To provide improved fiber-reinforced thermoplastic composite structural members, aircraft including the same, and/or related methods.SOLUTION: A fiber-reinforced thermoplastic composite structural member (FRTCSM) (20) includes a first thermoplastic sub-structure (30) and a second thermoplastic sub-structure (50). A first web (38) is welded to a second web (58). An aircraft includes at least one FRTCSM (20). The methods include: positioning the first thermoplastic sub-structure (30) and the second thermoplastic sub-structure (50) such that the first web (38) faces the second web (58); compressing the first web (38) and the second web (58) together; and welding the first web (38) and the second web (58) to one another.SELECTED DRAWING: Figure 5

    【課題】改良された繊維強化熱可塑性複合材構造部材、それを含む航空機、及び/又は関連方法を提供する。【解決手段】繊維強化熱可塑性複合材構造部材(FRTCSM)(20)は、第1の熱可塑性サブ構造(30)および第2の熱可塑性サブ構造(50)を含む。第1のウェブ(38)は、第2のウェブ(58)に溶接される。航空機は、少なくとも1つのFRTCSM(20)を含む。該方法は、第1のウェブ(38)が第2のウェブ(58)に面するように第1の熱可塑性サブ構造(30)と第2の熱可塑性サブ構造(50)を配置すること、第1のウェブ(38)と第2のウェブ(58)を共に圧縮すること、及び第1のウェブ(38)と第2のウェブ(58)とを互いに溶接することを含む。【選択図】図5


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    Title :

    FIBER-REINFORCED THERMOPLASTIC COMPOSITE STRUCTURAL MEMBERS, AIRCRAFT INCLUDING THE SAME, AND RELATED METHODS


    Additional title:

    繊維強化熱可塑性複合材構造部材、それを含む航空機、及び関連方法


    Contributors:

    Publication date :

    2024-11-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge





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