|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/135R; 244/135C; 244/136|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 12|
An aircraft fuel system has a fuel tank with first and second cells separated by one or more baffles. A venting system reduces pressure difference between the interior and exterior of the fuel tank, and an inerting system supplies oxygen-depleted gas to the fuel tank. The baffles permit the flow of fluid between the cells. The venting system has one or more vent nozzles within the fuel tank and in fluid communication with one or more vent ports. The inerting system has one or more inerting nozzles for injecting oxygen-depleted gas into the first and seco...
1. An aircraft fuel system comprising: a. a fuel tank with first and second cells separated by one or more baffles, the baffles permitting the flow of fluid between the first and second cells;b. a venting system for reducing any pressure difference between an interior and an exterior of the fuel tank, the venting system comprising one or more vent nozzles which are positioned within the fuel tank and in fluid communication with one or more vent ports, wherein the venting system has a venting capacity associated with each cell, and wherein the venting cap...