Accessory for aircraft

A fitting for an aircraft, the fitting comprising: two horns (1) joined to each other, each of the two horns defining a first portion (11) and a second portion (12); an outer plate (2) connected to the two horns (1); and a skin (3) joined to the outer panel (2), the skin (3) being independent of the...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: VIVALACIO RODRIGUEZ RUBEN, RAMIREZ BLANCO GONZALO
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:A fitting for an aircraft, the fitting comprising: two horns (1) joined to each other, each of the two horns defining a first portion (11) and a second portion (12); an outer plate (2) connected to the two horns (1); and a skin (3) joined to the outer panel (2), the skin (3) being independent of the horn (1). The fitting allows eliminating the radius of the fitting angle defined by the horn, eliminating two angles, ensuring that no rivet or similar joining element is installed in the horn, ensuring that there is no continuity of the layer in the marking region. 一种用于飞行器的配件,该配件包括:彼此连结的两个角形件(1),这两个角形件中的每个角形件均限定有第一部分(11)和第二部分(12);与两个角形件(1)连结的外板(2);以及连结至外板(2)的蒙皮(3),蒙皮(3)独立于角形件(1)。该配件允许消除由角形件限定的配件角度的半径,消除两个角度,确保没有铆钉或类似的连结元件安装在角形件中,确保在标记区域中不存在层的连续性。