| 摘要 |
The system (BZ/CSAS) has air supply sources for supplying air to the system. The air supply sources are formed by air conditioners (ACS1, ACS2) of an aircraft, air conditioning systems of the aircraft or by a combination of the air conditioners and the air conditioning systems of the aircraft. A heat exchanger cools or heats the air in the fuel cell emergency system. A vaporization radiator cools the air, and a water reservoir is integrated in the vaporization radiator, where water is stored in the water reservoir for cooling the air. An independent claim is also included for a method for operating a fuel cell emergency system of an aircraft. |
