FIELD: aircraft engineering.SUBSTANCE: device, an aerodynamic wing with an adaptively variable surface for compensating for turbulence, contains movable plates that have two axes of rotation, supported by elements of the wing frame. On the surface of each plate a sensor that measures the external pressure is located. Plates rotation is carried out by means of two executive servomechanisms under the control of a separate microcomputer, where receives information from the plate sensor and the current position of the plate. All microcomputers are connected to a network in which each microcomputer is connected only with microcomputers of neighboring plates.EFFECT: invention is aimed at improving the stability and stability of flight.1 cl, 2 dwg


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    Titel :

    АЭРОДИНАМИЧЕСКОЕ КРЫЛО ЛЕТАТЕЛЬНОГО АППАРАТА С АДАПТИВНО ИЗМЕНЯЮЩЕЙСЯ ПОВЕРХНОСТЬЮ


    Erscheinungsdatum :

    30.05.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung