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).

  • Patent number: 11731782
    Abstract: An air data probe includes a probe head defining a longitudinal axis between a forward tip and aft base. A port opening is defined in the forward tip. A first conduit is in fluid communication with the port opening to guide fluid flow from the port opening to a first chamber. The first chamber is downstream from the port opening. A second conduit, offset radially and circumferentially from the first conduit, is in fluid communication with the first chamber to guide fluid flow from the first chamber to a second chamber. The second chamber is downstream from the first chamber. The offset between the first and second conduits is configured to prevent particle ingestion from the port opening from entering the second conduit.
    Type: Grant
    Filed: October 7, 2021
    Date of Patent: August 22, 2023
    Assignee: Rosemount Aerospace Inc.
    Inventors: Timothy Thomas Golly, Greg A. Seidel, Paul Robert Johnson
  • Patent number: 11474123
    Abstract: A pitot tube includes an outer tube extending from a first tube end to second tube end, the second tube end defining a tip portion of the pitot tube, the tip portion including an inlet opening. A tube sleeve inside of the outer tube at least partially defines a tube passage extending from the first tube end to the second tube end. The tube sleeve includes a sleeve outer surface having a sleeve body portion having a first outer diameter and a sleeve tip portion located at the tip portion of the pitot tube. The sleeve tip portion has a second outer diameter smaller than the first outer diameter. A heating element is located between the outer tube and the tube sleeve at at least the sleeve tip portion.
    Type: Grant
    Filed: January 10, 2020
    Date of Patent: October 18, 2022
    Assignee: ROSEMOUNT AEROSPACE INC.
    Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson
  • Patent number: 11428707
    Abstract: A probe head of an air data probe includes an insert, a portion of a heater, an outer shell, a tip weld, and a braze. The insert includes a first end, a second end opposite the first end, and a body portion extending between the first end and the second end. The body portion includes a groove. The portion of the heater is positioned within the groove. The outer shell surrounds the insert and the portion of the heater. The outer shell includes a tip portion defining a first end of the outer shell and a body portion extending from the tip portion defining a second end of the outer shell. The tip weld is between the outer shell and the first end of the insert, and the braze is between the insert and the second end of the outer shell adjacent a second end of the insert. The portion of the heater is hermetically sealed between the insert and the outer shell.
    Type: Grant
    Filed: June 14, 2019
    Date of Patent: August 30, 2022
    Assignee: Rosemount Aerospace Inc.
    Inventors: Paul Robert Johnson, Timothy Thomas Golly, Greg Allen Seidel
  • Patent number: 11396063
    Abstract: A system used to additively manufacture an object layer-by-layer using direct energy deposition (DED) includes a base where the object is formed, a depositor configured to deposit material layer-by-layer on the base or a previously deposited layer of the object, an energy source configured to selectively direct an energized beam at the material to fuse a new layer of the material to a previously formed layer, and a heating element in contact with at least a portion of the base and configured to supply heat to the base.
    Type: Grant
    Filed: March 23, 2020
    Date of Patent: July 26, 2022
    Assignee: Rosemount Aerospace Inc.
    Inventors: Rudy Pitera, Scott Wigen, Paul Robert Johnson, Ryan Philip Chou
  • Publication number: 20220136884
    Abstract: A pitot tube includes an outer tube extending from a first tube end to second tube end. The second tube end defines a tip portion of the pitot tube. A tube sleeve is located inside of the outer tube and defines a tube passage extending from the first tube end to the second tube end. A heating element is located between the outer tube and the tube sleeve. The heating element is isolated from airflow into the tube passage. A method of forming a pitot tube includes installing a heating element to an outer surface of a tube sleeve, the tube sleeve defining a tube passage of the pitot tube. The tube sleeve is secured in an outer tube such that the heating element is between the tube sleeve and the outer tube and is isolated from airflow through the tube passage.
    Type: Application
    Filed: January 19, 2022
    Publication date: May 5, 2022
    Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson
  • Patent number: 11262227
    Abstract: A pitot tube includes an outer tube extending from a first tube end to second tube end. The second tube end defines a tip portion of the pitot tube. A tube sleeve is located inside of the outer tube and defines a tube passage extending from the first tube end to the second tube end. A heating element is located between the outer tube and the tube sleeve. The heating element is isolated from airflow into the tube passage. A method of forming a pitot tube includes installing a heating element to an outer surface of a tube sleeve, the tube sleeve defining a tube passage of the pitot tube. The tube sleeve is secured in an outer tube such that the heating element is between the tube sleeve and the outer tube and is isolated from airflow through the tube passage.
    Type: Grant
    Filed: September 23, 2019
    Date of Patent: March 1, 2022
    Assignee: ROSEMOUNT AEROSPACE INC.
    Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson
  • Publication number: 20220024602
    Abstract: An air data probe includes a probe head defining a longitudinal axis between a forward tip and aft base. A port opening is defined in the forward tip. A first conduit is in fluid communication with the port opening to guide fluid flow from the port opening to a first chamber. The first chamber is downstream from the port opening. A second conduit, offset radially and circumferentially from the first conduit, is in fluid communication with the first chamber to guide fluid flow from the first chamber to a second chamber. The second chamber is downstream from the first chamber. The offset between the first and second conduits is configured to prevent particle ingestion from the port opening from entering the second conduit.
    Type: Application
    Filed: October 7, 2021
    Publication date: January 27, 2022
    Applicant: Rosemount Aerospace Inc.
    Inventors: Timothy Thomas Golly, Greg A. Seidel, Paul Robert Johnson
  • Patent number: 11209330
    Abstract: A corrosion resistant apparatus for an air data probe with a 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: Grant
    Filed: July 1, 2020
    Date of Patent: December 28, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventors: Timothy Thomas Golly, Paul Robert Johnson, Greg Seidel
  • Publication number: 20210291299
    Abstract: A system used to additively manufacture an object layer-by-layer using direct energy deposition (DED) includes a base where the object is formed, a depositor configured to deposit material layer-by-layer on the base or a previously deposited layer of the object, an energy source configured to selectively direct an energized beam at the material to fuse a new layer of the material to a previously formed layer, and a heating element in contact with at least a portion of the base and configured to supply heat to the base.
    Type: Application
    Filed: March 23, 2020
    Publication date: September 23, 2021
    Inventors: Rudy Pitera, Scott Wigen, Paul Robert Johnson, Ryan Philip Chou
  • Publication number: 20210172973
    Abstract: 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: Application
    Filed: February 18, 2021
    Publication date: June 10, 2021
    Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson, Greg Seidel
  • Patent number: 10955433
    Abstract: 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.
    Type: Grant
    Filed: May 24, 2018
    Date of Patent: March 23, 2021
    Assignee: ROSEMOUNT AEROSPACE INC.
    Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson, Greg Seidel
  • Patent number: 10884014
    Abstract: A probe head of an air data probe includes an insert, a portion of a heater, an outer shell, a tip weld, and a braze. The insert includes a tip portion making up a tip of the air data probe, an end portion, and a body portion extending between the tip portion and the end portion. The body portion includes a groove. The portion of the heater is positioned within the groove. The outer shell surrounds the body portion of the insert and the portion of the heater. The tip weld is located between the tip portion of the insert and a first end of the outer shell, and the braze is located between the end portion of the insert and a second end of the outer shell. The portion of the heater is hermetically sealed between the insert and the outer shell.
    Type: Grant
    Filed: March 25, 2019
    Date of Patent: January 5, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventors: Timothy Thomas Golly, Paul Robert Johnson, Greg Allen Seidel
  • Publication number: 20200393484
    Abstract: A probe head of an air data probe includes an insert, a portion of a heater, an outer shell, a tip weld, and a braze. The insert includes a first end, a second end opposite the first end, and a body portion extending between the first end and the second end. The body portion includes a groove. The portion of the heater is positioned within the groove. The outer shell surrounds the insert and the portion of the heater. The outer shell includes a tip portion defining a first end of the outer shell and a body portion extending from the tip portion defining a second end of the outer shell. The tip weld is between the outer shell and the first end of the insert, and the braze is between the insert and the second end of the outer shell adjacent a second end of the insert. The portion of the heater is hermetically sealed between the insert and the outer shell.
    Type: Application
    Filed: June 14, 2019
    Publication date: December 17, 2020
    Inventors: Paul Robert Johnson, Timothy Thomas Golly, Greg Allen Seidel
  • Publication number: 20200333206
    Abstract: A corrosion resistant apparatus for an air data probe with a 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: Application
    Filed: July 1, 2020
    Publication date: October 22, 2020
    Inventors: Timothy Thomas Golly, Paul Robert Johnson, Greg Seidel
  • Publication number: 20200309808
    Abstract: A probe head of an air data probe includes an insert, a portion of a heater, an outer shell, a tip weld, and a braze. The insert includes a tip portion making up a tip of the air data probe, an end portion, and a body portion extending between the tip portion and the end portion. The body portion includes a groove. The portion of the heater is positioned within the groove. The outer shell surrounds the body portion of the insert and the portion of the heater. The tip weld is located between the tip portion of the insert and a first end of the outer shell, and the braze is located between the end portion of the insert and a second end of the outer shell. The portion of the heater is hermetically sealed between the insert and the outer shell.
    Type: Application
    Filed: March 25, 2019
    Publication date: October 1, 2020
    Inventors: Timothy Thomas Golly, Paul Robert Johnson, Greg Allen Seidel
  • Patent number: 10780502
    Abstract: A method of repairing an air data probe includes assessing an air data probe for a damaged portion. The method includes depositing a material on the air data probe to repair the damaged portion of the air data probe. An air data probe includes a probe body including a sense port inlet defined through a wall of the probe body. At least a portion of the wall surrounding the sense port inlet is defined by a deposited material having a different microstructure than a material defining another portion of the wall.
    Type: Grant
    Filed: October 12, 2018
    Date of Patent: September 22, 2020
    Assignee: Rosemount Aerospace Inc.
    Inventors: Timothy Thomas Golly, Paul Robert Johnson, Greg Allen Seidel, Ryan Chou, Rudy Pitera, Scott Wigen
  • Publication number: 20200233007
    Abstract: A pitot tube includes an outer tube extending from a first tube end to second tube end, the second tube end defining a tip portion of the pitot tube, the tip portion including an inlet opening. A tube sleeve inside of the outer tube at least partially defines a tube passage extending from the first tube end to the second tube end. The tube sleeve includes a sleeve outer surface having a sleeve body portion having a first outer diameter and a sleeve tip portion located at the tip portion of the pitot tube. The sleeve tip portion has a second outer diameter smaller than the first outer diameter. A heating element is located between the outer tube and the tube sleeve at at least the sleeve tip portion.
    Type: Application
    Filed: January 10, 2020
    Publication date: July 23, 2020
    Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson
  • Patent number: 10634530
    Abstract: 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: Grant
    Filed: January 29, 2018
    Date of Patent: April 28, 2020
    Assignee: Rosemount Aerospace, Inc.
    Inventors: Paul Robert Johnson, Aaron A. Cusher, Timothy Thomas Golly, Brian Daniel Matheis, Greg Seidel
  • Publication number: 20200114428
    Abstract: A method of repairing an air data probe includes assessing an air data probe for a damaged portion. The method includes depositing a material on the air data probe to repair the damaged portion of the air data probe. An air data probe includes a probe body including a sense port inlet defined through a wall of the probe body. At least a portion of the wall surrounding the sense port inlet is defined by a deposited material having a different microstructure than a material defining another portion of the wall.
    Type: Application
    Filed: October 12, 2018
    Publication date: April 16, 2020
    Inventors: Timothy Thomas Golly, Paul Robert Johnson, Greg Allen Seidel, Ryan Chou, Rudy Pitera, Scott Wigen
  • Publication number: 20200109982
    Abstract: A pitot tube includes an outer tube extending from a first tube end to second tube end. The second tube end defines a tip portion of the pitot tube. A tube sleeve is located inside of the outer tube and defines a tube passage extending from the first tube end to the second tube end. A heating element is located between the outer tube and the tube sleeve. The heating element is isolated from airflow into the tube passage. A method of forming a pitot tube includes installing a heating element to an outer surface of a tube sleeve, the tube sleeve defining a tube passage of the pitot tube. The tube sleeve is secured in an outer tube such that the heating element is between the tube sleeve and the outer tube and is isolated from airflow through the tube passage.
    Type: Application
    Filed: September 23, 2019
    Publication date: April 9, 2020
    Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson