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Priority to JP6132690UpriorityCriticalpatent/JPH0420898U/ja
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第1図及び第2図は、本考案に係る積層構造部 材を主翼外板部に適用した実施例の説明図である 。
1 and 2 are explanatory diagrams of an embodiment in which a laminated structural member according to the present invention is applied to a main wing outer plate portion.
Claims (1)
【実用新案登録請求の範囲】[Scope of utility model registration request] 航空機の外板部を構成する積層構造部材におい て、上記積層構造部材に形状記憶樹脂及び電熱メ ツシユを埋め込み、該電熱メツシユの通電領域を 選択することにより、上記外板部に加わる荷重を 緩和する方向に形状回復力を発現可能にしたこと を特徴とする積層構造部材。 In a laminated structural member constituting the outer skin of an aircraft, a shape memory resin and an electric heating mesh are embedded in the laminated structural member, and a current-carrying area of the electric heating mesh is selected to alleviate the load applied to the outer skin. A laminated structural member characterized by being able to exhibit shape recovery power.