Patents by Inventor David C. Briggs
David C. Briggs 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).
-
Patent number: 11148390Abstract: A multiple layer hollow cylinder is provided. An inner air-tight material is wrapped about at least a portion of a mandrel to form a plurality of first material loops. Each first material loop subsequent to an initial first material loop at least partially overlaps a previous first material loop. A resin-infused fabric material is wrapped over the inner air-tight material to form a plurality of second material loops. Each second material loop subsequent to an initial second material loop at least partially overlaps a previous second material loop. An outer air-tight transparent material is wrapped over the resin-infused fabric material to form a plurality of third material loops. Each third material loop subsequent to an initial third material loop at least partially overlaps a previous third material loop. Energy is directed about the outer air-tight transparent material to cure the resin-infused fabric material to form a hollow cylinder.Type: GrantFiled: November 9, 2016Date of Patent: October 19, 2021Assignee: Lockheed Martin CorporationInventors: Randy L. Gaigler, Matthew B. Ascari, David C. Briggs, Anthony J. Pellegrino, James A. Waicukauski
-
Patent number: 10518902Abstract: A UAV capture system including a cable array comprising at least two laterally-spaced cables carried by a first cable support structure. Catches disposed on respective port and starboard wings of a UAV are positioned to engage the cables when the UAV flies into them. A payout device pays out the engaged cables after they have been engaged by the UAV and a brake decelerates the UAV by resisting the pay out of the cables.Type: GrantFiled: March 14, 2016Date of Patent: December 31, 2019Assignee: Lockheed Martin CorporationInventors: David C. Briggs, Corey A. Fleischer, Greg W. Klein, Adam M. Knabe, George Gregory Miller, Michael W. Poppek
-
Publication number: 20180126689Abstract: A multiple layer hollow cylinder is provided. An inner air-tight material is wrapped about at least a portion of a mandrel to form a plurality of first material loops. Each first material loop subsequent to an initial first material loop at least partially overlaps a previous first material loop. A resin-infused fabric material is wrapped over the inner air-tight material to form a plurality of second material loops. Each second material loop subsequent to an initial second material loop at least partially overlaps a previous second material loop. An outer air-tight transparent material is wrapped over the resin-infused fabric material to form a plurality of third material loops. Each third material loop subsequent to an initial third material loop at least partially overlaps a previous third material loop. Energy is directed about the outer air-tight transparent material to cure the resin-infused fabric material to form a hollow cylinder.Type: ApplicationFiled: November 9, 2016Publication date: May 10, 2018Inventors: Randy L. Gaigler, Matthew B. Ascari, David C. Briggs, Anthony J. Pellegrino, James A. Waicukauski
-
Publication number: 20180086481Abstract: A UAV capture system including a cable array comprising at least two laterally-spaced cables carried by a first cable support structure. Catches disposed on respective port and starboard wings of a UAV are positioned to engage the cables when the UAV flies into them. A payout device pays out the engaged cables after they have been engaged by the UAV and a brake decelerates the UAV by resisting the pay out of the cables.Type: ApplicationFiled: March 14, 2016Publication date: March 29, 2018Inventors: David C. Briggs, Corey A. Fleischer, Greg W. Klein, Adam M. Knabe, George Gregory Miller, Michael W. Poppek
-
Patent number: 9822919Abstract: According to some aspects, a thermal insulation material is provided, comprising a first insulation layer having a cellular structure, wherein cells of the cellular structure comprise an inorganic insulator in a powder form and a second insulation layer comprising inorganic fibers. According to some aspects, a fire protection thermal insulation system is provided, comprising a first insulation layer having a cellular structure, wherein cells of the cellular structure comprise an inorganic insulator in a powder form, the first insulation layer on a fire facing side of the thermal insulation system, and a second insulation layer comprising inorganic fibers, the second insulation layer on a non-fire facing side of the thermal insulation system.Type: GrantFiled: January 30, 2015Date of Patent: November 21, 2017Assignee: Lockheed Martin CorporationInventors: David C. Briggs, Corey A. Fleischer
-
Patent number: 9784578Abstract: A wake test instrumentation and more particularly, systems and methods for determining wake velocities and directions are provided. The wake test instrument includes a linkage system mounted to a base and a pole pivotally mounted to the linkage system and which comprises a hydrofoil system. The wake test instrument further includes a hydrofoil system mounted to the pole. The wake test instrument further includes a water flow meter mounted to the pole which is structured to measure wake parameters.Type: GrantFiled: June 26, 2015Date of Patent: October 10, 2017Assignee: LOCKHEED MARTIN CORPORATIONInventors: David J. Bonitsky, David C. Briggs
-
Publication number: 20160377461Abstract: A wake test instrumentation and more particularly, systems and methods for determining wake velocities and directions are provided. The wake test instrument includes a linkage system mounted to a base and a pole pivotally mounted to the linkage system and which comprises a hydrofoil system. The wake test instrument further includes a hydrofoil system mounted to the pole. The wake test instrument further includes a water flow meter mounted to the pole which is structured to measure wake parameters.Type: ApplicationFiled: June 26, 2015Publication date: December 29, 2016Inventors: David J. Bonitsky, David C. Briggs
-
Patent number: 9382073Abstract: A reconfigurable modular transporting system and related components which can efficiently and effectively move containers and other items is disclosed. The transport system includes a plurality of track components structured to mate with one another by a complementary male connection and female connection at ends thereof. The transport system further includes at least one hub component comprising a rotating track assembly which aligns with male and female track assemblies connected to at least one of the track components. The transport system further includes a plurality of truck assemblies engagable to the plurality of track components and the rotating track of at least one hub component.Type: GrantFiled: June 27, 2014Date of Patent: July 5, 2016Assignee: LOCKHEED MARTIN CORPORATIONInventors: Jordan T. Ledford, Isaiah Abramson, David C. Briggs
-
Publication number: 20150375667Abstract: A reconfigurable modular transporting system and related components which can efficiently and effectively move containers and other items is disclosed. The transport system includes a plurality of track components structured to mate with one another by a complementary male connection and female connection at ends thereof. The transport system further includes at least one hub component comprising a rotating track assembly which aligns with male and female track assemblies connected to at least one of the track components. The transport system further includes a plurality of truck assemblies engagable to the plurality of track components and the rotating track of at least one hub component.Type: ApplicationFiled: June 27, 2014Publication date: December 31, 2015Inventors: Jordan T. LEDFORD, Isaiah ABRAMSON, David C. BRIGGS
-
Publication number: 20150219268Abstract: According to some aspects, a thermal insulation material is provided, comprising a first insulation layer having a cellular structure, wherein cells of the cellular structure comprise an inorganic insulator in a powder form and a second insulation layer comprising inorganic fibers. According to some aspects, a fire protection thermal insulation system is provided, comprising a first insulation layer having a cellular structure, wherein cells of the cellular structure comprise an inorganic insulator in a powder form, the first insulation layer on a fire facing side of the thermal insulation system, and a second insulation layer comprising inorganic fibers, the second insulation layer on a non-fire facing side of the thermal insulation system.Type: ApplicationFiled: January 30, 2015Publication date: August 6, 2015Applicant: Lockheed Martin CorporationInventors: David C. Briggs, Corey A. Fleischer
-
Publication number: 20150219269Abstract: According to some aspects, a thermal insulation material is provided, comprising a first insulation layer comprising an aerogel, and a second insulation layer comprising inorganic fibers, wherein a thickness of the second insulation layer is greater than a thickness of the first insulation layer. According to some aspects, a fire protection thermal insulation system is provided, comprising a first insulation layer comprising an aerogel, the first insulation layer on a fire facing side of the thermal insulation system, and a second insulation layer comprising inorganic fibers, the second insulation layer on a non-fire facing side of the thermal insulation system, wherein a thickness of the second insulation layer is greater than a thickness of the first insulation layer.Type: ApplicationFiled: January 30, 2015Publication date: August 6, 2015Applicant: Lockheed Martin CorporationInventors: Corey A. Fleischer, David C. Briggs, Linda M. Pelullo, James A. Waicukauski