Patents by Inventor Jocelyn Charis Damgaard

Jocelyn Charis Damgaard 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).

  • Retainer for suspended thermal protection elements in a gas turbine engine
    Patent number: 8572986
    Abstract: A hanger system includes a pin with a head section which defines a pin axis. A clip assembly captures the head section to permit movement of the pin within a hanger in a direction transverse to the pin axis. A fastener which retains the clip assembly to the hanger.
    Type: Grant
    Filed: July 27, 2009
    Date of Patent: November 5, 2013
    Assignee: United Technologies Corporation
    Inventors: Steven D. Roberts, Jocelyn Charis Damgaard
  • Flexible seal for gas turbine engine system
    Patent number: 8459936
    Abstract: A system includes a gas turbine engine, a nozzle structure located adjacent to the gas turbine engine, a flexible annular seal linking the gas turbine engine and the nozzle structure, the flexible annular seal having a plurality of corrugate sections arranged about a centerline, and a connection device secured to the gas turbine engine and to the nozzle structure. The connection device is adjustable to select a length of the flexible annular seal measured along the centerline.
    Type: Grant
    Filed: June 30, 2011
    Date of Patent: June 11, 2013
    Assignee: United Technologies Corporation
    Inventors: Jocelyn Charis Damgaard, Steven D. Roberts, Timothy Dale, Richard W. Monahan, David C. Pimenta
  • FLEXIBLE SEAL FOR GAS TURBINE ENGINE SYSTEM
    Publication number: 20120131928
    Abstract: A system includes a gas turbine engine, a nozzle structure located adjacent to the gas turbine engine, a flexible annular seal linking the gas turbine engine and the nozzle structure, the flexible annular seal having a plurality of corrugate sections arranged about a centerline, and a connection device secured to the gas turbine engine and to the nozzle structure. The connection device is adjustable to select a length of the flexible annular seal measured along the centerline.
    Type: Application
    Filed: June 30, 2011
    Publication date: May 31, 2012
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: Jocelyn Charis Damgaard, Steven D. Roberts, Timothy Dale, Richard W. Monahan, David C. Pimenta
  • RETAINER FOR SUSPENDED THERMAL PROTECTION ELEMENTS IN A GAS TURBINE ENGINE
    Publication number: 20110016880
    Abstract: A hanger system includes a pin with a head section which defines a pin axis. A clip assembly captures the head section to permit movement of the pin within a hanger in a direction traverse to the pin axis. A fastener which retains the clip assembly to the hanger.
    Type: Application
    Filed: July 27, 2009
    Publication date: January 27, 2011
    Inventors: Steven D. Roberts, Jocelyn Charis Damgaard