Power take-off system and gas turbine engine assembly...

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/36 (2006.01) F02C 7/275 (2006.01)

Patent

CA 2627380

A power take-off system (100,400,500) for a gas turbine engine assembly (10) is provided. The gas turbine engine includes a first spool (40) and a second spool (42), the power take-off system including a starter (102) coupled to the second spool, and a clutch assembly (200) coupled between the starter and the first spool, the clutch assembly configured to couple the first spool to the starter when starting the gas turbine engine assembly.

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