Patents by Inventor Marcus Felipe HORI OCHI

Marcus Felipe HORI OCHI 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).

  • Retractable leading edge wing slats having autonomously curvable airflow shield for noise-abatement
    Patent number: 11492096
    Abstract: Noise-abatement for a leading edge wing slat is provided by a noise-abatement airflow shield integral with the lower trailing edge of the slat, wherein the shield is reciprocally autonomously curveable from a substantially planar configuration when the slat is in a retracted position thereof and into a convexly curved configuration when the slat is in a deployed position thereof.
    Type: Grant
    Filed: September 1, 2017
    Date of Patent: November 8, 2022
    Assignees: EMBRAER S.A., USP—UNIVERSIDADE DE SÃO PAULO
    Inventors: Danillo Cafaldo Dos Reis, Leandro Guilherme Crenite Simões, Micael Gianini Valle Do Carmo, Fábio Santos Da Silva, Eduardo Lobão Capucho Coelho, Leandro Souza De Moura Lima, Paulo Anchieta Da Silva, Fernando Martini Catalano, Cecil Wagner Skaleski, Francisco Keller Klug, Marcus Felipe Hori Ochi
  • Noise abatement systems for retractable leading edge wing slats of an aircraft wing assembly
    Patent number: 11427303
    Abstract: Noise-abatement systems provide noise abatement to a wing assembly provided with a forward edge slat and include an elongate shield element which is unconnected but positionable adjacent to a lower trailing edge of the edge slat along a lengthwise extent thereof, and a support web having a distal end fixed to the shield element and a proximal end capable of fixation to an interior cove surface of the edge slat adjacent an upper trailing edge thereof. The support web will therefore allow movement of the shield element towards and away from the lower trailing edge of the edge slat between an operative position wherein the shield element is positioned adjacent to the lower trailing edge of the edge slat along the lengthwise extent thereof and an inoperative position wherein the edge slat is spaced from the trailing edge of the edge slat and positioned in the cove region thereof, respectively.
    Type: Grant
    Filed: September 1, 2017
    Date of Patent: August 30, 2022
    Assignees: EMBRAER S.A., USP—UNIVERSIDADE DE SÃO PAULO
    Inventors: Danillo Cafaldo Dos Reis, Leandro Guilherme Crenite Simões, Micael Gianini Valle Do Carmo, Eduardo Lobão Capucho Coelho, Leandro Souza De Moura Lima, Fernando Martini Catalano, Cecil Wagner Skaleski, Francisco Keller Klug, Marcus Felipe Hori Ochi
  • NOISE ABATEMENT SYSTEMS FOR RETRACTABLE LEADING EDGE WING SLATS OF AN AIRCRAFT WING ASSEMBLY
    Publication number: 20210070422
    Abstract: A noise-abatement systems (10) provide noise abatement to a wing assembly (Wp) provided with a forward edge slat (ES) and include an elongated shield element (20) which is unconnected but positionable adjacent to a lower trailing edge (16a) of the edge slat (ES) along a lengthwise extent thereof, and a support tab (24) having a distal end fixed to the shield element (20) and a proximal end capable of fixation to an interior cove surface of the edge slat (ES) adjacent an upper trailing edge (22) thereof.
    Type: Application
    Filed: September 1, 2017
    Publication date: March 11, 2021
    Inventors: Danillo Cafaldo DOS REIS, Leandro Guilherme CRENITE SIMOES, Micael Gianini, Valle DO CARMO, Eduardo Lobão CAPUCHO COELHO, Leandro Souza DE MOURA LIMA, Fernando MARTINI CATALANO, Cecil WAGNER SKALESKI, Francisco KELLER KLUG, Marcus Felipe HORI OCHI
  • RETRACTABLE LEADING EDGE WING SLATS HAVING AUTONOMOUSLY CURVABLE AIRFLOW SHIELD FOR NOISE-ABATEMENT
    Publication number: 20200346735
    Abstract: Noise-abatement for a leading edge wing slat is provided by a noise-abatement airflow shield integral with the lower trailing edge of the slat, wherein the shield is reciprocally autonomously curvable from a substantially planar configuration when the slat is in a retracted position thereof and into a convexly curved configuration when the slat is in a deployed position thereof.
    Type: Application
    Filed: September 1, 2017
    Publication date: November 5, 2020
    Inventors: Danillo Cafaldo DOS REIS, Leandro Guilherme CRENITE SIMÕES, Micael Gianini, Valle DO CARMO, Fábio Santos DA SILVA, Eduardo Lobão CAPUCHO COELHO, Leandro Souza DE MOURA LIMA, Paulo Anchieta DA SILVA, Fernando MARTINI CATALANO, Cecil WAGNER SKALESKI, Francisco KELLER KLUG, Marcus Felipe HORI OCHI