Patents by Inventor Federico Mattia Benzi

Federico Mattia Benzi 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: 11912416
    Abstract: Aircraft systems including a pressurized fuel tank containing a pressurized fuel, a turbo expander configured to receive the pressurized fuel from the fuel tank, the turbo expander configured to decrease a pressure of the pressurized fuel to generate low pressure fuel having pressure less than the pressurized fuel, a fuel-to-air heat exchanger configured to receive the low pressure fuel from the turbo expander as a first working fluid and air as a second working fluid, the heat exchanger configured to cool the air and warm the fuel, an aircraft cabin configured to receive the cooled air, and a fuel consumption system configured to consume the fuel to generate power.
    Type: Grant
    Filed: September 9, 2021
    Date of Patent: February 27, 2024
    Assignee: HAMILTON SUNDSTRAND CORPORATION
    Inventors: Giusi Quartarone, Erica Zavaglio, Federico Mattia Benzi, Ram Ranjan
  • Publication number: 20230080053
    Abstract: An environmental control system (ECS) for an aircraft includes a primary heat exchanger, a compressor including an inlet fluidically connected to the primary heat exchanger, a turbine operatively connected to the compressor, and a cryogenic fluid heat exchanger fluidically connected to the primary heat exchanger.
    Type: Application
    Filed: September 10, 2021
    Publication date: March 16, 2023
    Inventors: Sean C. Emerson, Giusi Quartarone, Joseph Turney, Ram Ranjan, Erica Zavaglio, Federico Mattia Benzi, Charles E. Lents
  • Publication number: 20230069975
    Abstract: Aircraft systems including a pressurized fuel tank containing a pressurized fuel, a turbo expander configured to receive the pressurized fuel from the fuel tank, the turbo expander configured to decrease a pressure of the pressurized fuel to generate low pressure fuel having pressure less than the pressurized fuel, a fuel-to-air heat exchanger configured to receive the low pressure fuel from the turbo expander as a first working fluid and air as a second working fluid, the heat exchanger configured to cool the air and warm the fuel, an aircraft cabin configured to receive the cooled air, and a fuel consumption system configured to consume the fuel to generate power.
    Type: Application
    Filed: September 9, 2021
    Publication date: March 9, 2023
    Inventors: Giusi Quartarone, Erica Zavaglio, Federico Mattia Benzi, Ram Ranjan