Patents by Inventor Daniel T. Haggerty

Daniel T. Haggerty 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: 8196845
    Abstract: A nozzle includes an inlet at an upstream end of the nozzle, a discharge outlet at a downstream end of the nozzle, and a fluid delivery passage extending between the inlet and the discharge outlet. Exterior and interior walls of the nozzle have downstream tip ends that are relatively longitudinally movable at one or more interfaces. An internal insulating gap is interposed between the interior and exterior walls to insulate fuel from ambient temperature conditions exterior to the nozzle. One or more flexible seal structures internal to the nozzle isolate a portion of the insulating gap from any ambient fluid entering into the gap through the one or more interfaces while providing relative movement between interior and exterior walls of the nozzle.
    Type: Grant
    Filed: July 29, 2010
    Date of Patent: June 12, 2012
    Assignee: Delavan Inc
    Inventors: Neal A. Thomson, Troy Hall, Daniel T. Haggerty, Mark Alan Caples
  • Patent number: 8079220
    Abstract: A fuel distribution manifold system for a gas turbine engine is disclosed that includes a plurality of interconnected manifold segments, each manifold segment extending between a pair of fittings, each manifold segment including at least one fuel transfer tube and a sealing tube that surrounds the at least one fuel transfer tube, wherein opposed end portions of the at least one fuel transfer tube are dynamically connected to the fittings and opposed end portions of the sealing tube are statically connected to the fittings.
    Type: Grant
    Filed: August 28, 2008
    Date of Patent: December 20, 2011
    Assignee: Delavan Inc
    Inventor: Daniel T. Haggerty
  • Publication number: 20100307161
    Abstract: A nozzle includes an inlet at an upstream end of the nozzle, a discharge outlet at a downstream end of the nozzle, and a fluid delivery passage extending between the inlet and the discharge outlet. Exterior and interior walls of the nozzle have downstream tip ends that are relatively longitudinally movable at one or more interfaces. An internal insulating gap is interposed between the interior and exterior walls to insulate fuel from ambient temperature conditions exterior to the nozzle. One or more flexible seal structures internal to the nozzle isolate a portion of the insulating gap from any ambient fluid entering into the gap through the one or more interfaces while providing relative movement between interior and exterior walls of the nozzle.
    Type: Application
    Filed: July 29, 2010
    Publication date: December 9, 2010
    Applicant: Delavan Inc
    Inventors: Neal A. Thomson, Troy Hall, Daniel T. Haggerty, Mark Caples
  • Publication number: 20100050645
    Abstract: A fuel distribution manifold system for a gas turbine engine is disclosed that includes a plurality of interconnected manifold segments, each manifold segment extending between a pair of fittings, each manifold segment including at least one fuel transfer tube and a sealing tube that surrounds the at least one fuel transfer tube, wherein opposed end portions of the at least one fuel transfer tube are dynamically connected to the fittings and opposed end portions of the sealing tube are statically connected to the fittings.
    Type: Application
    Filed: August 28, 2008
    Publication date: March 4, 2010
    Applicant: DELAVAN INC
    Inventor: Daniel T. Haggerty