Patents by Inventor Jack J. Esposito
Jack J. Esposito 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: 10190954Abstract: A composite test coupon includes a plurality of plies. The plurality of plies include first ply layers and second ply layers. The first ply layers have first fibers and a substantially uniform matrix material associated with the first fibers. The second ply layers have second fibers and a pre-stressed matrix material associated with the second fibers. The first fibers are oriented in a first direction, and the second fibers are oriented in a second direction that is different from the first direction. The pre-stressed matrix material includes stress induced cracks between the second fibers of each of the second ply layers.Type: GrantFiled: June 1, 2015Date of Patent: January 29, 2019Assignee: THE BOEING COMPANYInventors: Jack J. Esposito, Samuel J. Tucker
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Patent number: 10078041Abstract: One example of the present disclosure relates to a coupon. The coupon includes a first surface with a first circular channel and a second surface opposite and parallel to the first surface. The second surface is spaced a distance D0 from the first surface and includes a second circular channel concentric with the first circular channel. The coupon also includes a toroidal portion between the first circular channel and the second circular channel. The toroidal portion includes a rectangular sectional portion.Type: GrantFiled: July 6, 2017Date of Patent: September 18, 2018Assignee: The Boeing CompanyInventors: Joshua Shane Dustin, Jack J. Esposito, Alan W. Baker
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Patent number: 10035323Abstract: An article comprises a multi-directional textile of first reinforcing fiber tows extending in a first direction and second reinforcing fiber tows extending in a second direction. Filaments in the first fiber tows extend past a boundary of the textile and are spread. The tows are embedded in resin.Type: GrantFiled: September 23, 2013Date of Patent: July 31, 2018Assignee: The Boeing CompanyInventors: Kenneth H. Griess, Jack J. Esposito, Gary E. Georgeson
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Publication number: 20170307491Abstract: One example of the present disclosure relates to a coupon. The coupon includes a first surface with a first circular channel and a second surface opposite and parallel to the first surface. The second surface is spaced a distance D0 from the first surface and includes a second circular channel concentric with the first circular channel. The coupon also includes a toroidal portion between the first circular channel and the second circular channel. The toroidal portion includes a rectangular sectional portion.Type: ApplicationFiled: July 6, 2017Publication date: October 26, 2017Applicant: The Boeing CompanyInventors: Joshua Shane Dustin, Jack J. Esposito, Alan W. Baker
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Patent number: 9726586Abstract: One example of the present disclosure relates to a coupon. The coupon includes a first surface with a first circular channel and a second surface opposite and parallel to the first surface. The second surface is spaced a distance D0 from the first surface and includes a second circular channel concentric with the first circular channel. The coupon also includes a toroidal portion between the first circular channel and the second circular channel. The toroidal portion includes a rectangular sectional portion.Type: GrantFiled: July 9, 2014Date of Patent: August 8, 2017Assignee: The Boeing CompanyInventors: Joshua Shane Dustin, Jack J. Esposito, Alan W. Baker
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Publication number: 20170182738Abstract: A method and apparatus for forming a composite filler is presented. The method comprises cutting a number of layers from a composite material. The method also aligns the number of layers to form a composite filler having a cross-sectional shape. Each of the number of layers has fibers in plane with the cross-sectional shape.Type: ApplicationFiled: March 15, 2017Publication date: June 29, 2017Inventors: Kenneth H. Griess, Jack J. Esposito
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Patent number: 9630376Abstract: A method and apparatus for forming a composite filler is presented. The method comprises cutting a number of layers from a composite material. The method also aligns the number of layers to form a composite filler having a cross-sectional shape. Each of the number of layers has fibers in plane with the cross-sectional shape.Type: GrantFiled: September 22, 2014Date of Patent: April 25, 2017Assignee: THE BOEING COMPANYInventors: Kenneth H. Griess, Jack J. Esposito
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Publication number: 20160349160Abstract: A composite test coupon includes a plurality of plies. The plurality of plies include first ply layers and second ply layers. The first ply layers have first fibers and a substantially uniform matrix material associated with the first fibers. The second ply layers have second fibers and a pre-stressed matrix material associated with the second fibers. The first fibers are oriented in a first direction, and the second fibers are oriented in a second direction that is different from the first direction. The pre-stressed matrix material includes stress induced cracks between the second fibers of each of the second ply layers.Type: ApplicationFiled: June 1, 2015Publication date: December 1, 2016Inventors: Jack J. Esposito, Samuel J. Tucker
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Patent number: 9464975Abstract: A particular composite test specimen includes a first tab, a second tab, and a gage section between the first tab and the second tab. The first tab, the second tab, and the gage section are machined from a composite test blank. The composite test blank includes a plurality of plies arranged with first ply layers having fibers oriented in a first direction and second ply layers having fibers oriented in a second direction, where the first direction is different than the second direction.Type: GrantFiled: August 13, 2014Date of Patent: October 11, 2016Assignee: The Boeing CompanyInventors: Jack J. Esposito, Joshua S. Dustin
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Publication number: 20160082694Abstract: A method and apparatus for forming a composite filler is presented. The method comprises cutting a number of layers from a composite material. The method also aligns the number of layers to form a composite filler having a cross-sectional shape. Each of the number of layers has fibers in plane with the cross-sectional shape.Type: ApplicationFiled: September 22, 2014Publication date: March 24, 2016Inventors: Kenneth H. Griess, Jack J. Esposito
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Publication number: 20160047723Abstract: A particular composite test specimen includes a first tab, a second tab, and a gage section between the first tab and the second tab. The first tab, the second tab, and the gage section are machined from a composite test blank. The composite test blank includes a plurality of plies arranged with first ply layers having fibers oriented in a first direction and second ply layers having fibers oriented in a second direction, where the first direction is different than the second direction.Type: ApplicationFiled: August 13, 2014Publication date: February 18, 2016Inventors: Jack J. Esposito, Joshua S. Dustin
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Patent number: 9239236Abstract: An alignment apparatus for aligning a test panel with a testing machine may include a laser measuring system and an adjustment mechanism. The laser measuring system may include at least one laser measuring device coupled to a test fixture and/or a testing machine. The laser measuring system may generate laser measurement data representative of an orientation of a test panel relative to a platen and/or a loading axis of the testing machine. The adjustment mechanism may adjust, based on the laser measurement data, a location and/or orientation of the test panel relative to the platen and/or the loading axis in a manner such that the test panel is moved into substantially alignment with the platen and/or the loading axis.Type: GrantFiled: February 19, 2014Date of Patent: January 19, 2016Assignee: The Boeing CompanyInventors: Kenneth H. Griess, Jack J. Esposito
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Publication number: 20160011089Abstract: One example of the present disclosure relates to a coupon. The coupon includes a first surface with a first circular channel and a second surface opposite and parallel to the first surface. The second surface is spaced a distance D0 from the first surface and includes a second circular channel concentric with the first circular channel. The coupon also includes a toroidal portion between the first circular channel and the second circular channel. The toroidal portion includes a rectangular sectional portion.Type: ApplicationFiled: July 9, 2014Publication date: January 14, 2016Applicant: The Boeing CompanyInventors: Joshua Shane Dustin, Jack J. Esposito, Alan W. Baker
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Publication number: 20150233709Abstract: An alignment apparatus for aligning a test panel with a testing machine may include a laser measuring system and an adjustment mechanism. The laser measuring system may include at least one laser measuring device coupled to a test fixture and/or a testing machine. The laser measuring system may generate laser measurement data representative of an orientation of a test panel relative to a platen and/or a loading axis of the testing machine. The adjustment mechanism may adjust, based on the laser measurement data, a location and/or orientation of the test panel relative to the platen and/or the loading axis in a manner such that the test panel is moved into substantially alignment with the platen and/or the loading axis.Type: ApplicationFiled: February 19, 2014Publication date: August 20, 2015Applicant: The Boeing CompanyInventors: Kenneth H. Griess, Jack J. Esposito
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Publication number: 20150086745Abstract: An article comprises a multi-directional textile of first reinforcing fiber tows extending in a first direction and second reinforcing fiber tows extending in a second direction. Filaments in the first fiber tows extend past a boundary of the textile and are spread. The tows are embedded in resin.Type: ApplicationFiled: September 23, 2013Publication date: March 26, 2015Applicant: The Boeing CompanyInventors: Kenneth H. Griess, Jack J. Esposito, Gary E. Georgeson
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Patent number: 8707798Abstract: A testing apparatus for characterizing a tension strength of a fillet bond of a test specimen may include a lower fixture and an upper fixture. The test specimen may include a skin component bonded to a stiffener component. The lower fixture may maintain the stiffener component in a fixed position. The upper fixture may engage the skin component at a pair of discrete engagement locations on opposite sides of the fillet bond. The upper fixture may be mechanically coupled to a gimbal joint and may substantially isolate the filet bond from asymmetric bending during application of a tension test load to the fillet bond.Type: GrantFiled: June 25, 2012Date of Patent: April 29, 2014Assignee: The Boeing CompanyInventors: Paul S. Gregg, Brian S. Kasperson, Jack J. Esposito
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Publication number: 20130340534Abstract: A testing apparatus for characterizing a tension strength of a fillet bond of a test specimen may include a lower fixture and an upper fixture. The test specimen may include a skin component bonded to a stiffener component. The lower fixture may maintain the stiffener component in a fixed position. The upper fixture may engage the skin component at a pair of discrete engagement locations on opposite sides of the fillet bond. The upper fixture may be mechanically coupled to a gimbal joint and may substantially isolate the filet bond from asymmetric bending during application of a tension test load to the fillet bond.Type: ApplicationFiled: June 25, 2012Publication date: December 26, 2013Applicant: THE BOEING COMPANYInventors: Paul S. Gregg, Brian S. Kasperson, Jack J. Esposito