| 发明名称 |
ELECTRICAL DE-ICING FOR AIRCRAFT |
| 摘要 |
A heating element for in-flight de-icing of aircraft is disclosed. The heating element includes a carbon fiber material that is designed to be arranged on a component of an aircraft. The carbon fiber material includes at least two electrical contacts for connecting to an electrical wiring system, and at least one insulation layer for electrical insulation. |
| 申请公布号 |
US2017081033(A1) |
申请公布日期 |
2017.03.23 |
| 申请号 |
US201615272988 |
申请日期 |
2016.09.22 |
| 申请人 |
AIRBUS DEFENCE AND SPACE GMBH |
发明人 |
STEINWANDEL Juergen;JONKE Dietrich;PIRINGER Helmut |
| 分类号 |
B64D15/12;C23C16/44;C23C16/02;B05D3/02;C23C16/34;C23C16/32;C23C16/38;B05D1/22;C23C16/40 |
主分类号 |
B64D15/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A heating element for in-flight de-icing of aircraft, comprising:
a carbon fiber material for arrangement on a component of an aircraft, the carbon fiber material comprising: at least two electrical contacts for connecting to an electrical wiring system; and at least one insulation layer for electrical insulation. |
| 地址 |
Taufkirchen DE |
