Patents by Inventor Laurent REGNAULT

Laurent REGNAULT 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: 11485505
    Abstract: An aircraft (10) is described as including a reference axis extending along at least a portion of the aircraft, and a propulsion system having a thrust vector feature (43) defining generally a direction of thrust of the turbofan engine (18), the thrust vector feature (43) extending relative to a thrust vector axis, where the turbofan engine (18) is disposed on the aircraft with the thrust vector feature (43) oriented with respect to the reference axis of the aircraft.
    Type: Grant
    Filed: May 27, 2016
    Date of Patent: November 1, 2022
    Assignees: BOMBARDIER INC., AIRBUS CANADA LIMITED PARTNERSHIP
    Inventors: Alexandros Iliopoulos, Laurent Regnault, Marcin Kulczyk, Alain Richer
  • Patent number: 10509388
    Abstract: There is described a method and system for reshaping a component for assembly that may have been deformed pre-assembly and post-fabrication. As-fabricated measurements are used to determine a baseline for the component and as-mounted measurements are used to determine a deformation parameter as a function of the baseline. The component may be reshaped using correction displacements applied to a positioning device of an assembly tool to which the component is mounted for assembly.
    Type: Grant
    Filed: May 29, 2015
    Date of Patent: December 17, 2019
    Assignee: C SERIES AIRCRAFT LIMITED PARTNERSHIP
    Inventors: Laurent Regnault, Sebastien Sirois
  • Patent number: 10459434
    Abstract: There is described herein an inspection tool for use during the inspection of components as manufactured. The inspection tool allows the comparison of measurement data with nominal data and provides complementary information with regards to at least one feature of the component.
    Type: Grant
    Filed: September 21, 2015
    Date of Patent: October 29, 2019
    Assignees: BOMBARDIER INC., C SERIES AIRCRAFT LIMITED PARTNERSHIP
    Inventor: Laurent Regnault
  • Publication number: 20180162540
    Abstract: An aircraft (10) is described as including a reference axis extending along at least a portion of the aircraft, and a propulsion system having a thrust vector feature (43) defining generally a direction of thrust of the turbofan engine (18), the thrust vector feature (43) extending relative to a thrust vector axis, where the turbofan engine (18) is disposed on the aircraft with the thrust vector feature (43) oriented with respect to the reference axis of the aircraft.
    Type: Application
    Filed: May 27, 2016
    Publication date: June 14, 2018
    Inventors: Alexandros ILIOPOULOS, Laurent REGNAULT, Marcin KULCZYK, Alain RICHER
  • Publication number: 20180050824
    Abstract: There are described herein methods and systems for manufacturing and/or assembling components having datum features thereon used to derive datum reference frames. The datum reference frames provided on the components may serve as both manufacturing and assembly datum reference frames.
    Type: Application
    Filed: March 10, 2016
    Publication date: February 22, 2018
    Inventors: Laurent REGNAULT, Alexandros ILIOPOULOS, Sebastien SIROIS
  • Publication number: 20170248940
    Abstract: There is described herein an inspection tool for use during the inspection of components as manufactured. The inspection tool allows the comparison of measurement data with nominal data and provides complementary information with regards to at least one feature of the component.
    Type: Application
    Filed: September 21, 2015
    Publication date: August 31, 2017
    Inventor: Laurent REGNAULT
  • Publication number: 20170205800
    Abstract: There is described a method and system for reshaping a component for assembly that may have been deformed pre-assembly and post-fabrication. As-fabricated measurements are used to determine a baseline for the component and as-mounted measurements are used to determine a deformation parameter as a function of the baseline. The component may be reshaped using correction displacements applied to a positioning device of an assembly tool to which the component is mounted for assembly.
    Type: Application
    Filed: May 29, 2015
    Publication date: July 20, 2017
    Inventors: Laurent REGNAULT, Sebastien SIROIS