Patents by Inventor Gabriel H. CAMPOS NARANJO

Gabriel H. CAMPOS NARANJO 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).

  • Aircraft wing with displaceable winglet
    Patent number: 11492102
    Abstract: A wing having a main wing section with a forward spar and an aft spar extending through an internal cavity. The forward and aft spars are spaced apart and delimiting a dry segment of the internal cavity. A winglet is rotatably coupled to the main wing section by a cant hinge defining a cant axis about which the winglet rotates relative to the main wing section between an extended position in which the winglet is aligned with the main wing section, and a folded position in which the winglet is rotated about the cant axis. A linkage assembly disposed in the dry segment is pivotably mounted to one of the forward and aft spars and is coupled to the cant hinge. The linkage assembly is displaceable to apply a force to move the winglet between the extended position and the folded position during flight of the aircraft.
    Type: Grant
    Filed: February 20, 2020
    Date of Patent: November 8, 2022
    Inventors: Fengfeng Xi, Amin Moosavian, Jose Vieira De Sa, Gabriel H. Campos Naranjo
  • AIRCRAFT WING WITH DISPLACEABLE WINGLET
    Publication number: 20200269971
    Abstract: A wing having a main wing section with a forward spar and an aft spar extending through an internal cavity. The forward and aft spars are spaced apart and delimiting a dry segment of the internal cavity. A winglet is rotatably coupled to the main wing section by a cant hinge defining a cant axis about which the winglet rotates relative to the main wing section between an extended position in which the winglet is aligned with the main wing section, and a folded position in which the winglet is rotated about the cant axis. A linkage assembly disposed in the dry segment is pivotably mounted to one of the forward and aft spars and is coupled to the cant hinge. The linkage assembly is displaceable to apply a force to move the winglet between the extended position and the folded position during flight of the aircraft.
    Type: Application
    Filed: February 20, 2020
    Publication date: August 27, 2020
    Inventors: Fengfeng XI, Amin MOOSAVIAN, Jose VIEIRA DE SA, Gabriel H. CAMPOS NARANJO