Patents by Inventor Robert Selinsky, JR.

Robert Selinsky, JR. 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).

  • Systems and methods for combustor panel
    Patent number: 11175041
    Abstract: A combustor panel of a combustor may include a combustion facing surface, a cooling surface opposite the combustion facing surface, and heat transfer pins extending from the cooling surface. A grouping of the heat transfer pins may include a metallic coating.
    Type: Grant
    Filed: October 10, 2019
    Date of Patent: November 16, 2021
    Assignee: Raytheon Technologies Corporation
    Inventors: San Quach, John S. Tu, Robert M. Sonntag, Robert Selinsky, Jr., John J. Rup, Jr., Anthony Van
  • Combustor panel for gas turbine engine
    Patent number: 10684014
    Abstract: A heat shield panel for a gas turbine engine includes a substrate layer having a first substrate surface and a second substrate surface opposite the first substrate surface. The first substrate surface and the second substrate surface define a substrate layer thickness therebetween. One or more thermally protective coating layers are applied to the first substrate surface of the substrate layer. The one or more coating layers have a constant coating layer thickness and the substrate layer thickness tapers along an axial length of the heat shield panel.
    Type: Grant
    Filed: August 4, 2016
    Date of Patent: June 16, 2020
    Assignee: RAYTHEON TECHNOLOGIES CORPORATION
    Inventors: San Quach, Brian T. Hazel, Kaitlin M. Tomeo, Robert Selinsky, Jr., Aaron S. Butler, John S. Tu, William F. Werkheiser, Jessica L. Serra
  • SYSTEMS AND METHODS FOR COMBUSTOR PANEL
    Publication number: 20200041125
    Abstract: A combustor panel of a combustor may include a combustion facing surface, a cooling surface opposite the combustion facing surface, and heat transfer pins extending from the cooling surface. A grouping of the heat transfer pins may include a metallic coating.
    Type: Application
    Filed: October 10, 2019
    Publication date: February 6, 2020
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: SAN QUACH, JOHN S. TU, ROBERT M. SONNTAG, ROBERT SELINSKY, JR., JOHN J. RUP, JR., ANTHONY VAN
  • Systems and methods for combustor panel
    Patent number: 10480788
    Abstract: A combustor panel of a combustor may include a combustion facing surface, a cooling surface opposite the combustion facing surface, and heat transfer pins extending from the cooling surface. A grouping of the heat transfer pins may include a metallic coating.
    Type: Grant
    Filed: August 16, 2016
    Date of Patent: November 19, 2019
    Assignee: UNITED TECHNOLOGIES CORPORATION
    Inventors: San Quach, John S. Tu, Robert M. Sonntag, Robert Selinsky, Jr., John J. Rup, Jr., Anthony Van
  • Wall panel assembly for a gas turbine engine
    Patent number: 10386067
    Abstract: A wall panel assembly includes a first liner panel and a coating. The first liner panel has an inner first liner panel surface and a first liner panel outer surface each axially extending between a first liner panel first end and a first liner panel second end. The coating is disposed on at least one of the first liner panel inner surface and the first liner panel outer surface. The coating has an overall thickness that varies axially between the first liner panel first end and the first liner panel second end.
    Type: Grant
    Filed: September 15, 2016
    Date of Patent: August 20, 2019
    Assignee: UNITED TECHNOLOGIES CORPORATION
    Inventors: San Quach, Scott A. Elliott, Robert M. Sonntag, John S. Tu, Anthony Van, Joseph J. Sedor, Robert Selinsky, Jr., John J. Rup, Jr., Neil B. Ridgeway, Gerard V. Cadieux, Jeffrey Leon, Monica Pacheco-Tougas, Lisa A. Jenkins, Lisa Tse, Andrew Cervoni, Frank J. Trzcinski
  • WALL PANEL ASSEMBLY FOR A GAS TURBINE ENGINE
    Publication number: 20180073737
    Abstract: A wall panel assembly includes a first liner panel and a coating. The first liner panel has an inner first liner panel surface and a first liner panel outer surface each axially extending between a first liner panel first end and a first liner panel second end. The coating is disposed on at least one of the first liner panel inner surface and the first liner panel outer surface. The coating has an overall thickness that varies axially between the first liner panel first end and the first liner panel second end.
    Type: Application
    Filed: September 15, 2016
    Publication date: March 15, 2018
    Inventors: San Quach, Scott A. Elliott, Robert M. Sonntag, John S. Tu, Anthony Van, Joseph J. Sedor, Robert selinsky, JR., John J. Rup, JR., Neil B. Ridgeway, Gerard V. Cadieux, Jeffrey Leon, Monica Pacheco-Tougas, Lisa A. Jenkins, Lisa Tse, Andrew Cervoni, Frank J. Trzcinski
  • SYSTEMS AND METHODS FOR COMBUSTOR PANEL
    Publication number: 20180051879
    Abstract: A combustor panel of a combustor may include a combustion facing surface, a cooling surface opposite the combustion facing surface, and heat transfer pins extending from the cooling surface. A grouping of the heat transfer pins may include a metallic coating.
    Type: Application
    Filed: August 16, 2016
    Publication date: February 22, 2018
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: SAN QUACH, JOHN S. TU, ROBERT M. SONNTAG, ROBERT SELINSKY, JR., JOHN J. RUP, JR., ANTHONY VAN
  • COMBUSTOR PANEL FOR GAS TURBINE ENGINE
    Publication number: 20180038593
    Abstract: A heat shield panel for a gas turbine engine includes a substrate layer having a first substrate surface and a second substrate surface opposite the first substrate surface. The first substrate surface and the second substrate surface define a substrate layer thickness therebetween. One or more thermally protective coating layers are applied to the first substrate surface of the substrate layer. The one or more coating layers have a constant coating layer thickness and the substrate layer thickness tapers along an axial length of the heat shield panel.
    Type: Application
    Filed: August 4, 2016
    Publication date: February 8, 2018
    Inventors: San Quach, Brian T. Hazel, Kaitlin M. Tomeo, Robert Selinsky, JR., Aaron S. Butler, John S. Tu, William F. Werkheiser, Jessica L. Serra