


(
θ
)


=


(




0.2568
-

0.00882


(

θ
-
307

)


+

0.00414



(

θ
-
307

)

2


-







0.000908651



(

θ
-
307

)

3


+

0.00010077





7



(

θ
-
307

)

4


-







5.50309
×

10

-
6





(

θ
-
307

)

5


+

.20454
×

10

-
7





(

θ
-
307

)

6


-






11.95559
×

10

-
10





(

θ
-
307

)

7





)



D
0



;















when





307

°


θ


323

°


,







ρ


(
θ
)


=


(




0.2568
-

0.00882


(

θ
-
307

)


+

0.00414



(

θ
-
307

)

2


-







0.000908651



(

θ
-
307

)

3


+

0.00010077





7



(

θ
-
307

)

4


-







5.50309
×

10

-
6





(

θ
-
307

)

5


+

1.20454
×

10

-
7





(

θ
-
307

)

6


-






1.95559
×

10

-
10





(

θ
-
307

)

7





)



D
0



;















when





323

°


θ


360

°


,







ρ


(
θ
)


=


(




0.25618
+

0.00082668


(

θ
-
323

)


-

0.00031989





4



(

θ
-
323

)

2


+







4.17742
×

10

-
5





(

θ
-
323

)

3


-

2.08266
×

10

-
6





(

θ
-
323

)

4


+







4.80871
×

10

-
8





(

θ
-
323

)

5


-

4.18424
×

10

-
10





(

θ
-
323

)

6






)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross-section of said right screw 13 meets that:













when





0

°


θ


80

°


,











ρ


(
θ
)


=


(




0.28446
+

0.001730

θ

-

4.07776
×

10

-
6




θ
2


+







4.49932
×

10

-
7




θ
3


-

3.26681
×

10

-
9




θ
4






)



D
0



;















when





80

°


θ


100

°


,







ρ


(
θ
)


=


(




0.49331
+

0.00156


(

θ
-
80

)


+

3.82324
×

10

-
5





(

θ
-
80

)

2


-







4.32369
×

10

-
5





(

θ
-
80

)

3


+

5.05212
×

10

-
6





(

θ
-
80

)

4


-







2.3955
×

10

-
7





(

θ
-
80

)

5


+

4.02621
×

10

-
9





(

θ
-
80

)

6






)



D
0



;















when





100

°


θ


229

°


,







ρ


(
θ
)


=


(




0.49336
-

0.00325


(

θ
-
100

)


-

4.70431
×

10

-
6





(

θ
-
100

)

2


+







2.18207
×

10

-
7





(

θ
-
100

)

3


-

7.76735
×

10

-
10





(

θ
-
100

)

4






)



D
0



;















when





229

°


θ


305

°


,











ρ


(
θ
)


=

0.25






D
0



;















when





305

°


θ


360

°


,







ρ


(
θ
)


=


(




0.25
-

8.84562
×

10

-
5




(

θ
-
305

)


+

2.30409
×

10

-
5





(

θ
-
305

)

2


-







8.10513
×

10

-
7





(

θ
-
305

)

3


+

2.00086
×

10

-
8





(

θ
-
305

)

4


-






1.56195
×

10

-
10





(

θ
-
305

)

5





)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw; and


the screw compression ratio between the central screw 6 and the two lateral screws is in a range of 1-10.


A self-cleaning plasticizing venting and extruding process by co-rotating non-twin multi-screws carried out by the above-mentioned apparatus, characterized by particularly comprising the steps of:


(1) after the materials enter the barrel 1 from the feeding port 2, the central screw 6 and the two lateral screws co-rotate along the respective screw axis under the drive of the driving mechanism; when the materials enter the solid transporting zone 9, the feed materials are transported under the co-effects of the axial transporting force from the central screw 6 and the two lateral screws and the friction force from the central screw 6 and the two lateral screws, so that the materials are forced to move towards the discharging port 5 direction, at the same time the gases in the materials are discharged from the feeding port 2 as the materials are heated;


(2) when the materials move to the melting zone 10, the central screw 6 and the two lateral screws rotate in a relatively engagement mode so as to generate a periodical transport space for transporting the materials; the materials are melt under the co-effects of the friction heat generated from the high speed rotation of each of the screws and at the same time the external heat on the barrel 1; and the melting process is accelerated under the interwiping effect between the central screw 6 and the two lateral screws and the asymmetrical effect of the transport space, so that the materials become melts;


(3) when the melts enter the venting zone 11, the space consisted of the central screw 6 and the lateral screws and the inner cavity of the barrel 1 is suddenly enlarged, the materials are continuously stirred by the rotation of the central screw 6 and the two lateral screws, so that the gases are discharged from the venting port 4, and the melts move further towards the discharging port 5 direction;


(4) when the melts enter the compounding and extruding zone 12, the melts proceed under the periodical space effect generated by the rotation of the central screw 6 and the two lateral screws, the interfaces are facilitated to reorientate and regenerate continuously under the interwiping effect between the central screw 6 and the two lateral screws and the asymmetrical effect of the transport space, the materials are compounded and plasticized, and at the same time a self-cleaning effect is carried out by the interwiping effect between each of the screws, so that the melts are stably extruded from the discharging port 5; and


(5) the rotation speeds of said two lateral screws are the same, and the rotation speed ratio between each of the lateral screws and the central screw 6 is 2.0.


Embodiment 2

The present embodiment has the same structure as that in embodiment 1, except the following features: as shown in FIG. 3, the phase angle difference between the positions of said left screw 3 and right screw 13 is 180°, ie., the shape of the cross-section of said left screw 3 is the same as the curve shape formed after the cross-section of the right screw 13 is rotated counterclockwise by 180° along the center point of the cylinder groove of the barrel corresponding to the central screw. With the center points of the cylinder grooves of the barrel corresponding to the central screw 6 and each of the lateral screws respectively as poles, and the rays elicited horizontally rightwards from the poles (ie., in the orthogonal coordinate system, the rays in the positive direction of X axis of the connecting line through the center points of the cylinder grooves of the barrel) as polar axes, the shape curve of the cross-section of said central screw 6 meets that:













when





0

°


θ


23

°


,







ρ


(
θ
)


=


(




0.39546
+

0.00436





θ

-

0.000328898


θ
2


+

0.000049615


θ
3


-







2.50164
×

10

-
6




θ
4


+

5.0823
×

10

-
8




θ
5


-

4.85534
×

10

-
10




θ
6






)



D
0



;















when





23

°


θ


145

°


,







ρ


(
θ
)


=


(




0.48059
+

0.000898536


(

θ
-
23

)


-

0.000962297



(

θ
-
23

)

2


+







5.01749
×

10

-
5





(

θ
-
23

)

3


-

1.28633
×

10

-
6





(

θ
-
23

)

4


+







1.88747
×

10

-
8





(

θ
-
23

)

5


-

1.6028
×

10

-
10





(

θ
-
23

)

6


+







7.32557
×

10

-
13





(

θ
-
23

)

7


-

1.39342
×

10

-
15





(

θ
-
23

)

8






)



D
0



;















when





145

°


θ


202

°


,







ρ


(
θ
)


=


(




0.35035
-

0.00004415





4


(

θ
-
145

)


+

6.21993
×

10

-
5





(

θ
-
145

)

2


-







8.31288
×

10

-
6





(

θ
-
145

)

3


+

6.56112
×

10

-
7





(

θ
-
145

)

4


-







2.23522
×

10

-
8





(

θ
-
145

)

5


+

3.57533
×

10

-
10





(

θ
-
145

)

6


-






2.18353
×

10

-
12





(

θ
-
145

)

7





)



D
0



;















when





202

°


θ


225

°


,







ρ


(
θ
)


=


(




0.48074
-

0.00133


(

θ
-
202

)


+

0.00054249





5



(

θ
-
202

)

2


-







0.00014859





6



(

θ
-
202

)

3


+

8.56691
×

10

-
6





(

θ
-
202

)

4


-






1.51835
×

10

-
7





(

θ
-
202

)

5





)



D
0



;















when





225

°


θ


325

°


,







ρ


(
θ
)


=


(




0.34927
-

0.00583


(

θ
-
225

)


+

0.000183457



(

θ
-
225

)

2


-







5.41662
×

10

-
6





(

θ
-
225

)

2


+

1.25448
×

10

-
7





(

θ
-
225

)

4


-







1.7397
×

10

-
9





(

θ
-
225

)

5


+

1.27967
×

10

-
11





(

θ
-
225

)

6


-






3.77702
×

10

-
14





(

θ
-
225

)

7





)



D
0



;















when





325

°


θ


351

°


,







ρ


(
θ
)


=


(




0.35169
-

0.000591024


(

θ
-
325

)


+

0.00011694





2



(

θ
-
325

)

2


-







8.07623
×

10

-
6





(

θ
-
325

)

3


+

3.51208
×

10

-
7





(

θ
-
325

)

4


-






5.2224
×

10

-
9





(

θ
-
325

)

5





)



D
0



;















when





351

°


θ


360

°


,







ρ


(
θ
)


=


(




0.37187
+

0.00178


(

θ
-
351

)


+

0.00023854





1



(

θ
-
351

)

2


-






1.61095
×

10

-
5





(

θ
-
351

)

3





)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross-section of said right screw 13 meets that:













when





0

°


θ


13

°


,











ρ


(
θ
)


=


(




0.49645
+

0.00025651





2

θ

+

0.000149725


θ
2


-







2.18392
×

10

-
5




θ
3


+

6.8663
×

10

-
7




θ
4






)



D
0



;















when





13

°


θ


119

°


,











ρ


(
θ
)


=


(




0.49672
+

0.0016


(

θ
-
13

)


-

0.000160439



(

θ
-
13

)

2


+







3.66195
×

10

-
6





(

θ
-
13

)

3


-

4.18633
×

10

-
8





(

θ
-
13

)

4


+







2.44243
×

10

-
10





(

θ
-
13

)

5


-

5.70929
×

10

-
13





(

θ
-
13

)

6






)



D
0



;















when





119

°


θ


360

°


,







ρ


(
θ
)


=


(




0.39857
-

0.00147


(

θ
-
119

)


-

2.94068
×

10

-
5





(

θ
-
119

)

2


+







6.44036
×

10

-
7





(

θ
-
119

)

3


-

4.79428
×

10

-
9





(

θ
-
119

)

4


+







1.70193
×

10

-
11





(

θ
-
119

)

5


-

2.30605
×

10

-
14





(

θ
-
119

)

6






)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw; and


the rotation speeds of said two lateral screws are the same, and the rotation speed ratio between each of the lateral screws and the central screw 6 is 2.


Embodiment 3

The present embodiment has the same structure as that in embodiment 1, except the following features: as shown in FIG. 4, the phase angle difference between the positions of said left screw 3 and right screw 13 is 0°, ie., the shape of the cross-section of said left screw 3 is the same as the curve shape of the cross-section of the right screw 13; with the center points of the cylinder grooves of the barrel corresponding to the central screw 6 and each of the lateral screws respectively as poles, and the rays elicited horizontally rightwards from the poles (ie., in the orthogonal coordinate system, the rays in the positive direction of X axis of the connecting line through the center points of the cylinder grooves of the barrel) as polar axes, the shape curve of the cross section of said central screw 6 meets that:













when





0

°


θ


27

°


,







ρ


(
θ
)


=


(




0.28995
+

0.0029





θ

+

0.00010458





6


θ
2


+

1.35828
×

10

-
6




θ
3


-







6.80098
×

10

-
8




θ
4


+

3.45975
×

10

-
9




θ
5






)



D
0



;















when





27

°


θ


36

°


,











ρ


(
θ
)


=


(




0.4847
+

0.01065


(

θ
-
27

)


-

0.00186



(

θ
-
27

)

2


+







5.1776
×

10

-
6





(

θ
-
27

)

3


+

1.23985
×

10

-
6





(

θ
-
27

)

4






)



D
0



;















when





36

°


θ


60

°


,











ρ


(
θ
)


=


(




0.4418
-

0.01131


(

θ
-
36

)


+

0.00029056





3



(

θ
-
36

)

2


-







3.02877
×

10

-
6





(

θ
-
36

)

3


-

2.66377
×

10

-
8





(

θ
-
36

)

4






)



D
0



;















when





60

°


θ


120

°


,











ρ


(
θ
)


=


(




0.287
-

0.0025


(

θ
-
60

)


+

4.57118
×

10

-
5





(

θ
-
60

)

2


-







1.90487
×

10

-
7





(

θ
-
60

)

3


+

2.28021
×

10

-
9





(

θ
-
60

)

4






)



D
0



;















when





20

°


θ


147

°


,







ρ


(
θ
)


=


(




0.28995
+

0.0029


(

θ
-
120

)


+

0.000104586



(

θ
-
120

)

2


+







1.35828
×

10

-
6





(

θ
-
120

)

3


-

6.80098
×

10

-
8





(

θ
-
120

)

4


+






3.45975
×

10

-
9





(

θ
-
120

)

5





)



D
0



;















when





147

°


θ


156

°


,











ρ


(
θ
)


=


(




0.4847
+

0.01065


(

θ
-
147

)


-

0.00186



(

θ
-
147

)

2


+







5.1776
×

10

-
6





(

θ
-
147

)

3


+

1.23985
×

10

-
6





(

θ
-
147

)

4






)



D
0



;















when





156

°


θ


180

°


,







ρ


(
θ
)


=


(




0.4418
-

0.01131


(

θ
-
156

)


+

0.000290563



(

θ
-
156

)

2


-







3.02877
×

10

-
6





(

θ
-
156

)

3


-

2.66377
×

10

-
8





(

θ
-
156

)

4






)



D
0



;















when





180

°


θ


240

°


,







ρ


(
θ
)


=


(




0.287
-

0.0025


(

θ
-
180

)


+

4.57118
×

10

-
5





(

θ
-
180

)

2


-







1.90487
×

10

-
7





(

θ
-
180

)

3


+

2.28021
×

10

-
9





(

θ
-
180

)

4






)



D
0



;















when





240

°


θ


267

°


,







ρ


(
θ
)


=


(




0.28995
+

0.0029


(

θ
-
240

)


+

0.00010458





6



(

θ
-
240

)

2


+







1.35828
×

10
4




(

θ
-
240

)

2


-

6.80098
×

10

-
3





(

θ
-
240

)

4


+






3.45975
×

10

-
9





(

θ
-
240

)

5





)



D
0



;















when





267

°


θ


270

°


,







ρ


(
θ
)


=


(




0.4847
+

0.01065


(

θ
-
267

)


-

0.00186



(

θ
-
267

)

2


+







5.1776
×

10

-
6





(

θ
-
267

)

2


+

1.23985
×

10

-
4





(

θ
-
267

)

4






)



D
0



;















when





270

°


θ


300

°


,







ρ


(
θ
)


=


(




0.4418
-

0.01131


(

θ
-
270

)


+

0.00029056





3



(

θ
-
270

)

2


-







3.02877
×

10

-
4





(

θ
-
270

)

3


-

2.66377
×

10

-
3





(

θ
-
270

)

4






)



D
0



;















when





300

°


θ


360

°


,







ρ


(
θ
)


=


(




0.287
-

0.0025


(

θ
-
180

)


+

4.57118
×

10

-
5





(

θ
-
180

)

2


-







1.90487
×

10

-
7





(

θ
-
180

)

3


+

2.28021
×

10

-
9





(

θ
-
180

)

4






)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross-section of said right screw 13 meets that:













when





0

°


θ


85

°


,







ρ


(
θ
)


=


(




0.32013
+

0.000685205





θ

+

0.00011173






θ
2


-

5.88903
×

10

-
6




θ
3


+







1.80316
×

10

-
7




θ
4


-

3.03623
×

10

-
9




θ
5


+

2.64496
×

10

-
11




θ
6


-






9.23845
×

10

-
14




θ
7





)



D
0



;















when





85

°


θ


95

°


,







ρ


(
θ
)


=


(




0.494681
+

0.00179


(

θ
-
85

)


-

0.000479273



(

θ
-
85

)

2


+







0.00010662



(

θ
-
85

)

3


-

1.63619
×

10

-
5





(

θ
-
85

)

4


+







1.24974
×

10

-
6





(

θ
-
85

)

5


-

3.77964
×

10

-
8





(

θ
-
85

)

6






)



D
0



;















when





95

°


θ


180

°


,







ρ


(
θ
)


=


(




0.494832
-

0.000761246


(

θ
-
95

)


-

0.000126101



(

θ
-
95

)

2


+







4.25652
×

10

-
6





(

θ
-
95

)

3


-

7.13683
×

10

-
8





(

θ
-
95

)

4


+







5.9942
×

10

-
10





(

θ
-
95

)

5


-

1.98695
×

10

-
12





(

θ
-
95

)

6






)



D
0



;















when





180

°


θ


360

°


,







ρ


(
θ
)


=


(




0.31789
-

0.00133


(

θ
-
180

)


-

8.60877
×

10

-
6





(

θ
-
180

)

2


+







5.0898
×

10

-
7





(

θ
-
180

)

3


-

7.16212
×

10

-
9





(

θ
-
180

)

4


+







5.3005
×

10

-
11





(

θ
-
180

)

5


-

2.05365
×

10

-
13





(

θ
-
180

)

6


+







3.64972
×

10

-
16





(

θ
-
180

)

7


-

1.76708
×

10

-
19





(

θ
-
180

)

8






)



D
0



;






wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw; and


the rotation speeds of said two lateral screws are the same, and the rotation speed ratio between each of the lateral screws and the central screw 6 is 3.


Embodiment 4

The present embodiment has the same structure as that in embodiment 1, except the following features: as shown in FIG. 5, the phase angle difference between the positions of said left screw 3 and right screw 13 is 0°, ie., the shape of the cross-section of said left screw 3 is the same as that of the right screw 13. With the center points of the cylinder grooves of the barrel corresponding to the central screw 6 and each of the lateral screws respectively as poles, and the rays elicited horizontally rightwards from the poles (ie., in the orthogonal coordinate system, the rays in the positive direction of X axis of the connecting line through the center points of the cylinder grooves of the barrel) as polar axes, the shape curve of the cross-section of said central screw 6 meets that:











when





0

°


θ


50

°


,



ρ


(
θ
)


=

0.5


D
0



;














when





50

°


θ


90

°


,













ρ


(
θ
)


=


(




0.5
-

0.00309


(

θ
-
50

)


+







0.000168331



(

θ
-
50

)

2


-







8.44083
×

10

-
6





(

θ
-
50

)

3


+







2.19035
×

10

-
7





(

θ
-
50

)

4


-






2.06434
×

10

-
9





(

θ
-
50

)

5





)



D
0



;













when





90

°


θ


101

°


,



ρ


(
θ
)


=

0.455


D
0



;














when





101

°


θ


181

°


,













ρ


(
θ
)


=


(




0.455
-

0.00143


(

θ
-
101

)


-







0.000793059







(

θ
-
101

)

2


+







6.51522
×

10

-
5





(

θ
-
101

)

3


-







2.66487
×

10

-
6





(

θ
-
101

)

4


+







6.20495
×

10

-
8





(

θ
-
101

)

5


-







8.26745
×

10

-
10





(

θ
-
101

)

6


+







5.86449
×

10

-
12





(

θ
-
101

)

7


-






1.71691
×

10

-
14





(

θ
-
101

)

8





)



D
0



;













when





181

°


θ


193

°


,



ρ


(
θ
)


=

0.25


D
0



;














when





193

°


θ


244

°


,













ρ


(
θ
)


=


(




0.25
+

0.000361178






(

θ
-
193

)


-







0.000107545



(

θ
-
193

)

2


+







0.00002068



(

θ
-
193

)

3


-







1.60164
×

10

-
6





(

θ
-
193

)

4


+







6.82867
×

10

-
8





(

θ
-
193

)

5


-







1.63573
×

10

-
9





(

θ
-
193

)

6


+







2.06803
×

10

-
11





(

θ
-
193

)

7


-






1.07375
×

10

-
13





(

θ
-
193

)

8





)



D
0



;













when





244

°


θ

353

,













ρ


(
θ
)


=


(




0.31875
-

0.00104


(

θ
-
244

)


-







3.31524
×

10

-
5





(

θ
-
244

)

2


+







4.32237
×

10

-
6





(

θ
-
244

)

3


-







1.67168
×

10

-
7





(

θ
-
244

)

4


+







3.54572
×

10

-
9





(

θ
-
244

)

5


-







4.16652
×

10

-
11





(

θ
-
244

)

6


+







2.55218
×

10

-
13





(

θ
-
244

)

7


-






6.34643
×

10

-
16





(

θ
-
244

)

8





)



D
0



;













when





353

°


θ


360

°


,



ρ


(
θ
)


=

0.5


D
0



;













wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross-section of said right screw 13 meets that:











when





0

°


θ


12

°


,



ρ


(
θ
)


=

0.5


D
0



;














when





12

°


θ


93

°


,













ρ


(
θ
)


=


(




0.5
-

0.00165


(

θ
-
12

)


-







0.000134915



(

θ
-
12

)

2


+







0.000011814



(

θ
-
12

)

3


-







4.87051
×

10

-
7





(

θ
-
12

)

4


+







1.1766
×

10

-
8





(

θ
-
12

)

5


-







1.64659
×

10

-
10





(

θ
-
12

)

6


+







1.23355
×

10

-
12





(

θ
-
12

)

7


-






3.82327
×

10

-
15





(

θ
-
12

)

8





)



D
0



;













when





93

°


θ


173

°


,













ρ


(
θ
)


=


(




0.44967
-

0.0012


(

θ
-
93

)


-







0.000680386







(

θ
-
93

)

2


+







5.15007
×

10

-
5





(

θ
-
93

)

3


-







1.99396
×

10

-
6





(

θ
-
93

)

4


+







4.48589
×

10

-
8





(

θ
-
93

)

5


-







5.85347
×

10

-
10





(

θ
-
93

)

6


+







4.10152
×

10

-
12





(

θ
-
93

)

7


-






1.19263
×

10

-
14





(

θ
-
93

)

8





)



D
0



;













when





173

°


θ


230

°


,



ρ


(
θ
)


=

0.25


D
0



;














when





230

°


θ


272

°


,







ρ


(
θ
)


=


(




0.25
+

0.000575232






(

θ
-
230

)


-







0.000134433



(

θ
-
230

)

2


+







2.28201
×

10

-
5





(

θ
-
230

)

3


-







1.7105
×

10

-
6





(

θ
-
230

)

4


+







7.37301
×

10

-
8





(

θ
-
230

)

5


-







1.86726
×

10

-
9





(

θ
-
230

)

6


+







2.61628
×

10

-
11





(

θ
-
230

)

7


-






1.5782
×

10

-
13





(

θ
-
230

)

8





)



D
0



;














when





272

°


θ


283

°


,



ρ


(
θ
)


=

0.295


D
0



;














when





282

°


θ


360

°


,













ρ


(
θ
)


=


(




0.295
+

0.000132721


(

θ
-
283

)


+







4.58737
×

10

-
5





(

θ
-
283

)

2


-







3.34923
×

10

-
6





(

θ
-
283

)

3


+







2.15388
×

10

-
7





(

θ
-
283

)

4


-







6.89212
×

10

-
9





(

θ
-
283

)

5


+







1.18802
×

10

-
10





(

θ
-
283

)

6


-







1.04706
×

10

-
12





(

θ
-
283

)

7


+






3.70486
×

10

-
15





(

θ
-
283

)

8





)



D
0



;












wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw; and


the rotation speeds of said two lateral screws are the same, and the rotation speed ratio between each of the lateral screws and the central screw 6 is 1.


Embodiment 5

The present embodiment has the same structure as that in embodiment 1, except the following features: the rotation speeds of said two lateral screws are the same, and the rotation speed ratio between each of the lateral screws and the central screw is 0.5. The peak angle of the screw ridge of said central screw is in a range of 0-180°.


Embodiment 6

The present embodiment has the same structure as that in embodiment 1, except the following features: the rotation speeds of said two lateral screws are the same, and the rotation speed ratio between each of the lateral screws and the central screw is 0.5. The peak angle of the screw ridge of said central screw is in a range of 0-180°.


Embodiment 7

The present embodiment has the same structure as that in embodiment 1, except the following features: as shown in FIG. 6, said lateral screw is only one screw, which is provided on the side of the central screw, and engaged with the central screw; the inner cavity of said barrel is consisted of two cylinder grooves which have the same inner diameter and are communicated with each other, each of the cylinder grooves is fitted with the lateral screw, and the central screw respectively; the central axis distance between the two cylinder grooves is equal to the centerline distance between the central screw and the lateral screw, ie., (D0+Di)/2, at this time, D0/Di=1.25, wherein, D0 is an inner diameter of the cylinder groove of the barrel, and Di is a diameter of the screw. In the present embodiment, the lateral screw 15 corresponds to the right screw 13 in embodiment 1, and the central screw 14 corresponds to the central screw 6 in embodiment 1.


The lead of screw threads between the central screw 14 and the lateral screw 15 is in a range of 0.1-10000 D0.


With the center points of the cylinder grooves of the barrel corresponding to the central screw 14 and the lateral screw 15 respectively as poles, and the rays elicited horizontally rightwards from the poles (ie., in the orthogonal coordinate system, the positive direction of X axis) as polar axes, the starting position of the polar angle of each of the screws is a bisector of the peak angle of the screw ridge, with the counterclockwise direction as a positive direction.


The shape curve of the cross-section of said central screw 14 is symmetric with respective to the ray of θ=120° and the ray of θ=240°, and the polar angle is within 0°≦θ≦120°, the corresponding curve meets that:











when





0


θ


2

°


,



ρ


(
θ
)


=

0.5


D
0



;














when





2

°


θ


58

°


,













ρ


(
θ
)


=


(



















0.5
-

0.00243


(

θ
-
2

)


+







0.00106



(

θ
-
2

)

2


-

1.67316
×

10
4




(

θ
-
2

)

3


+










1.08849
×

10

-
5





(

θ
-
2

)

4


-










3.74006
×

10

-
7





(

θ
-
2

)

5


+










7.15583
×

10

-
9





(

θ
-
2

)

6


-










7.21345
×

10

-
11





(

θ
-
2

)

7


+









2.98968
×

10

-
13





(

θ
-
2

)

8





)



D
0



;













when





58

°


θ


62

°


,



ρ


(
θ
)


=

0.4


D
0



;














when





62

°


θ


118

°


,













ρ


(
θ
)


=


(




0.4
-

7.16547
×

10

-
4




(

θ
-
62

)


+







3.66366
×

10

-
4





(

θ
-
62

)

2


-







5.72993
×

10

-
5





(

θ
-
62

)

3


+







4.76052
×

10

-
6





(

θ
-
62

)

4


-







2.09619
×

10

-
7





(

θ
-
62

)

5


+







5.0282
×

10

-
9





(

θ
-
62

)

6


-







6.18021
×

10

-
11





(

θ
-
62

)

7


+






3.03396
×

10

-
13





(

θ
-
62

)

8





)



D
0



;













when





118

°


θ


120

°


,


ρ


(
θ
)


=

0.5


D
0















wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross section of said lateral screw 15 is symmetric with respective to the ray of θ=0° and the ray of θ=180° (ie., the positive direction of the X axial in the orthogonal coordinate system), and the polar angle is within 0°≦θ≦180°, the corresponding curve meets that:












when





0

°


θ


3

°


,



ρ


(
θ
)


=

0.4


D
0



;










when





3

°


θ


87

°


,














ρ


(
θ
)


=


(




0.40053
+

1.91042
×

10

-
4




(

θ
-
3

)


-







5.44854
×

10

-
5





(

θ
-
3

)

2


+







5.78786
×

10

-
6





(

θ
-
3

)

3


-







2.60181`
×

10

-
7





(

θ
-
3

)

4


+







6.77081
×

10

-
9





(

θ
-
3

)

5


-







1.00659
×

10

-
10





(

θ
-
3

)

6


+







7.9546
×

10

-
13





(

θ
-
3

)

7


-






2.59711
×

10

-
15





(

θ
-
3

)

8





)



D
0



;













when





87

°


θ


93

°


,



ρ


(
θ
)


=

0.5


D
0



;














when





93

°


θ


177

°


,













ρ


(
θ
)


=


(




0.5
+

5.59592
×

10

-
4




(

θ
-
93

)


-







3.44997
×

10

-
4





(

θ
-
93

)

2


+







1.95669
×

10

-
5





(

θ
-
93

)

3


-







6.25514
×

10

-
7





(

θ
-
93

)

4


+







1.2176
×

10

-
8





(

θ
-
93

)

5


-







1.43316
×

10

-
10





(

θ
-
93

)

6


+







9.29081
×

10

-
13





(

θ
-
93

)

7


-






2.54457
×

10

-
15





(

θ
-
93

)

8





)



D
0



;













when





177

°


θ


180

°


,



ρ


(
θ
)


=

0.4


D
0



;













wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw.


The rotation speed ratio between said lateral screw 15 and the central screw 14 is 1.5.


Embodiment 8

The present embodiment has the same structure as that in embodiment 7, except the following features: in the present embodiment, the lateral screw 15 corresponds to the right screw 13 in embodiment 1, and the central screw 14 corresponds to the central screw 6 in embodiment 1. As shown in FIG. 7, with the center points of the cylinder grooves of the barrel corresponding to the central screw 14 and the lateral screw 15 respectively as poles, and the rays elicited horizontally rightwards from the poles as polar axes,


the shape curve of the cross-section of said central screw 14 is symmetric with respective to the ray of θ=0° and the ray of θ=180°, and the polar angle is within 0°≦θ≦180°, the corresponding curve meets that:












when





0

°


θ


15

°


,



ρ


(
θ
)


=

0.5


D
0



;










when





15

°


θ


69.5

°


,














ρ


(
θ
)


=


(




0.5
-

0.00188


(

θ
-
15

)


-







8.21227
×

10

-
4





(

θ
-
15

)

2


+







8.53313
×

10

-
5





(

θ
-
15

)

3


-







4.61141
×

10

-
6





(

θ
-
15

)

4


+







1.48589
×

10

-
7





(

θ
-
15

)

5


-







2.82368
×

10

-
9





(

θ
-
15

)

6


+







2.90967
×

10

-
11





(

θ
-
15

)

7


-






1.25091
×

10

-
13





(

θ
-
15

)

8





)



D
0



;













when





69.5

°


θ


110.5

°


,



ρ


(
θ
)


=

0.35714


D
0



;














when





110.5

°


θ


165

°


,













ρ


(
θ
)


=


(




0.35714
+

3.98268
×

10

-
4




(

θ
-
110.5

)


-







1.91593
×

10

-
4





(

θ
-
110.5

)

2


+







3.54059
×

10

-
5





(

θ
-
110.5

)

3


-







2.64776
×

10

-
6





(

θ
-
110.5

)

4


+







1.08848
×

10

-
7





(

θ
-
110.5

)

5


-







2.49656
×

10

-
9





(

θ
-
110.5

)

6


+







3.00627
×

10

-
11





(

θ
-
110.5

)

7


-






1.48135
×

10

-
13





(

θ
-
110.5

)

8





)



D
0



;













when





165

°


θ


180

°


,



ρ


(
θ
)


=

0.5


D
0



;













wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross-section of said right screw is symmetric with respective to the ray of θ=0° and the ray of θ=180°, and the polar angle is within 0°≦θ≦180°, the corresponding curve meets that:












when





0

°


θ


41

°


,



ρ


(
θ
)


=

0.5


D
0



;










when





41

°


θ


150

°


,














ρ


(
θ
)


=


(




0.5
+

5.80648
×

10

-
4




(

θ
-
41

)


-







1.0674
×

10

-
4





(

θ
-
41

)

2


-






4.94415
×

10

-
7





(

θ
-
41

)

3








1.14699
×

10

-
7





(

θ
-
41

)

4


-






2.86057
×

10

-
9





(

θ
-
41

)

5








3.31268
×

10

-
11





(

θ
-
41

)

6


-






1.89458
×

10

-
13





(

θ
-
41

)

7







4.31702
×

10

-
16





(

θ
-
41

)

8





)



D
0



;













when





150

°


θ


180

°


,



ρ


(
θ
)


=

0.35714


D
0



;













wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw.


The rotation speed ratio between said lateral screw 15 and the central screw 14 is 2.0.


Embodiment 9

The present embodiment has the same structure as that in embodiment 7, except the following features: in the present embodiment, the lateral screw 15 corresponds to the right screw 13 in embodiment 1, and the central screw 14 corresponds to the central screw 6 in embodiment 1. As shown in FIG. 8, with the center points of the cylinder grooves of the barrel corresponding to the central screw 14 and the lateral screw 15 respectively as poles, and the rays elicited horizontally rightwards from the poles as polar axes,


the shape curve of the cross-section of said central screw is symmetric with respective to the ray of θ=120° and the ray of θ=240°, and the polar angle is within 0°≦θ≦120°, the corresponding curve meets that:












when





0

°


θ

10

,



ρ


(
θ
)


=

0.5


D
0



;










when





10

°


θ


58

°


,














ρ


(
θ
)


=


(




0.5
-

0.00831


(

θ
-
10

)


+







2.693515
×

10

-
4





(

θ
-
10

)

2


-







2.05095
×

10

-
5





(

θ
-
10

)

3


+







1.59416
×

10

-
6





(

θ
-
10

)

4


-







6.95534
×

10

-
8





(

θ
-
10

)

5


+







1.65362
×

10

-
9





(

θ
-
10

)

6


-







2.02237
×

10

-
11





(

θ
-
10

)

7


+






9.97816
×

10

-
14





(

θ
-
10

)

8





)



D
0



;














when





58

°


θ


62

°


,



ρ


(
θ
)


=

0.357143


D
0



;










when





62

°


θ


110

°


,














ρ


(
θ
)


=


(




0.35714
-

4.90697
×

10

-
5




(

θ
-
62

)


+






1.02434
×

10

-
5





(

θ
-
62

)

2








1.22629
×

10

-
6





(

θ
-
62

)

3


+







1.76059
×

10

-
7





(

θ
-
62

)

4


-







1.56233
×

10

-
8





(

θ
-
62

)

5


+







5.21936
×

10

-
10





(

θ
-
62

)

6


-







7.85637
×

10

-
12





(

θ
-
62

)

7


+






4.47471
×

10

-
14





(

θ
-
62

)

8





)



D
0



;













when





110

°


θ


120

°


,



ρ


(
θ
)


=

0.5


D
0



;













wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross-section of said right screw is symmetric with respective to the ray of θ=0° and the ray of θ=180°, and the polar angle is within 0°≦θ≦180°, the corresponding curve meets that:












when





0

°


θ


30

°


,



ρ


(
θ
)


=

0.35714


D
0



;










when





30

°


θ


174

°


,














ρ


(
θ
)


=


(




0.35714
-

1.2981
×

10

-
4




(

θ
-
30

)


+







4.15281
×

10

-
5





(

θ
-
30

)

2


-







2.15177
×

10

-
6





(

θ
-
30

)

3


+







6.69687
×

10

-
8





(

θ
-
30

)

4


-







1.10347
×

10

-
9





(

θ
-
30

)

5


+







9.90148
×

10

-
12





(

θ
-
30

)

6


-







4.55739
×

10

-
14





(

θ
-
30

)

7


+






8.37526
×

10

-
17





(

θ
-
30

)

8





)



D
0



;













when





174

°


θ


180

°


,



ρ


(
θ
)


=

0.5


D
0



;













wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw.


The rotation speed ratio between said lateral screw 15 and the central screw 14 is 3.0.


Embodiment 10

The present embodiment has the same structure as that in embodiment 7, except the following features: as shown in FIG. 9, with the center points of the cylinder grooves of the barrel corresponding to the central screw 14 and the lateral screw 15 respectively as poles, and the rays elicited horizontally rightwards from the poles as polar axes,


the shape curve of the cross-section of said central screw is symmetric with respective to the ray of θ=0°, the ray of θ=90°, and the ray of θ=270°, and the polar angle is within 0°≦θ≦90°, the corresponding curve meets that:












when





0

°


θ


3

°


,



ρ


(
θ
)


=

0.5


D
0



;










when





3

°


θ


87

°


,














ρ


(
θ
)


=


(




0.5
-

0.00776


(

θ
-
3

)


+







3.35014
×

10

-
5





(

θ
-
3

)

2


+







8.68488
×

10

-
6





(

θ
-
3

)

3


-







3.48947
×

10

-
7





(

θ
-
3

)

4


+







6.34905
×

10

-
9





(

θ
-
3

)

5


-







5.62555
×

10

-
11





(

θ
-
3

)

6


+






1.98268
×

10

-
13





(

θ
-
3

)

7





)



D
0



;













when





87

°


θ


90

°


,



ρ


(
θ
)


=

0.5


D
0



;













wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross-section of said lateral screw 15 is symmetric with respective to the ray of θ=0° and the ray of θ=180°, and the polar angle is within 0°≦θ≦180°, the corresponding curve meets that:











when





0

°


θ


12

°


,



ρ


(
θ
)


=

0.35714


D
0



;














when





12

°


θ


180

°


,













ρ


(
θ
)


=


(




0.35714
+

1.16393
×

10

-
4




(

θ
-
12

)


+







1.09189
×

10

-
6





(

θ
-
12

)

2


+







1.02469
×

10

-
7





(

θ
-
12

)

3


-







7.39494
×

10

-
10





(

θ
-
12

)

4


-






2.22006
×

10

-
12





(

θ
-
12

)

5








5.1641
×

10

-
14





(

θ
-
12

)

6


-






1.7693
×

10

-
16





(

θ
-
12

)

7





)



D
0



;












wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw.


The rotation speed ratio between said lateral screw 15 and the central screw 14 is 4.0.


Embodiment 11

The present embodiment has the same structure as that in embodiment 7, except the following features: as shown in FIG. 10, with the center points of the cylinder grooves of the barrel corresponding to the central screw 14 and the lateral screw 15 respectively as poles, and the rays elicited horizontally rightwards from the poles as polar axes,


the shape curve of the cross-section of said central screw is symmetric with respective to the ray of θ=0°, the ray of θ=72°, the ray of θ=144°, the ray of θ=216°, and the ray of θ=288°, and the polar angle is within 0°≦θ≦72°, the corresponding curve meets that:











when





0

°


θ


4

°


,



ρ


(
θ
)


=

0.5


D
0



;














when





4

°


θ


34

°


,













ρ


(
θ
)


=


(




0.5
-

0.02464


(

θ
-
4

)


+







0.00617



(

θ
-
4

)

2


-

9.00044
×

10

-
4





(

θ
-
4

)

3


+










7.03593
×

10

-
5





(

θ
-
4

)

4


-







2.98822
×

10

-
6





(

θ
-
4

)

5


+










6.51822
×

10

-
8





(

θ
-
4

)

6


-






5.71897
×

10

-
10





(

θ
-
4

)

7





)



D
0



;













when





34

°


θ


38

°


,



ρ


(
θ
)


=

0.4


D
0



;














when





38

°


θ


68

°


,













ρ


(
θ
)


=


(




0.4
+

2.66133
×

10

-
4




(

θ
-
38

)


-







4.49843
×

10

-
5





(

θ
-
38

)

2


+







3.42164
×

10

-
5





(

θ
-
38

)

3


-







4.56139
×

10

-
6





(

θ
-
38

)

4


+







3.02712
×

10

-
7





(

θ
-
38

)

5


-







9.6014
×

10

-
9





(

θ
-
38

)

6


+






1.16449
×

10

-
10





(

θ
-
38

)

7





)



D
0



;













when





68

°


θ


72

°


,



ρ


(
θ
)


=

0.5


D
0



;













wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw;


the shape curve of the cross-section of said lateral screw 15 is symmetric with respective to the ray of θ=0° and the ray of θ=180°, and the polar angle is within 0°≦θ≦180°, the corresponding curve meets that:












when





0

°


θ


20

°


,



ρ


(
θ
)


=

0.4


D
0



;










when





20

°


θ


170

°


,














ρ


(
θ
)


=


(




0.4
+

4.16738
×

10

-
4




(

θ
-
20

)


-







1.72721
×

10

-
5





(

θ
-
20

)

2


+







7.47552
×

10

-
7





(

θ
-
20

)

3


-







1.38142
×

10

-
8





(

θ
-
20

)

4


+







1.46263
×

10

-
10





(

θ
-
20

)

5


-







9.05881
×

10

-
13





(

θ
-
20

)

6


+







3.10626
×

10

-
15





(

θ
-
20

)

7


-






4.67939
×

10

-
18





(

θ
-
20

)

8





)



D
0



;













when





170

°


θ


180

°


,



ρ


(
θ
)


=

0.5


D
0



;














wherein, θ is a value corresponding to the polar angle degree, ρ is a polar radius, and D0 is an inner diameter of the cylinder groove of the barrel corresponding to said screw.


The rotation speed ratio between said lateral screw 15 and the central screw 14 is 5.0.


Each of the embodiments described above is the preferred embodiment of the present invention, but the embodiments of the present invention are not limited to the above-mentioned embodiments, any other changes, modifications, substitutions, combinations, and simplifications made without departing from the spirit and principle of the present invention, are all equivalent replacement modes, and should be encompassed within the protection scope of the present invention.

Claims
  • 1. A self-cleaning plasticizing venting and extruding apparatus by co-rotating non-twin multi-screws, comprising a screw mechanism, a barrel, a feeding port, a venting port, a discharging port, and a driving mechanism, wherein said driving mechanism is provided at the ends of the barrel respectively, and is connected to the screw mechanism; wherein said screw mechanism is provided inside the barrel, and placed horizontally, and the inner section of the barrel is divided into a solid transporting zone, a melting zone, a venting zone and a compounding and extruding zone; said feeding port is provided above the barrel of the solid transporting zone, said venting port is provided above the barrel of the venting zone, and both the feeding port and the venting port are communicated with the barrel; said discharging port is provided at the end of the barrel, characterized in that said screw mechanism comprises non-uniform shaped central screw and lateral screws, the axis of the central screw is coincided with that of the barrel, the lateral screws are engaged with the central screw, and the contour lines of the threads of the central screw and the lateral screws are tangent to the inner wall of the barrel; said driving mechanism is connected to the central screw and the lateral screws respectively, wherein: said lateral screws are two screws, left screw and right screw, which are provided on both sides of the central screw respectively, and engaged with the central screw;the inner cavity of said barrel is consisted of three cylinder grooves which are communicated with each other, each of the cylinder grooves is fitted with the left screw, the central screw and the right screw respectively; the central axis distances from the cylinder grooves on both sides to the cylinder groove at the central position are equal to the centerline distances from the central screw to the left screw and right screw;the shape of the cross-section of said left screw is the same as the curve shape formed after the cross-section of the right screw is rotated counterclockwise by 180° along the center point of the cylinder groove of the barrel corresponding to the central screw; with the center points of the cylinder grooves of the barrel corresponding to the central screw and each of the lateral screws respectively as poles, and the rays elicited horizontally rightwards from the poles as polar axes,the shape curve of the cross-section of said central screw meets that:
  • 2. A self-cleaning plasticizing venting and extruding apparatus by co-rotating non-twin multi-screws according to claim 1, characterized in that said driving mechanism comprises a main electric motor and a toothed gearing mechanism which are interconnected with each other, and said toothed gearing mechanism is connected to the central screw and the lateral screws respectively.
  • 3. A self-cleaning plasticizing venting and extruding apparatus by co-rotating non-twin multi-screws according to claim 1, characterized in that the peak angle of the screw ridge of said central screw is in a range of 0-180°.
  • 4. A self-cleaning plasticizing venting and extruding apparatus by co-rotating non-twin multi-screws according to claim 1, characterized in that the phase angle difference between the positions of said left screw and right screw is 0°, 90°, or 180°.
  • 5. A self-cleaning plasticizing venting and extruding apparatus by co-rotating non-twin multi-screws, comprising a screw mechanism, a barrel, a feeding port, a venting port, a discharging port, and a driving mechanism, wherein said driving mechanism is provided at the ends of the barrel respectively, and is connected to the screw mechanism wherein said screw mechanism is provided inside the barrel, and placed horizontally, and the inner section of the barrel is divided into a solid transporting zone, a melting zone, a venting zone and a compounding and extruding zone; said feeding port is provided above the barrel of the solid transporting zone, said venting port is provided above the barrel of the venting zone, and both the feeding port and the venting port are communicated with the barrel; said discharging port is provided at the end of the barrel, characterized in that said screw mechanism comprises non-uniform shaped central screw and lateral screws, the axis of the central screw is coincided with that of the barrel, the lateral screws are engaged with the central screw, and the contour lines of the threads of the central screw and the lateral screws are tangent to the inner wall of the barrel; said driving mechanism is connected to the central screw and the lateral screws respectively, wherein: said lateral screws are two screws, left screw and right screw, which are provided on both sides of the central screw respectively, and engaged with the central screw;the inner cavity of said barrel is consisted of three cylinder grooves which are communicated with each other, each of the cylinder grooves is fitted with the left screw, the central screw and the right screw respectively; the central axis distances from the cylinder grooves on both sides to the cylinder groove at the central position are equal to the centerline distances from the central screw to the left screw and right screw;the shape of the cross-section of said left screw is the same as the curve shape of the cross-section of the right screw; with the center points of the cylinder grooves of the barrel corresponding to the central screw and each of the lateral screws respectively as poles, and the rays elicited horizontally rightwards from the poles as polar axes,the shape curve of the cross-section of said central screw meets that:
  • 6. A self-cleaning plasticizing venting and extruding apparatus by co-rotating non-twin multi-screws, comprising a screw mechanism, a barrel, a feeding port, a venting port, a discharging port, and a driving mechanism, wherein said driving mechanism is provided at the ends of the barrel respectively, and is connected to the screw mechanism wherein said screw mechanism is provided inside the barrel, and placed horizontally, and the inner section of the barrel is divided into a solid transporting zone, a melting zone, a venting zone and a compounding and extruding zone; said feeding port is provided above the barrel of the solid transporting zone, said venting port is provided above the barrel of the venting zone, and both the feeding port and the venting port are communicated with the barrel; said discharging port is provided at the end of the barrel, characterized in that said screw mechanism comprises non-uniform shaped central screw and lateral screws, the axis of the central screw is coincided with that of the barrel, the lateral screws are engaged with the central screw, and the contour lines of the threads of the central screw and the lateral screws are tangent to the inner wall of the barrel; said driving mechanism is connected to the central screw and the lateral screws respectively, wherein: said lateral screw is one screw, which is provided on the side of the central screw, and engaged with the central screw; the inner cavity of said barrel is consisted of two cylinder grooves which are communicated with each other, each of the cylinder grooves is fitted with the lateral screw, and the central screw respectively; the central axis distance between the two cylinder grooves is equal to the centerline distance between the central screw and the lateral screw;with the center points of the cylinder grooves of the barrel corresponding to the central screw and the lateral screw respectively as poles, and the rays elicited horizontally rightwards from the poles as polar axes,the shape curve of the cross-section of said central screw is symmetric with respective to the ray of θ=120° and the ray of θ=240°, and the polar angle is within 0°≦θ≦120°, the corresponding curve meets that:
  • 7. A self-cleaning plasticizing venting and extruding method by co-rotating non-twin multi-screws carried out by using an apparatus according to claim 1, characterized by particularly comprising the steps of: (1) after the materials enter the barrel from the feeding port, the central screw and the lateral screw co-rotate along the axis of the respective screws under the drive of the driving mechanism; when the materials enter the solid transporting zone, the feed materials are transported under the co-effects of the axial transporting force from the central screw and the lateral screw and the friction force from the central screw and the lateral screw, so that the materials are forced to move towards the discharging port direction, at the same time the gases in the materials are discharged from the feeding port as the materials are heated;(2) when the materials move to the melting zone, the central screw and the lateral screw rotate in a relatively engaging mode so as to generate a periodical transport space for transporting the materials; the materials are melt under the co-effects of the friction heat generated from the high speed rotation of each of the screws and at the same time the external heat on the barrel; and the melting process is accelerated under the interwiping effect between the central screw and the lateral screw and the asymmetrical effect of the transport space, so that the materials become melts;(3) when the melts enter the venting zone, the space consisted of the central screw and the lateral screw and the inner cavity of the barrel is suddenly enlarged, the materials are continuously stirred by the rotation of the central screw and the lateral screw so that the gases are discharged from the venting port, and the melts move further towards the discharging port direction;(4) when the melts enter the compounding and extruding zone, the melts proceed under the periodical space effect generated by the rotation of the central screw and the lateral screw, the interfaces are facilitated to reorientate and regenerate continuously under the interwiping effect between the central screw and the lateral screw and the asymmetrical effect of the transport space, and the materials are compounded and plasticized, at the same time a self-cleaning effect is carried out by the interwiping effect between each of the screws, so that the melts are stably extruded from the discharging port.
Priority Claims (2)
Number Date Country Kind
2010 1 0201316 Jun 2010 CN national
2011 1 0149868 Jun 2011 CN national
PCT Information
Filing Document Filing Date Country Kind 371c Date
PCT/CN2011/075550 6/9/2011 WO 00 12/12/2012
Publishing Document Publishing Date Country Kind
WO2011/153951 12/15/2011 WO A
US Referenced Citations (9)
Number Name Date Kind
2802238 Colombo Aug 1957 A
4131371 Tynan Dec 1978 A
5048971 Wall et al. Sep 1991 A
6129873 Shelby et al. Oct 2000 A
7025491 Blach et al. Apr 2006 B2
7284897 Blach Oct 2007 B2
7654725 Sturm et al. Feb 2010 B2
20080181051 Yamaguchi et al. Jul 2008 A1
20080248152 Samann et al. Oct 2008 A1
Foreign Referenced Citations (2)
Number Date Country
101879777 Nov 2010 CN
S50-146660 Nov 1975 JP
Non-Patent Literature Citations (2)
Entry
International Search Report, issued in related PCT Application No. CN2011/075550, mailed Sep. 22, 2011, 5 pages.
Written Opinion of the International Searching Authority, issued in related PCT Application No. CN2011/075550, mailed Sep. 22, 2011, 5 pages.
Related Publications (1)
Number Date Country
20130089634 A1 Apr 2013 US