Flexible coupling for test bench of transmission gear box of helicopter type rotorcraft, has extreme flanges bored at center in annular shape and extending from internal extreme periphery to external extreme periphery

The coupling (100, 200) has extreme flanges (110, 210) bored at center and extending from a set of internal extreme peripheries (111, 211) to a set of external extreme peripheries (112, 212). Extreme flasks (120, 220) are bored at the center, and extend from another set of internal extreme peripheri...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	POGGIOLI FLORIAN, FRANCONE PIERRE, MERMOZ EMMANUEL
Format:	Patent
Sprache:	eng ; fre
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 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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