Patents by Inventor Robert R. Fogarty

Robert R. Fogarty 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: 11426742
    Abstract: A spray nozzle comprising a housing including a primary passage defining a primary axis, a series of secondary passages configured to provide swirl to a fluid passing therethrough circumferentially positioned around the housing, a series of standoffs circumferentially spread around an outer surface of the housing and located downstream along the primary axis of the series of swirling passages, wherein each of the swirling passages corresponds to a respective standoff of the series of standoffs, in order to control the swirl of the fluid.
    Type: Grant
    Filed: January 28, 2020
    Date of Patent: August 30, 2022
    Assignee: Collins Engine Nozzles, Inc.
    Inventors: Steve J. Myers, Philip E. O. Buelow, Robert R. Fogarty
  • Publication number: 20210229117
    Abstract: A spray nozzle comprising a housing including a primary passage defining a primary axis, a series of secondary passages configured to provide swirl to a fluid passing therethrough circumferentially positioned around the housing, a series of standoffs circumferentially spread around an outer surface of the housing and located downstream along the primary axis of the series of swirling passages, wherein each of the swirling passages corresponds to a respective standoff of the series of standoffs, in order to control the swirl of the fluid.
    Type: Application
    Filed: January 28, 2020
    Publication date: July 29, 2021
    Applicant: Delavan Inc.
    Inventors: Steve J. Myers, Philip E. O. Buelow, Robert R. Fogarty
  • Patent number: 10295187
    Abstract: A fuel nozzle for a gas turbine engine is disclosed which includes a nozzle body having a longitudinal axis, an elongated annular air passage defined within the nozzle body, and a plurality of circumferentially spaced apart axially extending swirl vanes disposed within the annular air passage, wherein each swirl vane has multiple joined leads and a variable thickness along the axial extent thereof.
    Type: Grant
    Filed: October 24, 2016
    Date of Patent: May 21, 2019
    Assignee: Rolls-Royce plc
    Inventors: Brandon P. Williams, Kevin E. Thompson, Robert R. Fogarty
  • Publication number: 20170038072
    Abstract: A fuel nozzle for a gas turbine engine is disclosed which includes a nozzle body having a longitudinal axis, an elongated annular air passage defined within the nozzle body, and a plurality of circumferentially spaced apart axially extending swirl vanes disposed within the annular air passage, wherein each swirl vane has multiple joined leads and a variable thickness along the axial extent thereof.
    Type: Application
    Filed: October 24, 2016
    Publication date: February 9, 2017
    Inventors: Brandon P. Williams, Kevin E. Thompson, Robert R. Fogarty
  • Publication number: 20130068856
    Abstract: A distributor for a pressure atomizer includes a distributor body having an upstream end defining an internal liquid circuit, a downstream end defining a spin chamber for swirling a liquid flowing therethrough, and an outboard peripheral surface extending from the upstream end to the downstream end. The upstream and downstream ends are spaced apart along a longitudinal axis. A inclined passage is defined in the outboard peripheral surface in fluid communication with the internal liquid circuit and with the spin chamber for producing a relatively wide spray angle for a given distributor body size. The inclined passage is angled to diverge from the longitudinal axis of the distributor body in a direction toward the downstream end.
    Type: Application
    Filed: September 21, 2011
    Publication date: March 21, 2013
    Applicant: Delavan Inc
    Inventors: Steve J. Myers, Robert R. Fogarty