Patents by Inventor Sandra POUSSIN

Sandra POUSSIN 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: 8537214
    Abstract: The invention relates to a method for adjustment of a harmonization compensation applied to alleviate a discrepancy of conformity between a video image transmitted by a video transducer (1) and projected by a head-up display device (5, 6), of an aircraft, and an external scene ahead of the aircraft. At least one equipment item of the aircraft—preferably the said HUD device—equipped with at least one control element accessible in the cockpit, is programmed to be able to function according to a nominal mode and according to a maintenance mode, in which at least one of its control elements, known as a redirected control element, is used to define the applied harmonization compensation. An operator activates the maintenance mode and starts an adjustment operation, in which he modifies in real time the applied harmonization compensation, by manipulating at least one redirected control element, until the video image is matched with the external scene.
    Type: Grant
    Filed: August 13, 2009
    Date of Patent: September 17, 2013
    Assignee: Airbus Operations SAS
    Inventors: Sandra Poussin, David Bideau, Laurent Coloma, Stephane Gauthier
  • Patent number: 8416151
    Abstract: A set of equipment items for an aircraft including a video transducer and at least two head-up display devices, wherein the video transducer and/or each HUD device is/are capable of defining the image to be projected by the HUD device on the basis of the display field of the HUD device and of one or more HUD/transducer errors, each HUD/transducer error being defined as being the difference between the HUD error of the corresponding HUD support around a direction and the transducer error around this same direction, the HUD error of an HUD support around a direction being the angular difference around this direction between the line of sight of the HUD support and a measuring reference line, and the transducer error around a direction being the angular difference around this direction between the line of sight of the transducer support and a measuring reference line.
    Type: Grant
    Filed: February 16, 2010
    Date of Patent: April 9, 2013
    Assignee: Airbus Operations SAS
    Inventors: Sandra Poussin, David Bideau, Laurent Coloma, Stephane Gauthier
  • Publication number: 20100265162
    Abstract: The invention relates to a set of equipment items for an aircraft comprising a video transducer (1) and at least two head-up display devices (2, 3), characterized in that the video transducer (1) and/or each HUD device (2, 3) is/are capable of defining the image to be projected by the said HUD device on the basis of the display field of the said HUD device and of one or more HUD/transducer errors, each HUD/transducer error being defined as being the difference between the HUD error of the corresponding HUD support around a direction and the transducer error around this same direction, the HUD error of an HUD support around a direction being the angular difference around this direction between the line of sight of the said HUD support and a measuring reference line, and the transducer error around a direction being the angular difference around this direction between the line of sight of the transducer support and a measuring reference line.
    Type: Application
    Filed: February 16, 2010
    Publication date: October 21, 2010
    Applicant: Airbus Operations (S.A.S.)
    Inventors: Sandra Poussin, David Bideau, Laurent Coloma, Stéphane Gauthier
  • Publication number: 20100060730
    Abstract: The invention relates to a method for adjustment of a harmonization compensation applied to alleviate a discrepancy of conformity between a video image transmitted by a video transducer (1) and projected by a head-up display device (5, 6), of an aircraft, and an external scene ahead of the aircraft. At least one equipment item of the aircraft—preferably the said HUD device—equipped with at least one control element accessible in the cockpit, is programmed to be able to function according to a nominal mode and according to a maintenance mode, in which at least one of its control elements, known as a redirected control element, is used to define the applied harmonization compensation. An operator activates the maintenance mode and starts an adjustment operation, in which he modifies in real time the applied harmonization compensation, by manipulating at least one redirected control element, until the video image is matched with the external scene.
    Type: Application
    Filed: August 13, 2009
    Publication date: March 11, 2010
    Applicant: Airbus Operations
    Inventors: Sandra POUSSIN, David Bideau, Laurent Coloma, Stephane Gauthier