MX2014004760A - Porous proppants. - Google Patents
Porous proppants.Info
- Publication number
- MX2014004760A MX2014004760A MX2014004760A MX2014004760A MX2014004760A MX 2014004760 A MX2014004760 A MX 2014004760A MX 2014004760 A MX2014004760 A MX 2014004760A MX 2014004760 A MX2014004760 A MX 2014004760A MX 2014004760 A MX2014004760 A MX 2014004760A
- Authority
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- Mexico
- Prior art keywords
- proppant
- porous
- less
- psi
- specific gravity
- Prior art date
Links
- 239000002245 particle Substances 0.000 claims abstract description 47
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims abstract description 45
- 229910010271 silicon carbide Inorganic materials 0.000 claims abstract description 35
- 239000011148 porous material Substances 0.000 claims abstract description 19
- 229910052581 Si3N4 Inorganic materials 0.000 claims abstract description 13
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 claims abstract description 13
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 8
- 239000010703 silicon Substances 0.000 claims abstract description 7
- 230000005484 gravity Effects 0.000 claims description 35
- 239000000203 mixture Substances 0.000 claims description 26
- 238000000034 method Methods 0.000 claims description 15
- 238000012360 testing method Methods 0.000 claims description 13
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 11
- 229910052799 carbon Inorganic materials 0.000 claims description 10
- 229910021426 porous silicon Inorganic materials 0.000 claims description 10
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 7
- 238000010438 heat treatment Methods 0.000 claims description 3
- 238000001665 trituration Methods 0.000 claims description 2
- 239000000463 material Substances 0.000 abstract description 19
- 239000012530 fluid Substances 0.000 abstract description 11
- 239000000919 ceramic Substances 0.000 abstract description 5
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 21
- 230000015572 biosynthetic process Effects 0.000 description 9
- 238000005755 formation reaction Methods 0.000 description 9
- 239000004576 sand Substances 0.000 description 9
- 230000035699 permeability Effects 0.000 description 8
- 238000005245 sintering Methods 0.000 description 5
- 229910052580 B4C Inorganic materials 0.000 description 4
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 description 4
- 238000009826 distribution Methods 0.000 description 4
- 230000007774 longterm Effects 0.000 description 4
- 238000012856 packing Methods 0.000 description 4
- 239000000377 silicon dioxide Substances 0.000 description 4
- 229910052814 silicon oxide Inorganic materials 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 3
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical group O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 description 3
- 230000004927 fusion Effects 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 229910052863 mullite Inorganic materials 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 238000011282 treatment Methods 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical group O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 2
- 235000012239 silicon dioxide Nutrition 0.000 description 2
- 239000012798 spherical particle Substances 0.000 description 2
- 206010003497 Asphyxia Diseases 0.000 description 1
- 229910052582 BN Inorganic materials 0.000 description 1
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 240000007049 Juglans regia Species 0.000 description 1
- 235000009496 Juglans regia Nutrition 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 229910001570 bauxite Inorganic materials 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 230000002902 bimodal effect Effects 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 239000012267 brine Substances 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 239000006229 carbon black Substances 0.000 description 1
- CREMABGTGYGIQB-UHFFFAOYSA-N carbon carbon Chemical compound C.C CREMABGTGYGIQB-UHFFFAOYSA-N 0.000 description 1
- 239000011203 carbon fibre reinforced carbon Substances 0.000 description 1
- 239000003575 carbonaceous material Substances 0.000 description 1
- -1 certain clays Chemical compound 0.000 description 1
- 239000003610 charcoal Substances 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 239000004927 clay Chemical group 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000007872 degassing Methods 0.000 description 1
- 238000000280 densification Methods 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- HNPSIPDUKPIQMN-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical group O=[Si]=O.O=[Al]O[Al]=O HNPSIPDUKPIQMN-UHFFFAOYSA-N 0.000 description 1
- 238000005538 encapsulation Methods 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 238000005469 granulation Methods 0.000 description 1
- 230000003179 granulation Effects 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000000135 prohibitive effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 238000001878 scanning electron micrograph Methods 0.000 description 1
- 239000002210 silicon-based material Substances 0.000 description 1
- HPALAKNZSZLMCH-UHFFFAOYSA-M sodium;chloride;hydrate Chemical compound O.[Na+].[Cl-] HPALAKNZSZLMCH-UHFFFAOYSA-M 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000005563 spheronization Methods 0.000 description 1
- 238000001694 spray drying Methods 0.000 description 1
- 230000000638 stimulation Effects 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 239000011135 tin Substances 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 235000020234 walnut Nutrition 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B43/00—Methods or apparatus for obtaining oil, gas, water, soluble or meltable materials or a slurry of minerals from wells
- E21B43/25—Methods for stimulating production
- E21B43/26—Methods for stimulating production by forming crevices or fractures
- E21B43/267—Methods for stimulating production by forming crevices or fractures reinforcing fractures by propping
Landscapes
- Life Sciences & Earth Sciences (AREA)
- Engineering & Computer Science (AREA)
- Geology (AREA)
- Mining & Mineral Resources (AREA)
- Physics & Mathematics (AREA)
- Environmental & Geological Engineering (AREA)
- Fluid Mechanics (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Ceramic Products (AREA)
- Carbon And Carbon Compounds (AREA)
Abstract
Ceramic ultra-lightweight porous proppants can be cost-effective for use in hydraulic fracturing operations. Silicon carbide and silicon nitride can advantageously provide a high degree of strength while having sufficient porosity to remain lightweight and facilitate fluid transport. Oxycarbides and oxynitrides of silicon are also suitable lightweight proppant materials. In one aspect, a porous proppant has a generally spherical shape with a particle diameter between 100 and 2,000 microns, median pore sizes between 1 and 50 microns, and a porosity between 10 and 70% of the total spherical volume. For a plurality of porous proppants, each porous proppant individually can form a proppant pack.
Description
POROUS POINTERS
PRIORITY CLAIM
This request claims priority to the provisional request of E.U.A. No. 61 / 549,878, entitled "Porous Planter" and filed on October 21, 2011, which is incorporated for reference in its entirety.
TECHNICAL FIELD
This invention discloses porous props for use in hydraulic fracturing, and methods of fabrication and use thereof.
BACKGROUND OF THE INVENTION
Hydraulic fracturing, or fracking, is a common stimulation technique used to increase the production of fluids from underground formations. In a typical hydraulic fracturing treatment, fracturing the treatment fluid containing a proppant material is injected into the formation at a pressure sufficiently high enough to cause the formation or elongation of the fractures in the reservoir. Proppant material remains in
the fracture after completing the treatment, where it serves to keep the fracture open, thereby increasing the ability of the fluids to migrate from the formation to the perforation through the fracture.
Many different materials have been used as proppant including sand, glass beads, walnut shells and metal shot. Sand-based sills are commonly used due to the low cost of sand. However, these proppants often can not be used in the depths where pressures are greater than approximately 2500 psi. The relatively recent increase in the use of hydraulic ramming, often referred to as hydraulic fracturing, has presented a need for proppants that have improved crushing forces.
Many hydraulic fracturing wells in depths greater than a few hundred feet and can subject proppant materials to pressures in excess of 10,000 psi. Therefore, strengthening coatings on sand and sintered ceramic proppant have been used to achieve greater crushing forces.
Two important proppant properties are crushing strength and density. High crushing force may be desirable for use in deeper fractures where pressures are greater, eg, greater than approximately 2500 psi. As the relative strength of several
materials increases, so they also have the respective particle densities. Tarpings that have higher densities may be more expensive to use, for example due to transportation costs. Accordingly, there is a need for ultra-lightweight proppant having increased crushing force.
BRIEF DESCRIPTION OF THE INVENTION
Porous ultra-light ceramic tiles can be cost effective for use in hydraulic fracturing operations. Silicon carbide and silicon nitride can advantageously provide a high degree of strength while having sufficient porosity to remain light and facilitate fluid transport. Oxicarbides and silicon oxynitrides are also suitable light propping materials.
In one aspect, a porous proppant has a generally spherical shape with a particle diameter between 100 and 2,000 microns, average pore sizes between 1 and 50 microns, and a porosity between 10 and 70% of the total spherical volume.
For a plurality of porous proppant, each porous proppant can individually form a proppant pack having a crushing force of at least
2,000 psi and an apparent specific gravity of 1.0 g / cc or less; a crushing force of at least 4,000 psi and an apparent specific gravity of 1.3 g / cc or less; a crushing force of at least 6,000 psi and an apparent specific gravity of 1.6 g / cc or less; a crushing force of at least 8,000 psi and an apparent specific gravity of 1.8 g / cc or less; a crushing force of at least 10,000 psi and an apparent specific gravity of 2.0 g / cc or less; or a crushing force of at least 12,000 psi and an apparent specific gravity of 2.2 g / cc or less.
For a plurality of porous proppant, each porous proppant can individually form a proppant pack that produces 10% or less of fines in a trituration test.
The porous particles can include silicon carbide, silicon nitride or a combination thereof. The porous particles may include 90% or more of silicon carbide. The porous particles may have a sphericity of 0.91 or greater, or 0.95 or greater. The porous particles may have a roundness of 0.91 or greater, or 0.95 or greater.
In another aspect, a composition includes a plurality of particles including silicon carbide, silicon nitride or a combination thereof, forming a porous proppant having a generally
spherical with a particle diameter between 100 and 2,000 microns, average pore sizes between 1 and 50 microns and a porosity between 10 and 70% of the total spherical volume.
For a plurality of compositions, each porous proppant can individually form a pack of proppant having a crushing force of at least 2,000 psi and an apparent specific gravity of 1.0 g / cc or less; a crushing force of at least 4,000 psi and an apparent specific gravity of 1.3 g / cc or less; a crushing force of at least 6,000 psi and an apparent specific gravity of 1.6 g / cc or less; a crushing force of at least 8,000 psi and an apparent specific gravity of 1.8 g / cc or less; a crushing force of at least 10,000 psi and an apparent specific gravity of 2.0 g / cc or less; or a crushing force of at least 12,000 psi and an apparent specific gravity of 2.2 g / cc or less.
For a plurality of compositions, each porous proppant can individually form a pack of proppant that produces 10% or less fines in a crushing test.
In the composition, the particles may have a sphericity of 0.91 or greater, or 0.95 or greater. The particles may have a roundness of 0.91 or greater, or 0.95 or greater.
In another aspect, a method of using a composition
of claim 15, which comprises injecting the composition into a hydrofracture.
In another aspect, a method of making a porous proppant includes heating a composition that includes a carbon source and a silicon source between 10 and 70% porosity of the total proppant volume thereby forming a carbide proppant. porous silicon.
The porous silicon carbide proppant can have a particle diameter of between 100 and 2,000 microns, average pore sizes between 1 and 50 microns, and a porosity between 10 and 70% of the total spherical volume.
Other aspects, modalities and characteristics will be apparent from the following description, drawings and claims.
BRIEF DESCRIPTION OF THE DRAWINGS
Figures 1-2 are SEM images of a porous proppant.
Figures 3A-3B show results of short-term conductivity and permeability test of porous proppant.
Figures 4A-4B show results of long-term conductivity and permeability test of a porous proppant.
DETAILED DESCRIPTION OF THE INVENTION
Two important physical attributes of proppant packages - packet strength and packet porosity - depend on many factors. Proppant density is also an important attribute. These three important attributes strongly influence the overall performance of the well's conductivity. Although there are many factors that determine the resistance to compression, porosity and density to achieve total conductivity, they can be categorized into four levels of importance.
The first and most important level (the objective) is conductivity. This determines the performance of the well. Permeability and other related flow terminology are associated with conductivity. It is well known that the strength and porosity of the proppant package are primary factors in the determination of conductivity. Accordingly, proppants provide increased well performance, for example, proppants that have strength and / or increased porosity, are desirable.
The second level of importance is combined strength and porosity. A proppant package must be strong in compression and do not produce fines that will plug the pores of the proppant package in the well. When the proppers are crushed they produce small fractions called fines
that can reduce the performance of the well. Therefore porous, strong proppant packs are more desirable for conductivity.
A third level of importance is the proppant density. Although the density does not affect the conductivity once a proppant package is in place, a less dense proppant can be supplied in the well before being installed. Lighter runners flow with water, brine or other fluid media to allow deeper penetration into the well.
Fourth level attributes that contribute to important attributes of a higher level include, but are not limited to: composition of the primary material; composition of secondary material; choke size of the composite grains of the primary material with itself or secondary composition; Sintered grain size of the composition of the primary material; volume of porosity - total volume in proppant; pore size; pore shape; open vs closed pores; sphericity / roundness; proppant particle size (eg sphere diameter); proppant particle size distribution; nature of the size distribution (for example, single-mode, bimodal, or other size distribution).
While many variables determine overall performance, the combined properties of strength and
Porosity mainly influence conductivity. A desirable proppant is one that has low density yet with high compressive force.
The failure mode of proppant packs typically involves the fracturing of individual proppers, under well-forming pressure, thus producing the smallest (fine) proppant particles. The clogging failure mode results from fines produced from crushing performance of the proppant at poorer conductivity when finer products are produced.
With reference to Figure 1, a porous proppant is generally indicated by the numeral 100. Porous stalk 100 may generally be spherical, ovoid, elongate, cylindrical or other, including an irregular shape. For example, the porous proppant can be spherical and has a Krumbein sphericity of less than about 0.5, at least 0.6 or at least 0.7, at least 0.8 or at least 0.9, and / or a roundness of at least 0.4, at least 0.5, at least 0.6, at least 0.7, at least 0.8 or at least 0.9. The term "spherical" can refer to the roundness and sphericity in the Krumbein and Sloss graph by visually classifying 10 to 20 randomly selected particles. Sphericity and roundness of at least .9 is more desirable to achieve greater strength at lower densities.
Porous stanchion 100 can be formed from any suitable oxide, carbide, or silicon nitride, boron, aluminum, zirconium, iron, titanium, zinc, tin, chromium, manganese, magnesium or calcium. For example, the porous proppant of a silicon carbide, a silicon nitride, a silicon oxide, an aluminum oxide, a boron carbide or a combination thereof can be formed. In some cases, the porous proppant 100 may be composed of at least 90% of the silicon carbide, at least 95% of silicon carbide, at least 98% of the silicon carbide, or at least 99% of the silicon carbide. . In some cases, porous proppant 100 may be composed of at least 90% silicon nitride, at least 95% silicon nitride, at least 98% silicon nitride, or at least 99% silicon nitride. . Porous bolster 100 can have a diameter ranging from about 1 miera to about 3,000 microns, for example, between about 100 and 2,000 microns. In some embodiments, porous proppant 100 has a diameter of approximately 500 microns.
The average pore sizes of the porous proppant can be between, for example, about 1 miera and about 50 microns, and the porosity can represent about 10% to about 70% of the total spherical volume. Pore sizes can be adapted in
size and volume to achieve different crushing forces for different well formations.
The porous proppant can have a crushing force greater than 10,000 psi with a specific gravity of less than 2.2 g / cc. The porous proppant may have a crushing force greater than 11,000 psi, greater than 12,000 psi, or higher. The porous proppant can have a specific gravity of less than 2.0 g / cc, less than 1.8 g / cc, less than 1.6 g / cc, less than 1.5 g / cc or less than 1.4 g / cc, or less. The porous proppant desirably combines the properties of high crushing strength and low density. For example, porous proppant can have a crushing force greater than 10,000 psi with a specific gravity of less than 2.2 g / cc; a crushing force greater than 11,000 psi with a specific gravity of less than 2.0 g / cc; a crushing force greater than 12,000 psi with a specific gravity of less than 1.8 g / cc; or even higher crushing forces combined with even smaller specific gravities.
Figure 2 shows a proppant with higher magnification than Figure 1. porous proppant 100 has a scaffold 110 that form heterogeneous pore structure of bars 120. The scaffold 110 imparts increased strength for proppant and proppant 100 can resist crushing forces over 12.000 psi.
In addition, pores 120 offer permeability so that, once injected in a hydrofracture, the released fluid can pass through the pores of the proppant as well as around the spaces formed by the packing of the particles. Non-porous fasteners, or those proppant modified with external surface treatments, are limited in the extraction of fluid as the fluid can only pass through the tortuous path created by the packing of the particles. Thus, porous proppant can greatly increase the amount of fluid extracted and also extracts the fluid faster than the proppant currently used.
Porous bolster 100 can be formed by reduction of silicon and carbon based materials, for example, to provide a porous proppant of silicon carbide. In one embodiment, a carbon source is reacted with a silicon source to form a porous silicon carbide by controlling the reaction to avoid densification. Alternatively, the pores can be formed during a sintering process. Template creation approaches can also be used to form pores.
A suitable carbon source can be derived from charcoal. Other suitable carbon sources include graphite or carbon black.
In some embodiments, a carbon source is combined with a source of silicon (such as a silicon dioxide, eg, silica or sand) and reduced in the presence of reducing agents to produce silicon carbide. The porosity resulting from oxygen degassing can impart porosity to the resulting silicon carbide. Silicon carbide powder can also be sintered without pressure to produce porous proppant. Reaction binding is another process that can be used to produce porous proppant. Any suitable method can be used to process a solid material into spherical particles, such as, for example, grinding, spray drying, spheronization, encapsulation, granulation or extrusion. In most embodiments, spherical particles are desirable. For example, the porous non-sintered source may have a Krumbien sphericity of 0.8 or higher, 0.9 or higher, 0.95 or higher, 0.98 or higher, or 0.99 or higher.
Sintering can be performed using any suitable method of heating a silicon carbide source, or a carbon source and a silicon source, including, for example, resistance, radiation, convection, induction, plasma, laser, microwave or other methods. Additional sintering aids can optionally be included, such as a polymeric binder or binders
organic The measurement of the sintering can be controlled by adjusting the temperature and duration. In a first phase of formation of a porous proppant, a reduction step of a carbon source and a silicon dioxide produces a porous silicon carbide. Therefore, a particulate carbon carbon source can produce particulate porous silicon carbide. In a second optional phase of formation a porous proppant, sintering particulate particulate silicon carbide particles can produce a controllable degree of fusion. Therefore, "choking" can occur between the porous silicon carbide particles, that is, the formation of bridges that bind porous silicon carbide particles. The bridges thus formed are desirably composed of silicon carbide, instead of a silicon oxide, which would result in a weak proppant of similar material with bridges composed of silicon carbide. Amounts of less than 10% of the oxides are preferable in the tightening regions (for example, oxides such as silicon oxide, alumina, zirconia, glass, mullite and other clay bonds) may be acceptable, whereby 90% or more of the porous proppant is composed of silicon carbide or silicon nitride. Boron carbide and boron nitride are also acceptable in the choke region at levels less than 10%. Preferably silicon carbide is bonded to silicon carbide as the region
of strangulation.
The throttling process can form a structure that has an additional level of porosity, that is, the porosity formed between the particles that are joined by bridges. Thus the resulting material can have a large-scale porosity (for example, of the order of one miera at 50 microns) between the particles; and porosity on a smaller scale (for example, in the order of less than one miera to 10 microns). Control over this large-scale porosity is achieved by controlling the degree of fusion between the particles. Higher temperatures and increased time promotes a higher degree of fusion. When they are fused to a higher degree, the bridges between the particles become larger and more numerous; Individual particles become less distant and more agglomerated.
Fine of less than 10% may be generally acceptable in crushing tests. 90% or larger original particle sizes should be retained in the sieve during a crushing test procedure. Crushing tests are not a substitute for current well performance or conductivity but are an adequate indicator of propping performance, and for comparisons of different propping materials.
Backward flow is another issue that can result in poor well conductivity performance.
The strength of the proppant pack is not only determined by the compressive strength of the proppant but also how well they stay in the pack. Lower density siding may have negative backward flow problems, then traditional coatings (resins) may be used in the porous props mentioned here to reduce or prevent backward flow articles.
Packed random shoring (similar to similar bulk density packing methods) produces more than 30% by volume to less than 70% by volume of the porous proppant packages. However, this does not include the porosity of the proppant by itself as it only includes the porous volume in the proppant package.
Many attributes and variables determine the porous volume of a proppant package such as packing method, particle size, particle shape and particle distribution. However, these properties combine to form a total package porosity that determines maximum conductivity in conjunction with the strength of the package.
Specific gravity is the density of the material and is also defined as the skeletal density of the porous proppant. The apparent specific gravity is the adjusted proppant density when considering the addition of the pore density with the material density
of the proppant.
For example, silicon carbide may have a specific gravity of 3.2 g / cc even if the proppant may have an apparent specific gravity of 1.6 g / cc when considering 50% of the volume of porosity. The term "density" of the proppant here refers to apparent specific gravity, density of volume or any other density term may be used elsewhere.
Sphericity and roundness of at least .9 is more desired to achieve greater strength at lower densities.
Suitable proppant particle sizes are in many cases 20/40 mesh. However, other mesh sizes can perform similar strength and density attribute results.
A mesh size range is determined by retaining all the proppant particles in the smaller mesh screen (such as 40 mesh) and allowing all proppant particles to pass through the larger mesh screen (such as 20 mesh). ).
The following discussion provides an example of the relationship between dense proppant strength and porous package strength.
Solid silicon carbide that has a proppant strength of 540,000 psi can produce 180,000 psi for
a single solid sphere, producing then 60,000 psi for a porous proppant pack of non-porous (dense) spheres. The result can decrease less than 10% fines after the crushing test.
Solid spheres made of silicon carbide can be "excessive" for most rock formations since porous silicon carbide produces a lightweight, strong solution compared to sand and sintered ceramics. Starting with the highest levels of compressive strength that allows porous silicon carbide to provide similar strength levels such as sand and ceramics, even at lower desirable densities.
The following discussion provides an example of porous proppant strength in relation to porous package strength.
Given 60,000 psi for 60% porous block, producing 20,000 psi for 60% a single porous sphere, then producing 6,000 psi for a 50% porous proppant package consisting of 60% porous spheres.
Table 1 below shows that silicon carbide is desirable for a lightweight proppant. Boron carbide can also be a good choice for proppant, but it can be cost prohibitive. Only widely available raw materials such as sand, certain clays, carbon, and aluminosilicate forms are
acceptable in terms of cost. The conversion of sand and carbon into porous applied carbide is a preferred embodiment for low density, high strength, low cost proppant.
TABLE 1
Material Strength Density Ratio of compressive proppant strength (gram / cc) to density
(psi)
Silica 165,343 2.6 63,593 Mullite 188,549 2.8 67,339 Alumina 377,098 3.8 99,236 Boron carbide 415,442 2.5 166,177 Silicon carbide 565,647 3.2 176,765
(Compressive strength per g)
EXAMPLES
EXAMPLE 1
Conductivity and short-term permeability
Figure 3A shows the results of a short-term conductivity test using a silicon carbide proppant (diamonds), a commercial sintered bauxite proppant (squares), and a commercially mixed aluminum oxide / silicon oxide proppant (triangles) ). Figure 3B shows the results of short-term permeability tests for the same materials.
EXAMPLE 2
Permeability and long-term conductivity
Figure 4A shows the results of a long-term conductivity test using a silicon carbide proppant; Figure 4B shows the results of a long-term permeability test using the same material.
EXAMPLE 3
Force measurements
Degree of proppant Force Density% Thin Compressive porous size (gram / cc) generated mesh
(psi)
99% SiC p / 1% oxide 5, 000 1.4 9% 30
90% SiC w / 10% mullite 8, 000 1.6 7% 20/40
99% SiC p / 1% oxide 10, 000 1.8 6% 30
98% SiC p / 2% oxide 12,000 2.2 9% 20/40
Other embodiments are within the scope of the following claims.
Claims (29)
1. - A porous proppant having a spherical shape generally with a particle diameter between 100 and 2,000 microns, average pore sizes between 1 and 50 microns, and a porosity between 10 and 70% of the total spherical volume.
2. - The plurality of porous proppant according to claim 1, characterized in that each porous proppant individually forms a pack of proppant having a crushing force of at least 2,000 psi and an apparent specific gravity of 1.0 g / cc or less.
3. - The plurality of porous proppant according to claim 1, characterized in that each porous proppant individually forms a pack of proppant having a crushing force of at least 4,000 psi and an apparent specific gravity of 1.3 g / cc or less.
4. - The plurality of porous proppant according to claim 1, characterized in that each porous proppant individually forms a package of proppant having a crushing force of at least 6,000 psi and an apparent specific gravity of 1.6 g / cc or less.
5. - The plurality of porous proppant according to claim 1, characterized in that each porous proppant individually forms a pack of proppant having a crushing force of at least 8,000 psi and an apparent specific gravity of 1.8 g / cc or less.
6. - The plurality of porous proppant according to claim 1, characterized in that each porous proppant individually forms a pack of proppant having a crushing force of at least 10,000 psi and an apparent specific gravity of 2.0 g / cc or less.
7. - The plurality of porous proppant according to claim 1, characterized in that each porous proppant individually forms a package of proppant having a crushing force of at least 12,000 psi and an apparent specific gravity of 2.2 g / cc or less.
8. - The plurality of porous proppant according to claim 1, characterized in that each porous proppant individually forms a pack of proppant that produces 10% or less fines in a test of crushing.
9. The porous proppant according to claim 1, characterized in that the porous particles include silicon carbide, silicon nitride or combinations thereof.
10. - The porous proppant according to claim 9, characterized in that the porous particles include 90% or more of silicon carbide.
11. The porous proppant according to claim 1, characterized in that the porous particles have a sphericity of 0.91 or greater.
12. - The porous proppant according to claim 1, characterized in that the porous particles have a roundness of 0.91 or greater.
13. The porous proppant according to claim 1, characterized in that the porous particles have a sphericity of 0.95 or greater.
14. The porous proppant according to claim 1, characterized in that the porous particles have a roundness of 0.95 or greater.
15. A composition comprising a plurality of particles including silicon carbide, silicon nitride, or a combination thereof, which form a porous proppant having a spherical shape generally with a particle diameter between 100 and 2,000 microns, size of average pore between 1 and 50 microns, and a porosity between 10 and 70% of the total spherical volume.
16. - The plurality of compositions according to claim 15, characterized in that each porous proppant individually forms a pack of proppant having a crushing force of at least 2,000 psi and an apparent specific gravity of 1.0 g / cc or less.
17. - The plurality of compositions according to claim 15, characterized in that each porous proppant individually forms a pack of proppant having a crushing force of at least 4,000 psi and an apparent specific gravity of 1.3 g / cc or less.
18. - The plurality of compositions according to claim 15, characterized in that each porous proppant individually forms a pack of proppant having a crushing force of at least 6,000 psi and an apparent specific gravity of 1.6 g / cc or less.
19. - The plurality of compositions according to claim 15, characterized in that each porous proppant individually forms a pack of proppant having a crushing force of at least 8,000 psi and an apparent specific gravity of 1.8 g / cc or less.
20. - The plurality of compositions according to claim 15, characterized in that each porous proppant individually forms a pack of proppant having a crushing force of at least 10,000 psi and an apparent specific gravity of 2.0 g / cc or less.
21. - The plurality of compositions according to claim 15, characterized in that each porous proppant individually forms a pack of proppant having a crushing force of at least 12,000 psi and an apparent specific gravity of 2.2 g / cc or less.
22. - The composition according to claim 15, characterized in that each porous proppant individually forms a pack of proppant that produces 10% or less fines in a trituration test.
23. - A method for using a composition according to claim 15, comprising injecting the composition in a hydrofracture.
24. - The composition according to claim 15, characterized in that the particles have a sphericity of 0.91 or greater.
25. - The composition according to claim 15, characterized in that the particles have a roundness of 0.91 or greater.
26. - The composition according to claim 15, characterized in that the particles have a sphericity of 0.95 or greater.
27. - The composition according to claim 15, characterized in that the particles have a roundness of 0.95 or greater.
28. A method for making a porous proppant, which comprises heating a composition that includes a carbon source and a silicon source between 10 and 70% porosity of the total proppant volume thereby forming a silicon carbide proppant.
29. The method according to claim 24, characterized in that the porous silicon carbide proppant has a particle diameter between 100 and 2,000 microns, average pore sizes between 1 and 50 microns, and a porosity between 10 and 70% of the volume total spherical
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US201161549878P | 2011-10-21 | 2011-10-21 | |
PCT/US2012/061329 WO2013059793A1 (en) | 2011-10-21 | 2012-10-22 | Porous proppants |
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US9670400B2 (en) | 2011-03-11 | 2017-06-06 | Carbo Ceramics Inc. | Proppant particles formed from slurry droplets and methods of use |
KR20150040309A (en) | 2012-08-01 | 2015-04-14 | 옥세인 머티리얼스, 인크. | Synthetic proppants and monodispersed proppants and methods of making the same |
US9815943B2 (en) | 2013-03-15 | 2017-11-14 | Melior Innovations, Inc. | Polysilocarb materials and methods |
US10221660B2 (en) | 2013-03-15 | 2019-03-05 | Melior Innovations, Inc. | Offshore methods of hydraulically fracturing and recovering hydrocarbons |
US9815952B2 (en) | 2013-03-15 | 2017-11-14 | Melior Innovations, Inc. | Solvent free solid material |
US9499677B2 (en) | 2013-03-15 | 2016-11-22 | Melior Innovations, Inc. | Black ceramic additives, pigments, and formulations |
US10167366B2 (en) | 2013-03-15 | 2019-01-01 | Melior Innovations, Inc. | Polysilocarb materials, methods and uses |
CA2849415C (en) | 2013-04-24 | 2017-02-28 | Robert D. Skala | Methods for fracturing subterranean formations |
US9481781B2 (en) | 2013-05-02 | 2016-11-01 | Melior Innovations, Inc. | Black ceramic additives, pigments, and formulations |
RU2016103368A (en) * | 2013-07-04 | 2017-08-10 | Мелиор Инновейшнз, Инк. | HIGH-STRENGTH SYNTHETIC LOW-DENSITY PROPANTS FOR HYDRAULIC GROUND REMOVAL AND HYDROCARBON EXTRACTION |
US9914872B2 (en) * | 2014-10-31 | 2018-03-13 | Chevron U.S.A. Inc. | Proppants |
WO2016195692A1 (en) | 2015-06-04 | 2016-12-08 | Halliburton Energy Services, Inc. | Porous proppants |
EP3317366A1 (en) | 2015-06-30 | 2018-05-09 | Dow Global Technologies LLC | Coating for controlled release |
MX2018000167A (en) | 2015-06-30 | 2018-03-26 | Dow Global Technologies Llc | Coating for capturing sulfides. |
CN107922823A (en) | 2015-06-30 | 2018-04-17 | 陶氏环球技术有限责任公司 | Composite product |
US20170030179A1 (en) * | 2015-07-31 | 2017-02-02 | Statoil Gulf Services LLC | Hydraulic fracturing and frac-packing using ultra light, ultra strong (ulus) proppants |
CA3027004A1 (en) | 2016-06-08 | 2017-12-14 | Dow Global Technologies Llc | Amide based coating |
US10190041B2 (en) * | 2016-08-02 | 2019-01-29 | University Of Utah Research Foundation | Encapsulated porous proppant |
US10844280B2 (en) | 2017-03-21 | 2020-11-24 | Dow Global Technologies Llc | Polyurethane based proppant coatings |
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US4547468A (en) * | 1981-08-10 | 1985-10-15 | Terra Tek, Inc. | Hollow proppants and a process for their manufacture |
EP1856374B1 (en) * | 2005-02-04 | 2011-11-02 | Oxane Materials, Inc. | A composition and method for making a proppant |
US8006759B1 (en) * | 2006-10-05 | 2011-08-30 | Imaging Systems Technology | Manufacture of strong, lightweight, hollow proppants |
MX2012007608A (en) * | 2009-12-31 | 2012-07-30 | Oxane Materials Inc | Ceramic particles with controlled pore and/or microsphere placement and/or size and method of making same. |
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