发明名称 |
AUXILIARY COOLING DEVICE FOR CONNECTION TO AN AIRCRAFT LIQUID COOLING SYSTEM |
摘要 |
An auxiliary cooling device is configured to be operated outside of an aircraft. The auxiliary cooling device is configured to be connected to an aircraft liquid cooling system which includes a refrigerating device, a coolant supply connection, a coolant discharge connection, and a control device. The auxiliary cooling device includes a cold source that is adapted to cool a coolant down to a desired low temperature, an auxiliary cooling device outlet which is connected to the cold source and connectable to the coolant supply connection. The auxiliary cooling device also includes an auxiliary cooling device inlet which is connected to the cold source and connectable to the coolant discharge connection of the aircraft liquid cooling system. |
申请公布号 |
EP2303698(A2) |
申请公布日期 |
2011.04.06 |
申请号 |
EP20090768989 |
申请日期 |
2009.06.24 |
申请人 |
AIRBUS OPERATIONS GMBH;AIRBUS SAS |
发明人 |
SOENMEZ, KENAN;LEROY, LUC |
分类号 |
B64F1/36 |
主分类号 |
B64F1/36 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|