Patents by Inventor Miguel Gasco Nunez

Miguel Gasco Nunez 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: 8911236
    Abstract: Training method for the simulation of an operation performed by at least one device which is part of a real apparatus, wherein the method comprises providing to display means overlaid images under controlled depth order of a virtual apparatus, and real images of said device, and providing a simulated response to control means, based on data of the position and behavior of said device and on data of the position and behavior of said virtual apparatus.
    Type: Grant
    Filed: October 1, 2009
    Date of Patent: December 16, 2014
    Assignee: EADS Construcciones Aeronauticas, S.A.
    Inventors: Miguel Gasco Nunez, Javier Alvarez Ortiz
  • Patent number: 8398023
    Abstract: Control station which comprises: a seat (10) for the operator of the said control station, the seat (10) comprising at least one arm rest (30), and a control and command assembly, said assembly comprising a control stick (1) with controls, mechanical components for transmitting and generating forces and movement to and from the control stick (1), components (17) for measuring the position of the control stick (1), and electronic components which are connected to the control stick (1) and via which the control and command assembly is operated, the control stick (1) of the said control station being incorporated in the seat (10), the control stick (1) being situated moreover on the armrest (30).
    Type: Grant
    Filed: July 2, 2010
    Date of Patent: March 19, 2013
    Assignee: EADS Construcciones Aeronauticas, S.A.
    Inventors: Miguel Gasco Núñez, Santiago Flores Giraldo
  • Patent number: 8328139
    Abstract: A method and device for in-flight including movable aerodynamic surfaces boom refueling operations using an articulated boom and a cable is disclosed.
    Type: Grant
    Filed: June 4, 2009
    Date of Patent: December 11, 2012
    Assignee: EADS Construcciones Aeronauticas, S.A.
    Inventor: Miguel Gasco Nunez
  • Publication number: 20110101176
    Abstract: Control station which comprises: a seat (10) for the operator of the said control station, the seat (10) comprising at least one arm rest (30), and a control and command assembly, said assembly comprising a control stick (1) with controls, mechanical components for transmitting and generating forces and movement to and from the control stick (1), components (17) for measuring the position of the control stick (1), and electronic components which are connected to the control stick (1) and via which the control and command assembly is operated, the control stick (1) of the said control station being incorporated in the seat (10), the control stick (1) being situated moreover on the armrest (30).
    Type: Application
    Filed: July 2, 2010
    Publication date: May 5, 2011
    Applicant: EADS CONSTRUCCIONES AERONAUTICAS, S.A.
    Inventors: Miguel Gasco Núñez, Santiago Flores Giraldo
  • Publication number: 20110027761
    Abstract: Training method for the simulation of an operation performed by at least one device which is part of a real apparatus, wherein the method comprises providing to display means overlaid images under controlled depth order of a virtual apparatus, and real images of said device, and providing a simulated response to control means, based on data of the position and behavior of said device and on data of the position and behavior of said virtual apparatus.
    Type: Application
    Filed: October 1, 2009
    Publication date: February 3, 2011
    Applicant: EADS CONSTRUCCIONES AERONAUTICAS, S.A.
    Inventors: Miguel Gasco Nunez, Javier Alvarez Ortiz
  • Publication number: 20100243812
    Abstract: Method and device for in-flight boom refuelling operations using an articulated boom (11) and a cable (18), said boom (11) comprising movable aerodynamic surfaces (16), said method comprising the following steps: a) from a completely stowed-away and retracted position of the boom (11), the cable (18) is initially released, thereby starting to lower the boom (11), such that the said cable (18) is kept tensioned during the whole of step a) by means of the force supplied by the movable aerodynamic surfaces (16) and/or the force of gravity acting on the boom (11); b) after reaching the maximum deployed position of the boom (11), or the bottom end of the flight envelope of the boom (11), release of the cable (18) is stopped; c) while keeping the length of released cable (18) fixed, the boom (11) is brought into a suitable position for commencing the manoeuvres for refuelling of the receiver aircraft; d) the manoeuvre for connecting the boom (11) to the receptacle of the receiver aircraft is started by means of
    Type: Application
    Filed: June 4, 2009
    Publication date: September 30, 2010
    Applicant: EADS Construcciones Aeronauticas, S.A.
    Inventor: Miguel GASCO NUNEZ