Methods of forming earth-boring tools including sinterbonded components
US-10144113-B2 · Dec 4, 2018 · US
US9700991B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9700991-B2 |
| Application number | US-201514874639-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 5, 2015 |
| Priority date | Nov 10, 2005 |
| Publication date | Jul 11, 2017 |
| Grant date | Jul 11, 2017 |
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Partially formed earth-boring rotary drill bits comprise a first less than fully sintered particle-matrix component having at least one recess, and at least a second less than fully sintered particle-matrix component disposed at least partially within the at least one recess. Each less than fully sintered particle-matrix component comprises a green or brown structure including compacted hard particles, particles comprising a metal alloy matrix material, and an organic binder material. The at least a second less than fully sintered particle-matrix component is configured to shrink at a slower rate than the first less than fully sintered particle-matrix component due to removal of organic binder material from the less than fully sintered particle-matrix components in a sintering process to be used to sinterbond the first less than fully sintered particle-matrix component to the at least a second less than fully sintered particle-matrix component. Earth-boring rotary drill bits comprise such components sinterbonded together.
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What is claimed is: 1. A method of forming an earth-boring rotary drill bit, comprising: tailoring a sinter-shrink rate of a first component to be greater than a sinter-shrink rate of at least a second component, wherein the first component and the second component each comprise an organic binder material; and co-sintering the first component and the at least a second component to remove at least a portion of the organic binder material and to cause the first component to at least partially contract upon and bond to the at least a second component. 2. The method of claim 1 , wherein tailoring a sinter-shrink rate of a first component to be greater than a sinter-shrink rate of a second component comprises selecting the first component and the second component to have at least one input parameter different from one another, the at least one input parameter selected from the group consisting of a particle size and size distribution, a pressing method, a compaction pressure, and a percentage of the organic binder material. 3. The method of claim 1 , wherein tailoring a sinter-shrink rate of a first component to be greater than a sinter-shrink rate of at least a second component comprises selecting the first component to have a first porosity and selecting the second component to have a second porosity lower than the first porosity. 4. The method of claim 1 , wherein tailoring a sinter-shrink rate of a first component to be greater than a sinter-shrink rate of at least a second component comprises uniaxially pressing the first component and isostatically pressing the second component. 5. The method of claim 1 , wherein tailoring a sinter-shrink rate of a first component to be greater than a sinter-shrink rate of at least a second component comprises applying a first compaction pressure to the first component and applying a second compaction pressure to the second component, wherein the second compaction pressure is greater than the first compaction pressure. 6. The method of claim 1 , wherein tailoring a sinter-shrink rate of a first component to be greater than a sinter-shrink rate of at least a second component comprises providing the first component having a first binder content and providing the second component having a second binder content, wherein the second binder content is greater than the first binder content. 7. The method of claim 1 , further comprising varying a composition of the first component from a composition of the second component. 8. The method of claim 1 , further comprising machining a recess in the first component. 9. The method of claim 8 , further comprising disposing the second component within the recess. 10. A method of forming an earth-boring rotary drill bit, comprising: disposing a first component adjacent a second component, wherein the first component and the second component each comprise a plurality of hard particles dispersed throughout a matrix material with an organic binder material, wherein the first component and the second component are each structured to form a portion of an earth-boring rotary drill bit, and wherein a sinter-shrink rate of the first component is greater than a sinter-shrink rate of the second component; and sintering the first component and the second component to remove at least a portion of the organic binder material and to cause the first component to contract and bond to the second component. 11. The method of claim 10 , wherein the first component exhibits a first porosity and the second component exhibits a second porosity lower than the first porosity. 12. The method of claim 10 , further comprising uniaxially pressing the first component and isostatically pressing the second component. 13. The method of claim 10 , further comprising applying a first compaction pressure to the first component and applying a second compaction pressure to the second component, wherein the second compaction pressure is greater than the first compaction pressure. 14. The method of claim 10 , wherein the first component has a first binder content and the second component has a second binder content greater than the first binder content. 15. The method of claim 10 , wherein the first component has a composition different from a composition of the second component. 16. The method of claim 10 , wherein disposing a first component adjacent a second component comprises disposing the second component within a recess in the first component. 17. A method of forming an earth-boring rotary drill bit, comprising: providing a first component with a first sinter-shrink rate and having an organic binder material; disposing at least a second component at least partially within at least a first recess defined by the first component, the at least a second component having a second sinter-shrink rate greater than zero and less than the first sinter-shrink rate; and at least substantially removing the organic binder material from the first component by co-sintering the first component and the at least a second component to cause the first component to shrink at least partially around and bond to the at least a second component. 18. The method of claim 17 , wherein the first component comprises a green component and the second component comprises a brown component. 19. The method of claim 17 , wherein disposing at least a second component at least partially within at least a first recess defined by the first component comprises disposing a tapered surface of the second component adjacent a tapered surface of the first component. 20. The method of claim 17 , wherein at least substantially removing the organic binder material from the first component comprises fully sintering the first component.
Rotary drag type drill bits with teeth, blades or like cutting elements, e.g. fork-type bits, fish tail bits (characterised by wear resisting parts E21B10/46; by conduits or nozzles for drilling fluid E21B10/60; by detachable or adjustable parts E21B10/62) · CPC title
Multiple heating or additional steps (B22F3/101 takes precedence) · CPC title
Sintering only · CPC title
involving the connection or repairing of preformed parts · CPC title
Aspects linked to processes or compositions used in powder metallurgy · CPC title
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