作者: Mehmet Altay
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摘要: An adsorption cooling system (1) for an aircraft, comprises evaporator (18), a first adsorber (2), with adsorbent adsorbing coolant evaporated in the (18) and second (4), containing wherein (2, 4) may be alternately operated mode desorption such that one adsorbs ad other can regenerated. A heat transfer is designed to transmit from going into absorption by means of fluid during transition phase which goes mode.