Patents by Inventor Luca COSSETTI

Luca COSSETTI 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: 12560127
    Abstract: A method for controlling at least a first turboshaft engine and a second turboshaft engine of a rotorcraft, which set a common kinematic linkage in motion, the rotorcraft having an output electric machine cooperating with a first output kinematic linkage of the first turboshaft engine, the rotorcraft having an input electric machine cooperating with a gas generator of the second turboshaft engine. The method includes the following steps: supplying fuel to the first turboshaft engine, operating the output electric machine in electrical energy generator mode, supplying fuel to the second turboshaft engine, and operating the input electric machine in motor mode in order to supply a second non-zero power to said common kinematic linkage.
    Type: Grant
    Filed: November 3, 2021
    Date of Patent: February 24, 2026
    Assignee: AIRBUS HELICOPTERS
    Inventors: Luca Cossetti, Francois Malburet
  • Publication number: 20250108930
    Abstract: A system comprising a connection device having a first shaft and a second shaft, the connection device comprising a free-wheel interposed between the first shaft and the second shaft that can only transmit engine torque from the first shaft to the second shaft when a motor mode is activated. The connection device comprises a coupler, the coupler being provided with a fusible section, the connection device comprising a dog clutch connection that can only transmit engine torque from the coupler to the first shaft when an electrical power generation mode is activated.
    Type: Application
    Filed: July 16, 2024
    Publication date: April 3, 2025
    Applicant: AIRBUS HELICOPTERS
    Inventors: Jean-Victor LAPEYRE, Luca COSSETTI
  • Publication number: 20220135239
    Abstract: A method for controlling at least a first turboshaft engine and a second turboshaft engine of a rotorcraft, which set a common kinematic linkage in motion, the rotorcraft having an output electric machine cooperating with a first output kinematic linkage of the first turboshaft engine, the rotorcraft having an input electric machine cooperating with a gas generator of the second turboshaft engine. The method includes the following steps: supplying fuel to the first turboshaft engine, operating the output electric machine in electrical energy generator mode, supplying fuel to the second turboshaft engine, and operating the input electric machine in motor mode in order to supply a second non-zero power to said common kinematic linkage.
    Type: Application
    Filed: November 3, 2021
    Publication date: May 5, 2022
    Applicant: AIRBUS HELICOPTERS
    Inventors: Luca COSSETTI, Francois MALBURET