Patents by Inventor Yonas T. Meshesha

Yonas T. Meshesha 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: 11235861
    Abstract: A vehicle control surface, such as an aircraft horizontal stabilizer, is hydraulically controlled using solenoid operated valves (SOVs) controlling directional control valves and/or rate control valves with small numbers of ports, e.g. a four port three position directional control value and/or a four port two position rate control valve.
    Type: Grant
    Filed: August 2, 2019
    Date of Patent: February 1, 2022
    Assignee: The Boeing Company
    Inventors: Derek M. Joseph, Kevin B. Eck, Christopher D. Feet, Yonas T. Meshesha, Timothy J. Soderquist, Barry D. Hance
  • Publication number: 20200140063
    Abstract: Systems and methods are provided for a hydraulic stabilizer trim actuator (HSTA). The HSTA may operate one or more movable control surfaces.
    Type: Application
    Filed: August 2, 2019
    Publication date: May 7, 2020
    Inventors: Derek M. JOSEPH, Kevin B. ECK, Christopher D. FEET, Yonas T. MESHESHA, Timothy J. SODERQUIST, Barry D. HANCE
  • Patent number: 10450056
    Abstract: Systems and methods are provided for a hydraulic stabilizer trim actuator (HSTA). The HSTA may operate one or more movable control surfaces. The HSTA operate responsive to commands issued by the pilot and/or by a controller and may include hydraulic architecture that minimizes the probability of an un-commanded movement or movement in the opposite direction of such commands.
    Type: Grant
    Filed: July 19, 2016
    Date of Patent: October 22, 2019
    Assignee: THE BOEING COMPANY
    Inventors: Derek M. Joseph, Kevin B. Eck, Christopher D. Feet, Yonas T. Meshesha, Timothy J. Soderquist, Barry D. Hance
  • Publication number: 20180022440
    Abstract: Systems and methods are provided for a hydraulic stabilizer trim actuator (HSTA). The HSTA may operate one or more movable control surfaces. The HSTA operate responsive to commands issued by the pilot and/or by a controller and may include hydraulic architecture that minimizes the probability of an un-commanded movement or movement in the opposite direction of such commands.
    Type: Application
    Filed: July 19, 2016
    Publication date: January 25, 2018
    Inventors: Derek M. Joseph, Kevin B. Eck, Christopher D. Feet, Yonas T. Meshesha, Timothy J. Soderquist, Barry D. Hance