HEAT EXCHANGER ASSEMBLY FOR AN AIRCRAFT
    2.
    发明公开

    公开(公告)号:EP4438985A1

    公开(公告)日:2024-10-02

    申请号:EP24167380.5

    申请日:2024-03-28

    发明人: DUROCHER, Eric S.

    摘要: A heat exchanger assembly (26) for an aircraft (1000) includes a housing (92), a heat exchanger (96), and a nozzle (152). The housing (92) includes an inner flow path wall (100), an outer flow path wall (102), an inner inflatable diaphragm (224), and an outer inflatable diaphragm (226). The inner flow path wall (100) and the outer flow path wall (102) form an air inlet (106) and an air outlet (108). The inner inflatable diaphragm (224) and the outer inflatable diaphragm (226) form a venturi channel (134) between the air inlet (106) and the air outlet (108). The heat exchanger (96) is disposed downstream of the venturi channel (134) within the air flow path (110). The nozzle (152) includes a nozzle housing (158) disposed within the air flow path (110). The nozzle housing (158) forms a nozzle inlet (176) and a nozzle outlet (178). The nozzle outlet (178) is disposed at the venturi channel (134).

    HOHLRAUM-X-MISCHER-WÄRMETAUSCHER
    4.
    发明公开

    公开(公告)号:EP3408014A1

    公开(公告)日:2018-12-05

    申请号:EP17701535.1

    申请日:2017-01-27

    申请人: BASF SE

    IPC分类号: B01F5/06 B01F15/06 F28D7/00

    摘要: The invention relates to a mixer-heat exchanger insert or a mixer-heat exchanger insert assembly and to a mixer-heat exchanger comprising a corresponding mixer-heat exchanger insert assembly which has an improved mixing and temperature control behavior and which is less prone to fouling. The mixer-heat exchanger insert comprises a first group of hollow body plates (10, 11) with an inner volume (13) and a second group of hollow body plates (20, 21) with an inner volume (23). The hollow body plates (10, 11) of the first group are inclined in a first direction (RI) relative to a longitudinal extension direction (L) of the mixer-heat exchanger insert (1), and the hollow body plates (20, 21) of the second group are inclined in a second direction (R2) relative to the longitudinal extension direction (L) of the mixer-heat exchanger insert (1). The hollow body plates (10, 11) of the first group laterally abut the hollow body plates (20, 21) of the second group, and the inner volumes (13) of the first hollow body plates (10, 11) are connected to the inner volumes (23) of the second hollow body plates (20, 21) such that the inner volumes (13) of the first group and the inner volumes (23) of the second group are part of a continuous total inner volume (13, 23) which is designed to conduct a temperature controlling fluid.

    FIN-AND-TUBE TYPE HEAT EXCHANGER, AND ITS RETURN BEND PIPE

    公开(公告)号:EP2042825B1

    公开(公告)日:2018-10-03

    申请号:EP07790611.3

    申请日:2007-07-11

    摘要: The invention provides a fin-and-tube heat exchanger using a return bend tube that allows further enhancement of the evaporative performance of the heat exchanger. The fin-and-tube heat exchanger, where a refrigerant is supplied inside tubing, has a hairpin tube portion where a plurality of hairpin tubes are arranged, a return bend tube portion where there are arranged a plurality of return bend tubes joined to respective hairpin tube ends of the hairpin tube portion, and a fin portion comprising a plurality of fins arranged at a predetermined spacing on the outer surface of the hairpin tubes. The heat exchanger comprises first grooves formed on the tube inner surface of the return bend tube. A first groove pitch (P1) of the first grooves in a cross section perpendicular to a tube axis, and a second groove pitch (P2) of spiral-shaped second grooves formed on the inner surface of the hairpin tube in a cross section perpendicular to a tube axis, satisfy a groove pitch ratio (P1/P2) of 0.65 to 2.2, while a first groove cross-sectional area (S1) per groove of the first grooves in a cross section perpendicular to the tube axis, and a second groove cross-sectional area (S2) per groove of the second grooves in a cross section perpendicular to the tube axis satisfy a groove cross-sectional area ratio (S1/S2) of 0.3 to 3.6.