Patents by Inventor Philippe Beauverger

Philippe Beauverger 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: 8975250
    Abstract: The present invention relates to 5-oxo-5,8-dihydropyrido[2,3-d]pyrimidine derivatives having Formula (I) as defined herein, their preparation and their therapeutic use.
    Type: Grant
    Filed: July 9, 2012
    Date of Patent: March 10, 2015
    Assignee: SANOFI
    Inventors: Philippe Beauverger, Guillaume Begis, Sandrine Biscarrat, Olivier Duclos, Gary McCort
  • Publication number: 20120277220
    Abstract: The present invention relates to 5-oxo-5,8-dihydropyrido[2,3-d]pyrimidine derivatives, to their preparation and to their therapeutic use.
    Type: Application
    Filed: July 9, 2012
    Publication date: November 1, 2012
    Applicant: SANOFI
    Inventors: Philippe BEAUVERGER, Guillaume BEGIS, Sandrine BISCARRAT, Olivier DUCLOS, Gary MCCORT
  • Patent number: 8281599
    Abstract: The invention relates to a device for damping the lateral forces due to jet separation that act on a rocket engine nozzle during a stage of starting or stopping the engine, the engine including at least two identical drive assemblies mounted on the nozzle to take up the lateral forces acting thereon, each drive assembly comprising a first member forming a strut, a second member forming an anchor structure, and an actuator. Each strut comprises means enabling it to act as a rigid strut so long as the lateral forces acting on the corresponding actuator remain below a determined force threshold, and as an element for peak limiting force and for dissipating residual kinetic energy once the forces acting on the actuator exceed the determined force threshold.
    Type: Grant
    Filed: June 22, 2009
    Date of Patent: October 9, 2012
    Assignee: SNECMA
    Inventors: Philippe Even, Philippe Beauverger, Christelle Branchet, Frédérick Millon
  • Patent number: 7988202
    Abstract: A branch connection stub for connection to a main pipe. The branch connection stub presents an outside surface of revolution and has at least one axial internal passage, a rear segment with a fastener flange, an intermediate segment, and a front segment having a free end presenting a circular outline suitable for being mounting by plane welding around a circular opening in the wall of the main pipe. The intermediate segment includes a first wall and a second wall forming between them an acute angle towards the internal passage. The branch connection stub is applicable to a hot heat exchanger for rocket engines.
    Type: Grant
    Filed: February 20, 2009
    Date of Patent: August 2, 2011
    Assignee: SNECMA
    Inventors: Bruno Bucher, Claude Pomies, André Chauvin, Philippe Beauverger
  • Publication number: 20090314895
    Abstract: The invention relates to a device for damping the lateral forces due to jet separation that act on a rocket engine nozzle during a stage of starting or stopping the engine, the engine including at least two identical drive assemblies mounted on the nozzle to take up the lateral forces acting thereon, each drive assembly comprising a first member forming a strut, a second member forming an anchor structure, and an actuator. Each strut comprises means enabling it to act as a rigid strut so long as the lateral forces acting on the corresponding actuator remain below a determined force threshold, and as an element for peak limiting force and for dissipating residual kinetic energy once the forces acting on the actuator exceed the determined force threshold.
    Type: Application
    Filed: June 22, 2009
    Publication date: December 24, 2009
    Applicant: SNECMA
    Inventors: Philippe Even, Philippe Beauverger, Christelle Branchet, Frederick Millon
  • Publication number: 20090224025
    Abstract: The invention relates to a branch connection stub for connection to a main pipe. The branch connection stub presents an outside surface of revolution and has at least one axial internal passage, a rear segment with a fastener flange, an intermediate segment, and a front segment having a free end presenting a circular outline suitable for being mounting by plane welding around a circular opening in the wall of the main pipe, said intermediate segment comprising a first wall and a second wall forming between them an acute angle towards the internal passage. The invention is applicable to a hot heat exchanger for rocket engines.
    Type: Application
    Filed: February 20, 2009
    Publication date: September 10, 2009
    Applicant: SNECMA
    Inventors: Bruno Bucher, Claude Pomies, Andre Chauvin, Philippe Beauverger