Patents by Inventor Jonathan David Embler
Jonathan David Embler 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: 11939086Abstract: A fuel tank comprises an interior wall, a sump, and a baffle that comprises a center fitting, a full-length containment petal, a partial-length containment petal, a dump tube. The full-length containment petal comprises a full-length side edge, extending radially outward from the center fitting. The partial-length containment petal comprises a partial-length side edge, extending radially outward from the center fitting. The dump tube is connected to the sump. The full-length side edge of the full-length containment petal is longer than the partial-length side edge of the partial-length containment petal. All of the partial-length side edge of the partial-length containment petal is attached to a linear portion of the full-length side edge of the full-length containment petal.Type: GrantFiled: August 18, 2021Date of Patent: March 26, 2024Assignee: The Boeing CompanyInventors: Jonathan David Embler, Tin Anh Luu, Morgan Ashley Lewis, John Matthew Nichols, Keith Charles Kreutztrager, Chinh Manh Cao, Jonathan Edward Toomey, Martin Edward Lozano, Alfredo Lopez
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Patent number: 11807353Abstract: A system and method for sending signals at temperatures associated with hypersonic speeds. A window system in a hypersonic aircraft is provided. The window system comprises a transmissive window in an aeroshell of the hypersonic aircraft, a thermal seal, a sensor, and a sensor housing assembly enclosing the sensor. The transmissive window comprises a facesheet and insulating material adjacent to the facesheet. The thermal seal surrounds a perimeter of the facesheet and seals the facesheet to the aeroshell. The window system is radio-frequency transparent at temperatures associated with hypersonic speeds. The window system is configured to operate at an insertion loss of less than one decibel at the hypersonic speeds.Type: GrantFiled: February 1, 2022Date of Patent: November 7, 2023Assignee: The Boeing CompanyInventors: Michael John Best, Sangvavann Heng, Tai Anh Lam, Peter Shaw, Jonathan David Embler
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Publication number: 20230242236Abstract: A system and method for sending signals at temperatures associated with hypersonic speeds. A window system in a hypersonic aircraft is provided. The window system comprises a transmissive window in an aeroshell of the hypersonic aircraft, a thermal seal, a sensor, and a sensor housing assembly enclosing the sensor. The transmissive window comprises a facesheet and insulating material adjacent to the facesheet. The thermal seal surrounds a perimeter of the facesheet and seals the facesheet to the aeroshell. The window system is radio-frequency transparent at temperatures associated with hypersonic speeds. The window system is configured to operate at an insertion loss of less than one decibel at the hypersonic speeds.Type: ApplicationFiled: February 1, 2022Publication date: August 3, 2023Inventors: Michael John Best, Sangvavann Heng, Tai Anh Lam, Peter Shaw, Jonathan David Embler
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Publication number: 20220258600Abstract: A composite tank for a reusable launch vehicle comprises a composite wall, having a first coefficient of thermal expansion. The composite wall comprises a first end, a second end, a central axis, which passes through the first end and through the second end, and a cylindrical interior surface. The composite tank also comprises slosh baffles, formed from a second material, having a second coefficient of thermal expansion that is different from the first coefficient of thermal expansion. Each of the slosh baffles is attached to the cylindrical interior surface of the composite wall. Each of the slosh baffles is annular and is separated from the cylindrical interior surface of the composite wall by a radial gap, selected, in part, based on a difference between the first coefficient of thermal expansion and the second coefficient of thermal expansion. The radial gap is configured to change responsive to changes in temperature of the composite tank.Type: ApplicationFiled: August 18, 2021Publication date: August 18, 2022Applicant: The Boeing CompanyInventors: Jonathan David Embler, John Matthew Nichols, Glenn William Torres, Jacob Ryan Szczudlak, William Preston Keith, Tin Anh Luu, Morgan Ashley Lewis, Keith Charles Kreutztrager, Jonathan Edward Toomey, Juan Carlos Guzman
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Publication number: 20220258874Abstract: A fuel tank comprises an interior wall, a sump, and a baffle that comprises a center fitting, a full-length containment petal, a partial-length containment petal, a dump tube. The full-length containment petal comprises a full-length side edge, extending radially outward from the center fitting. The partial-length containment petal comprises a partial-length side edge, extending radially outward from the center fitting. The dump tube is connected to the sump. The full-length side edge of the full-length containment petal is longer than the partial-length side edge of the partial-length containment petal. All of the partial-length side edge of the partial-length containment petal is attached to a linear portion of the full-length side edge of the full-length containment petal.Type: ApplicationFiled: August 18, 2021Publication date: August 18, 2022Applicant: The Boeing CompanyInventors: Jonathan David Embler, Tin Anh Luu, Morgan Ashley Lewis, John Matthew Nichols, Keith Charles Kreutztrager, Chinh Manh Cao, Jonathan Edward Toomey, Martin Edward Lozano, Alfredo Lopez
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Patent number: 8894919Abstract: A method for adding insulation or bulk absorbers into high temperature sandwich structures following fabrication is presented. A slurry of ceramic fibers and/or particles, opacified particles, fugitive fibers, organic binders and inorganic binders is prepared as an aqueous solution. The slurry is cast within a prepared sandwich structure, dried, and heated to form a low density ceramic core material to provide insulation or noise absorption. Following incorporation of the ceramic material, aerogels or phase change materials may also be added to provide additional thermal management benefits.Type: GrantFiled: July 18, 2012Date of Patent: November 25, 2014Assignee: The Boeing CompanyInventors: Leanne L. Lehman, Vann Heng, James Philip Ledesma, Jr., Jonathan David Embler
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Patent number: 8745819Abstract: Apparatus and methods provide for a bushing that compensates for thermal expansion and contraction to maintain a preload on a corresponding structure at various operating temperatures. According to embodiments described herein, a bushing may include two bushing components coupled to a load compensation sleeve between the two bushing components. The load compensation sleeve may have a coefficient of thermal expansion (CTE) greater than the two bushing components and the corresponding abutting structure. The configuration of the bushing components and load compensation sleeve, along with the corresponding CTE characteristics, maintains the preload imposed by the two bushing components on the structure throughout operations at various temperatures.Type: GrantFiled: November 18, 2011Date of Patent: June 10, 2014Assignee: The Boeing CompanyInventor: Jonathan David Embler
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Publication number: 20130125340Abstract: Apparatus and methods provide for a bushing that compensates for thermal expansion and contraction to maintain a preload on a corresponding structure at various operating temperatures. According to embodiments described herein, a bushing may include two bushing components coupled to a load compensation sleeve between the two bushing components. The load compensation sleeve may have a coefficient of thermal expansion (CTE) greater than the two bushing components and the corresponding abutting structure. The configuration of the bushing components and load compensation sleeve, along with the corresponding CTE characteristics, maintains the preload imposed by the two bushing components on the structure throughout operations at various temperatures.Type: ApplicationFiled: November 18, 2011Publication date: May 23, 2013Inventor: Jonathan David Embler