Patents by Inventor Thibault JAMON

Thibault JAMON 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: 10618665
    Abstract: A turbomachine casing (10) comprising an endoscopy port (12) and a member (14) mounted on and fixed to the casing and comprising a duct (16) that communicates with the port and that comprises an internal thread into which a cap (28) can be screwed, and means (22, 26) for fixing the member to the casing, characterised in that it further comprises a cover (30) mounted on the member and at least partially covering the fixing means in order to hinder, or indeed prevent, access to same when the cover is mounted on the member, the cover being arranged to allow free access to the duct when the cap is not screwed into the duct.
    Type: Grant
    Filed: May 28, 2014
    Date of Patent: April 14, 2020
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Florence Irene Noelle Leutard, Didier Noel Durand, Thibault Jamon
  • Patent number: 10502083
    Abstract: A turbomachine element includes a stator, a rotor, and a first sealing means for sealing between the rotor and the stator. The element is arranged to be active when the rotor is in the operating position of same around the axis of rotation thereof. The element includes an auxiliary pressure sealing means, sealing between the rotor and the stator and is arranged so that the two sealing means are active when the rotor is placed along the axis of rotation thereof during an assembly operation in a test position. In the test position, the rotor and the stator form an enclosure between said two sealing means.
    Type: Grant
    Filed: July 21, 2015
    Date of Patent: December 10, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Florence Irène Noëlle Leutard, Thibault Jamon, Olivier Renon
  • Publication number: 20170152754
    Abstract: A turbomachine element includes a stator, a rotor, and a first sealing means for sealing between the rotor and the stator. The element is arranged to be active when the rotor is in the operating position of same around the axis of rotation thereof. The element includes an auxiliary pressure sealing means, sealing between the rotor and the stator and is arranged so that the two sealing means are active when the rotor is placed along the axis of rotation thereof during an assembly operation in a test position. In the test position, the rotor and the stator form an enclosure between said two sealing means.
    Type: Application
    Filed: July 21, 2015
    Publication date: June 1, 2017
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Florence Irène Noëlle Leutard, Thibault Jamon, Olivier Renon
  • Publication number: 20160194088
    Abstract: A turbomachine casing (10) comprising an endoscopy port (12) and a member (14) mounted on and fixed to the casing and comprising a duct (16) that communicates with the port and that comprises an internal thread into which a cap (28) can be screwed, and means (22, 26) for fixing the member to the casing, characterised in that it further comprises a cover (30) mounted on the member and at least partially covering the fixing means in order to hinder, or indeed prevent, access to same when the cover is mounted on the member, the cover being arranged to allow free access to the duct when the cap is not screwed into the duct.
    Type: Application
    Filed: May 28, 2014
    Publication date: July 7, 2016
    Inventors: Florence Irene Noelle LEUTARD, Didier Noel DURAND, Thibault JAMON