Power take-off system and gas turbine engine assembly including same

摘要

A power take-off system (100) for a gas turbine engine assembly (10) is provided. The gas turbine engine (10) includes a first spool (40) and a second spool (42). The power take off system (100) further includes a starter (102) coupled to the first spool using a first shaft (112), and a generator (104) coupled to the second spool using a second shaft (122), the first shaft (112) is circumferentially offset from the second shaft (122) by an angle ±.