Patents by Inventor Tyler Andre Kafentzis
Tyler Andre Kafentzis 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: 12296575Abstract: An anisotropic composite material assembly comprising a first layer with a tensile modulus different from its compressive modulus and that exhibits variable modulus behavior. The first layer elastically buckle under compressions. A second layer has a tensile modulus substantially the same as its compressive modulus. The first and second layers are joined together, and the assembly is bendable in a first direction with an outer surface of the first layer being in compression and the assembly has a first bending stiffness during bending in the first direction. The assembly is bendable in a second direction opposite the first direction with the outer surface of the first layer being in tension, and the assembly has a second bending stiffness greater than the first bending stiffness during bending in the second direction.Type: GrantFiled: December 22, 2023Date of Patent: May 13, 2025Assignee: Carbitex, Inc.Inventors: Junus Ali Khan, Tyler Andre Kafentzis, Kevin Lynn Simmons, Keshava Bhamidipaty
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Publication number: 20240246314Abstract: An anisotropic composite material assembly comprising a first layer with a tensile modulus different from its compressive modulus and that exhibits variable modulus behavior. The first layer elastically buckle under compressions. A second layer has a tensile modulus substantially the same as its compressive modulus. The first and second layers are joined together, and the assembly is bendable in a first direction with an outer surface of the first layer being in compression and the assembly has a first bending stiffness during bending in the first direction. The assembly is bendable in a second direction opposite the first direction with the outer surface of the first layer being in tension, and the assembly has a second bending stiffness greater than the first bending stiffness during bending in the second direction.Type: ApplicationFiled: December 22, 2023Publication date: July 25, 2024Inventors: Junus Ali Khan, Tyler Andre Kafentzis, Kevin Lynn Simmons, Keshava Bhamidipaty
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Patent number: 11981116Abstract: An anisotropic composite material assembly comprising a first layer with a tensile modulus different from its compressive modulus and that exhibits variable modulus behavior. The first layer elastically buckle under compressions. A second layer has a tensile modulus substantially the same as its compressive modulus. The first and second layers are joined together, and the assembly is bendable in a first direction with an outer surface of the first layer being in compression and the assembly has a first bending stiffness during bending in the first direction. The assembly is bendable in a second direction opposite the first direction with the outer surface of the first layer being in tension, and the assembly has a second bending stiffness greater than the first bending stiffness during bending in the second direction.Type: GrantFiled: July 29, 2022Date of Patent: May 14, 2024Assignee: Carbitex, Inc.Inventors: Junus Ali Khan, Tyler Andre Kafentzis, Kevin Lynn Simmons, Keshava Bhamidipaty
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Publication number: 20230123404Abstract: This invention relates generally to flexible materials, especially those made of carbon fiber. The materials exhibit a first flexural modulus over a first range of flexural strain and a second flexural modulus over a second range of flexural strain. The materials provide advantages when used in an article of manufacture in which the performance may be improved by having a different flexural modulus depending on the amount of flexural strain, and thus dislocation, of the material.Type: ApplicationFiled: October 15, 2021Publication date: April 20, 2023Applicant: Epsitek LLCInventor: Tyler Andre Kafentzis
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Publication number: 20230105878Abstract: An anisotropic composite material assembly comprising a first layer with a tensile modulus different from its compressive modulus and that exhibits variable modulus behavior. The first layer elastically buckle under compressions. A second layer has a tensile modulus substantially the same as its compressive modulus. The first and second layers are joined together, and the assembly is bendable in a first direction with an outer surface of the first layer being in compression and the assembly has a first bending stiffness during bending in the first direction. The assembly is bendable in a second direction opposite the first direction with the outer surface of the first layer being in tension, and the assembly has a second bending stiffness greater than the first bending stiffness during bending in the second direction.Type: ApplicationFiled: July 29, 2022Publication date: April 6, 2023Inventors: Junus Ali Khan, Tyler Andre Kafentzis, Kevin Lynn Simmons, Keshava Bhamidipaty
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Patent number: 11407200Abstract: An anisotropic composite material assembly comprising a first layer with a tensile modulus different from its compressive modulus and that exhibits variable modulus behavior. The first layer elastically buckle under compressions. A second layer has a tensile modulus substantially the same as its compressive modulus. The first and second layers are joined together, and the assembly is bendable in a first direction with an outer surface of the first layer being in compression and the assembly has a first bending stiffness during bending in the first direction. The assembly is bendable in a second direction opposite the first direction with the outer surface of the first layer being in tension, and the assembly has a second bending stiffness greater than the first bending stiffness during bending in the second direction.Type: GrantFiled: September 28, 2020Date of Patent: August 9, 2022Assignee: Carbitex, Inc.Inventors: Junus Ali Khan, Tyler Andre Kafentzis, Kevin Lynn Simmons, Keshava Bhamidipaty
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Publication number: 20210162707Abstract: An anisotropic composite material assembly comprising a first layer with a tensile modulus different from its compressive modulus and that exhibits variable modulus behavior. The first layer elastically buckle under compressions. A second layer has a tensile modulus substantially the same as its compressive modulus. The first and second layers are joined together, and the assembly is bendable in a first direction with an outer surface of the first layer being in compression and the assembly has a first bending stiffness during bending in the first direction. The assembly is bendable in a second direction opposite the first direction with the outer surface of the first layer being in tension, and the assembly has a second bending stiffness greater than the first bending stiffness during bending in the second direction.Type: ApplicationFiled: September 28, 2020Publication date: June 3, 2021Inventors: Junus Ali Khan, Tyler Andre Kafentzis, Kevin Lynn Simmons, Keshava Bhamidipaty
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Patent number: 10786973Abstract: An anisotropic composite material assembly comprising a first layer with a tensile modulus different from its compressive modulus and that exhibits variable modulus behavior. The first layer elastically buckle under compressions. A second layer has a tensile modulus substantially the same as its compressive modulus. The first and second layers are joined together, and the assembly is bendable in a first direction with an outer surface of the first layer being in compression and the assembly has a first bending stiffness during bending in the first direction. The assembly is bendable in a second direction opposite the first direction with the outer surface of the first layer being in tension, and the assembly has a second bending stiffness greater than the first bending stiffness during bending in the second direction.Type: GrantFiled: March 30, 2018Date of Patent: September 29, 2020Assignee: Carbitex, Inc.Inventors: Kevin Lynn Simmons, Junus Ali Khan, Tyler Andre Kafentzis, Keshava Bhamidipaty
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Patent number: 10301769Abstract: An axially stretchable fiber-reinforced composite material, comprising an elastically deformable matrix having a low modulus of elasticity, and a fabric core encapsulated by the matrix. The core comprises first fibers interlaced with second fibers, with the first fibers being in a non-parallel orientation relative to the material's longitudinal axis, and the second fibers are non-parallel relative to the first fibers when the composite material is in a retracted position. The composite material is stretchable between the retracted and extended positions. The fibers have a high modulus of elasticity. The composite material has a non-linear modulus relative to elongation of the composite material between the retraced and extended positions. Movement of the material toward the extended position causes the first and second fibers to rotate relative to each other and in a direction toward alignment with the longitudinal axis, and the matrix material biases the composite material toward the retracted position.Type: GrantFiled: April 21, 2016Date of Patent: May 28, 2019Assignee: Carbitex, Inc.Inventors: Kevin Lynn Simmons, Tyler Andre Kafentzis, Junus Ali Khan
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Patent number: 10093085Abstract: Provided are methods for preparing fabric laminated with polymer film(s) and the laminated fabric prepared according to the methods disclosed herein. The laminated fabric has flexibility similar to fabric not laminated with polymer films and improved adhesion and tensile strength.Type: GrantFiled: June 10, 2016Date of Patent: October 9, 2018Assignee: Carbitex, Inc.Inventors: Kevin Lynn Simmons, Tyler Andre Kafentzis, Junus Ali Khan, Tyler Ross Carpenter, Matthew Patrick Westman
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Publication number: 20180222148Abstract: An anisotropic composite material assembly comprising a first layer with a tensile modulus different from its compressive modulus and that exhibits variable modulus behavior. The first layer elastically buckle under compressions. A second layer has a tensile modulus substantially the same as its compressive modulus. The first and second layers are joined together, and the assembly is bendable in a first direction with an outer surface of the first layer being in compression and the assembly has a first bending stiffness during bending in the first direction. The assembly is bendable in a second direction opposite the first direction with the outer surface of the first layer being in tension, and the assembly has a second bending stiffness greater than the first bending stiffness during bending in the second direction.Type: ApplicationFiled: March 30, 2018Publication date: August 9, 2018Inventors: Kevin Lynn Simmons, Junus Ali Khan, Tyler Andre Kafentzis, Keshava Bhamidipaty
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Patent number: 9993993Abstract: An anisotropic composite material assembly comprising a first layer with a tensile modulus different from its compressive modulus and that exhibits variable modulus behavior. The first layer elastically buckle under compressions. A second layer has a tensile modulus substantially the same as its compressive modulus. The first and second layers are joined together, and the assembly is bendable in a first direction with an outer surface of the first layer being in compression and the assembly has a first bending stiffness during bending in the first direction. The assembly is bendable in a second direction opposite the first direction with the outer surface of the first layer being in tension, and the assembly has a second bending stiffness greater than the first bending stiffness during bending in the second direction.Type: GrantFiled: July 26, 2016Date of Patent: June 12, 2018Assignee: Carbitex, Inc.Inventors: Kevin Lynn Simmons, Junus Ali Khan, Tyler Andre Kafentzis, Keshava Bhamidipaty
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Publication number: 20170157893Abstract: An anisotropic composite material assembly comprising a first layer with a tensile modulus different from its compressive modulus and that exhibits variable modulus behavior. The first layer elastically buckle under compressions. A second layer has a tensile modulus substantially the same as its compressive modulus. The first and second layers are joined together, and the assembly is bendable in a first direction with an outer surface of the first layer being in compression and the assembly has a first bending stiffness during bending in the first direction. The assembly is bendable in a second direction opposite the first direction with the outer surface of the first layer being in tension, and the assembly has a second bending stiffness greater than the first bending stiffness during bending in the second direction.Type: ApplicationFiled: July 26, 2016Publication date: June 8, 2017Inventors: Kevin Lynn Simmons, Junus Ali Khan, Tyler Andre Kafentzis, Keshava Bhamidipaty
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Publication number: 20160361909Abstract: Provided are methods for preparing fabric laminated with polymer film(s) and the laminated fabric prepared according to the methods disclosed herein. The laminated fabric has flexibility similar to fabric not laminated with polymer films and improved adhesion and tensile strength.Type: ApplicationFiled: June 10, 2016Publication date: December 15, 2016Inventors: Kevin Lynn Simmons, Tyler Andre Kafentzis, Junus Ali Khan, Tyler Ross Carpenter, Matthew Patrick Westman
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Publication number: 20160312398Abstract: An axially stretchable fiber-reinforced composite material, comprising an elastically deformable matrix having a low modulus of elasticity, and a fabric core encapsulated by the matrix. The core comprises first fibers interlaced with second fibers, with the first fibers being in a non-parallel orientation relative to the material's longitudinal axis, and the second fibers are non-parallel relative to the first fibers when the composite material is in a retracted position. The composite material is stretchable between the retracted and extended positions. The fibers have a high modulus of elasticity. The composite material has a non-linear modulus relative to elongation of the composite material between the retraced and extended positions. Movement of the material toward the extended position causes the first and second fibers to rotate relative to each other and in a direction toward alignment with the longitudinal axis, and the matrix material biases the composite material toward the retracted position.Type: ApplicationFiled: April 21, 2016Publication date: October 27, 2016Inventors: Kevin Lynn Simmons, Tyler Andre Kafentzis, Junus Ali Khan