Patents by Inventor Blake Simpson
Blake Simpson 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: 10774863Abstract: A blind fastener system including a sleeve and, optionally, a core bolt insertable into the sleeve, wherein at least one of the sleeve and the core bolt includes a lubricious metallic coating containing at least one of tin, bismuth, indium and aluminum.Type: GrantFiled: June 18, 2018Date of Patent: September 15, 2020Assignee: The Boeing CompanyInventors: Blake A. Simpson, Dave G. Ellsworth, Stephen G. Holley, Michael Howard-Edward Ware, Casey M. Cowell
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Publication number: 20200230691Abstract: A blind fastener tool with pulling fingers is provided. One embodiment is a tool for installing a blind fastener in a hole. The tool includes stationary fingers having tips protruding from a front end of the housing to contact a rim of a sleeve of the blind fastener. The tool also includes pulling fingers in the housing arranged longitudinally in spaces between the stationary fingers. Ends of the pulling fingers proximate to the front end are configured to radially expand to receive a drive element of the blind fastener, and to radially collapse to grip a collar of the drive element. The pulling fingers are configured to translate inside the housing to pull the drive element away from the sleeve as the stationary fingers contact the rim of the sleeve to form a bulb with the sleeve at a blind side of the hole.Type: ApplicationFiled: January 23, 2019Publication date: July 23, 2020Inventors: Blake A Simpson, David G Ellsworth, Casey M Cowell, Stephen G Holley
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Patent number: 10711814Abstract: An assembly comprising first and second structural elements having aligned holes, a fastener that occupies at least respective portions of the holes without a surrounding sleeve, and a mating part that is coupled to the fastener. The fastener comprises: a head; a circular cylindrical shank extending from the head; a mating portion comprising external projections; and a transition portion disposed between the shank and the mating portion. The transition portion comprises a tapered lead-in section that meets the shank at a shank/lead-in intersection and a radiused lead-in section that meets the tapered lead-in section. The tapered lead-in section tapers gradually in a first axial direction toward the mating portion and has a first profile that is linear and a taper angle equal to or less than 20 degrees, while the radiused lead-in section curves abruptly in the first axial direction and has a second profile that is a circular arc having a radius.Type: GrantFiled: February 20, 2017Date of Patent: July 14, 2020Assignee: The Boeing CompanyInventors: Blake A. Simpson, Tanni Sisco
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Publication number: 20200217349Abstract: A conductive fastening system, a fastened assembly, and a method of fastening an assembly composed of layers of carbon fiber reinforced plastic (“CFRP”) and/or metallic material includes fasteners with an electrically conductive coating and electrically conductive gap filler materials between the fasteners and sidewalls of holes formed through the layers of the assembly. The sidewalls of the holes are coated with the electrically conductive gap filler material by abrading, injection or spraying. The fasteners with the electrically conductive coating are inserted through the holes. The conductive coating on the fasteners and electrically conductive gap filler material work together to enhance electrical conductivity between the fastener and assembly. The conductive coating also acts as a lubricant to reduce the amount of force required to insert the fastener into the hole thereby reducing damage to the assembly.Type: ApplicationFiled: January 8, 2019Publication date: July 9, 2020Applicant: The Boeing CompanyInventors: Darrin M. Hansen, Blake A. Simpson, Shahriar Khosravani
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Patent number: 10641307Abstract: An assembly comprising first and second structural elements having aligned holes, an fastener that occupies at least respective portions of the holes without a surrounding sleeve, and a mating part that is coupled to the fastener. The fastener comprises: a head; a circular cylindrical shank extending from the head; a mating portion comprising external projections; and a transition portion disposed between the shank and the mating portion. The transition portion comprises a first radiused lead-in section that meets the shank at a shank/lead-in intersection and a second radiused lead-in section that meets the first radiused lead-in section. The first radiused lead-in section curves gradually in a first axial direction toward the mating portion and has a first profile that is a circular arc having a first radius, while the second radiused lead-in section curves abruptly in the first axial direction and has a second profile that is a circular arc having a second radius which is much smaller than the first radius.Type: GrantFiled: February 20, 2017Date of Patent: May 5, 2020Assignee: The Boeing CompanyInventors: Blake A. Simpson, Tanni Sisco, Todd E. Hubbell, Jeffrey A. Wilkerson
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Patent number: 10626908Abstract: An electromagnetic effect suppressing termination part is provided for a fastener formed of a metallic material, the fastener having a head, a shank, and a threaded portion opposite the head. The termination part includes a main body defining an internally threaded portion configured to threadably receive the threaded portion of the fastener, the internally threaded portion defining a thread major diameter. A collar is coupled to a distal end of the main body by a frangible web, wherein the main body, collar, and frangible web are formed of a metallic core coated by a layer of dielectric material. The frangible web, when broken, presents an exposed portion of the metallic core, wherein the frangible web includes an inner surface radially outwardly offset from the thread major diameter of the internally threaded portion by a setback distance.Type: GrantFiled: March 30, 2018Date of Patent: April 21, 2020Assignee: The Boeing CompanyInventors: Sean D. Morden, Blake A. Simpson, Tanni Sisco, Kwok-Tung Chan, Monica J. Brockway
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Patent number: 10603844Abstract: Apparatus and methods for injecting molten filler material into a hole. The method in accordance with one embodiment comprises: drilling a hole in a composite layer; heating filler material comprising an electrically conductive low-melting alloy to a molten state; inserting a nozzle having an internal channel system into the hole with a gap separating the nozzle and the hole; forcing molten filler material into, through and out of the internal channel system of the nozzle and into the gap; and retracting the nozzle from the hole. The nozzle may be rotary or not rotary.Type: GrantFiled: October 18, 2017Date of Patent: March 31, 2020Assignee: The Boeing CompanyInventors: Shahriar Khosravani, Blake A. Simpson, Darrin M. Hansen, Mark J. DuFour
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Publication number: 20190383319Abstract: A blind fastener system including a sleeve and, optionally, a core bolt insertable into the sleeve, wherein at least one of the sleeve and the core bolt includes a lubricious metallic coating containing at least one of tin, bismuth, indium and aluminum.Type: ApplicationFiled: June 18, 2018Publication date: December 19, 2019Applicant: The Boeing CompanyInventors: Blake A. Simpson, Dave G. Ellsworth, Stephen G. Holley, Michael Howard-Edward Ware, Casey M. Cowell
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Publication number: 20190301518Abstract: An electromagnetic effect suppressing termination part for a fastener formed of a metallic material, the fastener having a head, a shank, and a male threaded portion opposite the head, has a metallic core coated by a layer of dielectric material. An internal bore of the termination part includes an inner wall, a counterbore hole, and a cavity disposed therebetween. An outer surface includes an outer wall, and a frustoconical wall positioned proximally relative to the outer wall, the frustoconical wall extending radially outwardly from the outer wall and having an included angle of less than approximately 90 degrees. A seal is disposed in the counterbore hole, and the frustoconical wall is configured so that a compressive force applied to the frustoconical wall deforms the inner wall to conform to the male threaded portion of the fastener and deforms the seal to fill the cavity.Type: ApplicationFiled: March 30, 2018Publication date: October 3, 2019Applicant: The Boeing CompanyInventors: Sean D. Morden, Blake A. Simpson, Tanni Sisco, Kwok-Tung Chan, Monica J. Brockway
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Publication number: 20190301513Abstract: An electromagnetic effect suppressing termination part is provided for a fastener formed of a metallic material, the fastener having a head, a shank, and a threaded portion opposite the head. The termination part includes a main body defining an internally threaded portion configured to threadably receive the threaded portion of the fastener, the internally threaded portion defining a thread major diameter. A collar is coupled to a distal end of the main body by a frangible web, wherein the main body, collar, and frangible web are formed of a metallic core coated by a layer of dielectric material. The frangible web, when broken, presents an exposed portion of the metallic core, wherein the frangible web includes an inner surface radially outwardly offset from the thread major diameter of the internally threaded portion by a setback distance.Type: ApplicationFiled: March 30, 2018Publication date: October 3, 2019Applicant: The Boeing CompanyInventors: Sean D. Morden, Blake A. Simpson, Tanni Sisco, Kwok-Tung Chan, Monica J. Brockway
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Publication number: 20190111632Abstract: Apparatus and methods for injecting molten filler material into a hole. The method in accordance with one embodiment comprises: drilling a hole in a composite layer; heating filler material comprising an electrically conductive low-melting alloy to a molten state; inserting a nozzle having an internal channel system into the hole with a gap separating the nozzle and the hole; forcing molten filler material into, through and out of the internal channel system of the nozzle and into the gap; and retracting the nozzle from the hole. The nozzle may be rotary or not rotary.Type: ApplicationFiled: October 18, 2017Publication date: April 18, 2019Applicant: The Boeing CompanyInventors: Shahriar Khosravani, Blake A. Simpson, Darrin M. Hansen, Mark J. DuFour
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Publication number: 20190063485Abstract: A fastening device for coupling an assembly includes a fastener comprising a head, a threaded portion, and a shank extending between the head and the threaded portion. The fastening device also includes a coating formed around the fastener, wherein the coating is electrically conductive and comprises a varying thickness along the shank.Type: ApplicationFiled: August 25, 2017Publication date: February 28, 2019Inventors: Shahriar Khosravani, Darrin Michael Hansen, Blake A. Simpson, Junghyun Ahn
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Publication number: 20190032218Abstract: A method for treating surfaces of fasteners made of titanium alloy or corrosion-resistant steel using a sol-gel pretreatment process prior to the application of an aluminum pigment coating. The sol-gel pretreatment process produces an interface film on the fastener surface, which interface film comprises an organometallic-based network system. The interface film aids in improving adhesion and surface roughness when fasteners are used in interference fit conditions (i.e., the hole diameter is smaller than the fastener shank diameter).Type: ApplicationFiled: July 28, 2017Publication date: January 31, 2019Applicant: The Boeing CompanyInventors: Blake A. Simpson, Tanni Sisco
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Publication number: 20180238370Abstract: An assembly comprising first and second structural elements having aligned holes, an fastener that occupies at least respective portions of the holes without a surrounding sleeve, and a mating part that is coupled to the fastener. The fastener comprises: a head; a circular cylindrical shank extending from the head; a mating portion comprising external projections; and a transition portion disposed between the shank and the mating portion. The transition portion comprises a first radiused lead-in section that meets the shank at a shank/lead-in intersection and a second radiused lead-in section that meets the first radiused lead-in section. The first radiused lead-in section curves gradually in a first axial direction toward the mating portion and has a first profile that is a circular arc having a first radius, while the second radiused lead-in section curves abruptly in the first axial direction and has a second profile that is a circular arc having a second radius which is much smaller than the first radius.Type: ApplicationFiled: February 20, 2017Publication date: August 23, 2018Applicant: The Boeing CompanyInventors: Blake A. Simpson, Tanni Sisco, Todd E. Hubbell, Jeffrey A. Wilkerson
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Publication number: 20180238361Abstract: An assembly comprising first and second structural elements having aligned holes, a fastener that occupies at least respective portions of the holes without a surrounding sleeve, and a mating part that is coupled to the fastener. The fastener comprises: a head; a circular cylindrical shank extending from the head; a mating portion comprising external projections; and a transition portion disposed between the shank and the mating portion. The transition portion comprises a tapered lead-in section that meets the shank at a shank/lead-in intersection and a radiused lead-in section that meets the tapered lead-in section. The tapered lead-in section tapers gradually in a first axial direction toward the mating portion and has a first profile that is linear and a taper angle equal to or less than 20 degrees, while the radiused lead-in section curves abruptly in the first axial direction and has a second profile that is a circular arc having a radius.Type: ApplicationFiled: February 20, 2017Publication date: August 23, 2018Applicant: The Boeing CompanyInventors: Blake A. Simpson, Tanni Sisco