| 发明名称 |
SCALABLE AIR FILTER CONFIGURATION FOR FUEL TANK INERTING SYSTEM |
| 摘要 |
An aircraft fuel tank inerting system includes a filter apparatus and an air separation module configured to separate oxygen from a fluid stream. The filter apparatus includes a housing unit with a fluid inlet port configured to receive a first fluid stream, a fluid outlet port configured to deliver a second fluid stream, and a plurality of filter cartridges. Each of the plurality of filter cartridges is substantially the same and positioned within the housing unit. The air separation module is in fluid communication with the filter apparatus. |
| 申请公布号 |
US2016272339(A1) |
申请公布日期 |
2016.09.22 |
| 申请号 |
US201514663605 |
申请日期 |
2015.03.20 |
| 申请人 |
Hamilton Sundstrand Corporation |
发明人 |
D'Orlando Paul M.;DeValve Timothy D. |
| 分类号 |
B64D37/32;B01D46/54;B01D53/00;B01D46/00 |
主分类号 |
B64D37/32 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fuel tank inerting system comprising:
a filter apparatus comprising:
a housing unit with a fluid inlet port configured to receive a first fluid stream and a fluid outlet port configured to deliver a second fluid stream; anda plurality of filter cartridges, wherein each of the plurality of filter cartridges is substantially the same and is positioned within the housing unit; and an air separation module in fluid communication with the filter apparatus and configured to separate oxygen from the second fluid stream. |
| 地址 |
Windsor Locks CT US |
