Roller cone drill bits with optimized bearing structures

• US 9,493,990 B2
• Filed: 12/04/2007
• Issued: 11/15/2016
• Est. Priority Date: 03/02/2004
• Status: Active Grant

• Current Assignee: Halliburton Energy Services Incorporated (Halliburton Company)
• Original Assignee: Halliburton Energy Services Incorporated (Halliburton Company)
• Inventors: Chen, Shilin, Sui, Ping C.
• Primary Examiner(s): SWINNEY, JENNIFER B
• Application Number:
  US11/950,221
• Publication Number:
  US 20080087471A1
• Time in Patent Office: 3,269 Days
• Field of Search: 761/081, 761/082, 175/371
• US Class Current: 1/1
• CPC Class Codes: E21B 10/16 characterised by tooth form or arrangement
• CPC Class Codes: E21B 10/22 characterised by bearing, lubrication or sealing details

Abstract

A roller cone drill bit may include optimally designed bearing structures and cutting structures. The roller cone drill bit may include three cone assemblies rotatably mounted on respective spindles via respective bearing structures. Each cone assembly may have a respective cutting structure with a minimal moment center located along each respective axis of rotation. Each respective bearing structure has a center point located proximate each respective minimal moment center.

Claims

1. A computer implemented method for designing a roller cone drill bit having a bit body with at least a first support arm, a second support arm, and a third support arm with each support arm having a spindle extending therefrom along with a first cone assembly having a first cutting structure, a second cone assembly having a second cutting structure and a third cone assembly having a third cutting structure, the method comprising:

providing a computer configured to determine a minimal moment center of at least one cone assembly;

determining with the computer a first minimal moment center located along a first axis of rotation of the first cone assembly rotatably coupled around a first spindle where a first bending moment of the first spindle is minimized, the first minimal moment center determined based on the first cutting structure of the first cone assembly;

determining with the computer a second minimal moment center located along a second axis of rotation of the second cone assembly rotatably coupled around a second spindle where a second bending moment of the second spindle is minimized, the second minimal moment center determined based on the second cutting structure of the second cone assembly;

determining with the computer a third minimal moment center located along a third axis of rotation of the third cone assembly rotatably coupled around a third spindle where a third bending moment of the third spindle is minimized, the third minimal moment center determined based on the third cutting structure of the third cone assembly;

designing a first bearing assembly for the first spindle with the first bearing assembly having an associated center disposed proximate the first minimal moment center;

designing a second bearing assembly for the second spindle with the second bearing assembly having an associated center disposed proximate the second minimal moment center; and

designing a third bearing assembly for the third spindle with the third bearing assembly having an associated center disposed proximate the third minimal moment center.

2. The method of claim 1 further comprising:

determining the first minimal moment center based upon a first plurality of cutting element profile angles associated with the first cutting structure;

determining the second minimal moment center based upon a second plurality of cutting element profile angles associated with the second cutting structure; and

determining the third minimal moment center based upon a third plurality of cutting element profile angles associated with the third cutting structure.

3. The method of claim 1 further comprising:

determining the first minimal moment center based upon a first cone profile associated with the first cutting structure;

determining the second minimal moment center based upon a second cone profile associated with the second cutting structure; and

determining the third minimal moment center based upon a third cone profile associated with the third cutting structure.

4. The method of claim 1 further comprising:

determining the first minimal moment center based on a first plurality of insert profile angles and a first cone profile associated with the first cutting structure;

determining the second minimal moment center based on a second plurality of insert profile angles and a second cone profile associated with the second cutting structure; and

determining the third minimal moment center based on a third plurality of insert profile angles and a third cone profile associated with the third cutting structure.

5. The method of claim 1 further comprising changing the design of at least one of the bearing assemblies when the respective bearing center is not within a desired proximity of the location of the associated minimal moment center of the respective spindle.

6. A computer implemented method to design a roller cone drill bit having a bit body with at least a first support arm, a second support arm, and a third support arm with each support arm having a spindle extending therefrom along with a first cone assembly having a first cutting structure, a second cone assembly having a second cutting structure and a third cone assembly having a third cutting structure, the method comprising:

providing a computer configured to determine a minimal moment center of at least one cone assembly;

determining with the computer a first minimal moment center located along a first axis of rotation of the first cone assembly rotatably coupled around a first spindle where a first bending moment of the first spindle is minimized, the first minimal moment center determined based on the first cutting structure of the first cone assembly;

determining with the computer a second minimal moment center located along a second axis of rotation of the second cone assembly rotatably coupled around a second spindle where a second bending moment of the second spindle is minimized, the second minimal moment center determined based on the second cutting structure of the second cone assembly;

determining with the computer a third minimal moment center located along a third axis of rotation of the third cone assembly rotatably coupled around a third spindle where a third bending moment of the third spindle is minimized, the third minimal moment center determined based on the third cutting structure of the third cone assembly;

selecting a first bearing assembly for the first spindle with the first bearing assembly having an associated center disposed proximate the first minimal moment center;

selecting a second bearing assembly for the second spindle with the second bearing assembly having an associated center disposed proximate the second minimal moment center; and

selecting a third bearing assembly for the third spindle with the third bearing assembly having an associated center disposed proximate the third minimal moment center.

7. The method of claim 6 further comprising:

determining the first minimal moment center based upon a first insert profile angle of the first cutting structure;

determining the second minimal moment center based upon a second insert profile angle of the second cutting structure; and

determining the third minimal moment center based upon a third insert profile angle of the third cutting structure.

8. The method of claim 6 further comprising:

determining the first minimal moment center based upon a first cone profile associated with the first cutting structure;

determining the second minimal moment center based upon a second cone profile associated with the second cutting structure; and

determining the third minimal moment center based upon a third cone profile associated with the third cutting structure.

9. The method of claim 6 further comprising:

determining the first minimal moment center based on a set of insert profile angles and a first cone profile associated with the first cutting structure;

determining the second minimal moment center based on a set of insert profile angles and a second cone profile associated with the second cutting structure; and

determining the third minimal moment center based on a set of insert profile angles and a third cone profile associated with the third cutting structure.

10. The method of claim 6 further comprising changing a design associated with at least one of the selected bearing assemblies when the respective bearing center is not within a desired proximity of the location of the associated minimal moment center of the respective spindle.

11. A computer implemented method of designing a rotary drill bit having a bit body with at least a first support arm, a second support arm, and a third support arm and each support arm having a respective spindle extending therefrom along with a respective cone assembly operable to be rotatably disposed on each respective spindle comprising:

providing a computer configured to determine a bearing center point of at least one bearing assembly;

determining with the computer a first bearing center point on a first spindle for a first bearing assembly;

determining with the computer a second bearing center point on a second spindle for a second bearing assembly;

determining with the computer a third bearing center point on a third spindle for a third bearing assembly;

designing a first cutting structure for a first cone assembly such that the first bearing center point is proximate a first minimal moment center located along a first axis of rotation of the first cone assembly rotatably coupled around a first spindle where a first bending moment of the first spindle is minimized;

designing a second cutting structure for a second cone assembly such that the second bearing center point is proximate a second minimal moment center located along a second axis of rotation of the second cone assembly rotatably coupled around a second spindle where a second bending moment of the second spindle is minimized; and

designing a third cutting structure for a third cone assembly such that the third bearing center point is proximate a third minimal moment center located along a third axis of rotation of the third cone assembly rotatably coupled around a third spindle where a third bending moment of the third spindle is minimized.

12. The method of claim 11 further comprising:

modifying the first bearing assembly such that the first bearing center point is located closer to the first minimal moment center;

modifying the second bearing assembly such that the second bearing center point is located closer to the second minimal moment center; and

modifying the third bearing assembly such that the third bearing center point is located closer to the third minimal moment center.

13. The method of claim 11 further comprising:

the modifying of the first bearing assembly occurs simultaneously with modifying the first cutting structure;

the modifying of the second bearing assembly occurs simultaneously with modifying the second cutting structure; and

the modifying of the third bearing assembly occurs simultaneously with modifying the third cutting structure.

14. The method of claim 11 further comprising:

the modifying of the first bearing assembly and the modifying of the first cutting structure occurs iteratively;

the modifying of the second bearing assembly and the modifying of the second cutting structure occurs iteratively; and

the modifying of the third bearing assembly and the modifying of the third cutting structure occurs iteratively.