TESTING DEVICE FOR FUSELAGE SHELLS

The testing device has a test specimen with a complementary structure, which is connected to form a replacement section and devices are provided for fastening fuselage shell at the complementary structure. The replacement section is formed from N-fuselage shells (14) with N-shell coupling (13), wher...

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Bibliographische Detailangaben
Hauptverfasser:	BEST, ROALD, BERTHOLD, UDO, GÖTZE, MATTHIAS, GRÖTZSCHEL, GEORG, SACHSE, MIRKO
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES MEASURING PERFORMING OPERATIONS PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR TRANSPORTING
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Beschreibung
Zusammenfassung:	The testing device has a test specimen with a complementary structure, which is connected to form a replacement section and devices are provided for fastening fuselage shell at the complementary structure. The replacement section is formed from N-fuselage shells (14) with N-shell coupling (13), where N is an integer and is greater than 1. The complementary structure is formed from glass-fiber reinforced epoxy resin.