AU2014200669B2 - High strength proppants - Google Patents

High strength proppants Download PDF

Info

Publication number
AU2014200669B2
AU2014200669B2 AU2014200669A AU2014200669A AU2014200669B2 AU 2014200669 B2 AU2014200669 B2 AU 2014200669B2 AU 2014200669 A AU2014200669 A AU 2014200669A AU 2014200669 A AU2014200669 A AU 2014200669A AU 2014200669 B2 AU2014200669 B2 AU 2014200669B2
Authority
AU
Australia
Prior art keywords
oxides
weight percent
ceramic
particle
sintered
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
AU2014200669A
Other versions
AU2014200669A1 (en
Inventor
Kevin R. Dickson
Tihana Fuss
Laurie San-Miguel
Walter T. Stephens
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Saint Gobain Ceramics and Plastics Inc
Original Assignee
Saint Gobain Ceramics and Plastics Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from AU2009308774A external-priority patent/AU2009308774A1/en
Application filed by Saint Gobain Ceramics and Plastics Inc filed Critical Saint Gobain Ceramics and Plastics Inc
Priority to AU2014200669A priority Critical patent/AU2014200669B2/en
Publication of AU2014200669A1 publication Critical patent/AU2014200669A1/en
Application granted granted Critical
Publication of AU2014200669B2 publication Critical patent/AU2014200669B2/en
Ceased legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Compositions Of Oxide Ceramics (AREA)

Abstract

A sintered ceramic particle made from a ceramic material having a true density greater than 3.5 g/cc and a composition having no more than 30 weight percent silicon oxide and at least 15 weight percent iron oxide, based on the combined weight of the oxides of aluminum, iron and silicon, is disclosed. A process that utilizes an externally applied compressive force to make a ceramic particle is also disclosed

Description

AUSTRAIA PATENTS ACT 1990 REGULATION 32 Name of Applicant: SAINT -GOBAIN CERAMICS & PLASTICS INC Actual Inventor/s: LAURIE SAN-MIGUEL; KEVIN R. DICKSON; TIHANA FUSS; and WALTER T. STEPHENS. Address for Service; E, F. WELLINGTON & CO, Patent and Trade Mark Attorneys, 312 St. Klda Road, Melbourne, Southbank, Victoria, 3006. Invention Title: "HIGH STRENGTH PROPPANTS" Details of Associated Provisional Applications Nos: The following statement is a full description of this invention including the best method of performing it known to us. Next page is page I A CROSSREFERENCE TO RELATED APPLICATIONS This application is a d kisionaP application derived from Australian Patent Apph cation No. 2009308774 (.P(IY/US2009/062832: WO 2010/051481) claiming priority of US Application No. 12/262790, the entire text of which are hereby incorporated herein by reference. BACKGROUND OF THE INVENiION This invention generally relates to ceramic particles for use in a wide variety of industrial applications. Some of these applications include using a plurality of ceramic particles: as a proppant to facilitate the removal ofliquids and/or gases from wells that have been drilled into geological formations; as a media for scouring, grinding or polishing; as a bed support media in a chemical reactor; as a heat transfer media; as a filration media; and as roofing granules when applied to asphalt shingles. More specifically this invention is useful in applications that require a ceramic sphere that has high crush resistance. Even more specifically, this invention pertains to proppants that may be used in geological formations where the pressure exerted on the proppant exceeds the crush resistance of conventional proppants such as sand and resin coated sand, Examples of patents and published patent applications directed to proppants include: US 3,376930 US 4,032876; US 7,067,445 US 2006017661 and'US 2008/0000638, SUMMARY Embodiments of the present invention provide a ceramic particle that is suitable for use in doWnholc applications that require a high strength proppant, In one embodiment, the presentinvention includes a sintered parole comprisIng ceramic material.he ceramic material Comprises oxides of aluminum, irn and silicon. The silicon oxides represent no more than 30 weight percent of the oxides' combined weight. The iron oxides represent between 15 and 40 weight percent of the oxides> combined weight ITe densityofhe ceramic material exceeds 3.5 ghecC. Another embodiment relates to a process fior making a partiCle comprising a sintered ceramic material. The process may include the following steps. Mixing Next page is page 2
-IA-
at least a first metal oxide with one or or dry ingredients and at least one liquid thereby forming a mixture F ing at t or of te xure into a particle precursor Sintering the precursor, Heating the precursor and exerting an externally applied compressive force on the precursor thereby forming a sintered 5 ceramic particle BRIEF DESCRI ION OF THE DRAWINGS Fig. t.is a three phase diagram; Fig. 2 is a flow chart of a process used to manufacture a ceramic particle; and Fig. 3 is a line chart which shows crush resistance by plotting percentage of fines versus pressure. DETAILED DESCRIPTON Technology that uses particles to facilitate the removal of hydrocarbon based fluids, such as natural gas and etude oil, front downhole well bores has been documented in numerous patents and journal articles, The particles, which may 20 be referred to as proppants, are used to prop open fissures in the earth through which the gas and oil flow toward the well bore, In wells where proppants are not used, the fissures in the earth located closest to the well bore may collapse soon after the gas and oil located closest to the well bore have been removed. The collapse of the fissures limits the production of the well by preventing additional 25 oil and gas from moving toward the well bore. In contrast, the productivity of wells that use proppants may be improved because the proppants prop open the fissures in the earth that would otherwise close after removal of the hydrocarbon based fluids. The proppants are delivered into the fissures by mixing the proppants with a fracturing fluid which is fored through the Well bore and into 2 the fissures, When the fracturing fluid is removed, the particles remain lodged in the fissures thereby propping open the fissures, Due to the ongoing need to provide larger and larger quantities of natural gas and oil and the simultaneous depletion of readily available gas and oil located 5 near the surface of the earth, new wells must be drilled deeper than older wells in order to reach the previously untapped reservoirs of oil and gas. As the depth of the well bore increases, the pressure exerted on the proppant by the earth also increases, Consequently, proppant manufacturers need to produce proppants that can withstand higher pressures than proppants produced a few years ago in order 10 to resist cmshing at the deeper well depths, A proppant's ability to withstand crushing may be characterized as crush resistance which is a term commonly used to denote the strength of a proppant and may be determined using ISO 13503 2:2006(E). A strong proppant generates a lower weight percent crush resistance than a weak proppant at the same closure stress, For example, a proppant that has 15 a 2 weight percent crush resistance is considered to be a strong proppant and is preferred to a weak proppant that has a 10 weight percent crush resistance. Proppants may be made from either a naturally occurring material, such as sand, or from compositions that have been produced via a manufacturing process. An example of a composition used to manufacture proppants is a combination of 20 metal oxides, such as bauxite, that has been mixed with various additives, formed into a plurality of generally spherical balls and then sintered to form a plurality of ceramic proppants. While the exact chemical composition of bauxite may vary depending upon the location of the mine from which the bauxite is removed, most bauxites include between 60 and 90 weight percent A10 3 , Another example of a 25 composition chat may be used to manufacture proppants is commonly known as "red mud" which is a byproduct of the Bayer process for refining aluminum. This waste product typically comains oxidized iron, titanium, sodium, silica and other impurities. The chemical composition of the bauxite may be determined by preparing 30 a fused sample of the bauxite and then using an X-ray fluorescence (XRF) analytical apparatus to determine the weight percentages of aluminum oxides, iron oxides and silicon oxides. The fused sample may be prepared using a Claisse M4 Fluxer Fusion apparatus (manufactured by Claisse of Quebec City, Canada) as follows. Several grams of the bauxite are manually ground so that the bauxite 5 passes through a 75 pm (200 Tyler mesh) sieve. In a platinum crucible supplied by Claisse., 0000 g (± 0,0005 g) of the ground and screened bauxite is mixed with 8.0000 g (* 0,0005 g) of lithium borates 50-50 which contains a releasing agent such as LiBr or CsI. If the releasing agent is not included in the lithium borate, three drops of a releasing agent (25 w/v % LiBr or Cs) may be added. 10 The mixture in the crucible is then gradually heated in order to remove any organic materials, moisture, etc, Simulaneously, the crucible is rapidly spun so that centrifugal force caused by the spinning drives any entrapped gas from the molten material When the temperature of the molten bauxite in the crucible reaches approximately 1000"C, the material has been liquefied and the crucible is I5 tilted so that the molten bauxite flows into a disc mold, While the molten material is cooling in the disc mold, a fan blows air on the mold to facilitate the removal of heat. As the molten bauxite cools the material fuses and forms a disc shaped sample that measures approximately 3 cm wide and 4 mm thick. The disc should not contain any gas bubbles trapped therein. The chemical composition of the 20 cooled disc is then determined using a model MagiX Pro hilips X-Ray Fluorescence analyzer running IQ+ software. The same procedure may be used to determine the chemical composition of ceramic particles such as proppants, One of the criteria considered by proppant manufacturers when selecting a source of bauxite ore used to make proppants is the level of undesirable impurities 25 which are believed to degrade the perfonnance of the proppant Typical impurities include iron oxide and titanium oxide, Unfortunately, excessive amounts of iron ore may cause problems during the sintering step of the proppant manufacturing process because the sintering temperature of the iron ore may be substantially different than the sintering temperatures of aluminum oxide and 30 aluminum-silicon oxides, such as kaolin clay or mullite. "Sintering", as used 4 herein, means the joining of particles through the application of heat, This commonly results in densification, but not in all cases. Some commercially viable proppant manufacturers have considered sources of bauxite ore that have greater than a 15 weight percent iron oxide to be unsuitable for use as a raw material for 5 the production of proppants. In contrast, this application discloses that a source of bauxite that contains a quantity of a metal oxide previously considered to be unacceptable may be used to manufacture a proppant having improved resistance to crushing, Proppants may be made by selecting a source of bauxite ore that inherently contains: between 50 and 85 weight percent of a first metal oxide, such in as oxides of aluminum, which have a density greater than 37 g/ce between 15 to 40 weight percent of a second metal oxide, such as oxides of iron, which have a density greater than 3.9 g/e; and between 0 and 30 weight percent of a third metal oxide, such as oxides of silicon, which have a density no greater than 2,8 g/ce. Furthermore, a bauxite ore that does not naturally contain a sufficient level is of iron oxide may be mixed with a separate source of iron oxide to attain the improved performance in the proppant, The history of proppant development, as documented in some United States parents, has been inconsistent relative to teaching the best range of specific gravity for proppants. In the 1970s, US 4,068,718, which claims priority of an 20 application filed on May 17, 1974, disclosed a " high strength propping agent comprising particles of smtered bauxite having a specific gravity greater than about 3.4." However, during the 1980s, considerable effort was exerted by the proppamt. industry to produce proppants with specific gravity significantly less than 3,4, For example, US 4,680,230, which was filed on January 18, 1984, 25 quotes a study done for the US Department of Energy which describes an "ideal proppant" as having "a specific gravity less than two, At column 1, lines 49 to 65, this patent teaches away from using sintered bauxite as a proppant With regard to the use of material containing iron oxide to manufacture ceramic spheroids, such as a proppant tha has a high crush strength, US 4,632,876 teaches 30 "However, blast furnace slags, power plant slags and flyash can be used but 5 generally are not acceptable because their high iron oxide contents result in high densities, Iron oxide content of the mineral particulate should be substantially less than 9 weight percent, preferably less than 5%* In contrast to the parents described above, this invention discloses a 5 proppant wherein the proppant's ceramic material has an iron oxide content substantially higher tan previously considered feasible. As used herein, the phrase "ceramic material" refers to the collection of granules of inorganic. metal and non-metal, oxides, carbide and nitrides that have been foned into a sphere and sintered such that the individual granules adhere to one another thereby to forming a sintered particle, 'be ceramic material does not include volatile components, such as binders and liquids used to make the proppant, nor the polymers or other coatings that may be added to the particle after the sintering step, In one embodiment of this invention, the proppant contains at least a first metal oxide that includes oxides of aluminum and a second metal oxide that 15 contains oxides of iron and may include a third metal oxide that contains oxides of silicon. The weight percentages of the first, second and third metal oxides are calculated as Al20, FeA and Si), respectively, The quantity of oxides of iron in the proppant may represent between 15 and 40 weight percent, more preferably between 15 and 35 weight percent, even more preferably between 20 and 30 20 weight percent, of the oxide's combined weight, The quantity of oxides of silicon may represent between 0 and 30 weight percent, more preferably between 1 and 10 weight percent, of the oxide's combined weight, The weight percentages of the first, second and third metal oxides are calculated as a fraction of the combined weight of just these metal oxides. If the proppant includes other 25 components, such as a polymer coating applied to the surface of the proppant and/or a fourth metal oxide, neither the weight of the polymer nor the fourth metal oxide are included in the calculation of the weight percentages of the first, second and third metal oxides, The combined weight of the metal oxides may exceed 50 weight percent of the ceramic particle's total weight. 'he total weight of the 30 ceramic particle includes the weight of the first, second and third metal oxides 6 plus the weight of other metal oxides and impurities that remain after the particle has been sintered and prior to the addition of any coatings, fillers, etc. The combined weight of the first, second and third metal oxides may exceed 60 or even 70 weight percent of the ceramic particle's total weight. S Inaddition to the chemical compositions characteristics described above the density of the partice ceramic material exceeds 3.5 g/cc In some embodiments, the density of the paric's ceramic material may exceed 3.6 glec, 4s glcc42g oreen4 c used herein, the phrases "true density", "density of the ceramic material", "density of the particle's ceramic material" and to the "density of the proppant'a ceramic material" all refer to the true density of the solid ceramic matrix that forms the ceramic particle. As defined in die Dictionary of Ceramics, third edition, by Arthur Dodd and David Murfin, the true density of a porous solid is "defined as the ratio of the mass of the material to its true volume" which is then "defined as the volume of the solid material only, the is volume of any pores being neglected." A ceramic mateal's true density is characteristic of the ceramic inaterial's chemical compositin and crystalline phase(s). The: true density of the ceramic material is independent of the particle's porosity. The density of the proppant's ceramic material is determined according to ASTM Standard D02840-69 by weighing a sample, grinding the sample to less 20 than 100 mesh, measuring the volume of the sample with a helium pycnorneter (such as an SPY 03 Quantachrome stereopycuometer) and calculating the weight per cubic centimeter. The ceramic material's density is a physical pammeter that is distinct and separate from the pare's specific grvity. in contrast to the definition of 25 density provided above the phrases "specific gravity of the ceramic particle" and "Specific gravity of the proppant" both refe to the particle's apparent specific gravity which 3s defined in at Dictionary of Ceramics as "the ratio of the mass to the mass of a quantity of water that, at 4(2 ha,1s a volume equal to the apparent solid volume of the material at the temperature of measurement." For use herein 30 the apparent solid volume is defined as the volume of the solid material plus the volume of any sealed pores The specific gravity of the ceramic particle is directly impacted by the porosity incorporated into the particle, The porosity of the ceramic particles of this invention may range from 2 percent to 40 percent. Ceramic particles having porosity between 5 and 15 percent are feasibleThe 5 specific gravity of the ceramic particle may be determined using International Standard ISO 13503-2- The standard issued Nov12006. Apparent porosity in a ceramic body is defined as 1 minus the quotient of the apparent specific gravity divided by the true density, The true density of the ceramic material and the specific gravity of the 10 ceramic particle can be controlled independenly, For example, while holding the true density of the ceramic material constant, cemic particles having different levelsof porosity incorporated therein could be manufactured thereby resulting in ceramic particles having the same true density but different specific gravities. Similarly, while holding the level of porosity in several ceramic particles the 15 same, the compositions of the ceramic materials used to make the particles can be changed thereby resulting in particles having the same porosity but different tue densities Using the teachings provided herein, a proppant having a low specific gravity and high crush resistance can be made. The proppant may be made from a 20 high density material, such as ceramic material having a true density greater than 3.5 g/cc, while the proppant may have a low specific gravity, such as 2.8, due to the incorporation of pores in the proppant. Proppants that have even lower specific gravity, such as 2,5, 2.4 or 2.0 are feasible, Because high density ceramic material may have high strength and are therefore resistant to crushing, high 25 density ceramic materials may be desirable. However, proppants made from high true density materials may tend to prematurely settle out in a fracturing fluid when inserted in a well bore if the proppants specific gravity is approximately equal to the ceramic material's true density, Proppants having good crush resistance and low specific gravity can be attained if the true density of the ceramic material is 30 high enough to increase the crush resistance beyond the decrease in cmsh resistance caused by the incorporation of pores needed to lower the specific gravity of the proppant, Shown in Fig, 1 is a temary diagram l0 of a sintered ceramic particle that includes A1IO1 Fe/b and Si0 and assumes no porosity, Lines 12, 14 and 16 represent the true densities of the ceramic particles at 3.0 g/ce, 3,2 g/ee and 3A gC, respectively. Other lines that are generally parallel to lines 12,14 and 16 indicate the tre densities of the ceramic particles as marked on the phase diagram On this graph, the lowest density is approximately 2.7 g/c and the highest density is approximately 42 glc Hatched area I8 identifies the portion to of the diagram that contains no more than 30 weight percent SiO, 15 to 40 weight percent oxides of iron and the density of the ceramic material is 3.5 g/ec or higher. Proppants that fall within the hatched area have been found to have good crush resistance when evaluated for crush resistance at 1379 megapascals (MPa) which is equivalent to 20,00 psi, Shown in Fig. 2 is a flow chart of a process used to make a sintered ceramic particle of this invention, Step 20 represents mixing bauxite ore with dry ingredients, such as binders and pom former, and liquids, such as water, to form a free flowing powder which may be referred to herein as a mixture A binder may be one or more materials selected from organic starches such as drilling 20 starch, as well as gums or resins that are sold commercially for such purposes A binder may also be an inorganic materialuch as day or an acid, Binders are usually added in an amount less than 10 weight percent of the dry said content of the mix and may be added dry or as asolution. Instep 22,the mixturemay he processed through a machine, such as an Eirich R2 mixer, thereby forming at 2 least a portion of the mixture into a large number of smallspheres that may be referred to herein as particle precursors or proppara precursors. Particle precursors that are useful as proppants may be processed through a screening apparatus that incides a No.8 ASTM sieve designation; which has 236 mm apertures, and a No. 70 ASTM sieve designation which has 212 pi sieve 30 apertures. The proppants flow through the No. 8 sieve and do not flow through the No, 70 sieve, Step 24 represents sintering the precursors to improve the physical integrity of the precursors relative to the physical integrity of the precursors prior to heating. in step 26 the particle precursors may be heated and an externally applied compressive force exerted on the precursor thereby 5 producing a plurality of sintered particles Due to shrinkage which may occur during the sintering process, the average diameter of the sintered particles may be less than the average diameter of the particle precursor. Commercial processes used to manufacture proppants typically use a kiln to sinter the proppant greenware at atmospheric pressure. The kiln may be a 10 tubularly shaped rotating kiln that allows proppants to tumble as they move from one end of the kiln to the opposite end of the kiln. The maximum temperature in a kiln used to make proppants comprising primarily alumina may approach 1500"C In contrast to manufacturing proppants at atmospheric pressure. proppants with improved crush resistance may be manufactured by exerting an externally applied 15 compressive force on the proppant during the proppant manufacturing process. The externally applied compressive force may be any force that uniformly compresses the proppant from all directions toward the center of the proppant. An example of a suitable compressive technique is isostatic pressing. A specific embodiment of isostatic pressing is hot isostatic pressing which utilizes heated gas 20 to elevate the temperature of the particle, so that complete or partial sintering of the ceramic material can take place, and simultaneously exerting a force inwardly against all points of the particle's surface, Isostatic pressing may use a flexible rubber or elastomer container, commonly known as "tooling", into which the article to be pressed is inserted, 'The tooling is then placed into a vessel 25 containing hydraulic fluid, Hydrostatic pressure is then applied to the fluid. The process applies pressure n a uniform manner over the entire surface of the article resulting in the article having uniform density. An alternate approach is to sequentially sinter and compress the anicles. In one embodiment, the anicles. such as proppam precursors, are sintered and then hot isostatic pressing is used, to 30 apply pressure to all surfaces of the proppants. The sintering step improves the t0 physical integrity of the proppants, Bauxite based proppants may be sintered between 110000 and 150004. Another alternate approach is to use isostatic pressing to exert a compressive force on the proppant precursors and then sinter the compressed particles, 5 EXAMPLES To demonstrate the improved crush resistance of proppants of this invention, five lots of proppants, identified herein as Lots A, B, C, D and B, were 10 made and evaluated for crush resistance. The raw materials used to make the proppants are shown in Table L Lot A represents commercially available proppants that contained 9.5 weight percent oxides of iron in the sintered proppant, Lots B, C, D and E represent proppants having at least 15 weight percent oxides of iron, calculated as Fe 2 03 in the sintered proppant. A Is commercially available source of bauxite is available from Ferrous American Company of Littleton? Colorado, USA. A quantity of bauxite from this company was used to manufacture Iots B, C, D and 11 The composition of this bauxite included 64.0 weight percent Al2t, 25.8 weight percent Fe 2
O
3 and 4.0 weight percent SiO 2 . The ore also contained 3.2 weight percent TiC) 2 and trace amounts, 20 which is defined herein as less than I weight percent. of several other compounds such as MgO, CaD, CeO, and MuO. Lots A, B, C, D and E were made using a conventional proppant manutcturing process to fonn a plurality of small spheres known herein as proppant precursors or particle precursors, The process utilized an RV02 high-intensity shear mixer available from Fiich Machines, Inc, of 25 Gunce, Illinois, USA. The process included disposing the initial charge of bauxite into the mixer with both the pan and rotor rotating. The rotor speed was set at 80 percent of maximum speed, After 30 seconds, the demonized water was poured into the mixer directly onto the rotating bauxite, Approximately 30 seconds was used to distribute the water onto the bauxite, The Nmoistened bauxite 30 was allowed to rotate for three minutes during which time a plurality of spheres were formed. The rotor speed was Then Red~uced to minimum speed as the pan ccotnued torotate. The second charge of bauxite was then added slowly to the rotating spheres of bauxite The slow addition of bauxite took approximately three minutes and may be referred to as "dusting in" the bauxite After 5 completing the dusting in of the bauxite, the pan continued to rotate for approximately 20 seconds, The spheres of bauxite that had been coated with a layer of bauxite were removed from the mixer and may be referred to herein as proppant precursors or particle precursors. The precursors in lots A, B, C and D were then sintered in a rotating kiln at atmospheric pressure. Only the precursors 1o in lot E were made with a process that included the exertion ofaextemally applied compressive force on the proppant precursor The technique used to exert the externally applied compressive force is known as hot isostatic compression, The particle precursors in Lot E were sintered at 125TC. The sintered precursors were then simultaneously pressed at 352 kg/m (5,000 psi) and heated to 1200 0 C 15 for one hour. Heating the sintered precursors to 1200 0 C while exerting the compress ive forceo helped to prevent grain n growthi during the compression step. For lots A, B3 and C, screening was used to limit the particle size to those partiles that passed through a screen having 20 mesh openings and did not pass through a screen havig 40 mesh openngs Lots D and E were screened to limit the particle 20 sizes to those particles that passed through a screen having 30 mesh openings and did not pass through a screen having 50 mesh openings.
Table 1 Oxides of Ingredient A B C lIron oxide Bauxite greater ta 57.12% 57.12% 57,12% 57.12% 15 wt% ____ (ticst chargt> Irenoxide less 57.12% than IS wt % killing 1.14% 1.14% 1,14% 1,14% 114% Water 27,42% 27.42% 27.42% 27,42% 27,42% I1ron Oxide Bauxite greater in 14.28% 14,28% 14,28% 14,28% 15 wt% ____ (second chsge) I o~oe" 14.28% Mthan 5 wt % Proppants' Particle Size 20/40 20/40 20/40 30/50 30/50 Distribu tion 2040 2040 204 |3050 30_ *Precursors were sintered and then compressed using hot isratic Compression Fig, 3 is a line plot of crush resistance versus pressure for lots A, B, C, D 5 and E Line 28 (Lot A) represents the crush resistance of a commercially available sitered bauxite that contained 9.5 weight percent oxides of iron calculated as Fe20*. After exposure to 86,2 Mla (12,500 psi), approximately 55 weight percent of the proppan had been crushed to fines. Line 30 (Lot B) and line 32 (Lot C) represem the crush resistance of duplicate runs of a proppant that in had 25.8 weight percent oxides of iron calculated as FesO 5 and a 20/40 particle size. A t 103 MPa (15,)00 psi), an average of 4,5 weight percent of this proppant had been crushed to fines which is better than the crush resistance of the commercially available proppant at 86,2 MPa (12,500 psi) (see line 28), Line 34 (Lot D) and line 36 (Lot E) represent the crush resistance of a proppant that had 15 25.8 weight percent oxides of iron calculated as Fe 3 and 30/50 particle size. At 137.9 MPa (20,000 psi), the avenge crush resistance of the proppants in lots D 13 and E was approximately3.5 percent which is much better than the crush resistance of the proppants that contained less than 15 weight percent iron oxide at 862 MPa (2500 psi) (see lne 28 Thell data demonstrates that theproppants made with more than 15 weight percent oxides of iron (lots B, C, D and E) had better crush resistance than the proppants in lot A that had less than 15 weight percent oxides of iron Furthermore, the proppants in Lot E provided the best crushJ ressanuc. The abcve description is considered that of particular embodiments only. Modifications ofthe invention will occur to those skilled in the art and to those who make or use. theinvention Therefore, t is understood that the embodiments shown in the drawings and described above are merely for illustrative purposes and are not intended to limit the scope of the invention, which is defined by the following claims as interpreted according to the principles of patent law. A references erei to a patent document or otherimatter which is given as prior art is not taken as an admission that that document or prior art was part of common general knowledge at the priority date of any of the claims With reference to the use of the words) "comprise" or "comprises" or "comprising" in the foregoing description and/or in the following claims, unless the context requires otherwise, those words are used on the basis arnd clear understandings that they are to be interpreted inchivel rather than exclusively, and that each of those words is to be so interpreted in construing the foregoing description andior the following Claims 14

Claims (10)

1. A sintered particle comprising ceramic material, wherein said ceramic material comprises oxides of aluminum, iron and silicon; said oxides of silicon, calculated as SiT)O, represent no more than 30 weight percent of said oxides' combined weight; said oxides of iron, calculated as Fe 2 0 3 , represent between 20 and 40 weigin percent of said oxides combined weight; and said ceramic material's true density exceeds 3.5 ge. I The sintered particle of claim I wherein the combined weight of aid oxides exceeds 50 weight percent of said ceramic particles total weight. 3 The sintered particle of claim i wherein sai oxides of ion represent between 20 and 35 weight percent of said oxides' combine-d wxeiaht.
4. The sintered particle of claim wherein said oxides of iron represent between 20 and 30 weight percent of said oxides' combined weight 5, The sintered particle of claim I wherein said oxides of aluminum, calculated as AC, represent between 50 and 85 weight percent of said oxides combined weight.
6. The.sintered particle of claim 5 wherein said oxides of ahminum represent between 60 and 80 weight percent of saidoxide onedwigh 7, The sintered particle of claimwherein said oxides of silicon, calculated as Si, represent between I and 10 eight percent of said oxides combined weight.
8. A wintered paticle comprisingdceramic material, wherein said ceramct material comprises oxides ofainum, ion and siloon said oxides of siicon. calculated as SiO representno imore than 30 Weight percent of said oxides'combined weight; Said oxides of 15 iron, calculated as Fe 2 O 3 , represent between 15 and 40 weight percent of said oxides' combined weight; and said ceramic materialss true deunity exceeds 4,0 g/c. 9, The sintered particle of claim 8 wherein said ceramic materiaPs true density exceeds 4.5 10, A process, for making the sintered particle of any one of claims I to 9, comprising the steps of: a. mixing oxides of iron, aluminum and silicon with one or more dry ingredients and at least one liquid thereby forming a mixture; .forming t least a portion of said mixture into a particle precursor c.snterng said pecursor; d. heating and exerting an externally applied compressive force on said precursor thereby forming a sintered ceramic particle. 11IiTe process of claim 10 wherein step (d) comprises simultaneously compressing and heating said precursor.
12. The process of claim 10 wherein step (d) comprises sequentially compressing and heating said precursor.
13. The process of claim 12 wherein step (d) conprises compressing and then heating said precOUrso.
14. The process as in any one of claims 10 to 13 where n step (d) coprises using isostatic compression to compress said precursor until said sinered ceramic material true density exceeds 35i g/cc.
15.~~~ ThWrcs sIay one of claims 1to13 wherein step()copieusniottc oppression to copress said precursor untIl said sintered CeramiC m aris true density exceeds 4.0 a/,c 16
16. The process as in any one of claims 10 to 13 wherein step (d) comprises using isostatic compression to compress said precursor until said sintered ceramic material's true density exceeds 4.5 g/ec
17. The process of claim 10 wherein said mixture comprises between 50 and 85 weight percent of oxides of aluminum, between 20 and 35 weight percent of oxides of iron, and between I and 10 weight percent of oxides of silicon. 17
AU2014200669A 2008-10-31 2014-02-07 High strength proppants Ceased AU2014200669B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2014200669A AU2014200669B2 (en) 2008-10-31 2014-02-07 High strength proppants

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/262,790 2008-10-31
AU2009308774A AU2009308774A1 (en) 2008-10-31 2009-10-30 High strength proppants
AU2014200669A AU2014200669B2 (en) 2008-10-31 2014-02-07 High strength proppants

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
AU2009308774A Division AU2009308774A1 (en) 2008-10-31 2009-10-30 High strength proppants

Publications (2)

Publication Number Publication Date
AU2014200669A1 AU2014200669A1 (en) 2014-02-27
AU2014200669B2 true AU2014200669B2 (en) 2015-11-19

Family

ID=50153950

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2014200669A Ceased AU2014200669B2 (en) 2008-10-31 2014-02-07 High strength proppants

Country Status (1)

Country Link
AU (1) AU2014200669B2 (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4915887A (en) * 1988-04-04 1990-04-10 Corning Incorporated Method of preparing high temperature low thermal expansion ceramic
US5175133A (en) * 1989-12-22 1992-12-29 Comalco Aluminium Limited Ceramic microspheres
US5397759A (en) * 1978-08-28 1995-03-14 Torobin; Leonard B. Hollow porous microspheres made from dispersed particle compositions

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5397759A (en) * 1978-08-28 1995-03-14 Torobin; Leonard B. Hollow porous microspheres made from dispersed particle compositions
US4915887A (en) * 1988-04-04 1990-04-10 Corning Incorporated Method of preparing high temperature low thermal expansion ceramic
US5175133A (en) * 1989-12-22 1992-12-29 Comalco Aluminium Limited Ceramic microspheres

Also Published As

Publication number Publication date
AU2014200669A1 (en) 2014-02-27

Similar Documents

Publication Publication Date Title
CA2741860C (en) High strength proppants
AU569373B2 (en) Particulate ceramic useful as a proppant
US4944905A (en) Particulate ceramic useful as a proppant
US4623630A (en) Use of uncalcined/partially calcined ingredients in the manufacture of sintered pellets useful for gas and oil well proppants
US4658899A (en) Use of uncalcined/partially calcined ingredients in the manufacture of sintered pellets useful for gas and oil well proppants
US4427068A (en) Sintered spherical pellets containing clay as a major component useful for gas and oil well proppants
US4879181A (en) Sintered spherical pellets containing clay as a major component useful for gas and oil well proppants
US6780804B2 (en) Extended particle size distribution ceramic fracturing proppant
US7654323B2 (en) Electrofused proppant, method of manufacture, and method of use
JP2008513553A (en) Sintered spherical pellet
US20070023187A1 (en) Sintered spherical pellets useful for gas and oil well proppants
MX2014004760A (en) Porous proppants.
CN101657516A (en) High strength ceramic elements and manufacture method thereof and using method
CN101617019A (en) Propping agent and preparation method thereof
KR101391528B1 (en) Abrasive composition and article formed therefrom
AU2014200669B2 (en) High strength proppants
CA2597880C (en) Electrofused proppant, method of manufacture, and method of use

Legal Events

Date Code Title Description
FGA Letters patent sealed or granted (standard patent)
MK14 Patent ceased section 143(a) (annual fees not paid) or expired