Patents by Inventor Jose Alberto Cabello Moreno

Jose Alberto Cabello Moreno 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 control device
    Patent number: 8038093
    Abstract: The invention relates to a control surface (3) for an aerodynamic lifting surface (2) of aircraft comprising a main closing rib (9) located at one end of the control surface (3) to which a main torsion bar (8) is joined, the mentioned torsion bar (8) being joined at its other end to a lever system (14) on which at least one actuator (15) acts, such that it is possible to act on the rotation of the mentioned control surface (3) during the flight of the aircraft. The invention also relates to an actuation method for actuating such a control surface (3).
    Type: Grant
    Filed: February 21, 2008
    Date of Patent: October 18, 2011
    Assignee: Airbus Espana, S.L.
    Inventors: Raul Carlos Llamas Sandin, Alfonso Gonzalez Gozalbo, Jorge Pablo Verde Preckler, José Alberto Cabello Moreno, José Luis Collado Briceño
  • Aircraft tail assembly
    Patent number: 7896289
    Abstract: An aircraft tail assembly planform comprising curvilinear leading edges (21) and trailing edges (22), with an aircraft tail assembly configuration in which the hinge line (13) is rectilinear and has a non-constant percentage with respect to the chord (50) in each section (51), being the front (11) and rear (12) spars rectilinear with a non-constant percentage with respect to the chord (50) in each section (51), or being these spars (11, 12) curvilinear with a constant or non-constant percentage with respect to the chord (50) in each section (51).
    Type: Grant
    Filed: September 27, 2007
    Date of Patent: March 1, 2011
    Assignee: Airbus España, S.L.
    Inventors: Jorge Pablo Verde Preckler, José Alberto Cabello Moreno
  • Aircraft control device
    Publication number: 20090159755
    Abstract: The invention relates to a control surface (3) for an aerodynamic lifting surface (2) of aircraft comprising a main closing rib (9) located at one end of the control surface (3) to which a main torsion bar (8) is joined, the mentioned torsion bar (8) being joined at its other end to a lever system (14) on which at least one actuator (15) acts, such that it is possible to act on the rotation of the mentioned control surface (3) during the flight of the aircraft. The invention also relates to an actuation method for actuating such a control surface (3).
    Type: Application
    Filed: February 21, 2008
    Publication date: June 25, 2009
    Inventors: Alfonso Gonzalez Gozalbo, Jorge Pablo Verde Preckler, Jose Alberto Cabello Moreno, Jose Luis Collado Briceno, Raul Carlos Llamas Sandin
  • Aircraft tail assembly
    Publication number: 20090026311
    Abstract: An aircraft tail assembly planform comprising curvilinear leading edges (21) and trailing edges (22), with an aircraft tail assembly configuration in which the hinge line (13) is rectilinear and has a non-constant percentage with respect to the chord (50) in each section (51), being the front (11) and rear (12) spars rectilinear with a non-constant percentage with respect to the chord (50) in each section (51), or being these spars (11, 12) curvilinear with a constant or non-constant percentage with respect to the chord (50) in each section (51).
    Type: Application
    Filed: September 27, 2007
    Publication date: January 29, 2009
    Inventors: Jorge Pablo Verde Preckler, Jose Alberto Cabello Moreno