Patents by Inventor Damien Goujet

Damien Goujet 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: 11555522
    Abstract: A torque transmission system having multiple torque transmission pathways from a driving shaft to a driven shaft. The driving shaft extends from a lower segment to an upper segment via an intermediate segment, the driven shaft extending from a first segment to a second segment. The transmission system includes a nominal spline coupling that is operational in a nominal operating mode, a backup spline coupling between the driving shaft and the driven shaft that is inactive in the nominal operating mode, and a backup radial guide device between the driving shaft and the driven shaft that is inactive in the nominal operating mode.
    Type: Grant
    Filed: October 15, 2020
    Date of Patent: January 17, 2023
    Assignee: AIRBUS HELICOPTERS
    Inventor: Damien Goujet
  • Patent number: 11435029
    Abstract: A magnetic device for capturing metal wear particles in suspension in a lubrication fluid, the magnetic device being for inserting in a straight-line insertion direction of the magnetic device into a wall of a casing via a through orifice serving to put an inside volume of the casing containing the lubrication fluid into communication with an outside volume outside the casing, the magnetic device presenting a longitudinal axis X, the longitudinal axis X being for putting into coincidence with the direction for inserting the magnetic device into the casing, the magnetic device comprising a permanent magnet suitable for attracting the metal particles and a presence-detector member for detecting the metal particles attracted by the permanent magnet.
    Type: Grant
    Filed: September 18, 2019
    Date of Patent: September 6, 2022
    Assignee: AIRBUS HELICOPTERS
    Inventors: Benoit Basso, John Le Ru, Damien Goujet
  • Publication number: 20210130003
    Abstract: A torque transmission system having multiple torque transmission pathways from a driving shaft to a driven shaft. The driving shaft extends from a lower segment to an upper segment via an intermediate segment, the driven shaft extending from a first segment to a second segment. The transmission system includes a nominal spline coupling that is operational in a nominal operating mode, a backup spline coupling between the driving shaft and the driven shaft that is inactive in the nominal operating mode, and a backup radial guide device between the driving shaft and the driven shaft that is inactive in the nominal operating mode.
    Type: Application
    Filed: October 15, 2020
    Publication date: May 6, 2021
    Applicant: AIRBUS HELICOPTERS
    Inventor: Damien GOUJET
  • Publication number: 20200088350
    Abstract: A magnetic device for capturing metal wear particles in suspension in a lubrication fluid, the magnetic device being for inserting in a straight-line insertion direction of the magnetic device into a wall of a casing via a through orifice serving to put an inside volume of the casing containing the lubrication fluid into communication with an outside volume outside the casing, the magnetic device presenting a longitudinal axis X, the longitudinal axis X being for putting into coincidence with the direction for inserting the magnetic device into the casing, the magnetic device comprising a permanent magnet suitable for attracting the metal particles and a, presence-detector member for detecting the metal particles attracted by the permanent magnet.
    Type: Application
    Filed: September 18, 2019
    Publication date: March 19, 2020
    Applicant: AIRBUS HELICOPTERS
    Inventors: Benoit BASSO, John LE RU, Damien GOUJET
  • Patent number: 9829088
    Abstract: A triple circuit lubrication device for lubricating a mechanical system, the lubrication device being provided with two independent lubrication circuits, a tank common to both lubrication circuits and containing a lubrication liquid, and a tertiary circuit in which a tertiary liquid flows. Each lubrication circuit comprises pipes, and respective pressure sensors, pumps, heat exchangers, spray nozzles, and suction points for sucking up the lubrication liquid situated in the tank. The second suction point is situated below the high first suction point. The tertiary circuit comprises a third pump, a third pressure sensor, the second heat exchanger, and a third heat exchanger, thus serving to cool the lubrication liquid flowing through the second lubrication circuit.
    Type: Grant
    Filed: October 28, 2015
    Date of Patent: November 28, 2017
    Assignee: AIRBUS HELICOPTERS
    Inventor: Damien Goujet
  • Publication number: 20160123456
    Abstract: A triple circuit lubrication device for lubricating a mechanical system, the lubrication device being provided with two independent lubrication circuits, a tank common to both lubrication circuits and containing a lubrication liquid, and a tertiary circuit in which a tertiary liquid flows. Each lubrication circuit comprises pipes, and respective pressure sensors, pumps, heat exchangers, spray nozzles, and suction points for sucking up the lubrication liquid situated in the tank. The second suction point is situated below the high first suction point. The tertiary circuit comprises a third pump, a third pressure sensor, the second heat exchanger, and a third heat exchanger, thus serving to cool the lubrication liquid flowing through the second lubrication circuit.
    Type: Application
    Filed: October 28, 2015
    Publication date: May 5, 2016
    Inventor: Damien GOUJET
  • Patent number: 8523686
    Abstract: A coupling means (10) extending along a longitudinal axis of symmetry (100) from a first plate (11) towards a second plate (12), which plates are connected together by a link member (20). Said link member (20) is provided with a first hub (21) secured to said first plate (11) and with a second hub (22) secured to said second plate (12), a first end section (21?) of the first hub (21) being connected to a second end section (22?) of the second hub (22) by link means (30), said link means (30) comprising a first web (31) connecting said first end section (21?) to a maximum section (33) of said link means (30), said link means (30) having a second web (32) connecting a second end section (22?) of said second hub (22) to said maximum section (33).
    Type: Grant
    Filed: September 14, 2011
    Date of Patent: September 3, 2013
    Assignee: Eurocopter
    Inventor: Damien Goujet
  • Publication number: 20120077607
    Abstract: A coupling means (10) extending along a longitudinal axis of symmetry (100) from a first plate (11) towards a second plate (12), which plates are connected together by a link member (20). Said link member (20) is provided with a first hub (21) secured to said first plate (11) and with a second hub (22) secured to said second plate (12), a first end section (21?) of the first hub (21) being connected to a second end section (22?) of the second hub (22) by link means (30), said link means (30) comprising a first web (31) connecting said first end section (21?) to a maximum section (33) of said link means (30), said link means (30) having a second web (32) connecting a second end section (22?) of said second hub (22) to said maximum section (33).
    Type: Application
    Filed: September 14, 2011
    Publication date: March 29, 2012
    Applicant: EUROCOPTER
    Inventor: Damien Goujet