AIR BOTTOMING CYCLE AIR CYCLE SYSTEM SOURCE
摘要:
A turbine engine assembly (20) includes a tap (92) is at a location upstream of the combustor section (26) where a bleed airflow (64) is drawn. The bleed air is pressurized in an auxiliary compressor section (72), heated in an exhaust heat exchanger (82) and expanded through a power turbine (74) that is coupled to drive the auxiliary compressor section (72).
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