| 摘要 |
<p>An adsorption cooling system (1) for an aircraft comprises an evaporator (18), a first adsorber (2), which contains a first adsorption medium for adsorbing an adsorption coolant evaporated in the evaporator (18), and a second adsorber (4), which contains a second adsorption medium for adsorbing the adsorption coolant evaporated in the evaporator (18), the first and the second adsorber (2, 4) being adapted to be operated alternately in an adsorption mode and in a desorption mode, such that one adsorber (2, 4) can adsorb adsorption coolant and the other adsorber (2, 4) can be regenerated. A heat transfer system of the adsorption cooling system (1) is adapted to transfer heat energy, by means of a heat transfer fluid, during a transitional operating phase, during which one adsorber (2, 4) is brought from adsorption mode to desorption mode and the other adsorber (2, 4) is brought from desorption mode to adsorption mode, from the adsorber (2, 4) that is brought from desorption mode to adsorption mode to the adsorber (2, 4) that is brought from adsorption mode to desorption mode</p> |
