SINGLE DRIVE, DUAL CLUTCH DRIVE SYSTEM FOR AN AIRCRAFT ACCESSORY

A single drive, dual clutch accessory drive system (20) for an aircraft including an input shaft (66) connected to a low pressure spool (49) of a turbine engine. The input shaft (66) is rotatable at a first input speed and at a second input speed that is distinct from the first input speed. An outpu...

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Bibliographische Detailangaben
Hauptverfasser: FINKE, Aaron M, BLEWETT, Michael R
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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