|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B01D-053/22 B64D-037/32 B01D-005/00 B01D-053/26 A62C-003/08|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 44|
An on-board aircraft inert gas system includes a source of hydrocarbon, a source of gas comprising oxygen, and a first fluid flow path between the source of gas comprising oxygen and an inert gas output. A reactor is disposed along the first fluid flow path that reacts oxygen and hydrocarbon from the fuel tank gas space to produce an oxygen-depleted gas. A heat exchanger condenser removes some water from the oxygen-depleted gas. A water-permeable gas membrane separator receives the oxygen-depleted gas from the heat exchanger and outputs dried oxygen-depl...
1. An on-board aircraft inert gas system, comprising: a source of hydrocarbon;a source of a gas comprising oxygen;a first fluid flow path between the source of gas comprising oxygen and an inert gas output;a reactor disposed along the first fluid flow path comprising an inlet that receives hydrocarbon and the gas comprising oxygen and reacts the hydrocarbon with the oxygen to produce an oxygen-depleted gas comprising water vapor, and an outlet that outputs the oxygen-depleted gas comprising water vapor;a first heat exchanger comprising a water-condensing...