Patents by Inventor Bart Stevens
Bart Stevens 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: 20240327585Abstract: Disclosed herein are methods and compositions for preparing a surface comprising thermoplastic or thermoset material to receive a polysulfide or polythioether sealant or coating, the method comprising applying to the surface an activating composition consisting of a tetraalkoxide of a Group 4 metal, a complex of an alkoxide of a Group 4 metal, or a combination thereof.Type: ApplicationFiled: June 11, 2024Publication date: October 3, 2024Inventors: Daniel James Cowan, Bart Stevens, Jason Alan Bolles, Robert Frederick Rivers
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Patent number: 12043716Abstract: Disclosed herein are methods and compositions for preparing a surface comprising thermoplastic or thermoset material to receive a polysulfide or polythioether sealant or coating, the method comprising applying to the surface an activating composition consisting of a tetraalkoxide of a Group 4 metal, a complex of an alkoxide of a Group 4 metal, or a combination thereof.Type: GrantFiled: August 14, 2019Date of Patent: July 23, 2024Assignee: The Boeing CompanyInventors: Daniel James Cowan, Bart Stevens, Jason Alan Bolles, Robert Frederick Rivers
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Patent number: 11891189Abstract: A seal-cover assembly for a structure including a first side and a second side opposing the first side. The seal-cover assembly includes a cap defining a recess, and an insert fixed to the cap within the recess to form a cover unit. The cover unit is configured to be secured to the first side of the structure. The seal-cover assembly includes a fastener configured to be disposed through the structure from the second side of the structure. The fastener is attached to the cover unit relative to the second side without accessing the first side of the structure. Additionally, an aircraft includes the structure and the seal-cover assembly as discussed above. Furthermore, a method of assembling the seal-cover assembly to the structure includes the cover unit secured to the first side of the structure such that an interior of the cover unit is inaccessible from the first side.Type: GrantFiled: November 15, 2021Date of Patent: February 6, 2024Assignee: The Boeing CompanyInventors: Daniel James Cowan, Bart Stevens
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Patent number: 11863670Abstract: Disclosed are memory encryption systems and methods that rotate encryption keys for robust resistance against side-channel-analysis (SCA)-based attacks on communication paths between an encryption engine within a trust boundary and an external memory component. A key data structure has a plurality of keys that are used to encrypt a plurality of memory blocks in the external memory. The memory blocks encrypted with the oldest key of the key data structure are identified. Encrypted data is read from the identified memory blocks. The encrypted data is decrypted from the identified memory blocks. The data is then re-encrypted using the selected key that is newer than the oldest key, and re-written to the identified memory blocks.Type: GrantFiled: April 4, 2020Date of Patent: January 2, 2024Assignee: Cryptography Research, Inc.Inventors: Mark Evan Marson, Michael Hutter, Bart Stevens
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Patent number: 11851213Abstract: Methods and structural gap filler for one up assembly of structures. Drilling debris generated between the first component and the second component during drilling of an injection hole are encapsulated by injecting a structural gap filler through the injection hole and between the first component and the second component.Type: GrantFiled: October 14, 2022Date of Patent: December 26, 2023Assignee: The Boeing CompanyInventors: Daniel James Cowan, Shane Edward Arthur, Marianne Elizabeth Wilkinson, Mark W. Cleary, Bart Stevens
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Patent number: 11754111Abstract: A protection seal cap for enclosing an end portion of a fastener which extends from a structure, which includes a cap member, which includes a sidewall that defines an interior space within the cap member. The sidewall forms a continuous wall member positioned within the cap member. The continuous wall member defines an opening providing access to the interior space. The continuous wall member is configured to create an interference compression fit between the end portion of the fastener and the continuous wall member.Type: GrantFiled: March 16, 2020Date of Patent: September 12, 2023Assignee: The Boeing CompanyInventors: Daniel J. Cowan, Bart Stevens
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Patent number: 11732743Abstract: A cap system for enclosing a metallic fastener assembly extending through a structure, which includes a first securement mechanism positioned about a periphery of a nut member of the metallic fastener assembly, wherein the first securement mechanism comprises a plurality of continuous grooves which extend about the periphery of the nut member. The cap system further includes a cap member which includes a sidewall having an inner surface which defines a cavity dimensioned to receive the nut member and defines a second securement mechanism complementary configured to engage the first securement mechanism positioned about the periphery of the nut member. The cap system also includes an end of the sidewall of the cap member defines an opening which provides the nut member to have access into the cavity.Type: GrantFiled: February 19, 2021Date of Patent: August 22, 2023Assignee: The Boeing CompanyInventors: Bart Stevens, Daniel J. Cowan, Sean Auffinger, Brandon Mulligan
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Publication number: 20230256515Abstract: A workpiece and associated method includes fabricating, employing an additive manufacturing process, a raw workpiece from aluminum alloy that includes silicon; heat-treating the raw workpiece to produce an intermediate workpiece, including subjecting the raw workpiece to a first temperature environment, wherein the first temperature environment agglomerates silicon particles disposed on a surface of the raw workpiece; cleaning the intermediate workpiece without removing the silicon particles agglomerated on the surface thereof; and applying a conversion coating onto the surface of the intermediate workpiece.Type: ApplicationFiled: April 20, 2023Publication date: August 17, 2023Applicant: The Boeing CompanyInventors: Bart Stevens, Bruce M. Griffin, Michael Howard-Edward Ware, Richard G. Wire, Paul N. Wilson, Benjamin S. Stephenson
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Patent number: 11725687Abstract: A cap system for enclosing a metallic fastener assembly extending through a structure, which includes a first securement mechanism positioned about a periphery of a washer of the metallic fastener assembly wherein the first securement mechanism includes a first tab member extending in a direction transverse to a plane of a surface of the washer and a second tab member extending in a direction transverse to the plane of the surface of the washer spaced apart from the first tab member about the periphery of the washer. Cap system further includes a cap member which includes a sidewall having an inner surface which defines a cavity dimensioned to receive the washer and defines a second securement mechanism complementary configured to engage the first securement mechanism; and an end of the sidewall of the cap member defines an opening which provides the washer to have access into the cavity.Type: GrantFiled: January 22, 2021Date of Patent: August 15, 2023Assignee: The Boeing CompanyInventors: Daniel J. Cowan, Bart Stevens, Sean Auffinger, Brandon Mulligan, Carl A. Weeks
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Publication number: 20230114159Abstract: An antimicrobial coating composition is disclosed. The antimicrobial coating composition also includes a polymer having a plurality of alkene units and a plurality of macroCTA polymer units. The composition also includes one or more reactive silanes, one or more wetting agents, and one or more solvents. A method for applying an antimicrobial coating composition is disclosed. The method for applying an antimicrobial coating composition may include contacting a polymer, one or more wetting agents, one or more solvents, and one or more reactive silanes with one another to prepare an antimicrobial coating composition, homogenizing the antimicrobial coating composition, applying the antimicrobial coating composition to a substrate, and allowing the antimicrobial coating composition to dry at ambient conditions.Type: ApplicationFiled: October 7, 2021Publication date: April 13, 2023Applicant: The Boeing CompanyInventors: Bart STEVENS, Kay Y. BLOHOWIAK, Christopher GARNIER
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Publication number: 20220182232Abstract: Disclosed are memory encryption systems and methods that rotate encryption keys for robust resistance against side-channel-analysis (SCA)-based attacks on communication paths between an encryption engine within a trust boundary and an external memory component. A key data structure has a plurality of keys that are used to encrypt a plurality of memory blocks in the external memory. The memory blocks encrypted with the oldest key of the key data structure are identified. Encrypted data is read from the identified memory blocks. The encrypted data is decrypted from the identified memory blocks. The data is then re-encrypted using the selected key that is newer than the oldest key, and re-written to the identified memory blocks.Type: ApplicationFiled: April 4, 2020Publication date: June 9, 2022Inventors: Mark Evan Marson, Michael Hutter, Bart Stevens
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Publication number: 20220153430Abstract: A seal-cover assembly for a structure including a first side and a second side opposing the first side. The seal-cover assembly includes a cap defining a recess, and an insert fixed to the cap within the recess to form a cover unit. The cover unit is configured to be secured to the first side of the structure. The seal-cover assembly includes a fastener configured to be disposed through the structure from the second side of the structure. The fastener is attached to the cover unit relative to the second side without accessing the first side of the structure. Additionally, an aircraft includes the structure and the seal-cover assembly as discussed above. Furthermore, a method of assembling the seal-cover assembly to the structure includes the cover unit secured to the first side of the structure such that an interior of the cover unit is inaccessible from the first side.Type: ApplicationFiled: November 15, 2021Publication date: May 19, 2022Applicant: The Boeing CompanyInventors: Daniel James Cowan, Bart Stevens
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Patent number: 11236777Abstract: A protective seal cap assembly for enclosing an end portion of a fastener extending through a structure, which includes a cap member. The cap member includes a sidewall which defines an opening and defines an interior space within the sidewall and aligned with the opening, wherein the sidewall defines a central axis. The cap member further includes at least one rib which extends away from an interior surface of the sidewall within the interior space and extends in a direction along the central axis of the cap member.Type: GrantFiled: May 6, 2019Date of Patent: February 1, 2022Assignee: THE BOEING COMPANYInventors: Bart Stevens, Daniel J. Cowan, Sean Auffinger
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Publication number: 20210285481Abstract: A protection seal cap for enclosing an end portion of a fastener which extends from a structure, which includes a cap member, which includes a sidewall that defines an interior space within the cap member. The sidewall forms a continuous wall member positioned within the cap member. The continuous wall member defines an opening providing access to the interior space. The continuous wall member is configured to create an interference compression fit between the end portion of the fastener and the continuous wall member.Type: ApplicationFiled: March 16, 2020Publication date: September 16, 2021Inventors: Daniel J. Cowan, Bart Stevens
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Publication number: 20210230726Abstract: A method for processing a raw workpiece into a final workpiece is described, wherein the raw workpiece includes a metallic structure including silicon particles dispersed therein. The raw workpiece is fabricated employing an additive manufacturing process, in one embodiment. The method includes heat-treating the raw workpiece to produce an intermediate workpiece, wherein the heat-treating includes subjecting the raw workpiece to a first temperature environment for a time period to produce an intermediate workpiece to form agglomerated silicon particles, wherein the agglomerated silicon particles are disposed on a surface of the raw workpiece. The method further includes removing the agglomerated silicon particles that are disposed on the surface of the intermediate workpiece.Type: ApplicationFiled: January 24, 2020Publication date: July 29, 2021Applicant: The Boeing CompanyInventors: Bart Stevens, Bruce M. Griffin, Michael Howard-Edward Ware, Richard G. Wire, Paul N. Wilson, Benjamin S. Stephenson
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Publication number: 20210190124Abstract: A cap system for enclosing a metallic fastener assembly extending through a structure, which includes a first securement mechanism positioned about a periphery of a nut member of the metallic fastener assembly, wherein the first securement mechanism comprises a plurality of continuous grooves which extend about the periphery of the nut member. The cap system further includes a cap member which includes a sidewall having an inner surface which defines a cavity dimensioned to receive the nut member and defines a second securement mechanism complementary configured to engage the first securement mechanism positioned about the periphery of the nut member. The cap system also includes an end of the sidewall of the cap member defines an opening which provides the nut member to have access into the cavity.Type: ApplicationFiled: February 19, 2021Publication date: June 24, 2021Inventors: Bart Stevens, Daniel J. Cowan, Sean Auffinger, Brandon Mulligan
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Publication number: 20210164513Abstract: A cap system for enclosing a metallic fastener assembly extending through a structure, which includes a first securement mechanism positioned about a periphery of a washer of the metallic fastener assembly wherein the first securement mechanism includes a first tab member extending in a direction transverse to a plane of a surface of the washer and a second tab member extending in a direction transverse to the plane of the surface of the washer spaced apart from the first tab member about the periphery of the washer. Cap system further includes a cap member which includes a sidewall having an inner surface which defines a cavity dimensioned to receive the washer and defines a second securement mechanism complementary configured to engage the first securement mechanism; and an end of the sidewall of the cap member defines an opening which provides the washer to have access into the cavity.Type: ApplicationFiled: January 22, 2021Publication date: June 3, 2021Inventors: Daniel J. Cowan, Bart Stevens, Sean Auffinger, Brandon Mulligan, Carl A. Weeks
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Patent number: 10989244Abstract: A cap assembly for enclosing a metallic fastener which extends through a structure. The assembly includes a housing having an inner wall and an outer wall which extends about and is spaced apart from the inner wall defining a space positioned between the inner wall and outer wall. The assembly further includes a plunger member with a side wall portion secured to an end wall portion. The side wall portion of the plunger member has a thickness dimension smaller than a distance between the inner wall and the outer wall to position the sidewall portion of the plunger member within the space. With the side wall portion positioned within the space, the end wall portion is positioned in alignment with the inner wall and with an opening defined by and through the inner wall.Type: GrantFiled: November 20, 2018Date of Patent: April 27, 2021Assignee: THE BOEING COMPANYInventors: Sean Auffinger, Bart Stevens
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Patent number: 10982704Abstract: A containment cap assembly for enclosing a metallic fastener extending through a structure includes an inner cap with a projection extending from an outer surface of the inner cap and an outer cap includes a first end which defines an opening and includes an inner surface which defines a first space within the outer cap in communication with the opening. A dimension of the opening and of the first space defined by the inner surface of the outer cap are each greater than a dimension defined by the outer surface of the inner cap such that with positioning the inner cap within the outer cap, a second space is defined between the outer cap and the inner cap. A slot of the outer cap extends first curvilinear direction such that the projection positioned within the slot moves along first curvilinear direction with moving the inner cap into the outer cap.Type: GrantFiled: January 3, 2019Date of Patent: April 20, 2021Assignee: THE BOEING COMPANYInventors: Sean Auffinger, Bart Stevens
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Patent number: 10962043Abstract: A cap system for enclosing a metallic fastener assembly extending through a structure includes a first securement mechanism positioned about a periphery of a nut member of the metallic fastener assembly, wherein the first securement mechanism comprises threads which are interrupted as the threads extend about the periphery of the nut member and a cap member. The cap member includes a sidewall having an inner surface which defines a cavity dimensioned to receive the nut member and defines a second securement mechanism complementary configured to engage the first securement mechanism positioned about the periphery of the nut member and an end of the sidewall of the cap member defines an opening which provides the nut member to have access into the cavity.Type: GrantFiled: April 24, 2018Date of Patent: March 30, 2021Assignee: THE BOEING COMPANYInventors: Bart Stevens, Daniel J. Cowan, Sean Auffinger, Brandon Mulligan