| 发明名称 | Electromechanical actuator (EMA) heat sink integrated de-icing system | ||
| 摘要 | A de-icing system and method. An electromechanical actuator heat sink is operable to receive heat from an electromechanical actuator, and a heat distribution element is operable to distribute heat to a surface. A heat transportation device is operable to transport heat from the electromechanical actuator heat sink to the heat distribution element. | ||
| 申请公布号 | US9016633(B2) | 申请公布日期 | 2015.04.28 |
| 申请号 | US201113159390 | 申请日期 | 2011.06.13 |
| 申请人 | The Boeing Company | 发明人 | Asfia Julie Fatemeh;Blanding David;Coffman Jeffrey |
| 分类号 | B64D15/00;B64D15/02;B64D15/12;B64C13/50 | 主分类号 | B64D15/00 |
| 代理机构 | Ameh IP | 代理人 | Ameh IP ;Toosi Elahe;Campbell Lowell |
| 主权项 | 1. An aircraft de-icing system comprising: an electromechanical actuator heat sink operable to receive heat from an electromechanical actuator; a heat distribution element operable to distribute heat to an aerodynamic surface; a heat transportation device coupled to the electromechanical actuator heat sink and the heat distribution element, and operable to transport heat from the electromechanical actuator heat sink to the heat distribution element; and a controller module operable to regulate heat transfer from the electromechanical actuator to the heat distribution element. | ||
| 地址 | Chicago IL US | ||