| 发明名称 | Thermodynamically-optimized advanced fire suppression system | ||
| 摘要 | A fire suppression system for an aircraft includes an air separation module configured to receive exhaust air and ram air, conditioned compressor bleed air, and any combination thereof. The air separation module is also configured to provide nitrogen-enriched air and inert gas. The nitrogen-enriched air flows into a nitrogen-enriched air distribution network for fuel tank inerting. The inert gas flows into an inert gas distribution network for fire suppression in areas of the aircraft other than fuel tanks. | ||
| 申请公布号 | US9072921(B2) | 申请公布日期 | 2015.07.07 |
| 申请号 | US201213659204 | 申请日期 | 2012.10.24 |
| 申请人 | Hamilton Sundstrand Corporation | 发明人 | Ribarov Lubomir A.;Chattaway Adam;Seebaluck Dharmendr Len |
| 分类号 | A62C3/08;A62C35/02;A62C35/64;A62C99/00 | 主分类号 | A62C3/08 |
| 代理机构 | Kinney & Lange, P.A. | 代理人 | Kinney & Lange, P.A. |
| 主权项 | 1. A fire suppression system for an aircraft comprising: an air separation module configured to receive exhaust air and intake air and configured to provide nitrogen-enriched air and inert gas; a nitrogen-enriched air distribution network into which the nitrogen-enriched air flows for fuel tank inerting; and an inert gas distribution network into which the inert gas flows for fire suppression in areas of the aircraft other than fuel tanks. | ||
| 地址 | Windsor CT US | ||