Patents by Inventor Thierry LOUPIAS

Thierry LOUPIAS 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: 8998142
    Abstract: A device for linking a frame and a stringer of an aircraft structure, including a first portion connected to a support surface of a frame, a second portion connected to a support surface of a stringer and a third portion referred to as intermediary portion connecting the first portion to the second portion. The second portion is connected to the intermediary portion by means of an articulation allowing for a relative movement between the two portions along a rotation axis perpendicular to the support surface of the stringer. The first portion is connected to the intermediary portion by means of an articulation allowing for a relative movement between the two portions along a rotation axis parallel to the support surface of the frame and to the support surface of the stringer.
    Type: Grant
    Filed: August 31, 2012
    Date of Patent: April 7, 2015
    Assignee: Airbus Operations (SAS)
    Inventor: Thierry Loupias
  • Patent number: 8840066
    Abstract: A front part of an aircraft fuselage according to this invention comprises: frames (16) disposed transversely in relation to a longitudinal axis of the aircraft, an outer skin (14) fastened onto the frames (16), a landing-gear (2) stowage compartment comprising among other things longitudinal side walls (10) borne by frames (16), a panel (26) between each longitudinal side wall (10) and the outer skin (14) achieving sealing between the interior and the exterior of the aircraft.
    Type: Grant
    Filed: December 9, 2011
    Date of Patent: September 23, 2014
    Assignee: AIRBUS Operations S.A.S.
    Inventors: Thierry Loupias, Patrick Gouarderes
  • Publication number: 20130062470
    Abstract: A device for linking a frame and a stringer of an aircraft structure, including a first portion connected to a support surface of a frame, a second portion connected to a support surface of a stringer and a third portion referred to as intermediary portion connecting the first portion to the second portion. The second portion is connected to the intermediary portion by means of an articulation allowing for a relative movement between the two portions along a rotation axis perpendicular to the support surface of the stringer. The first portion is connected to the intermediary portion by means of an articulation allowing for a relative movement between the two portions along a rotation axis parallel to the support surface of the frame and to the support surface of the stringer.
    Type: Application
    Filed: August 31, 2012
    Publication date: March 14, 2013
    Applicant: AIRBUS OPERATIONS (SAS)
    Inventor: Thierry Loupias
  • Publication number: 20120153078
    Abstract: A front part of an aircraft fuselage according to this invention comprises: frames (16) disposed transversely in relation to a longitudinal axis of the aircraft, an outer skin (14) fastened onto the frames (16), a landing-gear (2) stowage compartment comprising among other things longitudinal side walls (10) borne by frames (16), a panel (26) between each longitudinal side wall (10) and the outer skin (14) achieving sealing between the interior and the exterior of the aircraft.
    Type: Application
    Filed: December 9, 2011
    Publication date: June 21, 2012
    Applicant: Airbus Operations (S.A.S.)
    Inventors: Thierry LOUPIAS, Patrick GOUARDERES