The invention discloses a self-tensioning wing rib, a wing and a skin laying method, the self-tensioning wing rib comprises a wing rib main body and a plurality of supporting rods, and the cross section of the wing rib main body is omega-shaped; the wing rib main body comprises a wing rib upper wing surface and a wing rib lower wing surface, the front ends of the wing rib upper wing surface and the wing rib lower wing surface are smoothly connected, and the rear ends of the wing rib upper wing surface and the wing rib lower wing surface are attached; the two ends of the supporting rod are connected to the wing rib upper wing face and the wing rib lower wing face respectively. According to the self-tensioning wing rib, the cross section of the wing rib body is in the omega shape, the self-tensioning adjusting function is achieved when a skin is laid, and the laying quality of the skin can be improved.
一种自张紧翼肋、机翼及蒙皮铺设方法,自张紧翼肋包括翼肋主体和多根撑杆,翼肋主体的截面为Ω型;翼肋主体包括翼肋上翼面和翼肋下翼面,翼肋上翼面与翼肋下翼面的前端光滑连接、后端相贴合;撑杆的两端分别连接于翼肋上翼面和翼肋下翼面。本发明涉及的自张紧翼肋,翼肋主体的截面设为Ω型,铺设蒙皮时具有自张紧的调节功能,能够改善蒙皮的铺设质量。
Self-tensioning wing rib, wing and skin laying method
一种自张紧翼肋、机翼及蒙皮铺设方法
2021-05-07
Patent
Electronic Resource
Chinese
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