Patents by Inventor Luiz Flavio FERNANDES

Luiz Flavio FERNANDES 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: 11608156
    Abstract: A slat track roller assembly is provided so as to mount a slat track operatively associated with a wing leading edge slat for movements between retracted and deployed conditions relative to a leading edge of an aircraft wing. The slat track roller assembly may include at least forward and aft pairs of roller mechanisms connected to a respective one of opposed wing ribs of the wing leading edge in operatively rolling contact with a respective opposed lateral edge of the slat track. At least one of the roller mechanisms is positionally adjustable relative to the respectively opposed lateral edge of the slat track so as to compensate for mechanical tolerances that may be present.
    Type: Grant
    Filed: March 16, 2020
    Date of Patent: March 21, 2023
    Assignee: YABORÄ INDÚSTRIA AERONÁUTICA S.A.
    Inventors: Erik Keiti Mino, Luiz Flavio Fernandes, Égon dos Santos Borges, Henrique Fonseca de Araujo
  • Patent number: 11427302
    Abstract: An aircraft wing is provided with a positionally fixed closure fairing to close a cut-out opening in the leading edge of the wing associated with a wing leading edge slat so as to direct incident airflow to the wing leading edge from a lower surface of the aircraft wing to an upper surface of the aircraft wing.
    Type: Grant
    Filed: March 16, 2020
    Date of Patent: August 30, 2022
    Assignee: YABORÃ INDÚSTRIA AERONÁUTICA S.A.
    Inventors: Égon Dos Santos Borges, Luiz Flavio Fernandes, Alexandre Takao Motoyama, Henrique Fonseca De Araujo, Nilson Luiz David, Rodrigo Milaré Granzoto, Gilberto Guerra Becker
  • Patent number: 11235854
    Abstract: An aircraft wing is provided with a shutter mechanism to close a cut-out opening in the leading edge of the wing when a leading edge wing slat associated with the wing leading edge is moved to a deployed condition.
    Type: Grant
    Filed: March 19, 2020
    Date of Patent: February 1, 2022
    Assignee: YABORÄ INDÚSTRIA AERONÁUTICA S.A.
    Inventors: Andre Ganam de Queiroz, Alexandre Takao Motoyama, Azelio Pasquini, Douglas Carrari Firming, Egon dos Santos Borges, Henrique Fonseca de Araujo, Luiz Flavio Fernandes, Nilson Luiz David
  • Publication number: 20200307768
    Abstract: A slat track roller assembly is provided so as to mount a slat track operatively associated with a wing leading edge slat for movements between retracted and deployed conditions relative to a leading edge of an aircraft wing. The slat track roller assembly may include at least forward and aft pairs of roller mechanisms connected to a respective one of opposed wing ribs of the wing leading edge in operatively rolling contact with a respective opposed lateral edge of the slat track. At least one of the roller mechanisms is positionally adjustable relative to the respectively opposed lateral edge of the slat track so as to compensate for mechanical tolerances that may be present.
    Type: Application
    Filed: March 16, 2020
    Publication date: October 1, 2020
    Inventors: Erik Keiti MINO, Luiz Flavio FERNANDES, Égon dos SANTOS BORGES, Henrique Fonseca de ARAUJO
  • Publication number: 20200307760
    Abstract: An aircraft wing is provided with a shutter mechanism to close a cut-out opening in the leading edge of the wing when a leading edge wing slat associated with the wing leading edge is moved to a deployed condition.
    Type: Application
    Filed: March 19, 2020
    Publication date: October 1, 2020
    Inventors: Andre Ganam de QUEIROZ, Alexandre Takao MOTOYAMA, Azelio PASQUINI, Douglas Carrari FIRMINO, Egon dos SANTOS BORGES, Henrique Fonseca de ARAUJO, Luiz Flavio FERNANDES, Nilson Luiz DAVID
  • Publication number: 20200307771
    Abstract: An aircraft wing is provided with a positionally fixed closure fairing to close a cut-out opening in the leading edge of the wing associated with a wing leading edge slat so as to direct incident airflow to the wing leading edge from a lower surface of the aircraft wing to an upper surface of the aircraft wing.
    Type: Application
    Filed: March 16, 2020
    Publication date: October 1, 2020
    Inventors: Égon DOS SANTOS BORGES, Luiz Flavio FERNANDES, Alexandre Takao MOTOYAMA, Henrique Fonseca DE ARAUJO, Nilson Luiz DAVID, Rodrigo Milaré GRANZOTO, Gilberto Guerra BECKER