B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 11/06 (2006.01) B64D 13/06 (2006.01)
Patent
CA 2668663
A cooling system (10) for cooling an aircraft device (12) comprises an evaporator (14, 16, 18) for receiving a fluid (F) which is to be evaporated, a first adsorber (24) which contains a medium (28) for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18), as well as a second adsorber (26) which contains a medium for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18). A control system (22) is adapted to establish or to interrupt a fluid connection between the evaporator (14, 16, 18) and the first and/or the second adsorber(s) (24, 26).
L'invention concerne un système de refroidissement (10) pour un dispositif (12) d'aéronef, ce système comprenant un évaporateur (14, 16, 18) recevant un fluide (F) à évaporer, un premier adsorbeur (24) qui contient un milieu (28) pour l'adsorption du fluide (F) évaporé dans l'évaporateur (14, 16, 18), ainsi qu'un second adsorbeur (26) qui contient un milieu pour l'adsorption du fluide (F) évaporé dans l'évaporateur (14, 16, 18). Un système de commande (22) est conçu pour établir ou interrompre la circulation de fluide entre l'évaporateur (14, 16, 18) et le premier et/ou le second adsorbeur (24, 26).
Colberg Carsten
Dreyhaupt Michael
Frey Andreas
Kerber Markus
Kiryaman Ahmet Kayihan
Airbus Deutschland Gmbh
Airbus Operations Gmbh
Oyen Wiggs Green & Mutala Llp
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