Patents by Inventor Pablo Manuel CALDERON GOMEZ

Pablo Manuel CALDERON GOMEZ 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 and method of operating an aircraft comprising an air separation device
    Patent number: 11724817
    Abstract: An aircraft including a combustion engine with a combustion chamber an injection device for injecting fuel in the combustion chamber and an air separation device adapted to separate air into an oxygen-enriched gas mix and an nitrogen-enriched gas mix, wherein the oxygen-enriched gas mix is injected into the combustion chamber with the fuel while the nitrogen-enriched gas mix is used to inert at least some portions of the aircraft in the environment of said combustion engine.
    Type: Grant
    Filed: December 14, 2021
    Date of Patent: August 15, 2023
    Assignee: AIRBUS OPERATIONS SL
    Inventors: Pablo Manuel Calderon Gomez, Carlos Casado-Montero
  • VALVE FOR DIVIDING A HYDRAULIC CIRCUIT AND HYDRAULIC CIRCUIT COMPRISING SAID VALVE
    Publication number: 20230175532
    Abstract: A valve for a hydraulic circuit for an aircraft, the valve being configured to unite or separate multiple circuit portions in at least two configurations. More particularly, the valve allows to create one hydraulic circuit or two independent hydraulic circuits in order to circulate a coolant in two distinct manners and thus to adapt the function of the hydraulic circuit to any of two distinct phases of the functioning of an engine of the aircraft.
    Type: Application
    Filed: December 1, 2022
    Publication date: June 8, 2023
    Inventors: Benjamin BOUVIER, Pablo Manuel CALDERON GOMEZ
  • AIRCRAFT AND METHOD OF OPERATING AN AIRCRAFT COMPRISING AN AIR SEPARATION DEVICE
    Publication number: 20220185495
    Abstract: An aircraft including a combustion engine with a combustion chamber an injection device for injecting fuel in the combustion chamber and an air separation device adapted to separate air into an oxygen-enriched gas mix and an nitrogen-enriched gas mix, wherein the oxygen-enriched gas mix is injected into the combustion chamber with the fuel while the nitrogen-enriched gas mix is used to inert at least some portions of the aircraft in the environment of said combustion engine.
    Type: Application
    Filed: December 14, 2021
    Publication date: June 16, 2022
    Inventors: Pablo Manuel CALDERON GOMEZ, Carlos CASADO-MONTERO