Patents by Inventor Jean-Luc Hubert Perrin

Jean-Luc Hubert Perrin 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: 7097432
    Abstract: A turbocharger having a variable geometry turbine inlet incorporating a cylindrical piston movable to vary the area of the inlet nozzle into the turbine. Vanes mounted to the piston for flow control in the nozzle are received through a slotted heat shield which provides smooth aerodynamic flow into the turbine blades. The vanes additionally incorporate a step having larger cord and depth that engages the surface of the heat shield and seals the slots with the piston in a closed position. An axial actuator is attached for operation of the piston.
    Type: Grant
    Filed: July 19, 2000
    Date of Patent: August 29, 2006
    Assignee: Honeywell International, Inc.
    Inventors: Alain Rene Lombard, Jean-Luc Hubert Perrin
  • Patent number: 7024855
    Abstract: A turbocharger having a variable geometry turbine inlet incorporates a piston movable to vary the area of the inlet nozzle into the turbine. Vanes extending from the heat shield for flow control in the nozzle are engaged by the piston in a first closed position. In a second open position, the piston is spaced from the vanes increasing the inlet nozzle area.
    Type: Grant
    Filed: November 30, 2000
    Date of Patent: April 11, 2006
    Assignee: Honeywell International, Inc.
    Inventors: Jean-Luc Hubert Perrin, Olivier Espasa, Marylene Ruffinoni, Alain Lombard, Philippe Joseph Muller
  • Patent number: 6694733
    Abstract: A turbocharger having a variable geometry turbine intake incorporating a mobile cylindrical piston (70) for varying the area of the induction nozzle in the turbine (18). Blades (90) mounted on the piston for controlling the flow in the nozzle penetrate through a slotted heat shield (92) having a central opening wherein the rear disc of the turbine wheel is embedded to provide a smooth aerodynamic flow in the turbine vanes. A shield (100) engaged between the heat screen and a central housing of the turbocharger prevents the gas from the rear disc cavity from recycling into the cavity housing the blades further enhancing the aerodynamic flow. An axial actuating device (77) is secured for operating the piston via a shaft coupled by a cross (72) to the piston and coupled to an actuating hub (118) in the actuating device by quick connect unthreaded connection (122).
    Type: Grant
    Filed: November 5, 2002
    Date of Patent: February 24, 2004
    Assignee: Honeywell Garrett SA
    Inventors: Luciano Labindo Bernardini, Alain Rene Lombard, Jean-Luc Hubert Perrin, Eric Joseph Viola
  • Publication number: 20040025504
    Abstract: The invention concerns a turbocharger with a variable geometry turbine comprising a mobile cylindrical piston (70) to modify the cross-section of the input nozzle to the turbine. Vanes (90) extending from a heat shield (92) for adjusting the flow of the nozzle are contacted by the piston in a first closed position. In a second open position, the piston is spaced apart from the vanes, thereby increasing the input nozzle cross-section.
    Type: Application
    Filed: April 28, 2003
    Publication date: February 12, 2004
    Inventors: Jean-Luc Hubert Perrin, Olivier Espasa, Marylene Ruffinoni, Alain Lombard, Philippe Joseph Muller