Patents by Inventor Alain Decocq

Alain Decocq 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: 11143031
    Abstract: A tool for balancing a turbine engine module in a balancer, the module including a stator, a rotor and a shaft, the balancer including at least one power drive unit and a table equipped with two support of the shaft of the module. The tool includes at least: one stator support, fixed on the table of the balancer behind the supports, a tubular false bearing, configured to support a bearing for guiding the rotor in the stator and protruding outside of the stator, a guiding sleeve of the shaft, confining a support of the false bearing, and received on the supports of the balancer, a rear support plate of the stator, fixed to the support of the stator, and immobilising the rotor with respect to the stator, a front support plate of the stator, fixed to the stator support, and immobilising and centring the false bearing.
    Type: Grant
    Filed: October 30, 2019
    Date of Patent: October 12, 2021
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Alain Roland Luinaud, Alain Decocq
  • Publication number: 20200131908
    Abstract: A tool for balancing a turbine engine module in a balancer, the module including a stator, a rotor and a shaft, the balancer including at least one power drive unit and a table equipped with two support of the shaft of the module. The tool includes at least: one stator support, fixed on the table of the balancer behind the supports, a tubular false bearing, configured to support a bearing for guiding the rotor in the stator and protruding outside of the stator, a guiding sleeve of the shaft, confining a support of the false bearing, and received on the supports of the balancer, a rear support plate of the stator, fixed to the support of the stator, and immobilising the rotor with respect to the stator, a front support plate of the stator, fixed to the stator support, and immobilising and centring the false bearing.
    Type: Application
    Filed: October 30, 2019
    Publication date: April 30, 2020
    Inventors: Alain Roland LUINAUD, Alain DECOCQ
  • Patent number: 10197467
    Abstract: A calibration rotor for a horizontal balancer, configured to be driven by a driver. The calibration rotor includes a main barrel that has a longitudinal axis and the periphery of which includes points for attaching balance weights that are evenly distributed in an axial and angular manner about the axis. A rotation guide is arranged at each end of the main barrel. The rotor is modular, and the rotation guide includes adapters (40, 42) which are capable of being configured to be attached to the ends of the barrel. The guide is of a first type, suitable for rotatably guiding the barrel on rollers, or of a second type, suitable for rotatably guiding the half-shell barrel. Each type of adapter has the same predetermined moment of inertia and is interchangeable on the barrel.
    Type: Grant
    Filed: June 29, 2016
    Date of Patent: February 5, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Alain Roland Luinaud, Alain Decocq, Christophe Guengant
  • Patent number: 10190655
    Abstract: Tooling for balancing a turbine engine module (10) in a balancing machine, the turbine engine module having at least one stator housing (14) and a rotor (16) having a shaft (18) with a longitudinal axis A and at least one blade stage (20) surrounded by the stator housing (14). The tooling has at least a balancing frame (14), having rotor (16) guide bearings, first and second annular plates (30, 32) designed to be attached to the stator housing (14), third and fourth attachment lugs (34, 36) provided on the balancing frame (24), to attach the first and second annular plates (30, 32) to the frame. A trolley is for transporting the frame (24), and a support (84, 94) for supporting the frame, provided on the balancing frame (24) and cooperating equally well with the balancing machine and with the trolley.
    Type: Grant
    Filed: June 21, 2016
    Date of Patent: January 29, 2019
    Assignee: SNECMA
    Inventors: Alain Roland Luinaud, Alain Decocq, Francois Viviande
  • Publication number: 20180172111
    Abstract: The invention relates to tooling for balancing a turbine engine module (10) in a balancing machine, said module having at least one stator housing (14) and a rotor (16) having a shaft (18) with a longitudinal axis A and at least one blade stage (20) surrounded by said stator housing (14), said tooling having at least a balancing frame (14), having rotor (16) guide bearings, first and second means (30, 32) designed to be attached to said stator housing (14), third and fourth means (34, 36) provided on said frame (24), to attach said first and second means (30, 32) to said frame, fifth means for transporting the frame (24), and sixth means (84, 94) for supporting the frame, provided on said frame (24) and cooperating equally well with the balancing machine and with the fifth means for transporting the frame (24).
    Type: Application
    Filed: June 21, 2016
    Publication date: June 21, 2018
    Inventors: Alain Roland LUINAUD, Alain DECOCQ, Francois VIVIANDE
  • Publication number: 20180149544
    Abstract: A calibration rotor for a horizontal balancer, configured to be driven by a driver. The calibration rotor includes a main barrel that has a longitudinal axis and the periphery of which includes points for attaching balance weights that are evenly distributed in an axial and angular manner about the axis. A rotation guide is arranged at each end of the main barrel. The rotor is modular, and the rotation guide includes adapters (40, 42) which are capable of being configured to be attached to the ends of the barrel. The guide is of a first type, suitable for rotatably guiding the barrel on rollers, or of a second type, suitable for rotatably guiding the half-shell barrel. Each type of adapter has the same predetermined moment of inertia and is interchangeable on the barrel.
    Type: Application
    Filed: June 29, 2016
    Publication date: May 31, 2018
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Alain Roland Luinaud, Alain Decocq, Christophe Guengant