Patents by Inventor Yann-Henri Laudrain

Yann-Henri Laudrain 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).

  • Publication number: 20200133245
    Abstract: A device for coordinated movement and/or orientation of a tracking tool relative to a portable tool handled by an operator on a production station allows a tracking tool to track the movements of a portable tool handled by an operator, without the intervention of an additional operator. Also described is a smoothing method using the device, as well as a smoothing station for implementing the method.
    Type: Application
    Filed: October 11, 2019
    Publication date: April 30, 2020
    Applicant: Airbus Operations S.A.S.
    Inventors: Yann-Henri Laudrain, Sébastien Martin
  • Patent number: 9827716
    Abstract: A process for direct fabrication of a part at a predetermined structural position. The process comprises: a) scanning, via a three-dimensional scanner, the structure in the region of the predetermined position; b) comparing a virtual surface mesh of the predetermined position with a real surface mesh of the predetermined position, the real surface mesh calculated based on data obtained from the scanning; c) determining the gaps between the two meshes; d) calculating the data for modeling an inserted part, the dimensions of which fill up the determined gaps, to obtain an inserted part model; e) merging of a virtual model of a part, linked with the predetermined position, with the inserted part model, to obtain a model adjusted to the geometry of the structure in the region of the predetermined position; f) fabricating, by material deposition, an adjusted part at the predetermined position based on the adjusted model.
    Type: Grant
    Filed: June 4, 2015
    Date of Patent: November 28, 2017
    Assignee: Airbus Operations (SAS)
    Inventor: Yann-Henri Laudrain
  • Publication number: 20150367579
    Abstract: A process for direct fabrication of a part at a predetermined structural position. The process comprises: a) scanning, via a three-dimensional scanner, the structure in the region of the predetermined position; b) comparing a virtual surface mesh of the predetermined position with a real surface mesh of the predetermined position, the real surface mesh calculated based on data obtained from the scanning; c) determining the gaps between the two meshes; d) calculating the data for modeling an inserted part, the dimensions of which fill up the determined gaps, to obtain an inserted part model; e) merging of a virtual model of a part, linked with the predetermined position, with the inserted part model, to obtain a model adjusted to the geometry of the structure in the region of the predetermined position; f) fabricating, by material deposition, an adjusted part at the predetermined position based on the adjusted model.
    Type: Application
    Filed: June 4, 2015
    Publication date: December 24, 2015
    Inventor: Yann-Henri Laudrain
  • Patent number: 9193460
    Abstract: Methods for transferring a payload such as passengers and/or luggage and/or freight between an airport and a cabin of an aircraft are provided. Air terminals, aircraft and removable cabin modules suitable for implementing these methods are also provided. An aircraft is provided which includes a removable cabin module. A docking module is also provided for transferring a removable cabin module between an aircraft and an airport. A method for modifying the internal configuration of the cabin of such an aircraft by replacing a removable cabin module of the aircraft is also provided.
    Type: Grant
    Filed: February 28, 2013
    Date of Patent: November 24, 2015
    Assignee: Airbus Operations (S.A.S.)
    Inventor: Yann-Henri Laudrain
  • Patent number: 8941817
    Abstract: Embodiments of the disclosure include methods in which locations within an aircraft fuselage are automatically pointed to and marked so that a part may be fastened at each marked location. A mobile assembly includes a video camera that may capture images of the aircraft fuselage. A plurality of predetermined locations may be visualized and verified by a successive implementation of a first image recognition process and a second image recognition process. The mobile assembly may then automatically point to the predetermined locations after each has been identified and mark each predetermined location.
    Type: Grant
    Filed: May 15, 2012
    Date of Patent: January 27, 2015
    Assignee: Airbus Operations (SAS)
    Inventors: Yann-Henri Laudrain, Marc Lelay
  • Publication number: 20130228651
    Abstract: Methods for transferring a payload such as passengers and/or luggage and/or freight between an airport and a cabin of an aircraft are provided. Air terminals, aircraft and removable cabin modules suitable for implementing these methods are also provided. An aircraft is provided which includes a removable cabin module. A docking module is also provided for transferring a removable cabin module between an aircraft and an airport. A method for modifying the internal configuration of the cabin of such an aircraft by replacing a removable cabin module of the aircraft is also provided.
    Type: Application
    Filed: February 28, 2013
    Publication date: September 5, 2013
    Applicant: AIRBUS OPERATIONS (S.A.S.)
    Inventor: Yann-Henri LAUDRAIN
  • Publication number: 20120300093
    Abstract: According to the invention, the system (1), composed of a mobile unit (2) comprising a video camera (3), points automatically a plurality of predetermined locations inside a structure (T) by a successive implementation of a first images recognition process and a second images recognition process by means of said video camera (3).
    Type: Application
    Filed: May 15, 2012
    Publication date: November 29, 2012
    Applicant: AIRBUS OPERATIONS SAS
    Inventors: Yann-Henri Laudrain, Marc Lelay
  • Publication number: 20080228454
    Abstract: The method for simulating bending of a tube by means of at least one bending machine comprises a step of calculating at least one cycle of bending commands (30, 35) related to at least one tube-manufacturing parameter as a function of a set of tube data (10) and of a set of technological data (20). There is obtained at least one three-dimensional geometric model (40) of at least one bending machine and associated mechanical tools as a function of at least one parameter (50) derived from the cycle of bending commands calculated in this way (30, 35). In accordance with the cycle of bending commands calculated in this way (35), obtaining a three-dimensional and kinematic simulation of the process in which the tube represented in this way by the set of tube data (10) is bent by means of at least one bending machine and associated mechanical tools represented in this way by the corresponding three-dimensional geometric model (40).
    Type: Application
    Filed: July 18, 2006
    Publication date: September 18, 2008
    Applicant: Airbus France
    Inventors: Yann-Henri Laudrain, Jean-Louis Lamotte