A gust compensation system 200 is configured to adaptively reduce gust loads exerted into an aircraft 100/500. The gust compensation system may include a first sensor 110 proximate to a front of the aircraft 100. The first sensor 110 is configured to output a first signal. A second sensor 120 may be distally located from the front of the aircraft 100. The second sensor 120 is configured to output a second signal. A gust signal sub-system 202 is configured to receive the first and second signals and generate a gust signal 226 based on analysis of the first and second signals. The gust signal sub-system 202 outputs the gust signal 226 and may modify a load parameter signal 220 in response to the gust signal 226 exceeding a load alleviation threshold.


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    Titel :

    СИСТЕМА И СПОСОБ КОМПЕНСАЦИИ ПОРЫВА ВОЗДУШНОЙ МАССЫ ДЛЯ ВОЗДУШНЫХ ЛЕТАТЕЛЬНЫХ АППАРАТОВ


    Erscheinungsdatum :

    2017-09-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen