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Passive load alleviation for a fiber reinforced wing box of an aircraft with a stiffened shell structure
Passive load alleviation for a fiber reinforced wing box of an aircraft with a stiffened shell structure
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机译:具有刚性壳结构的飞机的纤维增强机翼盒的被动载荷减轻
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摘要
Awing box of an aircraft with a stiffened shell structure, consisting of fiber reinforced material includes a skin for absorbing shear loads, and several stringers arranged on the inner side of the wing box for absorbing axial loads, in which at least 60% of the mass of the stiffened shell structure is concentrated in the stringers, wherein the stringers provide at least 80% of the axial stiffness of the stiffened shell structure. In the specific case of wing structure, this embodiment allows the use of unbalanced laminates for the skin to induce higher nose-down twist of the wing box without any loss in bending stiffness and so envisaging higher weight saving capability.
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