| 摘要 |
A system (200) and a method for providing cooling and power for an aircraft is provided. The system includes a turbine assembly (204) that includes a cooling unit (226) including a first turbine (248) rotatably coupled to a generator (250) by a first shaft (252). The power assembly further includes a power unit (228) including a second turbine (234) rotatably coupled to a compressor by a second shaft (236), the power unit coupled in flow communication with the cooling unit such that the first shaft and the second shaft are independently rotatable relative to one another.
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