Patents by Inventor Paula MÁS MÁS

Paula MÁS MÁS 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).

  • Main supporting structure of an aircraft lifting surface
    Patent number: 9387922
    Abstract: An aircraft lifting surface with a main supporting structure comprising upper and lower faces defining its aerodynamic profile, front and rear faces oriented towards, respectively, the leading and trailing edges, a first set of transverse ribs extended from the front face to the rear face and a second set of transverse ribs crossing the front face and/or the rear face. The integration of leading and trailing edge ribs in the main supporting structure allows a weight and cost reduction of aircraft lifting surfaces. A manufacturing method of said main supporting structure is also disclosed.
    Type: Grant
    Filed: November 19, 2013
    Date of Patent: July 12, 2016
    Assignee: Airbus Operations S.L.
    Inventors: Enrique Guinaldo Fernandez, Francisco Cruz Dominguez, Francisco Javier Honorato Ruiz, Paula Mas Mas, Iker Velez de Mendizabal Alonso, Carlos Garcia Nieto
  • Highly integrated structure including leading and trailing edge ribs for an aircraft lifting surface
    Patent number: 9381991
    Abstract: An aircraft lifting surface with a monolithic main supporting structure of a composite material including an upper skin having at least a part of the upper aerodynamic profile of the leading edge and/or of the trailing edge, a lower skin, a front spar, a rear spar, and leading edge ribs and/or a trailing edge ribs. The main supporting structure allows a weight and cost reduction of aircraft lifting surfaces.
    Type: Grant
    Filed: November 21, 2013
    Date of Patent: July 5, 2016
    Assignee: Airbus Operations S.L.
    Inventors: Enrique Guinaldo Fernandez, Francisco Cruz Dominguez, Francisco Javier Honorato Ruiz, Paula Más Más, Iker Vélez De Mendizábal Alonso, Carlos Garcia Nieto
  • Optimized torsion box for an aircraft
    Patent number: 9216812
    Abstract: An aircraft lifting surface with a torsion box of a composite material including an upper skin, a lower skin, a front spar, a rear spar, one or more intermediate spars and transverse ribs arranged between the rear spar and an adjacent intermediate spar and/or between the front spar and the adjacent intermediate spar.
    Type: Grant
    Filed: November 20, 2013
    Date of Patent: December 22, 2015
    Assignee: Airbus Operations S.L.
    Inventors: Enrique Guinaldo Fernadez, Francisco Cruz Dominguez, Francisco Javier Honorato Ruiz, Paula Más Más, Iker Vélez De Mendizábal Alonso, Carlos Garcia Nieto
  • MAIN SUPPORTING STRUCTURE OF AN AIRCRAFT LIFTING SURFACE
    Publication number: 20140151505
    Abstract: An aircraft lifting surface with a main supporting structure comprising upper and lower faces defining its aerodynamic profile, front and rear faces oriented towards, respectively, the leading and trailing edges, a first set of transverse ribs extended from the front face to the rear face and a second set of transverse ribs crossing the front face and/or the rear face. The integration of leading and trailing edge ribs in the main supporting structure allows a weight and cost reduction of aircraft lifting surfaces. A manufacturing method of said main supporting structure is also disclosed.
    Type: Application
    Filed: November 19, 2013
    Publication date: June 5, 2014
    Inventors: Enrique Guinaldo Fernandez, Francisco Cruz Dominguez, Francisco Javier Honorato Ruiz, Paula Mas Mas, Iker Velez de Mendizabal Alonso, Carlos Garcia Nieto
  • HIGHLY INTEGRATED STRUCTURE INCLUDING LEADING AND TRAILING EDGE RIBS FOR AN AIRCRAFT LIFTING SURFACE
    Publication number: 20140151506
    Abstract: The invention provides an aircraft lifting surface with a monolithic main supporting structure (14) of a composite material comprising an upper skin (21) including at least a part of the upper aerodynamic profile of the leading edge (11) and/or of the trailing edge (15), a lower skin, a front spar (18), a rear spar (20), a plurality of leading edge ribs and/or a plurality of trailing edge ribs. This main supporting structure allows a weight and cost reduction of aircraft lifting surfaces. The invention also provides a manufacturing method of said monolithic main supporting structure (14).
    Type: Application
    Filed: November 21, 2013
    Publication date: June 5, 2014
    Applicant: AIRBUS OPERATIONS S.L.
    Inventors: Enrique GUINALDO FERNANDEZ, Francisco CRUZ DOMINGUEZ, Francisco Javier HONORATO RUIZ, Paula MÁS MÁS, Iker VÉLEZ DE MENDIZÁBAL ALONSO, Carlos GARCIA NIETO
  • OPTIMIZED TORSION BOX FOR AN AIRCRAFT
    Publication number: 20140138486
    Abstract: The invention provides an aircraft lifting surface with a torsion box (13) of a composite material comprising an upper skin (21), a lower skin (23), a front spar (18), a rear spar (20), one or more intermediate spars (19, 19?) and a plurality of transverse ribs (25, 25?, . . . ) arranged between the rear spar (20) and its adjacent intermediate spar (19?) and/or between the front spar (18) and the adjacent intermediate spar (19) for improving its structural behavior. The invention also provides a manufacturing method of said torsion box.
    Type: Application
    Filed: November 20, 2013
    Publication date: May 22, 2014
    Applicant: AIRBUS OPERATIONS S.L.
    Inventors: Enrique GUINALDO FERNADEZ, Francisco CRUZ DOMINGUEZ, Francisco Javier HONORATO RUIZ, Paula MÁS MÁS, Iker VÉLEZ DE MENDIZÁBAL ALONSO, Carlos GARCIA NIETO