| 发明名称 | Engine and pod assembly for an aircraft, equipped with an anti-icing device including a source of radiation and pulse control unit connected to the source of radiation | ||
| 摘要 | An engine and pod assembly for an aircraft includes a pod receiving an engine having an air intake. A rotating nose cone extends on the nose cone, as well as a device for limiting the formation of ice. The device includes means for creating a circumferential heterogeneity of ice on the nose cone. | ||
| 申请公布号 | US8997451(B2) | 申请公布日期 | 2015.04.07 |
| 申请号 | US201013256308 | 申请日期 | 2010.03.12 |
| 申请人 | Sagem Defense Securite | 发明人 | Dufresne de Virel François;Pealat Michel;Joyez Patrick;Pontoizeau Bruce;Lacuisse Jean-François;Wintenberger Sylvie |
| 分类号 | F02G3/00;B64D15/00;B64D29/00;F02C7/047 | 主分类号 | F02G3/00 |
| 代理机构 | Muncy, Geissler, Olds & Lowe, P.C. | 代理人 | Muncy, Geissler, Olds & Lowe, P.C. |
| 主权项 | 1. An engine and pod assembly for an aircraft, comprising: a pod receiving an engine with an air intake through which a rotating nose cone extends, the pod including a device for limiting the formation of ice on the nose cone, wherein the device includes means for creating a circumferential heterogeneity of ice on the nose cone, and wherein the pod includes a source of radiation able to at least prevent the formation of ice and directed to the nose cone, with the source of radiation being connected to a pulse control unit synchronized with the rotation of the nose cone so that the radiation only hits a portion of the external surface of the nose cone. | ||
| 地址 | Paris FR | ||