Patents by Inventor Brian A. Gilkison

Brian A. Gilkison 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: 11714015
    Abstract: Apparatus and associated methods relate to sensing pressure and mitigating the error introduced by the thermoelectric effect. A pressure sensing device includes a pressure sensor, a temperature sensor, and an error correction device. The pressure sensor produces a voltage output proportional to a sensed pressure. The temperature sensor measures a first temperature at a first location and a second temperature at a second location to produce a temperature difference signal. The error correction device modifies the pressure output proportionally to the temperature difference signal to produce a temperature adjusted pressure output which compensates for error introduced from the temperature difference.
    Type: Grant
    Filed: March 29, 2022
    Date of Patent: August 1, 2023
    Assignee: ROSEMOUNT AEROSPACE INC.
    Inventors: Brandon T. Berg, Brian A. Gilkison
  • Patent number: 6892584
    Abstract: A pitot pressure sensing probe assembly is made up of individual components comprising a barrel formed with a longitudinal interior passageway and a conical end cap at its leading end. A strut that has stamped or formed sections secured together to form the strut with a compound curvature includes a neck that has a bore to receive a hub of the barrel. The end cap has a pitot port for sensing fluid pressure. The barrel includes a water trap at its leading end for trapping water and permitting it to drain through a hole in the conical end cap. The longitudinal internal passageyway carries the fluid pressure sensed by the pitot port to remote instruments. The individual components are easily formed and are secured together to make the pitot pressure sensing probe assembly.
    Type: Grant
    Filed: November 19, 2002
    Date of Patent: May 17, 2005
    Assignee: Rosemount Aerospace Inc.
    Inventors: Brian A. Gilkison, Marc C. Moore
  • Publication number: 20040093953
    Abstract: A pitot pressure sensing probe assembly is made up of individual components comprising a barrel formed with a longitudinal interior passageway and a conical end cap at its leading end. A strut that has stamped or formed sections secured together to form the strut with a compound curvature includes a neck that has a bore to receive a hub of the barrel. The end cap has a pitot port for sensing fluid pressure. The barrel includes a water trap at its leading end for trapping water and permitting it to drain through a hole in the conical end cap. The longitudinal internal passageyway carries the fluid pressure sensed by the pitot port to remote instruments. The individual components are easily formed and are secured together to make the pitot pressure sensing probe assembly.
    Type: Application
    Filed: November 19, 2002
    Publication date: May 20, 2004
    Inventors: Brian A. Gilkison, Marc C. Moore
  • Patent number: 6550344
    Abstract: A semi-flush air data sensing probe is formed as an elongated bubble housing directly supported on an aircraft surface having a generally longitudinally extending rounded outer edge surface with a rounded contoured leading end. The housing has top and bottom wall surfaces extending from the supporting surface to the rounded outer surface. The trailing end of the housing is smaller than the leading end and is contoured to provide for smooth airflow past the housing. A central longitudinally extending plane that bisects the housing and which is perpendicular to the supporting surface, forms a reference. A forwardly facing port is at the leading end and centered on the central plane, and a pair of angle of attack sensing ports are on the leading end and are symmetrically located on opposite sides of the longitudinally extending plane. A static pressure sensing port also is provided on the housing at a position along the rounded outer edge surface and spaced downstream from the leading end.
    Type: Grant
    Filed: May 4, 2001
    Date of Patent: April 22, 2003
    Assignee: Rosemount Aerospace Inc.
    Inventors: Thomas J. Bachinski, Timothy T. Golly, Roger D. Foster, Brian A. Gilkison
  • Publication number: 20020162401
    Abstract: A semi-flush air data sensing probe is formed as an elongated bubble housing directly supported on an aircraft surface having a generally longitudinally extending rounded outer edge surface with a rounded contoured leading end. The housing has top and bottom wall surfaces extending from the supporting surface to the rounded outer surface. The trailing end of the housing is smaller than the leading end and is contoured to provide for smooth airflow past the housing. A central longitudinally extending plane that bisects the housing and which is perpendicular to the supporting surface, forms a reference. A forwardly facing port is at the leading end and centered on the central plane, and a pair of angle of attack sensing ports are on the leading end and are symmetrically located on opposite sides of the longitudinally extending plane. A static pressure sensing port also is provided on the housing at a position along the rounded outer edge surface and spaced downstream from the leading end.
    Type: Application
    Filed: May 4, 2001
    Publication date: November 7, 2002
    Inventors: Thomas J. Bachinski, Timothy T. Golly, Roger D. Foster, Brian A. Gilkison
  • Patent number: D463989
    Type: Grant
    Filed: May 3, 2001
    Date of Patent: October 8, 2002
    Assignee: Rosemount Aerospace Inc.
    Inventors: Thomas J. Bachinski, Timothy T. Golly, Roger D. Foster, Brian A. Gilkison