The invention relates to a sealing strip, a control surface device, an aircraft wing and an aircraft. In order to improve sealing of a gap between control surfaces of an aircraft to enhance aerodynamics, the present invention provides a sealing strip for sealing a gap between convexly curved aerodynamic surface elements of an aircraft, such that the sealing strip has a convexly curved outer side, the sealing strip has a contour with a middle sealing section and welt sections, the welt sections are arranged at end portions of the contour for fastening the sealing strip to the aerodynamic surface element and protrude from the middle sealing section on an inner side, the middle sealing section is arranged between the welt sections, and the welt sections protrude from the middle sealing section on an inner side. And at least one longitudinal beam type reinforcing structure is arranged on the inner side part of the middle sealing part section. Furthermore, a control surface device, a wing and an aircraft comprising such a sealing strip as a weatherproof seal are described.

    本发明涉及密封条、控制表面装置、飞行器机翼和飞行器。为了改善对飞行器的控制表面之间的间隙的密封以增强空气动力学,本发明提供了一种密封条,该密封条用于密封飞行器的凸形弯曲的空气动力学表面元件之间的间隙,使得密封条具有凸形弯曲的外侧部,密封条具有带中间密封部段和贴边部段的轮廓,其中,贴边部段布置在轮廓的端部部分处以用于将密封条固定在空气动力学表面元件处并且贴边部段在内侧部上从中间密封部段突出,其中,中间密封部段布置在贴边部段之间,其中,在中间密封部段的内侧部上设置有至少一个纵梁型加强结构。此外,描述了包括这种密封条来作为防风雨密封件的控制表面装置、机翼和飞行器。


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    Title :

    Sealing strip, control surface device, aircraft wing and aircraft


    Additional title:

    密封条、控制表面装置、飞行器机翼和飞行器


    Contributors:

    Publication date :

    2024-09-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16J Kolben , PISTONS



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