Composition and method for making a proppant

• US 20070202318A1
• Filed: 03/27/2007
• Published: 08/30/2007
• Est. Priority Date: 02/04/2005
• Status: Active Grant

• Current Assignee: Halliburton Energy Services Incorporated (Halliburton Company)
• Original Assignee: Oxane Materials, Inc.
• Inventors: Smith, Russell, Barron, Andrew, Loscutova, John, Coker, Christopher, Skala, Robert
• Granted Patent: US 8,012,533 B2
• Time in Patent Office: Days
• US Class Current: 428/323
• CPC Class Codes: B01J 13/02 Making microcapsules or microballoons for medical preparations A61K9/50
• CPC Class Codes: B01J 13/206 Hardening; drying
• CPC Class Codes: C09K 8/805 Coated proppants
• CPC Class Codes: Y10T 428/25 Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles
• CPC Class Codes: Y10T 428/2991 Coated

Abstract

The present invention relates to proppants which can be used to prop open subterranean formation fractions. Proppant formulations are further disclosed which use one or more proppants of the present invention. Methods to prop open subterranean formation fractions are further disclosed. In addition, other uses for the proppants of the present invention are further disclosed, as well as methods of making the proppants.

Claims

1-76. -76. (canceled)

77. A method of forming a proppant, comprising providing a template sphere wherein said template sphere has one or more flaws on the surface of the template sphere;

removing or diminishing said one or more flaws with one or more chemical treatments, one or more mechanical treatments, one or more thermal treatments, one or more spark discharge treatments, or any combination thereof;

providing a shell around the entire outer surface of said template sphere after said removal or diminishing of one or more flaws, and then sintering said shell to form a continuous sintered shell.

78. The method of claim 77, wherein said chemical treatment is used and comprises treating said template sphere with a chemical that dissolves or otherwise reacts with one or more parts of the surface of the template sphere to remove or reduce said one or more flaws.

79. The method of claim 77, wherein said chemical treatment is used and comprises the preferential dissolution of one or more species contained in and/or on the template sphere.

80. The method of claim 79, wherein said one or more species is silica, such that said chemical treatment reduces the overall silica content.

81. The method of claim 78, wherein said chemical treatment comprises the application of sodium hydroxide, potassium hydroxide, calcium hydroxide, one or more acids, or any combination thereof to the surface of the template sphere.

82. The method of claim 77, wherein said mechanical treatment is used.

83. The method of claim 82, wherein said mechanical treatment comprises tumbling, tumbling in the presence of abrasive material, impingement, or any combination thereof.

84. The method of claim 77, wherein said thermal treatment is used and comprises a furnace, injection into a high temperature plasma flame, or other high temperature flames.

85. The method of claim 84, wherein said thermal treatment is conducted in the presence of reduced pressure or increased pressure relative to ambient pressure.

86. The method of claim 84, wherein during said thermal treatment, an active phase is present in order to react with one or more phases in the template sphere.

87. The method of claim 77, wherein said template sphere after removing or diminishing one or more flaws, has an aspect ratio of 5 or less.

88. The method of claim 77, wherein said template sphere after removing or diminishing one or more flaws, has an aspect ratio of 0.1 to 4.

89. The method of claim 77, wherein said template sphere after removing or diminishing one or more flaws, has an aspect ratio of 0.5 to 1.3.

90. The method of claim 77, wherein after removing or diminishing one or more flaws, the template sphere has a radius of curvature of from 0.5 microns to 100 microns.

91. The method of claim 77, wherein after removing or diminishing said one or more flaws, the overall surface area of the template sphere is reduced from 1% to 10% compared to the template sphere prior to the surface treatment.

97. The proppant formed by the process of claim 77.

92. A method of forming a proppant comprising providing a template sphere and forming a shell around the entire outer surface of said template sphere by a direct particle deposition from a slurry containing precursor particles that form the shell or coating and then drying or sintering said shell to form a continuous sintered shell.

93. The method of claim 92, wherein one or more sacrificial monolayers are first applied to the template sphere to induce covalent bonding or other attachment mechanisms between the surface of the template and the particles in suspension that form said shell.

94. A method of forming a proppant comprising providing a template sphere and forming a shell around the entire outer surface of said template sphere by direct nucleation and deposition of species onto the template sphere.

95. The method of claim 94, wherein said direct nucleation and deposition comprises a precipitation reaction.

96. The method of claim 95, wherein said precipitation reaction used to form said shell is accomplished through the adjustment of the pH of a solution that contains said template sphere, adjustment of temperature, adjustment of pressure, or any combination thereof.