|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B01D-053/32 B01D-053/26 B64D-037/32 C25B-009/18 F24F-003/14 A62C-003/08 B64D-013/02 B64D-013/06 A62C-099/00 B01D-053/30|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 6|
An on-board aircraft dried inert gas system includes a source inert gas containing water, an air cycle or vapor cycle cooling system, and a heat exchanger condenser. The heat exchanger condenser has a heat absorption side in thermal communication with the air cycle or vapor cycle cooling system. The heat exchanger condenser has a heat rejection side that receives the inert gas containing water and outputs dried inert gas.
1. An on-board aircraft dried inert gas system, comprising: a source of an inert gas comprising water;an air cycle cooling system comprising a primary heat exchanger, a compressor, a secondary heat exchanger, a turbine, and a condenser/reheater and a water removal unit, or a vapor cycle cooling system comprising a two-phase refrigerant cycled through a vapor-compression loop cycle comprising a compressor, a condenser, an expansion device, and an evaporator;a first heat exchanger condenser comprising a heat absorption side in thermal communication with th...