Patents by Inventor Jazzmin P. Martinez
Jazzmin P. Martinez 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: 11536352Abstract: A drive train linkage includes a drive arm having a drive arm pivot axis, a driven arm having a driven arm pivot axis, at least one first coupling member extending between and being rotatably coupled to each of the drive arm and driven arm, and at least one second coupling member extending between and being rotatably coupled to each of the drive arm and driven arm so that the at least one second coupling member opposes the at least one first coupling member, where the at least one first coupling member and the at least one second coupling member are coupled to both the drive arm and the driven arm so to form a substantially zero mechanical deadband coupling between the drive arm and the driven arm.Type: GrantFiled: September 26, 2018Date of Patent: December 27, 2022Assignee: The Boeing CompanyInventors: Richard W. Aston, Jazzmin P. Martinez, Michael J. Langmack, Emily C. Woods
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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: 20200096081Abstract: A drive train linkage includes a drive arm having a drive arm pivot axis, a driven arm having a driven arm pivot axis, at least one first coupling member extending between and being rotatably coupled to each of the drive arm and driven arm, and at least one second coupling member extending between and being rotatably coupled to each of the drive arm and driven arm so that the at least one second coupling member opposes the at least one first coupling member, where the at least one first coupling member and the at least one second coupling member are coupled to both the drive arm and the driven arm so to form a substantially zero mechanical deadband coupling between the drive arm and the driven arm.Type: ApplicationFiled: September 26, 2018Publication date: March 26, 2020Inventors: Richard W. ASTON, Jazzmin P. MARTINEZ, Michael J. LANGMACK, Emily C. WOODS
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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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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: 10087970Abstract: A sealant containment assembly for enclosing fasteners disposed within a confined space. The sealant containment assembly includes a first containment member and a second containment member that extend between two surfaces. The first and second containment members each include structure-engaging ends for engaging a structural member and the first and second containment members each include enclosure ends that connect the first and second containment members together to enclose the fasteners within a confined space defined by the first and second containment members, the first and second surfaces, the structural member and the connected enclosure ends. The assembly also includes at least one injection port disposed outside of the confined space but is in communication with at least one distribution port disposed inside the confined space for filling the confined space with sealant, thereby embedding the fasteners in sealant.Type: GrantFiled: April 29, 2016Date of Patent: October 2, 2018Assignee: The Boeing CompanyInventors: Richard W. Aston, Anna M. Tomzynska, Michael J. Langmack, Jazzmin P. Martinez
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Patent number: 9897130Abstract: This disclosure provides a cap assembly for encapsulating a fastener or portion of a fastener that protrudes from a surface and into a confined space. The cap assembly includes a plurality of nested sections that telescope a collapsed configuration to an extended configuration. The plurality of nested sections includes a base section that includes a base rim that engages the surface in the extended configuration. The plurality of nested sections also includes an end section that has an end wall. The end wall and the base rim define a length of the cap assembly in the extended configuration that is sufficient to encapsulate the fastener within the cap assembly with the base rim engaging the surface and the end wall spaced apart from a distal end of the fastener.Type: GrantFiled: April 15, 2016Date of Patent: February 20, 2018Assignee: The Boeing CompanyInventors: Richard W. Aston, Anna M. Tomzynska, Michael J. Langmack, Jazzmin P. Martinez
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Publication number: 20170314603Abstract: A sealant containment assembly for enclosing fasteners disposed within a confined space. The sealant containment assembly includes a first containment member and a second containment member that extend between two surfaces. The first and second containment members each include structure-engaging ends for engaging a structural member and the first and second containment members each include enclosure ends that connect the first and second containment members together to enclose the fasteners within a confined space defined by the first and second containment members, the first and second surfaces, the structural member and the connected enclosure ends. The assembly also includes at least one injection port disposed outside of the confined space but is in communication with at least one distribution port disposed inside the confined space for filling the confined space with sealant, thereby embedding the fasteners in sealant.Type: ApplicationFiled: April 29, 2016Publication date: November 2, 2017Applicant: The Boeing CompanyInventors: Richard W. Aston, Anna M. Tomzynska, Michael J. Langmack, Jazzmin P. Martinez
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Publication number: 20170298979Abstract: This disclosure provides a cap assembly for encapsulating a fastener or portion of a fastener that protrudes from a surface and into a confined space. The cap assembly includes a plurality of nested sections that telescope a collapsed configuration to an extended configuration. The plurality of nested sections includes a base section that includes a base rim that engages the surface in the extended configuration. The plurality of nested sections also includes an end section that has an end wall. The end wall and the base rim define a length of the cap assembly in the extended configuration that is sufficient to encapsulate the fastener within the cap assembly with the base rim engaging the surface and the end wall spaced apart from a distal end of the fastener.Type: ApplicationFiled: April 15, 2016Publication date: October 19, 2017Applicant: The Boeing CompanyInventors: Richard W. Aston, Anna M. Tomzynska, Michael J. Langmack, Jazzmin P. Martinez