| 发明名称 | Auxiliary power unit with integrated fire detection system | ||
| 摘要 | An Auxiliary Power Unit (“APU”) for an aircraft with reduced weight, but which at the same time meets all fire-related airworthiness standards. The APU comprises a metallic housing having mounts for attaching the housing to an external structure. The APU further comprises at least one temperature sensor suitable for detecting temperature under fire conditions. The temperature sensor is coupled with the mounts for sensing temperature at the housing. | ||
| 申请公布号 | US9481474(B2) | 申请公布日期 | 2016.11.01 |
| 申请号 | US201414583832 | 申请日期 | 2014.12.29 |
| 申请人 | Airbus Operations, S.L. | 发明人 | Casado Montero Carlos;Zamarro Martin Maria Cruz;Fernandez Lopez Pio |
| 分类号 | H02B1/26;B64D45/00;B64D41/00;F02C6/00;F02C7/20;F16H57/02;G01K1/14;G01K13/00 | 主分类号 | H02B1/26 |
| 代理机构 | Greer, Burns & Crain Ltd. | 代理人 | Greer, Burns & Crain Ltd. |
| 主权项 | 1. An auxiliary power unit for an aircraft comprising: a metallic housing having mounts for attaching the housing to an external structure, at least one temperature sensor suitable for detecting temperature under fire conditions, wherein said temperature sensor is coupled with a portion of the housing extending one third of the longer dimension of the housing from each mount for sensing temperature at the housing. | ||
| 地址 | Getafe (Madrid) ES | ||