Patents by Inventor Ghislain Maxime Romuald MADIOT

Ghislain Maxime Romuald MADIOT 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).

  • A Method For Improving Fuel Pyrolysis In A Wave Reformer Using Channel Area Contraction
    Publication number: 20240092636
    Abstract: This invention is for a hydrogen generation system using a wave reformer in which shock and expansion waves are created in a manner causing head-on colliding shock waves and multi-stage compression where reacting gases within the wave reformer are heated and compressed to thermally crack or decompose one or more fuel sources, such as hydrocarbon fuels, to generate a fuel product containing hydrogen, where the internal configuration of channels within the wave reformer are defined by a shaped portion along a length thereof.
    Type: Application
    Filed: September 19, 2023
    Publication date: March 21, 2024
    Applicant: New Wave Hydrogen, Inc.
    Inventors: Pejman Akbari, Colin D. Copeland, Stefan Tuechler, Ghislain Maxime Romuald Madiot
  • Dimensioning of the skeleton angle of the trailing edge of the arms crossing the by-pass flow of a turbofan
    Patent number: 11221020
    Abstract: A part or an assembly of parts of a splitter stage of a turbofan, including a plurality of obstacles including at least one a blade and at least one arm, and a platform from which the obstacles extend, wherein the arm is defined by a skeleton angle having a trailing value on the trailing edge of between 3° and 15°.
    Type: Grant
    Filed: September 2, 2016
    Date of Patent: January 11, 2022
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Ghislain Maxime Romuald Madiot, Jean Bertucchi, Damien Joseph Cellier, Irwin Pierre Robert Kernemp, Aurelien Mazzella
  • Intermediate housing hub comprising discharge flow guiding channels formed by the discharge fins
    Patent number: 11053846
    Abstract: The invention relates to an intermediate housing hub (2) comprising a discharge stream conduit (18) having a given length (L1), and discharge fins (22) extending in the discharge stream conduit (18) and having a given chord length (L2), the chord length (L2) of at least one of the discharge fins (22) being at least equal to 50% of the length of conduit (L1).
    Type: Grant
    Filed: December 28, 2017
    Date of Patent: July 6, 2021
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Julien Antoine Henri Jean Szydlowski, Romain Nicolas Lagarde, Ghislain Maxime Romuald Madiot, Benjamin Lukowski
  • Pylon of a propulsion unit
    Patent number: 11047300
    Abstract: A disclosed propulsion unit includes a pylon having a blade presenting a chord Cx and a downstream arm having a structural arm. The pylon has a first distance D between a trailing edge of a fan blade and a leading edge of the fan blade, a second distance d between said trailing edge of the blade and a leading edge of the structural arm, and a third distance L between the trailing edge of the blade and a mark located at a maximum thickness of the downstream arm. The pylon is dimensioned according to: a first quotient between D and Cx between 2.2 and 2.6, a second quotient between d and Cx between 1 and 1.2, and a third quotient between L and Cx between 4 and 7.
    Type: Grant
    Filed: November 21, 2018
    Date of Patent: June 29, 2021
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Hélène Madeleine Nicole Deparis, Pierre Grégoire Anton, Pradeep Cojande, Ghislain Maxime Romuald Madiot
  • INTERMEDIATE HOUSING HUB COMPRISING DISCHARGE FLOW GUIDING CHANNELS FORMED BY THE DISCHARGE FINS
    Publication number: 20190345875
    Abstract: The invention relates to an intermediate housing hub (2) comprising a discharge stream conduit (18) having a given length (L1), and discharge fins (22) extending in the discharge stream conduit (18) and having a given chord length (L2), the chord length (L2) of at least one of the discharge fins (22) being at least equal to 50% of the length of conduit (L1).
    Type: Application
    Filed: December 28, 2017
    Publication date: November 14, 2019
    Inventors: Julien Antoine Henri Jean SZYDLOWSKI, Romain Nicolas LAGARDE, Ghislain Maxime Romuald MADIOT, Benjamin LUKOWSKI
  • PYLON OF A PROPULSION UNIT
    Publication number: 20190153940
    Abstract: A disclosed propulsion unit includes a pylon having a blade presenting a chord Cx and a downstream arm having a structural arm. The pylon has a first distance D between a trailing edge of a fan blade and a leading edge of the fan blade, a second distance d between said trailing edge of the blade and a leading edge of the structural arm, and a third distance L between the trailing edge of the blade and a mark located at a maximum thickness of the downstream arm. The pylon is dimensioned according to: a first quotient between D and Cx between 2.2 and 2.6, a second quotient between d and Cx between 1 and 1.2, and a third quotient between L and Cx between 4 and 7.
    Type: Application
    Filed: November 21, 2018
    Publication date: May 23, 2019
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Hélène Madeleine Nicole Deparis, Pierre Grégoire Anton, Pradeep Cojande, Ghislain Maxime Romuald Madiot
  • DIMENSIONING OF THE SKELETON ANGLE OF THE TRAILING EDGE OF THE ARMS CROSSING THE BY-PASS FLOW OF A TURBOFAN
    Publication number: 20180252230
    Abstract: A part or an assembly of parts of a splitter stage of a turbofan, including a plurality of obstacles including at least one a blade and at least one arm, and a platform from which the obstacles extend, wherein the arm is defined by a skeleton angle having a trailing value on the trailing edge of between 3° and 15°.
    Type: Application
    Filed: September 2, 2016
    Publication date: September 6, 2018
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Ghislain Maxime Romuald MADIOT, Jean BERTUCCHI, Damien Joseph CELLIER, Irwin Pierre Robert KERNEMP, Aurelien MAZZELLA