Method and apparatus for aligning fastener holes (110, 306, 120, 316) of two components (102, 302, 112, 310). An alignment fixture (200) includes two mating fixtures (202, 330, 240, 370). Each mating fixture includes a reference plate (204, 332, 242, 372) that is aligned to the fastener holes of one of the components. Each mating fixture also includes an alignment device (220, 350, 250, 382). The alignment devices can be aligned with the respective reference plates such that the alignment between the reference plates and the fastener holes are transferred to the alignment devices. Once aligned, the alignment devices can be temporarily attached to the respective components at locations away from the fastener holes. The reference plates can then be removed. Thereafter, the components can be brought together such that mating features (224, 357, 254, 396) on the alignment devices engage. Engagement of the mating features aligns the two components such that the fastener holes on the components are aligned.
EXTERIOR INDEXING PROCESS AND TOOLING
AUSSENMARKIERUNGSVERFAHREN UND WERKZEUG
PROCÉDÉ ET OUTILLAGE D'INDEXATION EXTÉRIEURE
2018-02-28
Patent
Electronic Resource
English
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 / B21J FORGING , Schmieden / B23K Löten , SOLDERING OR UNSOLDERING / B23P Sonstige Metallbearbeitung , OTHER WORKING OF METAL / B23Q DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING , Einzelheiten, Bestandteile oder Zubehör für Werkzeugmaschinen, z.B. Anordnungen zum Kopieren oder Steuern / F16L PIPES , Rohre |
AUTOMOTIVE TOOLING EXPERIENCE WITH AIRCRAFT TOOLING & MANUFACTURING
SAE Technical Papers | 1954
|Engineering Index Backfile | 1949
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