Proppants and methods of making the same

US9975813B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9975813-B2
Application numberUS-201414903457-A
CountryUS
Kind codeB2
Filing dateAug 6, 2014
Priority dateAug 7, 2013
Publication dateMay 22, 2018
Grant dateMay 22, 2018

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  1. Title

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  2. Abstract

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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Abstract

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Synthetic ceramic proppants are described. Methods to make these proppants and methods of using these proppants are also described.

First claim

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What is claimed is: 1. A proppant comprising a porous core, wherein the porous core has an average core density of about less than 2.0 g/cm 3 ; and a shell surrounding the core, the shell including a transition region and an outer shell surrounding the transition region, wherein the shell surrounding the core has an average outer shell density of about 2.7 g/cm 3 to about 3.8 g/cm 3 , wherein the transition region has an average transition region density of about 2.9 g/cm 3 to about 4.0 g/cm 3 , wherein the transition region is formed by sintering a green body core at a temperature of about 500° C. to about 1500° C., wherein sintering a green body core causes the green body core to diffuse into the shell forming the transition region, wherein the transition region is about 2 wt. % to about 69 wt. % of the diffused green body core; wherein an average transition region density is greater than an average outer shell density and the average shell density is greater than an average core density. 2. The proppant of claim 1 , wherein the average transition region density is at least 5% greater than the average outer shell density, and/or the average transition region density is at least 5% greater than the average core density. 3. The proppant of claim 1 , wherein the core is substantially hollow. 4. The proppant of claim 1 , wherein the core, the transition region, the outer shell, or any combination thereof comprises graphene. 5. A proppant comprising a porous core, a transition region surrounding the core, and an outer shell surrounding the transition region, wherein the shell surrounding the core has an average outer shell density of about 2.7 g/cm 3 to about 3.8 g/cm 3 , wherein the transition region has an average transition region density of about 2.9 g/cm 3 to about 4.0 g/cm 3 , wherein the transition region is formed by sintering a green body core at a temperature of about 1200° C. to about 2000° C., wherein sintering a green body core causes the green body core to diffuse into the shell foiming the transition region, wherein the transition region is about 5 wt. % to about 49 wt. % of the diffused green body core, wherein an average transition region porosity is less than an average outer shell porosity and the average outer shell porosity is less than an average core porosity. 6. The proppant of claim 5 , wherein a) the average transition region porosity is less than the average outer shell porosity, or b) the average transition region porosity is less compared to the average core porosity, or both a) and b). 7. The proppant of claim 5 , wherein the core is substantially hollow and the average core porosity is about greater than 40 vol. % based on the total volume of the core. 8. The proppant of claim 1 , wherein the average core porosity is about greater than 40 vol. % based on the total core volume. 9. The proppant of claim 1 , wherein the average shell porosity is about 5 vol. % to about 10 vol. % based on the total volume of the shell. 10. The proppant of claim 1 , wherein the average transition region porosity is about 0 vol. % to about 5 vol. % based on the total volume of the transition region. 11. The proppant of claim 1 , wherein the green body core comprises low melting components. 12. The proppant of claim 11 , wherein the low melting components are present in an amount of about 2.85 wt. % to about 3.7 wt. % based on the total weight of the core composition. 13. The proppant of claim 1 , wherein the proppant has a change in sphericity of about 0.5% to about 5%. 14. The proppant of claim 1 , wherein the proppant comprises a glass-ceramic material. 15. The proppant of claim 14 , wherein the glass-ceramic material comprises aluminum oxide and silicon oxide. 16. The proppant of claim 15 , wherein the aluminum oxide and silicon oxide are present before sintering in a ratio of about 0.5 to about 2.3. 17. The proppant of claim 14 , wherein the glass-ceramic material has a crystallinity of about 5 vol. % to about 100 vol. %. 18. The proppant of claim 5 , wherein the average shell porosity is about 5 vol. % to about 10 vol. % based on the total volume of the shell. 19. The proppant of claim 5 , wherein the average transition region porosity is about 0 vol. % to about 5 vol. % based on the total volume of the transition region. 20. The proppant of claim 5 , wherein the proppant comprises a glass-ceramic material.

Assignees

Inventors

Classifications

  • Spheres · CPC title

  • Burning or sintering processes (C04B33/32 takes precedence {; powder metallurgy B22F}) · CPC title

  • millimeter or submillimeter sized, i.e. larger than 0,1 mm · CPC title

  • Green bodies or pre-forms with well-defined density · CPC title

  • Alumina or aluminates · CPC title

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What does patent US9975813B2 cover?
Synthetic ceramic proppants are described. Methods to make these proppants and methods of using these proppants are also described.
Who is the assignee on this patent?
Halliburton Energy Services Inc
What technology area does this patent fall under?
Primary CPC classification C04B35/78. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Tue May 22 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).