| 发明名称 |
ENERGY HARVESTER, AIRCRAFT COMPONENT COMPRISING THE ENERGY HARVESTER AND AN AIRCRAFT COMPRISING THE ENERGY HARVESTER OR THE AIRCRAFT COMPONENT |
| 摘要 |
An energy harvester for an aircraft comprises a first portion, a second portion and an energy storing unit. The first portion includes a charge collecting device having an electrical permittivity different to the one of air. The charge collecting device is configured to be exposed to an air flow. The second portion is configured to be exposed to air and includes a conductive material. The energy storing unit is electrically connected between the first portion and the second portion. |
| 申请公布号 |
US2015180371(A1) |
申请公布日期 |
2015.06.25 |
| 申请号 |
US201414574724 |
申请日期 |
2014.12.18 |
| 申请人 |
Airbus Defence and Space GmbH |
发明人 |
Becker Thomas;Elefsiniotis Alexandros;Schmid Ulrich |
| 分类号 |
H02N1/04;B64D41/00 |
主分类号 |
H02N1/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An energy harvester for an aircraft, comprising:
a first portion including a charge collecting device having an electrical permittivity different to that of air, the charge collecting device being configured to be exposed to an air flow; a second portion configured to be exposed to air, the second portion including a conductive material; and an energy storing unit electrically connected between the first portion and the second portion. |
| 地址 |
Ottobrunn DE |
