The invention provides an integral wallboard of a helicopter. The integral wallboard comprises a frame laying layer, a beam laying layer, a skin laying layer and a stringer laying layer, wherein the frame paving layer, the beam paving layer, the skin paving layer and the stringer paving layer are paved once and co-cured to form the wall plate. The invention further provides a helicopter integral wallboard laying method. The method comprises the steps that 101, non-shared laying laying of the skin and the stringer is carried out; step 201, after the non-shared paving layer of the skin and the stringer is paved, paving a frame edge strip paving layer; step 301, after laying of the frame edge strip laying layer is finished, laying of a common laying layer of the skin and the stringer and laying of other laying layers of the stringer are carried out; and step 401, after laying of the skin and stringer shared laying layer is finished, laying of a frame beam laying layer is carried out.
本申请提供了一种直升机整体壁板,所述壁板包括:框铺层、梁铺层、蒙皮铺层和长桁铺层;其中,所述框铺层、梁铺层、蒙皮铺层和长桁铺层经过一次铺设共固化形成所述壁板。本申请还提供了一种直升机整体壁板铺层方法,所述方法包括:步骤101、进行蒙皮与长桁非共用铺层铺设;步骤201、在所述蒙皮与长桁非共用铺层铺设结束后,进行框缘条铺层铺设;步骤301、在所述框缘条铺层铺设结束后,进行蒙皮与长桁共用铺层及长桁其他铺层铺设;步骤401、在所述蒙皮与长桁共用铺层铺设结束后,进行框梁铺层铺设。
Helicopter integral panel and layering method
一种直升机整体壁板和铺层方法
2023-03-14
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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