| 发明名称 |
Device and Method for Deicing and/or Preventing Ice Formation and Profile Element and Aircraft Having Such a Device |
| 摘要 |
In order to maintain a surface region of an aircraft free of ice in a particularly energy-efficient manner, a device for deicing and/or for preventing ice formation is provided on an aircraft. The device includes a heat emitting device for emitting heat at a surface region of the aircraft, the heat emitting device is designed to dissipate heat along a line in order to produce a predetermined breaking point or a predetermined breaking line or parting line in ice accumulating on the surface region. |
| 申请公布号 |
US2015129720(A1) |
申请公布日期 |
2015.05.14 |
| 申请号 |
US201414539491 |
申请日期 |
2014.11.12 |
| 申请人 |
Airbus Defence and Space GmbH |
发明人 |
STROBL Tobias;STORM Stefan;RAPS Dominik;HAUK Tobias |
| 分类号 |
B64D15/16;B64D15/20 |
主分类号 |
B64D15/16 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A device for de-icing or for preventing ice formation for an aircraft, comprising:
a heat emitting device configured to emit heat at a surface region of the aircraft, wherein the heat emitting device is configured to dissipate heat along a line in order to produce a predetermined breaking point, a predetermined breaking line, or parting line in ice accumulating on the surface region. |
| 地址 |
Ottobrunn DE |
