Patents by Inventor Miguel Angel Aguirre

Miguel Angel Aguirre 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).

  • Publication number: 20240133339
    Abstract: A propulsion unit including: a gas generator including a compressor, a combustion chamber, a turbine, at least two compressed-air propulsion modules, each propulsion module including: a fan, a compressed-air turbine configured to drive the rotation of the fan, a manifold allowing the respective turbines of the compressed-air propulsion modules to be supplied with compressed air, wherein the manifold is configured to collect and mix: at least a portion of the flow that has passed through the combustion chamber of the gas generator, typically as it leaves the turbine, and at least one bypass flow, the bypass flow being a flow of air which is not passed through the combustion chamber of the gas generator.
    Type: Application
    Filed: October 13, 2020
    Publication date: April 25, 2024
    Applicants: INSTITUT SUPERIEUR DE L'AERONAUTIQUE ET DE L'ESPAC, SAFRAN, SAFRAN AIRCRAFT ENGINES
    Inventors: Patrick GONIDEC, Miguel Angel AGUIRRE, Sébastien DUPLAA, Bernard ROBIC, Benoit RODRIGUEZ, Nicolas Jérôme Jean TANTOT
  • Patent number: 11866183
    Abstract: An aircraft includes a fuselage carrying a nacelle of the aircraft offset relative to a wing of the aircraft. The nacelle forms an air inlet fairing of a propulsion assembly. The nacelle includes a lower wall and an upper wall delimiting together a height of the nacelle. The lower wall includes an air inlet edge being contiguous with a trailing edge of the wing.
    Type: Grant
    Filed: April 15, 2022
    Date of Patent: January 9, 2024
    Assignees: Safran Nacelles, Safran Aircraft Engines, INSTITUT SUPERIEUR DE L'AÉRONAUTIQUE ET DE L'ESPACE
    Inventors: Patrick Gonidec, Miguel Angel Aguirre, Nicolas Tantot, Bruno Beutin, Bernard Robic, Sébastien Duplaa
  • Publication number: 20220242583
    Abstract: An aircraft includes a fuselage carrying a nacelle of the aircraft offset relative to a wing of the aircraft. The nacelle forms an air inlet fairing of a propulsion assembly. The nacelle includes a lower wall and an upper wall delimiting together a height of the nacelle. The lower wall includes an air inlet edge being contiguous with a trailing edge of the wing.
    Type: Application
    Filed: April 15, 2022
    Publication date: August 4, 2022
    Applicants: Safran Nacelles, SAFRAN AIRCRAFT ENGINES, INSTITUT SUPERIEUR DE L'AERONAUTIQUE ET DE L'ESPACE
    Inventors: Patrick Gonidec, Miguel Angel Aguirre, Nicolas Tantot, Bruno Beutin, Bernard Robic, Sébastien Duplaa
  • Publication number: 20040268192
    Abstract: Starting from an unlimited number of events or conditions (1), (1′) . . . (1n) together with there respective detectors (2), (2′) . . . (2n) that are combined with a transition detector (3), that relieves information from the “external reactivation pin” (4) and via an external “system control” pin (5). It is possible to watch over both combinational and time events, or to be exact watch over combinational events during execution, and in combination with time dependence generate a flag or signal to register an event, freeze the circuit, communicate that an event has been produced and aid in the identification of the event and the analysis of the system from a graphical or similar user interface.
    Type: Application
    Filed: August 30, 2004
    Publication date: December 30, 2004
    Inventors: Miguel Angel Aguirre Echanove, Jonathan Tombs, Antonio Torralba Silgado, Leopoldo Garcia Franquelo