| 发明名称 |
AIRCRAFT HYBRID FUEL SYSTEM |
| 摘要 |
An aircraft hybrid fuel system includes a main tank and a set of flexible bladders, the main tank and the set of flexible bladders defining a fuel containment space. The system further includes a set of pathways coupling the set of flexible bladders to the main tank. The set of pathways is constructed and arranged to vent gas out of the set of flexible bladders into the main tank while fuel from a fuel source is provided into the fuel containment space defined by the main tank and the set of flexible bladders. Along these lines, each flexible bladder can be provisioned with a fuel port to provide fuel, and a separate vent port to vent gas to the main tank. |
| 申请公布号 |
US2016096630(A1) |
申请公布日期 |
2016.04.07 |
| 申请号 |
US201514963716 |
申请日期 |
2015.12.09 |
| 申请人 |
AAI Corporation |
发明人 |
Hall Brandon R. |
| 分类号 |
B64D37/04;B64C39/02;B64D37/16 |
主分类号 |
B64D37/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft hybrid fuel system, comprising:
a main tank; a set of flexible bladders, the main tank and the set of flexible bladders defining a fuel containment space; and a set of pathways coupling the set of flexible bladders to the main tank, the set of pathways being constructed and arranged to vent gas out of the set of flexible bladders into the main tank while fuel from a fuel source is provided into the fuel containment space defined by the main tank and the set of flexible bladders. |
| 地址 |
Hunt Valley MD US |
