Patents by Inventor Michael John Langmack
Michael John Langmack 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: 11885579Abstract: An additively manufactured heat transfer device is disclosed, including an enclosure portion with outer walls. The outer walls contain an inner channel configured to direct a flow of coolant fluid. The heat transfer device further includes a fluid intake port and a fluid outtake port, each connected to the first inner channel. The fluid intake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion into the inner channel, and the fluid outtake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion out of the inner channel. The inner channel is defined by internal walls, and the enclosure portion and the internal walls form a single additively manufactured unit.Type: GrantFiled: April 27, 2021Date of Patent: January 30, 2024Assignee: The Boeing CompanyInventors: Richard W. Aston, Matthew Joseph Herrmann, Michael John Langmack, Nicole M. Hastings, Sumit K. Purohit
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Patent number: 11878819Abstract: A satellite assembly is disclosed, including a satellite and a shroud. The satellite is stowed in a launch vehicle and the shroud includes a frame supporting a flexible thermal blanket enclosing the satellite.Type: GrantFiled: December 16, 2021Date of Patent: January 23, 2024Assignee: The Boeing CompanyInventors: Richard W. Aston, Emily Colleen Woods, Rachel Elizabeth Zilz, Michael John Langmack, Nicole Marie Hastings
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Patent number: 11811137Abstract: An additively manufactured antenna device is disclosed, including a base portion and a body portion. The body portion is attached to the base portion and includes a lattice stiffening structure configured to eliminate secondary printing support.Type: GrantFiled: August 3, 2021Date of Patent: November 7, 2023Assignee: The Boeing CompanyInventors: Richard W. Aston, Martin W. Bieti, Michael John Langmack, Nicole M. Hastings, Nicole Diane Schoenborn
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Patent number: 11725774Abstract: An isolation coupler for coupling a functional element to a support structure includes a first bracket. The first bracket includes a number of first-bracket sides. The number of first-bracket sides forms a closed polygonal shape, in plan view. The isolation coupler further includes a number of isolators coupled to each one of the first-bracket sides. The isolation coupler also includes a second bracket. The second bracket includes a number of second-bracket sides. The second bracket sides are coupled to the isolators. The number of second-bracket sides is equal to the number of first-bracket sides and forms the closed polygonal shape, in plan view. The isolators separate each one of the first-bracket sides from a corresponding one of the second-bracket sides to attenuate a load transferred from the first bracket to the second bracket.Type: GrantFiled: July 19, 2021Date of Patent: August 15, 2023Assignee: The Boeing CompanyInventors: Richard W. Aston, Michael John Langmack, Anna M. Tomzynska, Matthew Herrmann, Emily C. Woods
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Publication number: 20220194635Abstract: A satellite assembly is disclosed, including a satellite and a shroud. The satellite is stowed in a launch vehicle and the shroud includes a frame supporting a flexible thermal blanket enclosing the satellite.Type: ApplicationFiled: December 16, 2021Publication date: June 23, 2022Applicant: The Boeing CompanyInventors: Richard W. Aston, Emily Colleen Woods, Rachel Elizabeth Zilz, Michael John Langmack, Nicole Marie Hastings
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Publication number: 20220194632Abstract: A satellite apparatus is disclosed, including a housing having first and second opposing walls, and a support structure inside the housing spanning the first and second walls. The support structure is structurally connected to the housing only at the first and second walls, and an end portion of the support structure is configured for connection to a launch vehicle by a separation system.Type: ApplicationFiled: December 16, 2021Publication date: June 23, 2022Applicant: The Boeing CompanyInventors: Richard W. Aston, Emily Colleen Woods, Rachel Elizabeth Zilz, Michael John Langmack, Nicole Marie Hastings
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Publication number: 20210362230Abstract: An additively manufactured antenna device is disclosed, including a base portion and a body portion. The body portion is attached to the base portion and includes a lattice stiffening structure configured to eliminate secondary printing support.Type: ApplicationFiled: August 3, 2021Publication date: November 25, 2021Applicant: The Boeing CompanyInventors: Richard W. Aston, Martin W. Bieti, Michael John Langmack, Nicole M. Hastings, Nicole Diane Schoenborn
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Publication number: 20210341098Abstract: An isolation coupler for coupling a functional element to a support structure includes a first bracket. The first bracket includes a number of first-bracket sides. The number of first-bracket sides forms a closed polygonal shape, in plan view. The isolation coupler further includes a number of isolators coupled to each one of the first-bracket sides. The isolation coupler also includes a second bracket. The second bracket includes a number of second-bracket sides. The second bracket sides are coupled to the isolators. The number of second-bracket sides is equal to the number of first-bracket sides and forms the closed polygonal shape, in plan view. The isolators separate each one of the first-bracket sides from a corresponding one of the second-bracket sides to attenuate a load transferred from the first bracket to the second bracket.Type: ApplicationFiled: July 19, 2021Publication date: November 4, 2021Applicant: The Boeing CompanyInventors: Richard W. Aston, Michael John Langmack, Anna M. Tomzynska, Matthew Herrmann, Emily C. Woods
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Patent number: 11105459Abstract: An isolation coupler for coupling a functional element to a support structure includes a first bracket. The first bracket includes a number of first-bracket sides. The number of first-bracket sides forms a closed polygonal shape, in plan view. The isolation coupler further includes a number of isolators coupled to each one of the first-bracket sides. The isolation coupler also includes a second bracket. The second bracket includes a number of second-bracket sides. The second bracket sides are coupled to the isolators. The number of second-bracket sides is equal to the number of first-bracket sides and forms the closed polygonal shape, in plan view. The isolators separate each one of the first-bracket sides from a corresponding one of the second-bracket sides to attenuate a load transferred from the first bracket to the second bracket.Type: GrantFiled: December 10, 2018Date of Patent: August 31, 2021Assignee: The Boeing CompanyInventors: Richard W. Aston, Michael John Langmack, Anna M. Tomzynska, Matthew Herrmann, Emily C. Woods
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Patent number: 11103925Abstract: An additively manufactured antenna device is disclosed, including a base portion and a body portion. The body portion is attached to the base portion and includes a lattice stiffening structure configured to eliminate secondary printing support.Type: GrantFiled: March 22, 2018Date of Patent: August 31, 2021Assignee: The Boeing CompanyInventors: Richard W. Aston, Martin W. Bieti, Michael John Langmack, Nicole M. Hastings, Nicole Diane Schoenborn
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Publication number: 20210247140Abstract: An additively manufactured heat transfer device is disclosed, including an enclosure portion with outer walls. The outer walls contain an inner channel configured to direct a flow of coolant fluid. The heat transfer device further includes a fluid intake port and a fluid outtake port, each connected to the first inner channel. The fluid intake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion into the inner channel, and the fluid outtake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion out of the inner channel. The inner channel is defined by internal walls, and the enclosure portion and the internal walls form a single additively manufactured unit.Type: ApplicationFiled: April 27, 2021Publication date: August 12, 2021Applicant: The Boeing CompanyInventors: Richard W. Aston, Matthew Joseph Herrmann, Michael John Langmack, Nicole M. Hastings, Sumit K. Purohit
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Patent number: 11015872Abstract: An additively manufactured heat transfer device is disclosed, including an enclosure portion with outer walls. The outer walls contain an inner channel configured to direct a flow of coolant fluid. The heat transfer device further includes a fluid intake port and a fluid outtake port, each connected to the first inner channel. The fluid intake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion into the inner channel, and the fluid outtake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion out of the inner channel. The inner channel is defined by internal walls, and the enclosure portion and the internal walls form a single additively manufactured unit.Type: GrantFiled: June 29, 2018Date of Patent: May 25, 2021Assignee: The Boeing CompanyInventors: Richard W. Aston, Matthew Joseph Herrmann, Michael John Langmack, Nicole M. Hastings, Sumit K. Purohit
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Patent number: 10907697Abstract: A mounting device is disclosed, including a first torsion bar structure having an elongated axis and opposing end portions connected by a middle portion. The mounting device further includes a second torsion bar structure having an elongated axis and opposing end portions connected by a middle portion. The middle portions of the first and second torsion bar structures are connected. The end portions of the first torsion bar structure are configured for attachment to a vehicle, and the end portions of the second torsion bar structure are configured for attachment to an accessory. The first and second torsion bar structures are configured to decrease transmission of vibration frequencies between the vehicle and the accessory.Type: GrantFiled: April 20, 2018Date of Patent: February 2, 2021Assignee: The Boeing CompanyInventors: Richard W. Aston, Michael John Langmack, Jazzmin P. Martinez, Emily Colleen Woods
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Publication number: 20200182398Abstract: An isolation coupler for coupling a functional element to a support structure includes a first bracket. The first bracket includes a number of first-bracket sides. The number of first-bracket sides forms a closed polygonal shape, in plan view. The isolation coupler further includes a number of isolators coupled to each one of the first-bracket sides. The isolation coupler also includes a second bracket. The second bracket includes a number of second-bracket sides. The second bracket sides are coupled to the isolators. The number of second-bracket sides is equal to the number of first-bracket sides and forms the closed polygonal shape, in plan view. The isolators separate each one of the first-bracket sides from a corresponding one of the second-bracket sides to attenuate a load transferred from the first bracket to the second bracket.Type: ApplicationFiled: December 10, 2018Publication date: June 11, 2020Applicant: The Boeing CompanyInventors: Richard W. Aston, Michael John Langmack, Anna M. Tomzynska, Matthew Herrmann, Emily C. Woods
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Publication number: 20200003497Abstract: An additively manufactured heat transfer device is disclosed, including an enclosure portion with outer walls. The outer walls contain an inner channel configured to direct a flow of coolant fluid. The heat transfer device further includes a fluid intake port and a fluid outtake port, each connected to the first inner channel. The fluid intake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion into the inner channel, and the fluid outtake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion out of the inner channel. The inner channel is defined by internal walls, and the enclosure portion and the internal walls form a single additively manufactured unit.Type: ApplicationFiled: June 29, 2018Publication date: January 2, 2020Applicant: The Boeing CompanyInventors: Richard W. Aston, Matthew Joseph Herrmann, Michael John Langmack, Nicole M. Hastings, Sumit K. Purohit
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Publication number: 20190323571Abstract: A mounting device is disclosed, including a first torsion bar structure having an elongated axis and opposing end portions connected by a middle portion. The mounting device further includes a second torsion bar structure having an elongated axis and opposing end portions connected by a middle portion. The middle portions of the first and second torsion bar structures are connected. The end portions of the first torsion bar structure are configured for attachment to a vehicle, and the end portions of the second torsion bar structure are configured for attachment to an accessory. The first and second torsion bar structures are configured to decrease transmission of vibration frequencies between the vehicle and the accessory.Type: ApplicationFiled: April 20, 2018Publication date: October 24, 2019Applicant: The Boeing CompanyInventors: Richard W. Aston, Michael John Langmack, Jazzmin P. Martinez, Emily Colleen Woods
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Publication number: 20190291186Abstract: An additively manufactured antenna device is disclosed, including a base portion and a body portion. The body portion is attached to the base portion and includes a lattice stiffening structure configured to eliminate secondary printing support.Type: ApplicationFiled: March 22, 2018Publication date: September 26, 2019Applicant: The Boeing CompanyInventors: Richard W. Aston, Martin W. Bieti, Michael John Langmack, Nicole M. Hastings, Nicole Diane Schoenborn
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Patent number: 10364860Abstract: Systems and methods for dampening dynamic loading between two bodies are described. An example dampening system includes a non-ferrous metal body attached to a second body and a stack of magnets attached to a third body. The stack of magnets is movably disposed within or around the non-ferrous metal body, and adjacent magnets are arranged in an opposed polar relationship, whereby relative movement of said second and third bodies is damped. An example method of dampening dynamic loading includes arranging a plurality of magnets along an axis to form at least one pair of magnets having an opposed polar relationship along the axis. The method further includes axially moving the at least one pair of magnets relative to a non-ferrous metal body, so as to dampen dynamic loading of a payload attached to a vehicle.Type: GrantFiled: December 8, 2017Date of Patent: July 30, 2019Assignee: The Boeing CompanyInventors: Steven F. Griffin, Richard W. Aston, Jazzmin P. Martinez, Michael John Langmack, Christopher R. Shurilla
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Publication number: 20190178325Abstract: Systems and methods for dampening dynamic loading between two bodies are described. An example dampening system includes a non-ferrous metal body attached to a second body and a stack of magnets attached to a third body. The stack of magnets is movably disposed within or around the non-ferrous metal body, and adjacent magnets are arranged in an opposed polar relationship, whereby relative movement of said second and third bodies is damped. An example method of dampening dynamic loading includes arranging a plurality of magnets along an axis to form at least one pair of magnets having an opposed polar relationship along the axis. The method further includes axially moving the at least one pair of magnets relative to a non-ferrous metal body, so as to dampen dynamic loading of a payload attached to a vehicle.Type: ApplicationFiled: December 8, 2017Publication date: June 13, 2019Inventors: Steven F. Griffin, Richard W. Aston, Jazzmin P. Martinez, Michael John Langmack, Christopher R. Shurilla
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Patent number: 9537340Abstract: An apparatus comprises a first plurality of walls, a second plurality of walls, and a plurality of channels formed by the first plurality of walls and the second plurality of walls. The second plurality of walls meets the first plurality of walls at substantially right angles and forms a housing with a first side and a second side. The plurality of channels extends through the housing from the first side to the second side. The plurality of channels has a first plurality of openings on the first side. The plurality of channels has a second plurality of openings on the second side. The plurality of channels has substantially a same shape and is configured to receive a plurality of battery cells.Type: GrantFiled: March 31, 2014Date of Patent: January 3, 2017Assignee: THE BOEING COMPANYInventors: Richard W. Aston, Michael John Langmack