DOWNHOLE TURBINE ASSEMBLY

• US 20160341012A1
• Filed: 12/09/2014
• Published: 11/24/2016
• Est. Priority Date: 12/09/2014
• Status: Active Grant

• Current Assignee: Halliburton Energy Services Incorporated (Halliburton Company)
• Original Assignee: Halliburton Energy Services Incorporated (Halliburton Company)
• Inventors: RILEY, Benjamin Scott, CHAMBERS, Larry DeLynn
• Granted Patent: US 10,280,717 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: E21B 41/0085 Adaptations of electric power generating means for use in boreholes

Abstract

A downhole turbine assembly includes a stator housing having one or more stator blades positioned within the stator housing and extending radially inward therefrom. A rotor shaft having a first end and a second end is rotatably positioned within the stator housing and has a first portion exhibiting a first diameter and a second portion exhibiting a second diameter greater than the first diameter. One or more rotor blades are secured to the second portion for rotation with the rotor shaft, and a first bearing assembly is positioned at the first end and a second bearing assembly is positioned at the second end. At least one of the bearing housings provides a primary flow path and a secondary flow path, and one or more radial bearings and one or more thrust bearings are arranged in the secondary flow path.

Claims

1. A downhole turbine assembly, comprising:

a stator housing having one or more stator blades positioned within the stator housing and extending radially inward therefrom;

a rotor shaft rotatably positioned within the stator housing and having a first portion exhibiting a first diameter and a second portion exhibiting a second diameter greater than the first diameter, the first portion including an upper first portion provided at a first end of the rotor shaft and terminating at an upper bearing shoulder and a lower first portion provided at a second end of the rotor shaft and terminating at a lower bearing shoulder;

one or more rotor blades secured to the second portion for rotation with the rotor shaft and being interleaved with the one or more stator blades; and

a first bearing assembly positioned at the first end and a second bearing assembly positioned at the second end, the first and second bearing assemblies each including a bearing housing, one or more radial bearings, and one or more thrust bearings,

wherein at least one of the bearing housings provides a primary flow path and a secondary flow path, and wherein the one or more radial bearings and the one or more thrust bearings are arranged in the secondary flow path.

2. The downhole turbine assembly of claim 1, wherein the one or more radial bearings and the one or more thrust bearings each include a rotor shaft component, the turbine assembly further comprising:

a first mechanical fastener secured to the first end of the rotor shaft to preload the rotor shaft components of the upper bearing assembly against the upper bearing shoulder; and

a second mechanical fastener secured to the second end of the rotor shaft to preload the rotor shaft components of the lower bearing assembly against the lower bearing shoulder.

3. The downhole turbine assembly of claim 2, wherein at least one of the first and second mechanical fasteners is an output coupling that operatively couples the rotor shaft to a driven component.

4. The downhole turbine assembly of claim 1, further comprising a stator lock ring that secures the one or more stator blades within the stator housing, wherein the stator lock ring preloads the one or more stator blades against a stator shoulder defined on an inner radial surface of the stator housing.

5. The downhole turbine assembly of claim 1, wherein the one or more rotor blades are secured to the second portion of the rotor shaft with a rotor lock ring that forces the one or more rotor blades against a rotor shoulder defined on the rotor shaft.

6. The downhole turbine assembly of claim 1, wherein at least one of the one or more rotor blades is keyed to the second portion of the rotor shaft.

7. The downhole turbine assembly of claim 1, wherein rotor shaft exhibits a polygonal cross-sectional shape and the one or more rotor blades are shaped to mate with the polygonal cross-sectional shape to secure the one or more rotor blades to the second portion.

8. The downhole turbine assembly of claim 1, wherein axially adjacent mating faces of two or more of the one or more rotor blades interlock to prevent relative rotation.

9. The downhole turbine assembly of claim 1, wherein one or both of the plurality of stators and the plurality of rotors are clocked.

10. The turbine assembly of claim 1, wherein the primary and secondary flow paths receive a fluid and the primary flow path receives a greater flow of the fluid as compared to the secondary flow path.

11. The downhole turbine assembly of claim 1, wherein at least one of the one or more radial bearings and the one or more thrust bearings comprises a bearing made of an ultra-hard material.

12. The downhole turbine assembly of claim 11, wherein the at least one of the one or more radial bearings and the one or more thrust bearings is a polycrystalline diamond (PDC) bearing comprising one or more PDC discs.

13. The downhole turbine assembly of claim 12, further comprising a substrate coupled to the bearing housing, wherein the one or more PDC discs are brazed into the substrate.

14. The downhole turbine assembly of claim 1, wherein at least one of the one or more radial bearings and the one or more thrust bearings comprises a bearing selected from the group consisting of a ball bearing, a needle bearing, a marine bearing, an oil lubricated bearing, and any combination thereof.

15. The downhole turbine assembly of claim 1, further comprising a flow tube that defines a flow tube shoulder, wherein the stator housing and the bearing housings of the first and second bearing assemblies are each sized to be inserted into the flow tube and preloaded against the flow tube shoulder with a coupling.

16. A method, comprising:

circulating a fluid to a downhole turbine assembly, the downhole turbine assembly including;

a stator housing having one or more stator blades positioned within the stator housing and extending radially inward therefrom; and

a rotor shaft rotatably positioned within the stator housing and having a first portion exhibiting a first diameter and a second portion exhibiting a second diameter greater than the first diameter, the first portion including an upper first portion provided at a first end of the rotor shaft and terminating at an upper bearing shoulder and a lower first portion provided at a second end of the rotor shaft and terminating at a lower bearing shoulder;

rotating the rotor shaft as the fluid impinges upon one or more rotor blades secured to the second portion of the rotor shaft;

assuming radial and thrust loads on the rotor shaft with a first bearing assembly positioned at the first end and a second bearing assembly positioned at the second end, the first and second bearing assemblies each including a bearing housing, one or more radial bearings, and one or more thrust bearings, wherein at least one of the bearing housings provides a primary flow path and a secondary flow path; and

flowing a first portion of the fluid through the primary flow path, and flowing a second portion of the fluid through the secondary flow path, wherein the one or more radial bearings and the one or more thrust bearings are arranged in the secondary flow path.

17. The method of claim 16, wherein the one or more radial bearings and the one or more thrust bearings each include a rotor shaft component, the method further comprising:

preloading the rotor shaft components of the upper bearing assembly against the upper bearing shoulder by securing a first mechanical fastener secured to the first end of the rotor shaft; and

preloading the rotor shaft components of the lower bearing assembly against the lower bearing shoulder by securing a second mechanical fastener secured to the second end of the rotor shaft.

18. The method of claim 17, wherein at least one of the first and second mechanical fasteners is an output coupling, the method further comprising:

operatively coupling the rotor shaft to a driven component via the output coupling; and

transmitting rotational energy to the driven component via the output coupling.

19. The method of claim 16, further comprising a stator lock ring that secures the one or more stator blades within the stator housing, wherein the stator lock ring preloads the one or more stator blades against a stator shoulder defined on an inner radial surface of the stator housing.

20. The method of claim 16, further comprising securing the one or more rotor blades to the second portion of the rotor shaft with a rotor lock ring that forces the one or more rotor blades against a rotor shoulder defined on the rotor shaft.

21. The method of claim 16, wherein circulating the fluid to the downhole turbine assembly is preceded by:

introducing the downhole turbine assembly into a flow tube that defines a flow tube shoulder; and

securing the downhole turbine assembly within the flow tube with a coupling that preloads the stator housing and the bearing housings of the first and second bearing assemblies against the flow tube shoulder.