To provide a bulkhead joint method for a fuselage of an aircraft.SOLUTION: A bulkhead joint assembly 312 includes a strap section 314 configured to be secured to an aft section of a fuselage and a forward section of the fuselage and extend past a bulkhead 300 of the fuselage. The bulkhead joint assembly 312 also includes a chord 318 engaging and secured to the strap section 314, where the chord 318 is configured to extend along the bulkhead 300 to transfer a force received from the bulkhead 300 in shear between the chord 318 and the strap section 314.SELECTED DRAWING: Figure 3

    【課題】航空機の胴体部の隔壁連結方法を提供する。【解決手段】隔壁連結アセンブリ312は、胴体部の後方セクション及び胴体部の前方セクションに固定されるよう構成されているとともに、胴体部の隔壁300を超えて延びるストラップ片314を含む。隔壁連結アセンブリ312は、さらに、ストラップ片314に係合し、固定されたコード318を含む。コード318は、隔壁300に沿って延びており、隔壁300から受ける力をコード318とストラップ片314の間のせん断力として伝達するよう構成されている。【選択図】図3


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    Title :

    BULKHEAD JOINT ASSEMBLY


    Additional title:

    隔壁連結アセンブリ


    Contributors:
    JOEL JOSEPH (author) / PAUL DIEP (author) / BERNHARD DOPKER (author) / MARK J BUCKLEY (author)

    Publication date :

    2020-06-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile



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