Method of manufacturing an aircraft assembly tool

A method of producing an aircraft assembly tool for supporting an aircraft component comprising calculating a plurality of predetermined positions and corresponding orientations in space at which the aircraft is to be supported, designing a fixture frame at predetermined locations of the frame assoc...

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Bibliographische Detailangaben
Hauptverfasser:	FOWLER KEVIN J, MCKEOWN RUSSELL P, SCOTT WILLIAM S, CHEETHAM SIMON
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AVIATION COMBINED OPERATIONS COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR OTHER WORKING OF METAL PERFORMING OPERATIONS TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TRANSPORTING UNIVERSAL MACHINE TOOLS
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Beschreibung
Zusammenfassung:	A method of producing an aircraft assembly tool for supporting an aircraft component comprising calculating a plurality of predetermined positions and corresponding orientations in space at which the aircraft is to be supported, designing a fixture frame at predetermined locations of the frame associated with the predetermined positions, constructing the fixture frame, providing pick-up devices with receiving elements, securing the pick-up devices to the fixture frame, and adjusting each receiving element.