A system for controlling a magnitude of a sonic boom caused by off-design operation of a supersonic aircraft includes a sensor configured to detect a condition of the supersonic aircraft. The system further includes a control surface that is mounted to a wing of the supersonic aircraft. The system still further includes a processor communicatively coupled to the sensor and operatively coupled with the control surface. The processor is configured to (1) receive information from the sensor indicative of the condition of the supersonic aircraft, (2) determine that there is a deviation between a lift distribution and a design-condition lift distribution based on the information, and (3) control the control surface to move in a manner that reduces the deviation. The magnitude of the sonic boom is reduced when the deviation is reduced.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Systems and methods for controlling a magnitude of a sonic boom


    Beteiligte:
    FREUND DONALD (Autor:in)

    Erscheinungsdatum :

    2015-12-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    SYSTEMS AND METHODS FOR CONTROLLING A MAGNITUDE OF A SONIC BOOM

    FREUND DONALD | Europäisches Patentamt | 2020

    Freier Zugriff

    SYSTEMS AND METHODS FOR CONTROLLING A MAGNITUDE OF A SONIC BOOM

    FREUND DONALD | Europäisches Patentamt | 2019

    Freier Zugriff

    Systems and methods for controlling a magnitude of a sonic boom

    FREUND DONALD | Europäisches Patentamt | 2016

    Freier Zugriff

    SYSTEMS AND METHODS FOR CONTROLLING A MAGNITUDE OF A SONIC BOOM

    FREUND DONALD | Europäisches Patentamt | 2016

    Freier Zugriff

    SYSTEMS AND METHODS FOR CONTROLLING A MAGNITUDE OF A SONIC BOOM

    FREUND DONALD | Europäisches Patentamt | 2020

    Freier Zugriff