| 发明名称 |
AIRCRAFT AIR CONDITIONING SYSTEM AND METHOD OF OPERATING AN AIRCRAFT AIR CONDITIONING SYSTEM |
| 摘要 |
An aircraft air conditioning system comprising an ambient air supply line having a first end connected to an ambient air inlet and a second end connected to a mixer of the aircraft air conditioning system so as to supply ambient air to the mixer. A first compressor is arranged in the ambient air supply line and is adapted to compress the ambient air flowing through the ambient air supply line. A bleed air supply line allows a flow of bleed air bled off from an engine or an auxiliary power unit therethrough. A bleed air turbine is driven by the bleed air flowing through the bleed air supply line and is coupled to the first compressor so as to drive the first compressor. |
| 申请公布号 |
US2016083100(A1) |
申请公布日期 |
2016.03.24 |
| 申请号 |
US201514859610 |
申请日期 |
2015.09.21 |
| 申请人 |
Airbus Operations GmbH |
发明人 |
Bammann Holger;Klimpel Frank;Brunswig Hans |
| 分类号 |
B64D13/06 |
主分类号 |
B64D13/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft air conditioning system comprising:
an ambient air supply line having a first end connected to an ambient air inlet and a second end connected to a mixer of the aircraft air conditioning system so as to supply ambient air to the mixer, a first compressor arranged in the ambient air supply line and being adapted to compress the ambient air flowing through the ambient air supply line, a bleed air supply line having a first end connected to an engine or an auxiliary power unit and a second end connected to an aircraft environment, and a bleed air turbine driven by the bleed air flowing through the bleed air supply line and being coupled to the first compressor so as to drive the first compressor. |
| 地址 |
Hamburg DE |
