发明名称 Switchable heat exchanger configuration for air cycle cooling apparatus
摘要 In a normal mode, a primary heat exchanger for heated bleed airflow is situated upstream of an aircraft air conditioner compressor. A secondary heat exchanger is located downstream of the compressor. In response to hot and humid environmental conditions, three-way switching valves reposition the primary heat exchanger downstream of the compressor. The result will be the reduction of heat exchange exit temperature, which translates into lower turbine inlet and outlet temperatures at satisfactory airflow rates.
申请公布号 US5309724(A) 申请公布日期 1994.05.10
申请号 US19920945709 申请日期 1992.09.16
申请人 GRUMMAN AEROSPACE CORPORATION 发明人 SCHREIBER, MELVIN;YURMAN, RICHARD
分类号 B64D13/06;F25B9/00;(IPC1-7):F25B9/00 主分类号 B64D13/06
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