Patents by Inventor Raul CALDERON

Raul CALDERON 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: 9767229
    Abstract: The invention relates to a method for simulating the unsteady aerodynamic loads being exerted on the external structure of an aircraft, notably in the context of a simulation of the buffeting of a wing surface in an airflow. The method includes a step of measurement of pressure (410) at different points of a grid, a step of calculation of the spectral density at these points (420) followed by extrapolation/interpolation operations to calculate the missing measurements (430), a step of estimation of the pressure coherence (440) for each pair of points of the grid, a step of estimation of the interspectral pressure density (450) for these same pairs of points, from the coherence thus estimated, and a step of calculation of the aerodynamic loads (460) by summing the real part of the interspectral density for the area of the wing surface having a separation of the boundary layer.
    Type: Grant
    Filed: September 11, 2013
    Date of Patent: September 19, 2017
    Assignee: Airbus Operations (S.A.S.)
    Inventors: Raul Calderon, Christophe David
  • Publication number: 20140081609
    Abstract: The invention relates to a method for simulating the unsteady aerodynamic loads being exerted on the external structure of an aircraft, notably in the context of a simulation of the buffeting of a wing surface in an airflow. The method includes a step of measurement of pressure (410) at different points of a grid, a step of calculation of the spectral density at these points (420) followed by extrapolation/interpolation operations to calculate the missing measurements (430), a step of estimation of the pressure coherence (440) for each pair of points of the grid, a step of estimation of the interspectral pressure density (450) for these same pairs of points, from the coherence thus estimated, and a step of calculation of the aerodynamic loads (460) by summing the real part of the interspectral density for the area of the wing surface having a separation of the boundary layer.
    Type: Application
    Filed: September 11, 2013
    Publication date: March 20, 2014
    Applicant: AIRBUS OPERATIONS (SAS)
    Inventors: Raul CALDERON, Christophe David
  • Patent number: 4059995
    Abstract: A liquid level indicator comprises a mercury-filled U-tube having a plurality of branches and calibrating rods for insertion into the branches. One arm of the U-tube is subject to the hydrostatic pressure in the receptacle holding the liquid whose level is to be indicated, and the level of mercury in the other arm indicates the liquid level via a colored liquid.
    Type: Grant
    Filed: July 28, 1976
    Date of Patent: November 29, 1977
    Inventor: Raul Calderon De Palacio