FIELD: aviation.SUBSTANCE: invention relates to aeronautical engineering. The aircraft wing is made of composite material dissymmetrical biconvex profile. The shape of the wing bottom surface rear part is completely identical to the shape of the wing upper surface rear part, extended beyond the rear edge. The wing upper surface is integral with the primary part of the wing lower surface. To produce the wing with constant chord the matrix is required.EFFECT: invention intended to simplify the wing manufacture.1 dwg

    Изобретение относится к авиационной технике. Крыло самолета выполнено из композитного материала несимметричного двояковыпуклого профиля. Форма задней части нижней поверхности крыла полностью идентична форме задней части верхней поверхности крыла, продолженной за пределы задней кромки. Верхняя поверхность крыла выполнена заодно с начальной частью нижней поверхности крыла. Для изготовления крыла с постоянной хордой необходима матрица. Изобретение направлено на упрощение изготовления крыла. 1 ил.


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    Title :

    AIRCRAFT WING


    Additional title:

    КРЫЛО САМОЛЕТА


    Contributors:

    Publication date :

    2017-02-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B29D PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE , Herstellen besonderer Gegenstände aus Kunststoff oder aus Stoffen in plastischem Zustand / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge



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