Patents by Inventor Paul Robert Johnson
Paul Robert Johnson 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: 10613112Abstract: An air data probe includes a strut including a socket defining an interior surface of the strut and an interior groove extending radially into the interior surface. The air data probe also includes a probe head partially positioned within the socket, the probe head including an exterior surface and an exterior groove extending radially into the exterior surface, the exterior groove being axially alignable with the interior groove. The air data probe further includes a retaining ring partially positionable within the exterior groove and partially positionable within the interior groove when the exterior groove and the interior groove are axially aligned to axially retain the probe head to the strut while allowing the probe head to rotate relative to the strut.Type: GrantFiled: January 19, 2018Date of Patent: April 7, 2020Assignee: Rosemount Aerospace Inc.Inventors: Timothy Thomas Golly, Paul Robert Johnson, Greg Seidel
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Patent number: 10564173Abstract: An air data probe includes a housing and a probe head with a body, total pressure and alpha chambers, total pressure and alpha ports, and alpha drain ports. The total pressure chamber extends through a radial center of the body. The alpha chambers are disposed radially outward from the total pressure chamber. The total pressure port is disposed in a distal end of the body is collinear with a centerline axis of the body. The total pressure chamber is in fluid communication with the total pressure port and with the housing. The alpha ports are disposed downstream of the total pressure port and upstream of the housing. The alpha chambers are in fluid communication with the alpha ports. The alpha drain ports are disposed downstream from the alpha port and upstream from the housing. The alpha drain ports fluidly communicate with the alpha chamber.Type: GrantFiled: May 9, 2018Date of Patent: February 18, 2020Assignee: Rosemount Aerospace, Inc.Inventors: Mackenzie Whalen, James Barron Egberg, Paul Robert Johnson
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Publication number: 20190346476Abstract: An air data probe includes a housing and a probe head with a body, total pressure and alpha chambers, total pressure and alpha ports, and alpha drain ports. The total pressure chamber extends through a radial center of the body. The alpha chambers are disposed radially outward from the total pressure chamber. The total pressure port is disposed in a distal end of the body is collinear with a centerline axis of the body. The total pressure chamber is in fluid communication with the total pressure port and with the housing. The alpha ports are disposed downstream of the total pressure port and upstream of the housing. The alpha chambers are in fluid communication with the alpha ports. The alpha drain ports are disposed downstream from the alpha port and upstream from the housing. The alpha drain ports fluidly communicate with the alpha chamber.Type: ApplicationFiled: May 9, 2018Publication date: November 14, 2019Inventors: Mackenzie Whalen, James Barron Egberg, Paul Robert Johnson
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Publication number: 20190316946Abstract: A corrosion resistant sleeve for an air data probe with the sleeve being cylindrical in shape with a first end and a second end, at least one circumferentially extending groove on an outside of the sleeve configured to accommodate coils of a heater, and a bore at a center of the sleeve and extending between the first end and the second end configured to provide a pneumatic pathway that allows atmospheric conditions to reach measurement equipment of the air data probe.Type: ApplicationFiled: December 15, 2017Publication date: October 17, 2019Inventors: Timothy Thomas Golly, Paul Robert Johnson, Greg Seidel
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Publication number: 20190293676Abstract: An air data probe includes a probe body including a probe wall. The probe body is formed from a first material by direct energy metal deposition. An insert is positioned in the probe wall. The insert is formed from a second material different from the first material. The insert is encapsulated in the probe wall via the direct energy metal deposition. A method of forming an air data probe includes forming one or more thermally conductive inserts, and encapsulating the one or more inserts into a wall of an air data probe via direct energy metal deposition. The air data probe is formed from a first material and the one or more inserts are formed from a second material different from the first material.Type: ApplicationFiled: May 24, 2018Publication date: September 26, 2019Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson, Greg Seidel
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Publication number: 20190227094Abstract: An air data probe includes a strut including a socket defining an interior surface of the strut and an interior groove extending radially into the interior surface. The air data probe also includes a probe head partially positioned within the socket, the probe head including an exterior surface and an exterior groove extending radially into the exterior surface, the exterior groove being axially alignable with the interior groove. The air data probe further includes a retaining ring partially positionable within the exterior groove and partially positionable within the interior groove when the exterior groove and the interior groove are axially aligned to axially retain the probe head to the strut while allowing the probe head to rotate relative to the strut.Type: ApplicationFiled: January 19, 2018Publication date: July 25, 2019Inventors: Timothy Thomas Golly, Paul Robert Johnson, Greg Seidel
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Publication number: 20190186974Abstract: A corrosion resistant sleeve for an air data probe with the sleeve being cylindrical in shape with a first end and a second end, at least one circumferentially extending groove on an outside of the sleeve configured to accommodate coils of a heater, and a bore at a center of the sleeve and extending between the first end and the second end configured to provide a pneumatic pathway that allows atmospheric conditions to reach measurement equipment of the air data probe.Type: ApplicationFiled: December 15, 2017Publication date: June 20, 2019Inventors: Timothy Thomas Golly, Paul Robert Johnson, Greg Seidel
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Patent number: 10281303Abstract: An air data probe has a pitot tube with a tap at a forward end that defines an inner flow path. The inner flow path decreases in the cross-sectional area until reaching a throat. The inner flow path has cross-sections that are generally cylindrical and also has sections of removed material.Type: GrantFiled: March 23, 2015Date of Patent: May 7, 2019Assignee: Rosemount Aerospace, Inc.Inventors: Paul Robert Johnson, Aaron A Cusher, Timothy Thomas Golly, Brian Daniel Matheis, Greg Seidel
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Publication number: 20180356438Abstract: A pitot tube includes a substantially cylindrical body portion having an interior defining a flow passage. A tip portion extends along a pitot tube axis from the body portion. The tip portion includes a high thermal conductive insert. The body portion and the tip portion including the high thermal conductive insert are integrally formed.Type: ApplicationFiled: August 10, 2017Publication date: December 13, 2018Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson
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Publication number: 20180238723Abstract: A method of forming a pitot tube includes forming a substantially cylindrical body portion including an outer surface, a tip portion having an inlet opening and an interior defining a flow passage, radially tapering the outer surface from the body portion toward the inlet opening, and disposing at least one electrical coil including one or more coil wraps along the flow passage of the pitot tube.Type: ApplicationFiled: April 19, 2018Publication date: August 23, 2018Inventors: Greg Seidel, Timothy Thomas Golly, Paul Robert Johnson
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Patent number: 10024877Abstract: A method of making an air data probe may comprise forming a probe body, forming an interior cavity into the probe body, applying a protective shell to the probe body by an additive manufacturing technique, inserting a heating element into the interior cavity, machining a final profile of the air data probe, and forming a sensing port comprising a port passage defined through the probe body and lined by a portion of the protective shell.Type: GrantFiled: August 21, 2017Date of Patent: July 17, 2018Assignee: Rosemount Aerospace, Inc.Inventors: Timothy Thomas Golly, Matthew P. Anderson, Paul Robert Johnson, Greg Seidel
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Publication number: 20180149501Abstract: An air data probe has a pitot tube with a tap at a forward end that defines an inner flow path. The inner flow path decreases in the cross-sectional area until reaching a throat. The inner flow path has cross-sections that are generally cylindrical and also has sections of removed material. Other embodiment have unique shapes.Type: ApplicationFiled: January 29, 2018Publication date: May 31, 2018Inventors: Paul Robert Johnson, Aaron A. Cusher, Timothy Thomas Golly, Brian Daniel Matheis, Greg Seidel
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Patent number: 9976882Abstract: A method of forming a pitot tube includes forming a substantially cylindrical body portion including an outer surface, a tip portion having an inlet opening and an interior defining a flow passage, radially tapering the outer surface from the body portion toward the inlet opening, and disposing at least one electrical coil including one or more coil wraps along the flow passage of the pitot tube.Type: GrantFiled: October 26, 2015Date of Patent: May 22, 2018Assignee: ROSEMOUNT AEROSPACE INC.Inventors: Greg Seidel, Timothy Thomas Golly, Paul Robert Johnson
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Publication number: 20170343576Abstract: A method of making an air data probe may comprise forming a probe body, forming an interior cavity into the probe body, applying a protective shell to the probe body by an additive manufacturing technique, inserting a heating element into the interior cavity, machining a final profile of the air data probe, and forming a sensing port comprising a port passage defined through the probe body and lined by a portion of the protective shellType: ApplicationFiled: August 21, 2017Publication date: November 30, 2017Applicant: Rosemount Aerospace, Inc.Inventors: Timothy Thomas Golly, Matthew P. Anderson, Paul Robert Johnson, Greg Seidel
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Patent number: 9772345Abstract: An air data probe is disclosed. The air data probe may include a probe body having an interior cavity and coated by a protective shell. A sensing port may be disposed in the air data probe and may extend through the probe body. The sensing port may also be lined by the protective shell. The protective shell may be made of an austenitic nickel-chromium alloy, or stainless steel, or any relatively corrosion resistant material. The probe body may be made of nickel, or a nickel alloy, or any relatively thermally conductive material. The protective shell may be joined to the probe body by additive manufacturing, such as laser cladding. In this manner, an air data probe capable withstanding high temperatures without corrosion and yet also being relatively thermally conductive is disclosed.Type: GrantFiled: February 17, 2016Date of Patent: September 26, 2017Assignee: ROSEMOUNT AEROSPACE, INC.Inventors: Timothy Thomas Golly, Matthew P. Anderson, Paul Robert Johnson, Greg Seidel
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Publication number: 20170219397Abstract: A pitot tube includes a substantially cylindrical body portion having an interior defining a flow passage and a tip portion extending along a pitot tube axis from the body portion. The tip portion includes a disk, a tip cover and a high thermal conductive insert disposed between the disk and the tip cover and in thermal contact with both.Type: ApplicationFiled: April 5, 2016Publication date: August 3, 2017Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson
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Patent number: 9719820Abstract: A pitot tube includes a substantially cylindrical body portion having an interior defining a flow passage and a tip portion extending along a pitot tube axis from the body portion. The tip portion includes a disk, a tip cover and a high thermal conductive insert disposed between the disk and the tip cover and in thermal contact with both.Type: GrantFiled: April 5, 2016Date of Patent: August 1, 2017Assignees: GOODRICH AEROSPACE SERVICES PRIVATE LIMITED, ROSEMOUNT AEROSPACE INC.Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson
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Patent number: 9631960Abstract: A pitot tube includes a substantially cylindrical body portion having an interior defining a flow passage, and a tip portion extending along a pitot tube axis from the body portion. The tip portion includes an inlet opening, a radially tapered outer surface extending from the body portion toward the inlet opening, one or more bulkheads disposed at the interior to limit travel of particles ingested into the interior, at least one drain opening disposed directly adjacent to one of the one or more bulkheads, and one or more electrical coils comprising one or more coil wraps disposed at an interior of the pitot tube. The one or more coil wraps establish a variable watt density along the interior of the pitot tube. The one or more coil wraps also establish a variable watt density downstream of one or more of the one or more bulkheads.Type: GrantFiled: October 26, 2015Date of Patent: April 25, 2017Assignee: ROSEMOUNT AEROSPACE INC.Inventors: Greg Seidel, Timothy Thomas Golly, Paul Robert Johnson
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Patent number: 9606137Abstract: A pitot tube includes a wall that extends longitudinally along an axis. The wall defines an inlet aperture at a longitudinal end of the wall, an outlet aperture opposite the inlet aperture, an interior cavity extending from the inlet aperture to an outlet aperture, a passage extending through and perpendicular to the wall having an outlet along an exterior surface of the wall, and an augmenting feature configured to reduce a static pressure at the outlet of the passage. In another embodiment, a wall defines a passage and an augmenting feature that modifies a flow direction of fluid flowing across an outlet of the passage such that a static pressure of the fluid at the outlet is reduced relative to the wall without the augmenting feature.Type: GrantFiled: June 17, 2015Date of Patent: March 28, 2017Assignee: Rosemount Aerospace Inc.Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson
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Publication number: 20160370400Abstract: A pitot tube includes a wall that extends longitudinally along an axis. The wall defines an inlet aperture at a longitudinal end of the wall, an outlet aperture opposite the inlet aperture, an interior cavity extending from the inlet aperture to an outlet aperture, a passage extending through and perpendicular to the wall having an outlet along an exterior surface of the wall, and an augmenting feature configured to reduce a static pressure at the outlet of the passage. In another embodiment, a wall defines a passage and an augmenting feature that modifies a flow direction of fluid flowing across an outlet of the passage such that a static pressure of the fluid at the outlet is reduced relative to the wall without the augmenting feature.Type: ApplicationFiled: June 17, 2015Publication date: December 22, 2016Applicant: Rosemount Aerospace Inc.Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson