Patents by Inventor Miles TRUMPER

Miles TRUMPER 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).

  • Aircraft gas turbine with variable bypass nozzle by deforming element
    Patent number: 8850824
    Abstract: The present invention relates to an aircraft gas turbine with a core engine which is surrounded by a bypass duct enclosed radially outwards by a bypass wall, with a radially inner wall of the bypass duct forming with the radially outer bypass wall a bypass nozzle, and with the radially inner wall including an adjusting element extending along the circumference of the inner wall and being deformable radially outwards.
    Type: Grant
    Filed: July 3, 2012
    Date of Patent: October 7, 2014
    Assignee: Rolls-Royce Deutschland Ltd & Co KG
    Inventors: Predrag Todorovic, Miles Trumper
  • Aircraft gas turbine with variable bypass nozzle
    Publication number: 20130008147
    Abstract: The present invention relates to an aircraft gas turbine with a core engine 10 which is surrounded by a bypass duct 29 enclosed radially outwards by a bypass wall 30, with a radially inner wall 31 of the bypass duct 29 forming with the radially outer bypass wall 30 a bypass nozzle 32, and with the radially inner wall 31 including an adjusting element 33 extending along the circumference of the inner wall 31 and being deformable radially outwards.
    Type: Application
    Filed: July 3, 2012
    Publication date: January 10, 2013
    Applicant: ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
    Inventors: Predrag TODOROVIC, Miles TRUMPER