Patents by Inventor Irwin Pierre Robert KERNEMP

Irwin Pierre Robert KERNEMP 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).

  • Dimensioning of the skeleton angle of the trailing edge of the arms crossing the by-pass flow of a turbofan
    Patent number: 11221020
    Abstract: A part or an assembly of parts of a splitter stage of a turbofan, including a plurality of obstacles including at least one a blade and at least one arm, and a platform from which the obstacles extend, wherein the arm is defined by a skeleton angle having a trailing value on the trailing edge of between 3° and 15°.
    Type: Grant
    Filed: September 2, 2016
    Date of Patent: January 11, 2022
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Ghislain Maxime Romuald Madiot, Jean Bertucchi, Damien Joseph Cellier, Irwin Pierre Robert Kernemp, Aurelien Mazzella
  • Heat exchanger fitted with upstream cover to reduce disturbance to fluid flow in a turbomachine
    Patent number: 10837706
    Abstract: A heat exchanger designed to be fixed to a turbomachine wall delimiting a gas flow stream, this exchanger including a body with a front face through which the gas flow passes; an attachment face to the wall; an external face opposite the attachment face and connected to the front face; two lateral faces connected to the front face; a cover surrounding the front face and extending along the prolongation of the external face and the lateral faces, to delimit an intake with an area smaller than the area of the front face, this intake being located upstream from the front face relative to the gas flow stream.
    Type: Grant
    Filed: June 8, 2018
    Date of Patent: November 17, 2020
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Romain Jean-Claude Ferrier, Irwin Pierre Robert Kernemp, Jonathan David Robert Langridge
  • DIMENSIONING OF THE SKELETON ANGLE OF THE TRAILING EDGE OF THE ARMS CROSSING THE BY-PASS FLOW OF A TURBOFAN
    Publication number: 20180252230
    Abstract: A part or an assembly of parts of a splitter stage of a turbofan, including a plurality of obstacles including at least one a blade and at least one arm, and a platform from which the obstacles extend, wherein the arm is defined by a skeleton angle having a trailing value on the trailing edge of between 3° and 15°.
    Type: Application
    Filed: September 2, 2016
    Publication date: September 6, 2018
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Ghislain Maxime Romuald MADIOT, Jean BERTUCCHI, Damien Joseph CELLIER, Irwin Pierre Robert KERNEMP, Aurelien MAZZELLA