| 发明名称 |
Engine assembly of an aircraft including a display unit |
| 摘要 |
An engine assembly comprising an engine and a pod surrounding the engine that is equipped, upstream according to the direction of entry of air into the engine, with a fan provided with blades, the pod having an upstream air intake. The engine assembly also comprises a display unit including at least one light ring arranged in the air intake upstream of the fan, the light ring including at least one row of light-emitting diodes and being configured to emit at least one light beam and to project it on the blades of the fan. |
| 申请公布号 |
US2016355276(A1) |
申请公布日期 |
2016.12.08 |
| 申请号 |
US201615171171 |
申请日期 |
2016.06.02 |
| 申请人 |
Airbus Operations (SAS) |
发明人 |
Porte Alain;Chelin Frederic;Rehm Wolfgang;Papin Nathalie;Moreno Gonzalez Irene |
| 分类号 |
B64D47/00;F04D27/00;B64D27/10;F01D25/24;F02C7/04;F04D29/32;F04D29/38 |
主分类号 |
B64D47/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An engine assembly comprising:
an engine and a pod surrounding the engine, the engine being equipped, upstream according to the direction of entry of air into the engine, with a fan provided with blades, said pod having upstream an air intake, said air intake being arranged upstream of the fan, the engine assembly comprising at least one display unit arranged in the air intake, said display unit including at least one light ring arranged in the air intake upstream of the fan, said light ring including at least one row of light-emitting diodes and being configured to emit at least one light beam and to project it on the blades of the fan. |
| 地址 |
Toulouse FR |
