Airplane fuselage

An airplane fuselage including a plurality of individual subassemblies having components that are aligned using coordination holes. The components include an assembly of panels, a plurality of stringer clips, a plurality of frame members, shear ties, and a floor grid made of a plurality of crossmemb...

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Bibliographische Detailangaben
Hauptverfasser:	MICALE, ANTONIO C
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CHAMBERS PROVIDED WITH MANIPULATION DEVICES COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOTDIRECTED TO A PARTICULAR RESULT COMBINED OPERATIONS CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g.ARRANGEMENTS FOR COPYING OR CONTROLLING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HAND TOOLS HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS MACHINE TOOLS MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OFPARTICULAR DETAILS OR COMPONENTS MANIPULATORS METAL-WORKING NOT OTHERWISE PROVIDED FOR MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS OTHER WORKING OF METAL PERFORMING OPERATIONS PHYSICS PORTABLE POWER-DRIVEN TOOLS REGULATING TRANSPORTING UNIVERSAL MACHINE TOOLS
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Beschreibung
Zusammenfassung:	An airplane fuselage including a plurality of individual subassemblies having components that are aligned using coordination holes. The components include an assembly of panels, a plurality of stringer clips, a plurality of frame members, shear ties, and a floor grid made of a plurality of crossmembers. The coordination holes are drilled in selected components and are located at positions on the subassemblies to accurately align the subassemblies relative to each other so the spatial relationship between key features of the subassemblies make them self-locating and intrinsically determinant of the final contour and configuration of the airplane fuselage, independent of hard tooling.