Patents by Inventor Jérémy Giordan

Jérémy Giordan 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: 10871402
    Abstract: A device for measuring the characteristics of an air flow intended to be mounted in an annular duct having a longitudinal axis in a turbine engine, comprising supporting means which support means for measuring the characteristics of an air flow. According to the invention, the supporting means comprise at least one first support including a main branch supporting first measuring means and a second support, structurally independent of the first support and including a main branch supporting second measuring means, with the first support and the second support being so formed that the main branch of the first support extends over a distance greater than the main branch of the second support in a common direction of extension of the branches.
    Type: Grant
    Filed: March 29, 2018
    Date of Patent: December 22, 2020
    Assignee: Safran Aircraft Engines
    Inventors: Jérémy Giordan, Florian Joseph Bernard Kockenpo, Thibault Xavier Alexis Berranger, Pascal Léon Georges Beilvert
  • Patent number: 10519801
    Abstract: An annular air flow passage, particularly for a turbine engine, comprising two radially internal and external annular walls. A measuring element is elongated in a direction between the internal and external annular walls, and a first of the internal or external ends of the element is fixed rigidly to a first of the internal or external walls. The element includes at least one tubular cavity extending along the element and supplied with pressurized fluid.
    Type: Grant
    Filed: November 29, 2016
    Date of Patent: December 31, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Jérémy Giordan, Valentine Lucette Bader, André Pierre Jean Xavier Leroux, Stéphane Rousselin
  • Publication number: 20180283960
    Abstract: A device for measuring the characteristics of an air flow intended to be mounted in an annular duct having a longitudinal axis in a turbine engine, comprising supporting means which support means for measuring the characteristics of an air flow. According to the invention, the supporting means comprise at least one first support including a main branch supporting first measuring means and a second support, structurally independent of the first support and including a main branch supporting second measuring means, with the first support and the second support being so formed that the main branch of the first support extends over a distance greater than the main branch of the second support in a common direction of extension of the branches.
    Type: Application
    Filed: March 29, 2018
    Publication date: October 4, 2018
    Applicant: Safran Aircraft Engines
    Inventors: Jérémy Giordan, Florian Joseph Bernard Kockenpo, Thibault Xavier Alexis Berranger, Pascal Léon Georges Beilvert
  • Publication number: 20170152757
    Abstract: An annular air flow passage, particularly for a turbine engine, comprising two radially internal and external annular walls. A measuring element is elongated in a direction between the internal and external annular walls, and a first of the internal or external ends of the element is fixed rigidly to a first of the internal or external walls. The element includes at least one tubular cavity extending along the element and supplied with pressurized fluid.
    Type: Application
    Filed: November 29, 2016
    Publication date: June 1, 2017
    Applicant: Safran Aircraft Engines
    Inventors: Jérémy Giordan, Valentine Lucette Bader, André Pierre Jean Xavier Leroux, Stéphane Rousselin