Patents by Inventor Corbin S. Glenn
Corbin S. Glenn has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 10253603Abstract: A method of controlling a dynamic pressure created during detonation of a shaped charge comprises: positioning the shaped charge in a wellbore, wherein the shaped charge comprises a main explosive load, wherein a substance is included in the main explosive load or is positioned adjacent to the main explosive load, wherein the substance increases or decreases the dynamic pressure or increases or decreases the duration of a pressure pulse created during detonation of the shaped charge; whereas a substantially identical shaped charge without the substance does not increase or decrease the dynamic pressure nor increase or decrease the duration of the pressure pulse during detonation. A method of controlling the balance of a portion of a wellbore comprises: positioning the shaped charge in the portion of the wellbore; and creating a desired balance in the portion of the wellbore.Type: GrantFiled: February 5, 2013Date of Patent: April 9, 2019Assignee: Halliburton Energy Services, Inc.Inventors: Antony Forbes Grattan, Dennis James Haggerty, Corbin S. Glenn
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Patent number: 10151569Abstract: An initiator comprises: a first explosive substance, wherein the first explosive substance comprises a secondary explosive, and wherein at least the first explosive substance is capable of being initiated. The initiator comprises effectively no primary explosive. The secondary explosive can be a thermally-stable secondary explosive. A method of using an initiator comprises: initiating the initiator.Type: GrantFiled: February 5, 2013Date of Patent: December 11, 2018Assignee: Halliburton Energy Services, Inc.Inventors: Corbin S. Glenn, Thomas Jeffrey Wuensche, Justine Marie Davidson, James Marshall Barker, David John Leidel
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Patent number: 9617194Abstract: A shaped charge liner comprises a powder, and the powder comprises a blend of particles. The particles comprise a core material, a first reactant material in intimate contact with the core material, and a second reactant material in intimate contact with the first reactant, where the core material has a density greater than 10 grams per cubic centimeter (g/cc).Type: GrantFiled: July 2, 2014Date of Patent: April 11, 2017Assignee: Halliburton Energy Services, Inc.Inventor: Corbin S. Glenn
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Publication number: 20160003600Abstract: An initiator comprises: a first explosive substance, wherein the first explosive substance comprises a secondary explosive, and wherein at least the first explosive substance is capable of being initiated. The initiator comprises effectively no primary explosive. The secondary explosive can be a thermally-stable secondary explosive. A method of using an initiator comprises: initiating the initiator.Type: ApplicationFiled: February 5, 2013Publication date: January 7, 2016Applicant: HALLIBURTON ENERGY SERVICES, INC.Inventors: Corbin S. Glenn, Thomas Jeffrey Wuensche, Justine Marie Davidson, James Marshall Barker, David John Leidel
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Publication number: 20150376992Abstract: A method of controlling a dynamic pressure created during detonation of a shaped charge comprises: positioning the shaped charge in a wellbore, wherein the shaped charge comprises a main explosive load, wherein a substance is included in the main explosive load or is positioned adjacent to the main explosive load, wherein the substance increases or decreases the dynamic pressure or increases or decreases the duration of a pressure pulse created during detonation of the shaped charge; whereas a substantially identical shaped charge without the substance does not increase or decrease the dynamic pressure nor increase or decrease the duration of the pressure pulse during detonation. A method of controlling the balance of a portion of a wellbore comprises: positioning the shaped charge in the portion of the wellbore; and creating a desired balance in the portion of the wellbore.Type: ApplicationFiled: February 5, 2013Publication date: December 31, 2015Inventors: Antony Forbes Grattan, Dennis James Haggerty, Corbin S. Glenn
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Publication number: 20140314614Abstract: A shaped charge liner comprises a powder, and the powder comprises a blend of particles. The particles comprise a core material, a first reactant material in intimate contact with the core material, and a second reactant material in intimate contact with the first reactant, where the core material has a density greater than 10 grams per cubic centimeter (g/cc).Type: ApplicationFiled: July 2, 2014Publication date: October 23, 2014Inventor: Corbin S. Glenn
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Patent number: 8807213Abstract: A perforation gun. The perforation gun comprises a tool body, the tool body defining at least one shouldered hole wherein the shouldered hole comprises a hole through a wall of the tool body and a shoulder that is thinner than the wall of the tool body and at least one perforating explosive charge disposed within the tool body.Type: GrantFiled: June 14, 2012Date of Patent: August 19, 2014Assignee: Halliburton Energy Services, Inc.Inventors: Jerry L. Walker, Corbin S. Glenn, Bryan D. Powell
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Patent number: 8794153Abstract: A shaped charge liner comprises a powder, and the powder comprises a blend of particles. The particles comprise a core material, a first reactant material in intimate contact with the core material, and a second reactant material in intimate contact with the first reactant, where the core material has a density greater than 10 grams per cubic centimeter (g/cc).Type: GrantFiled: May 3, 2012Date of Patent: August 5, 2014Assignee: Halliburton Energy Services, Inc.Inventor: Corbin S. Glenn
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Publication number: 20140131097Abstract: A perforation gun. The perforation gun comprises a tool body, the tool body defining at least one shouldered hole wherein the shouldered hole comprises a hole through a wall of the tool body and a shoulder that is thinner than the wall of the tool body and at least one perforating explosive charge disposed within the tool body.Type: ApplicationFiled: June 14, 2012Publication date: May 15, 2014Applicant: HALLIBURTON ENERGY SERVICES, INC.Inventors: Jerry L. Walker, Corbin S. Glenn, Bryan D. Powell
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Patent number: 8381652Abstract: A shaped charge liner is provided. The shaped charge liner comprises a first material denser than 10 grams per cubic centimeter (g/cc) and a reactive material. The first material is concentrated in a middle of the liner and decreased in at least one of an apex and a skirt of the liner, and the reactive material is concentrated in at least one of the apex and the skirt of the liner and decreased in the middle of the liner.Type: GrantFiled: March 9, 2010Date of Patent: February 26, 2013Assignee: Halliburton Energy Services, Inc.Inventor: Corbin S. Glenn
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Publication number: 20120234194Abstract: A shaped charge liner comprises a powder, and the powder comprises a blend of particles. The particles comprise a core material, a first reactant material in intimate contact with the core material, and a second reactant material in intimate contact with the first reactant, where the core material has a density greater than 10 grams per cubic centimeter (g/cc).Type: ApplicationFiled: May 3, 2012Publication date: September 20, 2012Applicant: HALLIBURTON ENERGY SERVICES, INC.Inventor: Corbin S. Glenn
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Publication number: 20110219978Abstract: A shaped charge liner is provided. The shaped charge liner comprises a first material denser than 10 grams per cubic centimeter (g/cc) and a reactive material. The first material is concentrated in a middle of the liner and decreased in at least one of an apex and a skirt of the liner, and the reactive material is concentrated in at least one of the apex and the skirt of the liner and decreased in the middle of the liner.Type: ApplicationFiled: March 9, 2010Publication date: September 15, 2011Applicant: HALLIBURTON ENERGY SERVICES, INC.Inventor: Corbin S. Glenn
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Patent number: 6851471Abstract: A perforating gun assembly useful in hydrocarbon well completion. The gun is assembled in a carrier made from straight walled tubing as a primary structural member with complementary male and female threads cut into opposite ends so that gun assemblies may be directly connected together. The male coupling includes a reinforcing sleeve threaded into an internal thread. An alignment pin is positioned in the carrier extending through the reinforcing ring and into the interior of the carrier. A charge assembly includes a charge holder tube with upper and lower alignment fixtures. The lower alignment fixture includes an alignment slot for mating with the alignment pin and a shoulder for supporting the charge assembly on the sleeve. The upper alignment fixture has an alignment pin for mating with an alignment slot in the carrier. A retainer ring may be threaded into the upper female threads to prevent removal of the charge assembly from the carrier.Type: GrantFiled: May 2, 2003Date of Patent: February 8, 2005Assignee: Halliburton Energy Services, Inc.Inventors: Darren R. Barlow, Dennis R. Crowdis, William J. Gilbert, Jr., Corbin S. Glenn
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Publication number: 20040216866Abstract: A perforating gun assembly useful in hydrocarbon well completion. The gun is assembled in a carrier made from straight walled tubing as a primary structural member with complementary male and female threads cut into opposite ends so that gun assemblies may be directly connected together. The male coupling includes a reinforcing sleeve threaded into an internal thread. An alignment pin is positioned in the carrier extending through the reinforcing ring and into the interior of the carrier. A charge assembly includes a charge holder tube with upper and lower alignment fixtures. The lower alignment fixture includes an alignment slot for mating with the alignment pin and a shoulder for supporting the charge assembly on the sleeve. The upper alignment fixture has an alignment pin for mating with an alignment slot in the carrier. A retainer ring may be threaded into the upper female threads to prevent removal of the charge assembly from the carrier.Type: ApplicationFiled: May 2, 2003Publication date: November 4, 2004Inventors: Darren R. Barlow, Dennis R. Crowdis, William J. Gilbert, Corbin S. Glenn
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Publication number: 20030183113Abstract: The present disclosure suggests a method to remove well bore fluid from the path of a shaped-charge jet in order to reduce the effect it has on the jet tip. This most preferred embodiment uses a precursor liner and a primary liner both pressed in the same housing. In the most preferred embodiment, the primary liner is similar or equivalent to a standard big hole shaped charge liner. The precursor liner is pressed into the apex end of the primary liner and upon detonation is intended to form an initial very fast moving precursor jet to open a path through the fluid of the well bore annulus for the following primary jet. In the preferred embodiment the precursor liner is made from different material, preferably a less dense material and/or a material having a higher sound speed, than the material forming the primary liner.Type: ApplicationFiled: March 12, 2002Publication date: October 2, 2003Inventors: Darren R. Barlow, Corbin S. Glenn