Patents by Inventor Remi STEPHAN

Remi STEPHAN 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: 11359748
    Abstract: A connection system comprising: a dispensing member; a receiving member; first sealing means and second sealing means arranged at the interface between the dispensing member and the receiving member to enable redundant leak-tight engagement between the dispensing member and the receiving member; a control chamber defined between the first sealing means and the second sealing means; and means for measuring the current pressure in the control chamber so as to detect a gas leak.
    Type: Grant
    Filed: September 21, 2018
    Date of Patent: June 14, 2022
    Assignee: SAFRAN POWER UNITS
    Inventors: Rémi Stephan, Matthieu Baron, Théophile Horde
  • Publication number: 20200217436
    Abstract: A connection system comprising: a dispensing member; a receiving member; first sealing means and second sealing means arranged at the interface between the dispensing member and the receiving member to enable redundant leak-tight engagement between the dispensing member and the receiving member; a control chamber defined between the first sealing means and the second sealing means; and means for measuring the current pressure in the control chamber so as to detect a gas leak.
    Type: Application
    Filed: September 21, 2018
    Publication date: July 9, 2020
    Applicant: SAFRAN POWER UNITS
    Inventors: Rémi Stephan, Matthieu Baron, Théophile Horde
  • Publication number: 20180195437
    Abstract: A turbomachine air starter, including a first compartment wherein non-overrunning elements of the air starter are situated, corresponding to elements which are only run in the turbomachine starting phase, and a second compartment wherein overrunning elements of the air starter are situated, corresponding to the elements which are run throughout an operating time of the turbomachine, including the starting phase. The first compartment includes an oil receptacle for oil splash lubrication of the non-overrunning elements, and the second compartment includes an AWC type oil cavity for lubrication of the overrunning elements supplied by the lubrication oil return of the overrunning elements, in turn supplied with pressurized lubrication oil supplied by the turbomachine, the receptacle and the cavity being internal to the air starter.
    Type: Application
    Filed: December 19, 2014
    Publication date: July 12, 2018
    Applicant: MICROTURBO
    Inventors: Remi STEPHAN, Pierre Charles MOUTON