发明名称 AN INTEGRATED ENVIRONMENTAL CONTROL SYSTEM FOR A HELICOPTER
摘要 <p>A compact, lightweight integrated environmental control (IEC) system for a helicopter incorporates in operative combination an environmental control system (ECS) and a nuclear/biological/chemical life support system (NBC LSS). The IEC system includes a refrigerant subsystem, a regenerative heat exchange apparatus, a decontamination subsystem, and an airflow distribution network, and is operative to provide super-cooled, super-dry, decontaminated airflow, in seriatim, directly to left and right mission equipment package bays and the cockpit for cooling of avionics/electronic modules and crew comfort. The IEC system is further operative to directly provide cooled, super-dry, decontaminated airflow for cooling of avionics/electronic modules of the mid mission equipment package bay and for over pressurizing the left and right mission equipment package bays to preclude contaminant infiltration thereof.</p>
申请公布号 EP0673330(B1) 申请公布日期 1997.03.12
申请号 EP19940904435 申请日期 1993.12.13
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 FRAWLEY, ROBERT, C.;BARNARD, RICHARD, S.;PERROTA, THOMAS
分类号 B01D50/00;B01D51/00;B64D;B64D13/00;B64D13/04;B64D13/08;F22D;F25B9/00;F25D9/00;(IPC1-7):B64D13/00 主分类号 B01D50/00
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