Patents by Inventor Stephane Ortet

Stephane Ortet 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: 9310145
    Abstract: A device comprises equipment (101) with a heat source, a cold part (102) relative to the equipment, and a thermal conductor element (103) capable of conducting the heat from the equipment to the cold part. The element (103) is such that, under certain thermal conditions above a given thermal condition, the equipment and the cold part are essentially thermally isolated.
    Type: Grant
    Filed: December 17, 2012
    Date of Patent: April 12, 2016
    Assignee: AIRBUS OPERATIONS S.A.S.
    Inventors: Emile Colongo, Stephane Ortet
  • Patent number: 9046567
    Abstract: An equipment burn-in method, which includes the equipment undergoing treatment in an oven, the oven undergoing cycles including at least one temperature-rise and/or temperature-fall transition, for which ventilation of the equipment is cut off during at least part of a temperature transition of the oven.
    Type: Grant
    Filed: June 23, 2009
    Date of Patent: June 2, 2015
    Assignee: AIRBUS OPERATIONS S.A.S.
    Inventor: Stephane Ortet
  • Patent number: 8576577
    Abstract: The invention relates to avionics equipment including a motherboard (108), at least one daughterboard (150) and, for each daughterboard, two supporting slides (116) attached directly to the motherboard and bearing the daughterboard. The invention also includes at least one mechanical connecting part (122A to 122D, 128A, 128B) between the motherboard (108) and at least one of the following: a backplane board (112) connected to an avionic connector (124), an avionic connector (124) and the rear face (106) of the avionics equipment.
    Type: Grant
    Filed: May 29, 2008
    Date of Patent: November 5, 2013
    Assignee: Airbus Operations SAS
    Inventor: Stephane Ortet
  • Publication number: 20130098594
    Abstract: A device comprises equipment (101) with a heat source, a cold part (102) relative to the equipment, and a thermal conductor element (103) capable of conducting the heat from the equipment to the cold part. The element (103) is such that, under certain thermal conditions above a given thermal condition, the equipment and the cold part are essentially thermally isolated.
    Type: Application
    Filed: December 17, 2012
    Publication date: April 25, 2013
    Inventors: Emile COLONGO, Stephane Ortet
  • Patent number: 8148644
    Abstract: An electronic card that includes at least two superimposed conducting layers with an insulation layer between the two conducting layers, the two conducting layers each including a utility conducting portion and a conducting portion at the periphery of the utility conducting portion with an insulating portion between the conducting portions, the insulating portion of a first of the two layers being offset relative to the insulating portion of the second of the layers. An aircraft includes a housing in which at least one such card is provided.
    Type: Grant
    Filed: February 18, 2008
    Date of Patent: April 3, 2012
    Assignee: Airbus Operations SAS
    Inventors: Stephane Ortet, Vincent Rebeyrotte, David Rousset
  • Publication number: 20110169514
    Abstract: An equipment burn-in method, which includes the equipment undergoing treatment in an oven, the oven undergoing cycles including at least one temperature-rise and/or temperature-fall transition, for which ventilation of the equipment is cut off during at least part of a temperature transition of the oven.
    Type: Application
    Filed: June 23, 2009
    Publication date: July 14, 2011
    Applicant: AIRBUS OPERATIONS (inc. as a Soc. par Act. Simpl.)
    Inventor: Stephane Ortet
  • Publication number: 20100319965
    Abstract: An electronic card that includes at least two superimposed conducting layers with an insulation layer between the two conducting layers, the two conducting layers each including a utility conducting portion and a conducting portion at the periphery of the utility conducting portion with an insulating portion between the conducting portions, the insulating portion of a first of the two layers being offset relative to the insulating portion of the second of the layers. An aircraft includes a housing in which at least one such card is provided.
    Type: Application
    Filed: February 18, 2008
    Publication date: December 23, 2010
    Inventors: Stephane Ortet, Vincent Rebeyrotte, David Rousset
  • Publication number: 20100188831
    Abstract: The invention relates to avionics equipment including a motherboard (108), at least one daughterboard (150) and, for each daughterboard, two supporting slides (116) attached directly to the motherboard and bearing the daughterboard. The invention also includes at least one mechanical connecting part (122A to 122D, 128A, 128B) between the motherboard (108) and at least one of the following: a backplane board (112) connected to an avionic connector (124), an avionic connector (124) and the rear face (106) of the avionics equipment.
    Type: Application
    Filed: May 29, 2008
    Publication date: July 29, 2010
    Applicant: Airbus Operations
    Inventor: Stephane Ortet
  • Publication number: 20100012311
    Abstract: A device comprises equipment (101) with a heat source, a cold part (102) relative to the equipment, and a thermal conductor element (103) capable of conducting the heat from the equipment to the cold part. The element (103) is such that, under certain thermal conditions above a given thermal condition, the equipment and the cold part are essentially thermally isolated.
    Type: Application
    Filed: July 17, 2007
    Publication date: January 21, 2010
    Applicant: Airbus France
    Inventors: Emile Colongo, Stephane Ortet
  • Publication number: 20090283251
    Abstract: A device comprises equipment (501) with a heat source having a maximum thermal operation condition, a cold part (502) relative to the equipment and an element (503) capable of transmitting the heat from the equipment to the cold part. The element (503) is capable of causing the transmitted heat to be limited for thermal conditions above a specified threshold below said maximum condition.
    Type: Application
    Filed: July 17, 2007
    Publication date: November 19, 2009
    Applicant: Airbus France
    Inventors: Emile Colongo, Stephane Ortet