Patents by Inventor Rene Bosson

Rene Bosson 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: 10571295
    Abstract: A method and device for monitoring an avionics software application via its execution duration, related computer program and avionics system are disclosed. In one aspect, the method, executed on a platform hosting an operating system, is implemented by an electronic monitoring device. The avionics software application includes one or several software processing operations to be executed, the platform is configured to be on board an aircraft. The method includes: monitoring the execution duration of the avionics software application, through the verification, upon expiration of at least one predefined execution times, of the completion of the execution of at least one software processing operation of the avionics software application; and updating a status of the avionics software application based on the monitoring of the execution duration of the avionics software application.
    Type: Grant
    Filed: October 8, 2018
    Date of Patent: February 25, 2020
    Assignee: Thales
    Inventors: Marc Fumey, Joël Henri René Bosson, Tarik Aegerter, Yves Meyer, Hubert Lacquit
  • Publication number: 20190107415
    Abstract: A method and device for monitoring an avionics software application via its execution duration, related computer program and avionics system are disclosed. In one aspect, the method, executed on a platform hosting an operating system, is implemented by an electronic monitoring device. The avionics software application includes one or several software processing operations to be executed, the platform is configured to be on board an aircraft. The method includes: monitoring the execution duration of the avionics software application, through the verification, upon expiration of at least one predefined execution times, of the completion of the execution of at least one software processing operation of the avionics software application; and updating a status of the avionics software application based on the monitoring of the execution duration of the avionics software application.
    Type: Application
    Filed: October 8, 2018
    Publication date: April 11, 2019
    Inventors: Marc Fumey, Joël Henri René BOSSON, Tarik AEGERTER, Yves MEYER, Hubert LACQUIT
  • Patent number: 5427498
    Abstract: The centrifugal pump with an open-faced impeller comprises at least one open-faced impeller having blades placed inside a casing defining both a delivery pipe and a suction pipe facing the base of the blades situated in the vicinity of a central shaft for driving the impeller. An active axial balancing system for the rotary assembly is integrated in the impeller and comprises a balancing chamber interposed between the rear face of the body of the impeller and an outer rear portion of the casing, the impeller itself acting as the balancing turntable. A shroud-forming intermediate part is prevented from rotating relative to the casing and is interposed between an outer front portion of the casing and the impeller, a cavity is formed between the outer front portion of the casing and the intermediate part to receive a back pressure of predetermined value serving, in operation, to maintain small clearance without contact between the intermediate part that is prevented from rotating and the blades of the impeller.
    Type: Grant
    Filed: November 24, 1993
    Date of Patent: June 27, 1995
    Assignee: Societe Europeenne de Propulsion
    Inventors: Jean-Robert Lehe, Andre Beaurain, Rene Bosson, Etienne Tiret
  • Patent number: 5385442
    Abstract: A centrifugal pump with an open-faced impeller for conveying a working liquid, the pump comprising at least one open-faced impeller provided with blades placed inside a casing defining a suction pipe facing the bottoms of the blades in the vicinity of a central shaft that drives the impeller and forming a part of a rotary assembly, and a delivery pipe fitted with a fixed diffuser disposed facing the peripheral ends of the blades. An active axial balancing system for the rotary assembly, which balancing system is integrated in the impeller and comprises a balancing chamber interposed between the rear face of the body of the impeller and an outer rear portion of the casing.
    Type: Grant
    Filed: November 24, 1993
    Date of Patent: January 31, 1995
    Assignee: Societe Europeenne de Propulsion
    Inventors: Jean-Robert Lehe, Andre Beaurain, Rene Bosson, Etienne Tiret