A heated leading edge structure (15) for an aircraft (1) includes a leading edge panel (17) having an outer surface (27) configured to be in contact with an ambient flow (28) and an inner surface (29) opposite the outer surface (27), and includes a heater device (19) configured to heat the leading edge panel (17). And a heater device (19) mounted to the inner surface (29) of the leading edge panel (17) for heating the leading edge panel (17), the heater device (19) being detachably mounted to the inner surface (29) of the leading edge panel (17). The invention also discloses a slat comprising such a heated leading edge structure, a wing comprising such a heated leading edge structure or slat, and an aircraft comprising such a heated leading edge structure, slat or wing.

    本发明公开了一种用于飞行器(1)的加热前缘结构(15),所述前缘结构包括前缘面板(17),所述前缘面板具有被配置为与环境流(28)接触的外表面(27)以及与所述外表面(27)相反的内表面(29),并且包括加热器装置(19),所述加热器装置安装到所述前缘面板(17)的内表面(29)用于加热所述前缘面板(17),所述加热器装置(19)以可拆卸的方式安装到所述前缘面板(17)的内表面(29)。本发明还公开了包括这种加热前缘结构的缝翼、包括这种加热前缘结构或缝翼的机翼、以及包括这种加热前缘结构、缝翼或机翼的飞行器。


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    Title :

    Heated leading edge structure for aircraft, slat, wing and aircraft


    Additional title:

    用于飞行器的加热前缘结构、缝翼、机翼以及飞行器


    Contributors:

    Publication date :

    2022-09-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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