PROBLEM TO BE SOLVED: To provide a method for assembling an aircraft structure assembly without use of any shimming, locating fixtures, or final-hole-size drill jigs.SOLUTION: The method includes supporting first and second frame sections (302, 304) on respective adjustable supports (310), and positioning the interconnecting frame section (306) therebetween. The method includes aligning first pre-drilled mating holes (316) in the interconnecting frame section with first pre-drilled mating holes (314) in the first and second frame sections (302, 304), and installing fasteners (318) though the aligned, first pre-drilled mating holes. The method includes positioning a structural mating section (308) relative to the first and second frame sections and the interconnecting frame section and aligning second pre-drilled mating holes (320) in the structural mating section with second pre-drilled mating holes (322, 324), and installing fasteners (326) through the aligned, second pre-drilled mating holes to secure the structural mating section.SELECTED DRAWING: Figure 3

    【課題】シム連結、位置決め固定具、穴サイズ穿孔冶具を用いず、航空機構造アセンブリを組み立てる方法。【解決手段】第1及び第2のフレームセクション(302、304)を各調節式支持部材(310)に支持し、相互接続フレームセクション(306)を配置する。相互接続フレームセクションの第1の事前穿孔連結穴(316)を、第1及び第2のフレームセクション(302、304)の第1の事前穿孔連結穴(314)とアラインメントし、第1の事前穿孔連結穴に留め具(318)を取り付ける。第1及び第2のフレームセクション及び相互接続フレームセクションに対して、構造連結セクション(308)を配置し、構造連結セクションの第2の事前穿孔連結穴(320)を第2の事前穿孔連結穴(322、324)とアライメントし、第2の事前穿孔連結穴に留め具(326)を取り付けることによって、構造連結セクションを固定する。【選択図】図3


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    Title :

    ASSEMBLY OF AIRCRAFT STRUCTURE ASSEMBLY WITHOUT SHIMMING, LOCATING FIXTURES OR FINAL-HOLE-SIZE DRILL JIGS


    Additional title:

    シム連結、位置決め固定具、又は、最終穴サイズ穿孔冶具を用いない航空機構造アセンブリの組み立て


    Contributors:

    Publication date :

    2016-12-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge



    ASSEMBLY OF AN AIRCRAFT STRUCTURE ASSEMBLY WITHOUT SHIMMING, LOCATING FIXTURES OR FINAL-HOLE-SIZE DRILL JIGS

    TURNER DAVID RAY / ERION DONALD L / FINCHAMP TERESA M et al. | European Patent Office | 2018

    Free access

    Assembly of an aircraft structure assembly without shimming, locating fixtures or final-hole-size drill jigs

    TURNER DAVID RAY / ERION DONALD L / FINCHAMP TERESA M et al. | European Patent Office | 2018

    Free access

    ASSEMBLY OF AN AIRCRAFT STRUCTURE ASSEMBLY WITHOUT SHIMMING, LOCATING FIXTURES OR FINAL-HOLE-SIZE DRILL JIGS

    TURNER DAVID RAY / ERION DONALD L / FINCHAMP TERESA M et al. | European Patent Office | 2016

    Free access

    ASSEMBLY OF AN AIRCRAFT STRUCTURE ASSEMBLY WITHOUT SHIMMING, LOCATING FIXTURES OR FINAL-HOLE-SIZE DRILL JIGS

    TURNER DAVID RAY / ERION DONALD L / FINCHAMP TERESA M et al. | European Patent Office | 2016

    Free access