Patents by Inventor Carlos Eduardo Viana Ribeiro

Carlos Eduardo Viana Ribeiro 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).

  • Flight guidance controller interface
    Patent number: 11442471
    Abstract: Methods and systems are provided including a flight guidance controller interface. The flight guidance controller interface includes a rotatable knob including a rotatable element disposed around a periphery of a touch control display. A graphical presentation is output on the touch control display including a plurality of sections. The plurality of sections includes an indication of respective functions of an automatic flight control system. A touch input is received to one of the plurality of sections, thereby activating control of a corresponding one of the respective functions of the automatic flight control system. A rotation input to the rotatable element is received, thereby providing information about a value for the corresponding one of the respective functions of the automatic flight control system.
    Type: Grant
    Filed: April 27, 2020
    Date of Patent: September 13, 2022
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Jan Urbanec, Carlos Eduardo Viana Ribeiro
  • FLIGHT GUIDANCE CONTROLLER INTERFACE
    Publication number: 20210333806
    Abstract: Methods and systems are provided including a flight guidance controller interface. The flight guidance controller interface includes a rotatable knob including a rotatable element disposed around a periphery of a touch control display. A graphical presentation is output on the touch control display including a plurality of sections. The plurality of sections includes an indication of respective functions of an automatic flight control system. A touch input is received to one of the plurality of sections, thereby activating control of a corresponding one of the respective functions of the automatic flight control system. A rotation input to the rotatable element is received, thereby providing information about a value for the corresponding one of the respective functions of the automatic flight control system.
    Type: Application
    Filed: April 27, 2020
    Publication date: October 28, 2021
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Jan Urbanec, Carlos Eduardo Viana Ribeiro