公开(公告)号：EP4310430A1

公开(公告)日：2024-01-24

申请号：EP22382694.2

申请日：2022-07-19

申请人： Airbus Operations, S.L.U. ,  Airbus Operations Limited ,  Airbus Defence and Space GmbH

发明人： MARTINO GONZÁLEZ, Esteban ,  LINARES VILLEGAS, Mario ,  BAYONA REVILLA, Lucía ,  MILBOURN, Gareth ,  JULLIEN, David ,  CARRETERO BENIGNOS, Jorge

IPC分类号： F28D15/02

摘要： The present invention provides a heat exchanger module comprising: at least one hollow chamber comprising an inner volume configured to house a fluid, said chamber further comprising a fluid inlet and a fluid outlet, wherein the inlet of the chamber is configured to be in fluidic communication with a source of fluid, at least one hollow enclosure extending outwardly from a surface of the hollow chamber, said hollow enclosure comprising an inner volume housing a working fluid, wherein said working fluid is a working fluid configured to undergo a phase change in an operative mode of the heat exchanger module, wherein the hollow enclosure is configured to be in fluidic communication with a source providing a second fluid, wherein an enclosure root of said hollow enclosure is inserted in the hollow chamber, extending into the inner volume of said hollow chamber, such that in an operative mode a fluid flowing through the hollow chamber from the inlet to the outlet bathes the outer surface of said enclosure root.