Patents by Inventor Graham M Upton

Graham M Upton 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: 6582186
    Abstract: A vane assembly 40 for use within a gas turbine engine has a main vane portion 42 with an internal cavity 44. A cavity insert 46 is located within the cavity 44, close to the wall 48 to define transpiration cooling paths. Cooling air leaves the insert 46 through apertures directed at the wall 48, to produce impingement cooling. The transpiration cooling paths are extended back to the trailing edge 66 by means of a fairing 54. The use of a fairing in addition to the insert allows more complicated cavity shapes to be filled.
    Type: Grant
    Filed: August 10, 2001
    Date of Patent: June 24, 2003
    Assignee: Rolls-Royce plc
    Inventors: Rez Manzoori, Michael J L Percival, Graham M Upton
  • Publication number: 20020028133
    Abstract: A vane assembly 40 for use within a gas turbine engine has a main vane portion 42 with an internal cavity 44. A cavity insert 46 is located within the cavity 44, close to the wall 48 to define transpiration cooling paths. Cooling air leaves the insert 46 through apertures directed at the wall 48, to produce impingement cooling. The transpiration cooling paths are extended back to the trailing edge 66 by means of a fairing 54. The use of a fairing in addition to the insert allows more complicated cavity shapes to be filled.
    Type: Application
    Filed: August 10, 2001
    Publication date: March 7, 2002
    Inventors: Rez Manzoori, Michael J. L. Percival, Graham M. Upton