An on-board aircraft dried inert gas system includes a source inert gas (38) containing water, an air cycle or vapor cycle cooling system (140), and a heat exchanger condenser (118). 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.
ON-BOARD AIRCRAFT DRIED INERT GAS SYSTEM
TROCKENES INERTGASSYSTEM AN BORD EINES FLUGZEUGS
SYSTÈME DE GAZ INERTE SÉCHÉ EMBARQUÉ SUR UN AÉRONEF
2019-10-02
Patent
Electronic Resource
English
ON-BOARD AIRCRAFT ELECTROCHEMICAL INERT GAS GENERATION SYSTEM
European Patent Office | 2020
|ON-BOARD AIRCRAFT ELECTROCHEMICAL INERT GAS GENERATION SYSTEM
European Patent Office | 2020
|