Patents by Inventor Pierre G. J. Hebert

Pierre G. J. Hebert 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: 5520216
    Abstract: A rotary valve assembly is disclosed in which a rotary valve member is located within a casing having one or more fluid inlets and a plurality of fluid outlets. The rotary valve member has a fluid conduit which extends in a generally radial direction and which communicates with the fluid inlet. Fluid orifices communicate with the fluid conduit and exit through opposite sides of the rotary valve member to thereby minimize, or eliminate altogether, axial forces acting on the rotary valve member. Fluid outlet passages communicate with the two fluid orifices during at least pan of the rotation of the rotary valve member to direct the pressurized fluid to the valve outlets. The rotary valve may include a pair of rotary valve members drivingly connected to each other such that they rotate synchronously. The connection may include gear teeth formed on the adjacent peripheries of the rotary valve members such that rotation of one of the valve members causes rotation of the other.
    Type: Grant
    Filed: February 3, 1995
    Date of Patent: May 28, 1996
    Assignee: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation S.N.E.C.M.A.
    Inventors: Guv d'Agostino, Jean-Marie Brocard, Pierre G. J. Hebert, Franck Liotte, Eric C. Lorne, Claude Maillard, Alain Tiepel
  • Patent number: 5413143
    Abstract: A rotary valve assembly is disclosed in which a rotary valve member is located within a casing having one or more fluid inlets and a plurality of fluid outlets. The rotary valve member has a fluid conduit which extends in a generally radial direction and which communicates with the fluid inlet. Fluid orifices communicate with the fluid conduit and exit through opposite sides of the rotary valve member to thereby minimize, or eliminate altogether, axial forces acting on the rotary valve member. Fluid outlet passages communicate with the two fluid orifices during at least part of the rotation of the rotary valve member to direct the pressurized fluid to the valve outlets. The rotary valve may include a pair of rotary valve members drivingly connected to each other such that they rotate synchronously. The connection may include gear teeth formed on the adjacent peripheries of the rotary valve members such that rotation of one of the valve members causes rotation of the other.
    Type: Grant
    Filed: February 2, 1994
    Date of Patent: May 9, 1995
    Assignee: Societe Nationale D'Etude et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
    Inventors: Guy d'Agostino, Jean-Marie Brocard, Pierre G. J. Hebert, Franck Liotte, Eric C. Lorne, Claude Maillard, Alain Tiepel
  • Patent number: 5307838
    Abstract: A rotary valve assembly is disclosed in which a rotary valve member is located within a casing having one or more fluid inlets and a plurality of fluid outlets. The rotary valve member has a fluid conduit which extends in a generally radial direction and which communicates with the fluid inlet. Fluid orifices communicate with the fluid conduit and exit through opposite sides of the rotary valve member to thereby minimize, or eliminate altogether, axial forces acting on the rotary valve member. Fluid outlet passages communicate with the two fluid orifices during at least part of the rotation of the rotary valve member to direct the pressurized fluid to the valve outlets. The rotary valve may include a pair of rotary valve members drivingly connected to each other such that they rotate synchronously. The connection may include gear teeth formed on the adjacent peripheries of the rotary valve members such that rotation of one of the valve members causes rotation of the other.
    Type: Grant
    Filed: January 7, 1993
    Date of Patent: May 3, 1994
    Assignee: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (S.N.E.C.M.A)
    Inventors: Guy d'Agostino, Jean-Marie Brocard, Pierre G. J. Hebert, Franck Liotte, Eric C. Lorne, Claude Maillard, Alain Tiepel
  • Patent number: 5284020
    Abstract: A system for supplying fuel to a plurality of fuel injectors of a gas turbine engine is disclosed having first and second fuel distributors and a fuel transfer device which enables fuel to flow from the fuel source to the first and second fuel distributors as a function of the fuel flow rate. The fuel transfer device enables fuel to flow through the first fuel distributor under low fuel flow conditions. The first fuel distributor sequentially supplies fuel to each of a plurality of groups of fuel injectors when the fuel flow rate is below a predetermined threshold value. When the fuel flow exceeds a high threshold value, the fuel transfer device enables fuel to flow through the second fuel distributor which supplies fuel to all of the fuel injectors of the engine.
    Type: Grant
    Filed: December 14, 1992
    Date of Patent: February 8, 1994
    Assignee: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation ("S.N.E.C.M.A.")
    Inventors: Jean-Marie Brocard, Pierre G. J. Hebert, Thierry N. de Jongh