IP Library Granted Patent US 11,421,693
Granted Patent B2
US 11,421,693 · App. 16/881,753 · Granted Aug 23, 2022

Progressing cavity device with cutter disks

Inventor: Edmond Tate Coghlan (Talmo, GA)
Assignee: Roper Pump Company, LLC
F04D7/045F01C19/025F04C2/1075F04C13/004F04C13/005F04D29/2288F01C1/101F01C21/104F04C13/008F04C14/28F04C2230/22F04C2230/231F04C2280/02F05B2240/10F05C2201/0448
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Quick Facts
Patent No.
US 11,421,693
App. No.
16/881,753
Granted
Aug 23, 2022
Kind
B2
Abstract

A stator for a helical gear device includes a first section having first helically convoluted chamber with a set of radially inwardly extending lobes and a second section adjacent to the first section. The second section includes a stack of cutter disks. Each cutter disk includes a front surface, a rear surface, an interior surface defining a central opening extending from the front surface to the rear surface, a forward cutting edge, and a rearward cutting edge. The interior surface forms a same number of lobes for the central opening as the set of radially inwardly extending lobes in the first section. Each cutter disk is aligned along a common centerline, and each cutter disk is rotated slightly relative to each other to form a second helically convoluted chamber with a same pitch as the first helically convoluted chamber. The second helically convoluted chamber exposes, to materials passing through, portions of the forward cutting edge or the rearward cutting edge of each cutter disk.

Claims (54)

1. A stator for a helical gear device, comprising:

a first section including a stack of cutter disks, each of the cutter disks including:

a front surface,

a rear surface,

an interior surface defining a central opening extending from the front surface to the rear surface,

a first cutting edge along the front surface and the interior surface, and

a second cutting edge along the rear surface and the interior surface, wherein the interior surface has a concave contour between the first cutting edge and the second cutting edge,

the interior surface forming a same number of lobes for the central opening as a set of radially inwardly extending lobes, each of the cutter disks being aligned along a common centerline, and each of the cutter disks being rotated slightly relative to each other such that the stack of cutter disks forms a first helically convoluted chamber with the set of radially inwardly extending lobes,

wherein the first helically convoluted chamber in the stack of cutter disks exposes, to materials passing through the first helically convoluted chamber, portions of the first cutting edge or the second cutting edge of each of the cutter disks.

2. The stator of claim 1 , further comprising:

a second section including a second helically convoluted chamber with a same pitch as the first helically convoluted chamber, and

a cylindrical outer housing to which the first section and the second section are secured.

3. The stator of claim 2 , wherein the first section is upstream of the second section.

4. The stator of claim 2 , wherein the first section is downstream of the second section.

5. The stator of claim 2 , wherein the second section includes an elastically deformable elastomeric material.

6. The stator of claim 2 , wherein the second section includes a plurality of metal disks, the metal disks having a smaller thickness then the cutter disks.

7. The stator of claim 1 , wherein the interior surface comprises a V-shape between the first cutting edge and the second cutting edge.

8. The stator of claim 1 , wherein the first section further comprises:

a bonding member fixedly attached to the cutter disks to bond the cutter disks together as the stack.

9. The stator of claim 1 , wherein the cutter disks include metal disks.

10. The stator of claim 9 , wherein the cutter disks include hardened tool steel.

11. The stator of claim 1 , wherein the cutter disks have a thickness between 0.1 inches and 1 inch.

12. The stator of claim 1 , further comprising:

a rigid retention ring fixedly attached to an end of the stack, the rigid retention ring having a central aperture being circular in cross-section and having a constant diameter, the constant diameter of the central aperture of the rigid retention ring being substantially equal to another major diameter of a rotor, the rigid retention ring supporting the rotor disposed in the first helically convoluted chamber.

13. A helical gear device, comprising:

a rotor including one or more radially outwardly extending helical lobes; and

a stator including:

a first section including a stack of cutter disks, each of the cutter disks including:

a front surface,

a rear surface,

an interior surface defining a central opening extending from the front surface to the rear surface,

a first cutting edge along the front surface and the interior surface, and

a second cutting edge along the rear surface and the interior surface, wherein the interior surface has a concave contour between the first cutting edge and the second cutting edge,

the interior surface forming a same number of lobes for the central cavity as a set of radially inwardly extending lobes, each of the cutter disks being aligned along a common centerline, and each of the cutter disks being rotated slightly relative to each other such that the stack of cutter disks forms a first helically convoluted chamber with the set of radially inwardly extending lobes,

wherein the first helically convoluted chamber in the stack of cutter disks exposes, to materials passing through the first helically convoluted chamber, portions of the first cutting edge or the second cutting edge of each of the cutter disks.

14. The helical gear device of claim 13 , further comprising:

a second section including a second helically convoluted chamber with a same pitch as the first helically convoluted chamber; and

a cylindrical stator housing, the first section and the second section being secured within the cylindrical stator housing.

15. The helical gear device of claim 13 , the stator further comprising:

a rigid sleeve defining a cylindrical chamber section for supporting the rotor.

16. The helical gear device of claim 13 , wherein the cutter disks are metal disks.

17. The helical gear device of claim 13 , wherein the cutter disks have a thickness along the common centerline between 0.1 inches and 1 inch.

18. The helical gear device of claim 17 , wherein at least some of the cutter disks have a thickness along the common centerline of at least 0.5 inches.

19. The helical gear device of claim 13 , wherein at least some of the cutter disks have a different thickness than other of the cutter disks.

20. A stator for a helical gear device, comprising:

a first section including a stack of cutter disks, each of the cutter disks including:

a front surface,

a rear surface,

an interior surface defining a central opening extending from the front surface to the rear surface,

a first cutting edge along the front surface and the interior surface, and

a second cutting edge along the rear surface and the interior surface,

the interior surface forming a same number of lobes for the central opening as a set of radially inwardly extending lobes, each of the cutter disks being aligned along a common centerline, and each of the cutter disks being rotated slightly relative to each other such that the stack of cutter disks forms a first helically convoluted chamber with the set of radially inwardly extending lobes,

wherein the interior surface of each of the cutter disks forms an acute angle along one of the first cutting edge or the second cutting edge, and

wherein the first helically convoluted chamber in the stack of cutter disks exposes, to materials passing through the first helically convoluted chamber, portions of the first cutting edge or the second cutting edge of each of the cutter disks.

Assignments (6)
CORRECTIVE ASSIGNMENT TO CORRECT THE PATENT NUMBER PREVIOUSLY RECORDED AT REEL: 61997 FRAME: 614. ASSIGNOR(S) HEREBY CONFIRMS THE SECURITY AGREEMENT. Recorded Nov 13, 2025
From: ALPHA TECHNOLOGIES SERVICES LLC; AMOT CONTROLS LLC; COMPRESSOR CONTROLS LLC; CORNELL PUMP COMPANY LLC; DYNISCO INSTRUMENTS LLC; HANSEN TECHNOLOGIES LLC; METRIX INSTRUMENT CO., L.P.; PETROLEUM ANALYZER COMPANY L.P.; ROPER HOLDINGS, LLC; ROPER INDUSTRIAL PRODUCTS INVESTMENT COMPANY LLC; ROPER PUMP COMPANY LLC; STRUERS LLC; VIA TRAN CORPORATION
To: UBS AG, STAMFORD BRANCH, AS COLLATERAL AGENT
Reel/Frame 073434/0453 →
RELEASE OF SECOND LIEN PATENT SECURITY INTERESTS Recorded May 30, 2025
From: ROYAL BANK OF CANADA
To: AGR INTERNATIONAL, INC.; ALPHA TECHNOLOGIES SERVICES LLC; AMOT CONTROLS LLC; COMPRESSOR CONTROLS LLC; CORNELL PUMP COMPANY LLC; DYNISCO INSTRUMENTS LLC; HANSEN TECHNOLOGIES LLC; METRIX INSTRUMENT CO., L.P.; PETROLEUM ANALYZER COMPANY L.P.; ROPER HOLDINGS, LLC; ROPER INDUSTRIAL PRODUCTS INVESTMENT COMPANY LLC; ROPER PUMP COMPANY LLC; STRUERS LLC; VIATRAN CORPORATION
Reel/Frame 071476/0346 →
SECURITY AGREEMENT (FIRST LIEN) Recorded Nov 28, 2022
From: ALPHA TECHNOLOGIES SERVICES LLC; AMOT CONTROLS LLC; COMPRESSOR CONTROLS LLC; CORNELL PUMP COMPANY LLC; DYNISCO INSTRUMENTS LLC; HANSEN TECHNOLOGIES LLC; METRIX INSTRUMENT CO., L.P.; PETROLEUM ANALYZER COMPANY L.P.; ROPER HOLDINGS, LLC; ROPER INDUSTRIAL PRODUCTS INVESTMENT COMPANY LLC; ROPER PUMP COMPANY LLC; STRUERS LLC; VIATRAN CORPORATION
To: UBS AG, STAMFORD BRANCH, AS COLLATERAL AGENT
Reel/Frame 061997/0614 →
SECURITY AGREEMENT (SECOND LIEN) Recorded Nov 28, 2022
From: ALPHA TECHNOLOGIES SERVICES LLC; AMOT CONTROLS LLC; COMPRESSOR CONTROLS LLC; CORNELL PUMP COMPANY LLC; DYNISCO INSTRUMENTS LLC; HANSEN TECHNOLOGIES LLC; METRIX INSTRUMENT CO., L.P.; PETROLEUM ANALYZER COMPANY L.P.; ROPER HOLDINGS, LLC; ROPER INDUSTRIAL PRODUCTS INVESTMENT COMPANY LLC; ROPER PUMP COMPANY LLC; STRUERS LLC; VIATRAN CORPORATION
To: ROYL BANK OF CANADA, AS COLLATERAL AGENT
Reel/Frame 062003/0566 →
CHANGE OF NAME Recorded May 31, 2022
From: ROPER PUMP COMPANY
To: ROPER PUMP COMPANY, LLC
Reel/Frame 060220/0134 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 22, 2020
From: COGHLAN, EDMOND TATE
To: ROPER PUMP COMPANY
Reel/Frame 052743/0557 →
Continuity (3)
Continuation 15724362 · Oct 4, 2017
Provisional Application 62414874 · Oct 31, 2016
Related Publication 20200284262A1 · Sep 10, 2020
Cited By (1)
US 12,704,022