Patents by Inventor Austin E. Mann
Austin E. Mann 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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Publication number: 20250296147Abstract: A method for manufacturing an article includes consolidating a metallic powder composition into a consolidated preform, applying a supersolidus heat treatment to the consolidated preform during or after consolidating the metallic powder composition to yield a heat treated preform, and reducing a cross-sectional area of the heat treated preform by thermo-mechanical processing to yield a processed preform.Type: ApplicationFiled: March 22, 2024Publication date: September 25, 2025Applicant: The Boeing CompanyInventors: Austin E. Mann, Ali Yousefiani, Dana G. Smith, Paul N. Wilson, Scott Cummings
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Publication number: 20250215535Abstract: A refractory complex concentrated alloy includes about 12-22 wt. % chromium (Cr), about 22-35 wt. % molybdenum (Mo), about 15-50 wt. % tantalum (Ta), about 10-20 wt. % titanium (Ti), and aluminum (Al). The refractory complex concentrated alloy is characterized by a matrix phase having a body-centered cubic crystal structure.Type: ApplicationFiled: June 24, 2022Publication date: July 3, 2025Applicants: The Boeing Company, Missouri University of Science & TechnologyInventors: Austin E. Mann, Ali Yousefiani, Joseph Newkirk
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Publication number: 20250164367Abstract: A material testing system and method includes a testpiece, a test bed, and a data collector. The testpiece includes a body that extends along an axis and a hollow interior that is formed by the body. The test bed internally pressurizes the hollow interior of the testpiece. The data collector acquires data representing the testpiece.Type: ApplicationFiled: November 22, 2023Publication date: May 22, 2025Applicant: The Boeing CompanyInventors: Ali Yousefiani, Joseph S. Indeck, Bruno Zamorano Senderos, Austin E. Mann, Scott Cummings
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Publication number: 20250050414Abstract: A method for manufacturing a wrought metallic article from a metallic-powder composition includes steps of: consolidating the metallic-powder composition to yield a consolidated preform having a cross-sectional area and a relative density of less than 100 percent; reducing the cross-sectional area of the consolidated preform via at least one forming pass of one of a cogging process and a rotary incremental forming process, thereby yielding an intermediate preform; and reducing the cross-sectional area of the intermediate preform via at least one forming pass of another of the cogging process and the rotary incremental forming process.Type: ApplicationFiled: August 9, 2023Publication date: February 13, 2025Applicant: The Boeing CompanyInventors: Austin E. Mann, Joseph A. Pecina, Ali Yousefiani
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Patent number: 12111330Abstract: A material compatibility test design system and method, allowing for the testing of characteristics of behavior of materials in extreme environments, the method including concurrently exposing a test specimen to a first environment and a second environment, the test specimen having an outside surface and an inside surface, the inside surface defining an internal volume, includes exposing the outside surface of the test specimen to the first environment for a predetermined period of time, the first environment comprising a first temperature, a first pressure and a first composition. The method further includes exposing the inside surface of the test specimen to the second environment for a second predetermined period of time, the second environment comprising a second temperature, a second pressure and a second composition.Type: GrantFiled: February 16, 2022Date of Patent: October 8, 2024Assignee: The Boeing CompanyInventors: Bruno Zamorano Senderos, Ali Yousefiani, Austin E. Mann, Michael F. Stoia
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Patent number: 11938541Abstract: A method for manufacturing a wrought metallic article from metallic-powder compositions comprises steps of (1) compacting the metallic-powder composition to yield a compact, having a surface, a cross-sectional area, and a relative density of less than 100 percent, (2) reducing the cross-sectional area of the compact via an initial forming pass of a rotary incremental forming process so that the compact has a decreased cross-sectional area, and (3) reducing the decreased cross-sectional area of the compact via a subsequent forming pass of the rotary incremental forming process by a greater percentage than that, by which the cross-sectional area of the compact was reduced during the initial forming pass.Type: GrantFiled: June 9, 2021Date of Patent: March 26, 2024Assignee: The Boeing CompanyInventors: Austin E. Mann, Ali Yousefiani, Joe Pecina
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Patent number: 11846010Abstract: A method for making an aluminum alloy includes steps of (1) weighing out starting materials to achieve a mass of material having a composition that includes aluminum, about 1.8 to about 5.6 percent by weight copper, about 0.6 to about 2.6 percent by weight lithium, and at least one of lanthanum up to about 1.5 percent by weight, strontium up to about 1.5 percent by weight, cerium up to about 1.5 percent by weight, and praseodymium up to about 1.5 percent by weight; (2) loading said starting materials into a crucible; (3) inserting said crucible into a chamber; (4) evacuating said chamber to a predetermined vacuum level; (5) melting said starting materials to form a molten mass; and (6) casting said molten mass into a mold.Type: GrantFiled: May 21, 2021Date of Patent: December 19, 2023Assignee: The Boeing CompanyInventors: Austin E. Mann, Andrew H. Baker, Rajiv Mishra, Sivanesh Palanivel
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Publication number: 20230258484Abstract: A material compatibility test design system and method, allowing for the testing of characteristics of behavior of materials in extreme environments, the method including concurrently exposing a test specimen to a first environment and a second environment, the test specimen having an outside surface and an inside surface, the inside surface defining an internal volume, includes exposing the outside surface of the test specimen to the first environment for a predetermined period of time, the first environment comprising a first temperature, a first pressure and a first composition. The method further includes exposing the inside surface of the test specimen to the second environment for a second predetermined period of time, the second environment comprising a second temperature, a second pressure and a second composition.Type: ApplicationFiled: February 16, 2022Publication date: August 17, 2023Applicant: The Boeing CompanyInventors: Bruno Zamorano Senderos, Ali Yousefiani, Austin E. Mann, Michael F. Stoia
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Patent number: 11465243Abstract: An interlayered structure for joining of dissimilar materials, includes a first material substrate, a second material substrate having a composition dissimilar from a composition of the first material substrate, and a plurality of interlayers disposed between the first material substrate and the second material substrate, including a first interlayer nearest to the first material substrate and a last interlayer nearest to the second material substrate. The first interlayer has a composition selected to have a maximum solid solubility within the composition of the first material substrate that is greater than or equal to the other interlayers' solubility within the composition of the first material substrate. The last interlayer has a composition selected to have a maximum solid solubility within the composition of the second material substrate that is greater than or equal to the other interlayers' solubility within the composition of the second material substrate.Type: GrantFiled: June 13, 2018Date of Patent: October 11, 2022Assignee: The Boeing CompanyInventors: Austin E. Mann, Ali Yousefiani
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Publication number: 20220193766Abstract: A method for manufacturing a wrought metallic article from metallic-powder compositions comprises steps of (1) compacting the metallic-powder composition to yield a compact, having a surface, a cross-sectional area, and a relative density of less than 100 percent, (2) reducing the cross-sectional area of the compact via an initial forming pass of a rotary incremental forming process so that the compact has a decreased cross-sectional area, and (3) reducing the decreased cross-sectional area of the compact via a subsequent forming pass of the rotary incremental forming process by a greater percentage than that, by which the cross-sectional area of the compact was reduced during the initial forming pass.Type: ApplicationFiled: June 9, 2021Publication date: June 23, 2022Applicant: The Boeing CompanyInventors: Austin E. Mann, Ali Yousefiani, Joe Pecina
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Publication number: 20210277508Abstract: A method for making an aluminum alloy includes steps of (1) weighing out starting materials to achieve a mass of material having a composition that includes aluminum, about 1.8 to about 5.6 percent by weight copper, about 0.6 to about 2.6 percent by weight lithium, and at least one of lanthanum up to about 1.5 percent by weight, strontium up to about 1.5 percent by weight, cerium up to about 1.5 percent by weight, and praseodymium up to about 1.5 percent by weight; (2) loading said starting materials into a crucible; (3) inserting said crucible into a chamber; (4) evacuating said chamber to a predetermined vacuum level; (5) melting said starting materials to form a molten mass; and (6) casting said molten mass into a mold.Type: ApplicationFiled: May 21, 2021Publication date: September 9, 2021Applicant: The Boeing CompanyInventors: Austin E. Mann, Andrew H. Baker, Rajiv Mishra, Sivanesh Palanivel
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Patent number: 10857628Abstract: An interlayered structure for joining of dissimilar materials includes: a first material substrate; a second material substrate having a composition dissimilar from a composition of the first material substrate; and a plurality of interlayers disposed between the first material substrate and the second material substrate, including a first interlayer nearest to the first material substrate and a last interlayer nearest to the second material substrate. The first interlayer has a composition selected to have a maximum solid solubility within the composition of the first material substrate that is greater than or equal to the other interlayers within the composition of the first material substrate, and the last interlayer has a composition selected to have a maximum solid solubility within the composition of the second material substrate that is greater than or equal to the other interlayers within the composition of the second material substrate.Type: GrantFiled: November 6, 2017Date of Patent: December 8, 2020Assignee: The Boeing CompanyInventor: Austin E. Mann
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Publication number: 20190134756Abstract: An interlayered structure for joining of dissimilar materials includes: a first material substrate; a second material substrate having a composition dissimilar from a composition of the first material substrate; and a plurality of interlayers disposed between the first material substrate and the second material substrate, including a first interlayer nearest to the first material substrate and a last interlayer nearest to the second material substrate. The first interlayer has a composition selected to have a maximum solid solubility within the composition of the first material substrate that is greater than or equal to the other interlayers within the composition of the first material substrate, and the last interlayer has a composition selected to have a maximum solid solubility within the composition of the second material substrate that is greater than or equal to the other interlayers within the composition of the second material substrate.Type: ApplicationFiled: November 6, 2017Publication date: May 9, 2019Applicant: The Boeing CompanyInventor: Austin E. Mann
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Publication number: 20190134755Abstract: An interlayered structure for joining of dissimilar materials, includes a first material substrate, a second material substrate having a composition dissimilar from a composition of the first material substrate, and a plurality of interlayers disposed between the first material substrate and the second material substrate, including a first interlayer nearest to the first material substrate and a last interlayer nearest to the second material substrate. The first interlayer has a composition selected to have a maximum solid solubility within the composition of the first material substrate that is greater than or equal to the other interlayers' solubility within the composition of the first material substrate. The last interlayer has a composition selected to have a maximum solid solubility within the composition of the second material substrate that is greater than or equal to the other interlayers' solubility within the composition of the second material substrate.Type: ApplicationFiled: June 13, 2018Publication date: May 9, 2019Applicant: The Boeing CompanyInventors: Austin E. Mann, Ali Yousefiani
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Publication number: 20180291489Abstract: An aluminum alloy including aluminum, about 1.8 to about 5.6 percent by weight copper, about 0.6 to about 2.6 percent by weight lithium, and at least one of lanthanum up to about 1.5 percent by weight, strontium up to about 1.5 percent by weight, cerium up to about 1.5 percent by weight and praseodymium up to about 1.5 percent by weight.Type: ApplicationFiled: April 11, 2017Publication date: October 11, 2018Applicant: The Boeing CompanyInventors: Austin E. Mann, Andrew H. Baker, Rajiv Mishra, Sivanesh Palanivel