Patents by Inventor Jonathan Carrotte

Jonathan Carrotte 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: 9562691
    Abstract: An airblast fuel injector is provided for a fuel spray nozzle of a gas turbine engine. The injector has an annular air passage for the passage of a swirling air flow therethrough. The swirling air flow is used by the injector to produce an atomized fuel spray. The air passage contains a swirler for producing the swirling air flow, the swirler comprising a circumferential row of vanes which span inner and outer side walls of the air passage. Viewed on a longitudinal section through the injector, the air passage has a bend downstream of the swirler, the bend changing the direction of the air passage. The vanes are configured to introduce a radial component to the air flow exiting the swirler, the radial component guiding the air flow around the bend.
    Type: Grant
    Filed: September 19, 2014
    Date of Patent: February 7, 2017
    Assignee: ROLLS-ROYCE plc
    Inventors: Christopher Ford, Ashley Gavin Barker, Alastair Duncan Walker, Jonathan Carrotte
  • Publication number: 20150089920
    Abstract: An airblast fuel injector is provided for a fuel spray nozzle of a gas turbine engine. The injector has an annular air passage for the passage of a swirling air flow therethrough. The swirling air flow is used by the injector to produce an atomised fuel spray. The air passage contains a swirler for producing the swirling air flow, the swirler comprising a circumferential row of vanes which span inner and outer side walls of the air passage. Viewed on a longitudinal section through the injector, the air passage has a bend downstream of the swirler, the bend changing the direction of the air passage. The vanes are configured to introduce a radial component to the air flow exiting the swirler, the radial component guiding the air flow around the bend.
    Type: Application
    Filed: September 19, 2014
    Publication date: April 2, 2015
    Inventors: Christopher FORD, Ashley Gavin BARKER, Alastair Duncan WALKER, Jonathan CARROTTE
  • Publication number: 20080087019
    Abstract: A combustion chamber for a gas turbine engine comprising at least one Helmholtz resonator having a resonator cavity and a resonator neck in flow communication with the interior of the combustion chamber. The cavity extends around at least part of the neck and is spaced apart therefrom to define a cooling chamber therebetween. The cooling chamber allows the neck and the cavity to be cooled with a flow of cooling air. The sunken neck allows the resonator to be located within enclosures with minimal volume without compromising on the damping properties afforded.
    Type: Application
    Filed: May 31, 2007
    Publication date: April 17, 2008
    Inventors: Michael Macquisten, Anthony Moran, Michael Whiteman, Jonathan Carrotte, Ashley Barker