Apparatus for producing cement building material

• US 4,944,595 A
• Filed: 08/19/1988
• Issued: 07/31/1990
• Est. Priority Date: 08/19/1988
• Status: Expired due to Fees

• Current Assignee: E. Khashoggi Industries, LLC
• Original Assignee: Concrete Technology Corporation
• Inventors: Hodson, Simon
• Primary Examiner(s): Hornsby, Harvey C.
• Assistant Examiner(s): Haugland, Scott J.
• Application Number:
  US07/234,819
• Time in Patent Office: 711 Days
• Field of Search: 366/64, 366/65, 366/66, 366/67, 366/263, 366/264, 366/265, 366/292, 366/293, 366/295, 366/302, 366/307, 366/137, 366/327, 366/329, 366/330
• US Class Current: 366/65
• CPC Class Codes: B01F 2025/91 Direction of flow or arrangement of feed and discharge openings
• CPC Class Codes: B01F 27/50 Pipe mixers, i.e. mixers wherein the materials to be mixed flow continuously through pipes, e.g. column mixers
• CPC Class Codes: B01F 27/80 with stirrers rotating about a substantially vertical axis
• CPC Class Codes: B01F 27/86 co-operating with deflectors or baffles fixed to the receptacle

Abstract

A cement paste generator produces a paste with improved workability. The cement paste generator includes a housing, a shaft and a series of blades and baffles which have critical dimensions.

Claims

1. In an apparatus for producing cement paste, the apparatus of the type including a hollow generally barrel-shaped enclosure having a bottom and a central longitudinally disposed rotatable shaft and having a feed inlet to receive cement and water and a discharge outlet to dispense the resulting paste, the inner wall of the enclosure including an upper cylindrical portion above and adjacent to a middle conical portion which is above and adjacent to a lower conical portion, the enclosure including a thrust generating assembly having:

a downthrust generating component which includes a substantially horizontal set of upper downthrust blades is spaced relationship relative to each other, and a lower set of downthrust blades in a spaced relationship relative to each other, each of such blades having a leading and a trailing edge;

an upthrust generating component which includes substantially horizontal upper upthrust blades in spaced relationship relative to each other, each of the upper upthrust blades having a leading and a trailing edge and being coupled to one of the substantially horizontal upper downthrust blades outwardly of the upper downthrust blades, and substantially vertical lower upthrust blades in spaced relationship relative to each other, each of such lower upthrust blades having a leading edge and a trailing edge; and

upper and lower baffles extending from the inner walls of the enclosure toward the shaft, the upper baffle having a lower end and the lower baffle having an upper end, the lower end of the upper baffle and upper end of the lower baffles being spaced from each other providing a baffle space, the lower baffle having a lower free edge, wherein each of the upper upthrust blades is rotatable within the baffle space,

the improvement wherein,

the ratio of R1 to H1 ranges from 0.39 to 0.45, the ratio of R1 to R2 ranges from 0.80 to 0.83, the ratio of R1 to H2 ranges from 0.59 to 0.61, the ratio of R1 to R3 ranges from 0.36 to 0.41, the ratio of R1 to H3 ranges from 0.30 to 0.32, the ratio of R1 to H2a ranges from 0.001 to 1.0, the ratio of R1 to H3a ranges from 0.001 to 1.0, G1 is 0.20±

0.124 inches, G5 is 0.25±

0.125 inches, and V ranges from a height of H1+H2+H3 to H1+H2+H3+4R1,

where R1 is the radius of the cylindrical portion of the inner wall of the housing,

R2 is the radius of the cylindrical portion of the inner wall of the housing along the horizontal plane containing the upper edge of the lower upthrust blade,

R3 is the radius of the lower conical portion of the inner wall of the housing along the horizontal plane containing the lower edge of the lower upthrust blade,

H1 is the distance along the shaft between the horizontal plane containing the leading edge of the upper upthrust blade and the horizontal plane containing lower end of the cylindrical portion of the housing,

H2 is the distance along the shaft between the horizontal plane containing lower end of the cylindrical portion of the housing and the lower end of the middle conical portion of the housing,

H3 is the distance along the shaft between the horizontal plane containing the lower end of the middle portion of the housing and the horizontal plane containing the lower end of the lower conical portion of the housing,

H2a is the smallest vertical distance between the upper edge of the lower downthrust blade and the plane containing the largest radius of the middle conical portion,

H3a is the smallest vertical distance between the bottom and the lower edge of the lower upthrust blade,

G1 is the smallest distance between the leading edge of the upper upthrust blade and the lower edge of the upper baffle,

G5 is the smallest distance between the trailing edge of the lower upthrust blade and the lower free edge of the opposing lower baffle, and

wherein R1 ranges from 4.0 to 48.0 inches.

2. The apparatus of claim 1 wherein G2 is 0.20±

0.125, G3 is 0.20±

0.125, G4 is 0.38±

0.125 and G6 is 0.50±

0.125, wherein

G2 is the smallest distance between the trailing edge of the upper upthrust blade and the upper edge of the lower baffle,

the lower baffle having an outer edge, and G3 is the smallest horizontal distance between the trailing edge of the lower downthrust blade and the outer edge of the lower baffle,

each upper downthrust blade having a free end, and G4 is the smallest distance between the free end of the upper upthrust blade and the cylindrical inner wall portion of the enclosure, and

G6 is the smallest distance between the leading edge of the lower upthrust blade and the lower conical inner wall portion of the enclosure.

3. The apparatus of claim 2 wherein, in inches, R1=24.75, H1=9.75, R2=19.81, H2=14.50, R3=9.00, H3=7.75, G1-G3=0.20, G4=0.38, G5=0.25 and G6=0.50.

4. The apparatus of claim 2 wherein, in inches, R1=8.00, H1=3.60, R2=6.50, H2=4.90, R3=3.25, H3=2.37, G1-G3=0.20, G4=0.38, G5=0.25 and G6=0.50.

5. The apparatus of claim 2 wherein, in inches, R1=24.00, H1=11.75, R2=19.81, H2=12.50, R3=9.00, H3=7.50, G1-G3=0.20, G4=0.38, G5=0.25 and G6=0.50.

6. The apparatus of claim 2 wherein each of the lower upthrust blades is flat and substantially vertical and is coupled to the shaft by a lower collar.

7. The apparatus of claim 6 wherein the leading and trailing edges are inclined relative to each other.

8. The apparatus of claim 1 wherein each of the upper downthrust blades is substantially horizontal and is coupled to the shaft.

9. The apparatus of claim 8 wherein the outer periphery of the upper downthrust blades is interconnected by an upper annular support ring.

10. The apparatus of claim 1 wherein each of the upper upthrust blades is substantially horizontal and affixed to the outer portion of the upper downthrust blades.

11. The apparatus of claim 1 wherein each of the lower downthrust blades is upwardly inclined.

12. The apparatus of claim 11 wherein the lower portion of each of the inclined lower downthrust blades is attached to the shaft by an intermediate collar.

13. The apparatus of claim 12 wherein the upper portion of each of the lower downthrust blades is interconnected by an annular support ring such that the lower downthrust blades form a substantially conical configuration relative to the shaft.

14. The apparatus of claim 11 wherein each of the inclined lower downthrust blades comprises a partial helical spiral configuration.

15. The apparatus of claim 1 wherein the hollow enclosure comprises a substantially cylindrical upper portion, an annular intermediate inclined portion and an annular lower inclined portion.

16. The apparatus of claim 15 wherein each lower baffle has a lower portion provided with an inner edge, wherein the lower downthrust blades form a conical plane, wherein the substantially vertical lower upthrust blades have lower edges, and wherein the annular lower inclined portion, the inner edges of the lower portion of the lower baffles and the conical plane formed by the lower downthrust blades and the lower edges of the substantially vertical lower upthrust blades, are substantially parallel relative to each other.

17. The apparatus of claim 15, wherein the lower baffles have lower portions provided with lower edges and the lower upthrust blades have upper edges, and wherein the lower edges of the lower portion of the lower baffles are substantially parallel to the upper edges of the lower upthrust blades.

18. In an apparatus for producing cement paste, the apparatus of the type including a generally hollow enclosure having a rotatable shaft, the inner wall of the enclosure including a substantially cylindrical portion adjacent to and abutting a first substantially conical portion which is adjacent to and abutting a second substantially conical portion, the second substantially conical portion having an end extended from the point of abutment of the first and second substantially conical portions, the enclosure including a thrust generating assembly having:

a downthrust generating component which includes a first set of downthrust blades, and a second set of downthrust blades, each of such blades having a first and a second edge;

an upthrust generating component which includes a first set of upthrust blades, each blade of the first set of upthrust blades having a first and a second edge and being coupled to one of the blades of the first set of downthrust blades to extend outwardly of the first set of downthrust blades, and a second set of upthrust blades, each blade of the second set of upthrust blades having a first edge and a second edge; and

first and second baffles extending from the inner walls of the enclosure toward the shaft, the first and second baffles having respective ends which are spaced from each other providing a baffle space between the respective ends, wherein the first set of upthrust blades is arranged to be rotatable within the baffle space,

the improvement wherein,

the ratio of R1 to H1 ranges from 0.39 to 0.45, the ratio of R1 to R2 ranges from 0.80 to 0.83, the ratio of R1 to H2 ranges from 0.59 to 0.61, the ratio of R1 to R3 ranges from 0.36 to 0.41, the ratio of R1 to H3 ranges from 0.30 to 0.32, the ratio of R1 to H2a ranges from 0.001 to 1.0, the ratio of R1 to H3a ranges from 0.001 to 1.0, G1 is 0.20±

0.124 inches, G5 is 0.25±

0.125 inches, and V ranges from a height of H1+H2+H3 to H1+H2+H3+4R1,

where R1 is the radius of the substantially cylindrical portion of the inner wall of the housing,

R2 is the radius of the substantially cylindrical portion of the inner wall of the housing along the plane containing the first edge of the second upthrust blade,

R3 is the radius of the second substantially conical portion of the inner wall of the housing along the plane containing the second edge of each second upthrust blade,

H1 is the distance along the shaft between the plane containing the first edge of each first upthrust blade and the plane containing the point of abutment of the substantially cylindrical portion and the first substantially conical portion of the housing,

H2 is the distance along the shaft between the plane containing the point of abutment of the substantially cylindrical portion and the first substantially conical portion of the housing and the point of abutment of the first and second substantially conical portions of the housing,

H3 is the distance along the shaft between the plane containing the point of abutment of the first and second substantially conical portions of the housing and the plane containing the extended end of the second substantially conical portion of the housing,

H2a is the smallest distance between the first edge of the second downthrust blades and the plane containing the largest radius of the first substantially conical portion,

H3a is the smallest distance between the extended end of the second substantially conical portion and the second edge of the second upthrust blades,

G1 is the smallest distance between the first edge of the first upthrust blades and the end of the first baffle,

G5 is the smallest distance between the second edge of the second upthrust blades and the end of the second baffle, and

wherein R1 ranges from 4.0 to 48.0 inches.

19. The apparatus of claim 18 wherein G2 is 0.20±

0.125, G3 is 0.20±

0.125, G4 is 0.38±

0.125 and G6 is 0.50±

0.125, wherein

G2 is the smallest distance between the second edge of the first upthrust blades and the end of the second baffle,

the second baffle having an outer edge, and G3 is the smallest distance between the second edge of the second downthrust blades and the outer edge of the second baffle,

each first downthrust blade having a free end, and G4 is the smallest distance between the free end of the first upthrust blades and the substantially cylindrical inner wall portion of the enclosure, and

G6 is the smallest distance between the first edge of the second upthrust blade and the second substantially conical inner wall portion of the enclosure.

20. The apparatus of claim 18 wherein each of the first downthrust blades is secured with the shaft and has an outer portion extended from the shaft, and each of the first upthrust blades is secured with the outer portion of a respective one of the first blades.