Patents by Inventor Faisal GOUSSOUS

Faisal GOUSSOUS 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).

  • Methods and systems for flight data based parameter tuning and deployment
    Patent number: 10592636
    Abstract: A system, computer-readable medium, and a method including receiving flight data engine measurements for at least one engine of the specific aircraft asset; receiving flight data aerodynamics measurements for the specific aircraft asset; combining a physics based parametric aerodynamic performance model tuned for the specific aircraft asset using the flight data aerodynamics measurements and a physics based engine model tuned for the specific aircraft asset using the flight data engine measurements; calculating, based on the combined tuned aerodynamic performance model and the tuned engine model, a performance model for the specific aircraft asset as a whole; and storing a record of the calculated performance model for the specific aircraft asset for a future deployment.
    Type: Grant
    Filed: March 17, 2017
    Date of Patent: March 17, 2020
    Assignee: General Electric Company
    Inventors: Liling Ren, Faisal Goussous, Meet Patel, Filippo Liverini, Sean Hwang, David Lax, Mark Darnell
  • METHODS AND SYSTEMS FOR FLIGHT DATA BASED PARAMETER TUNING AND DEPLOYMENT
    Publication number: 20180268100
    Abstract: A system, computer-readable medium, and a method including receiving flight data engine measurements for at least one engine of the specific aircraft asset; receiving flight data aerodynamics measurements for the specific aircraft asset; combining a physics based parametric aerodynamic performance model tuned for the specific aircraft asset using the flight data aerodynamics measurements and a physics based engine model tuned for the specific aircraft asset using the flight data engine measurements; calculating, based on the combined tuned aerodynamic performance model and the tuned engine model, a performance model for the specific aircraft asset as a whole; and storing a record of the calculated performance model for the specific aircraft asset for a future deployment.
    Type: Application
    Filed: March 17, 2017
    Publication date: September 20, 2018
    Inventors: Liling REN, Faisal GOUSSOUS, Meet PATEL, Filippo LIVERINI, Sean HWANG, David LAX, Mark DARNELL