A structured panel (100) is provided that includes a first skin (102) with a plurality of perforations (114), a second skin (104) and a core (106). The core (106) forms a plurality of cavities vertically between the first skin (102) and the second skin (104). Each of the cavities is respectively fluidly coupled with one or more of the perforations (114). The cavities include a first cavity. An element of the core (106) is configured with a multi-layered structure. The multi-layered structure includes a first layer and a second layer attached to the first layer. The first layer is configured with a first rib projecting into the first cavity.
提供了一种结构化面板,所述结构化面板包括具有多个穿孔的第一蒙皮、第二蒙皮以及芯部。所述芯部在所述第一蒙皮与所述第二蒙皮之间竖直地形成多个腔。所述腔中的每一者分别与所述穿孔中的一者或多者流体联接。所述腔包括第一腔。所述芯部的元件被配置成具有多层结构。所述多层结构包括第一层和附接到所述第一层的第二层。所述第一层被配置成具有突出到所述第一腔中的第一肋。
Structure panel with multi-panel structure
具有多面板结构的结构化面板
2020-11-24
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |