Patents by Inventor Mark Zsurka

Mark Zsurka 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: 11022047
    Abstract: An external turning vane includes a vane body extending radially from the inner cowl and disposed upstream from an inlet of the secondary flow system, the vane body configured to turn an airflow in a bypass flow path towards an axial direction to minimize separation between the airflow and the secondary flow system.
    Type: Grant
    Filed: August 7, 2019
    Date of Patent: June 1, 2021
    Assignee: Raytheon Technologies Corporation
    Inventors: Mark Zsurka, Laurel F. Carlson
  • Publication number: 20210040897
    Abstract: An external turning vane includes a vane body extending radially from the inner cowl and disposed upstream from an inlet of the secondary flow system, the vane body configured to turn an airflow in a bypass flow path towards an axial direction to minimize separation between the airflow and the secondary flow system.
    Type: Application
    Filed: August 7, 2019
    Publication date: February 11, 2021
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: Mark Zsurka, Laurel F. Carlson
  • Patent number: 10487744
    Abstract: Aspects of the disclosure are directed to a system associated with an engine of an aircraft comprising: a duct, an inlet coupled to the duct, and a fence coupled to the inlet or located upstream of the inlet. In some embodiments, the system further comprises a valve body coupled to the duct. In some embodiments, the valve body includes at least one valve that is configured to rotate between a closed state and an open state.
    Type: Grant
    Filed: May 23, 2016
    Date of Patent: November 26, 2019
    Assignee: United Technologies Corporation
    Inventors: Keith A. Post, Daniel W. Shannon, Steven H. Zysman, Mark Zsurka, Diego H. de la Riva, Sudarshan N. Koushik
  • Patent number: 10240561
    Abstract: A gas turbine engine includes an aerodynamic track fairing adjacent to a convergent-divergent nozzle, the aerodynamic track fairing including a localized curvature along an outside edge. The aerodynamic track fairing is configured to offset a circumferential pressure gradient otherwise introduced in part by a transition between the convergent-divergent nozzle with the aerodynamic track fairing.
    Type: Grant
    Filed: March 13, 2014
    Date of Patent: March 26, 2019
    Assignee: United Technologies Corporation
    Inventor: Mark Zsurka
  • Publication number: 20170335771
    Abstract: Aspects of the disclosure are directed to a system associated with an engine of an aircraft comprising: a duct, an inlet coupled to the duct, and a fence coupled to the inlet or located upstream of the inlet. In some embodiments, the system further comprises a valve body coupled to the duct. In some embodiments, the valve body includes at least one valve that is configured to rotate between a closed state and an open state.
    Type: Application
    Filed: May 23, 2016
    Publication date: November 23, 2017
    Inventors: Keith A. Post, Daniel W. Shannon, Steven H. Zysman, Mark Zsurka, Diego H. de la Riva, Sudarshan N. Koushik
  • Publication number: 20160040627
    Abstract: A gas turbine engine includes an aerodynamic track fairing adjacent to a convergent-divergent nozzle, the aerodynamic track fairing including a localized curvature along an outside edge. The aerodynamic track fairing is configured to offset a circumferential pressure gradient otherwise introduced in part by a transition between the convergent-divergent nozzle with the aerodynamic track fairing.
    Type: Application
    Filed: March 13, 2014
    Publication date: February 11, 2016
    Inventor: Mark Zsurka