Patents by Inventor Claude-Gaston Corbin

Claude-Gaston Corbin 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).

  • Instrumented flow passage of a turbine engine
    Patent number: 9856743
    Abstract: An annular air flow passage for a turbine engine such as a turbojet or a turboprop, crossed by an instrumented rod that includes mechanism(s) for measuring characteristics of a flow potentially traveling along the passage, the rod extending between an outer annular wall and an inner annular wall of the passage. Outer connection(s) fasten(s) an outer end of the instrumented rod to the outer wall in a manner that is rigid in all directions, and inner connection(s) fasten(s) an inner end of the instrumented rod to the inner wall, in a manner that is rigid in the circumferential direction and that has at least one degree of freedom to move in a first direction extending between the inner and outer walls of the passage and having at least a radial component.
    Type: Grant
    Filed: May 27, 2015
    Date of Patent: January 2, 2018
    Assignee: Safran Aircraft Engines
    Inventors: Florian Kockenpo, Jermone Acquaviva, Claude Gaston Corbin, Jeremy Giordan, Nicolas Seigneuret, Nicolas Lamarche
  • Instrumented flow passage of a turbine engine
    Publication number: 20150345335
    Abstract: The invention relates to an annular air flow passage (33) for a turbine engine such as a turbojet or a turboprop, crossed by an instrumented rod (50) that includes means for measuring characteristics of a flow potentially traveling along the passage, said rod extending between an outer annular wall (48) and an inner annular wall (42) of the passage. According to the invention, outer connection means (60, 86) fasten an outer end (58) of the instrumented rod to the outer wall in a manner that is rigid in all directions, and inner connection means (62) fasten an inner end (56) of the instrumented rod to the inner wall, in a manner that is rigid in the circumferential direction and that has at least one degree of freedom to move in a first direction (51) extending between the inner and outer walls (42, 48) of the passage and having at least a radial component.
    Type: Application
    Filed: May 27, 2015
    Publication date: December 3, 2015
    Inventors: Florian Kockenpo, Jermone Acquaviva, Claude Gaston Corbin, Jeremy Giordan, Nicolas Seigneuret, Nicolas Lamarche
  • Turbomachine stator flap, and a method of manufacturing it
    Patent number: 6676378
    Abstract: A turbomachine stator flap including a structural beam which is formed integrally with a structural core for a vane, and fastening portions, and a composite envelope surrounding the structural core and forming at least the aerodynamic profile of the vane.
    Type: Grant
    Filed: December 10, 2001
    Date of Patent: January 13, 2004
    Assignee: SNECMA Moteurs
    Inventors: Claude-Gaston Corbin, Jean-Marie Le Francois, Cyrille Mathias
  • Turbomachine stator flap, and a method of manufacturing it
    Publication number: 20020071766
    Abstract: The flap comprises a structural beam which is formed integrally with a structural core for a vane, and fastening portions, and a composite envelope surrounding the structural core and forming at least the aerodynamic profile of the vane.
    Type: Application
    Filed: December 10, 2001
    Publication date: June 13, 2002
    Applicant: SNECMA MOTEURS
    Inventors: Claude-Gaston Corbin, Jean-Marie Le Francois, Cyrille Mathias