An apparatus and method of forming a hybrid heat exchanger 12 including a first manifold 42 defining a first fluid inlet 60 and a second manifold 46 defining a second fluid inlet 70. A monolithic core body 16 includes a first set of flow passages 30 in fluid communication with the first manifold 42 and a second set of flow passages 34 is in communication with the second manifold 46. At least a portion of the first manifold 42 or the second manifold 46 has a tunable coefficient of thermal expansion that is less than a coefficient of thermal expansion of the structurally rigid monolithic core 16.
熱交換器アセンブリ
2021-06-02
Patent
Electronic Resource
Japanese
IPC: | F28F Einzelheiten von Wärmetauschern oder Wärmeübertragungsvorrichtungen für allgemeine Verwendung , DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F28D Wärmetauscher, soweit in keiner anderen Unterklasse vorgesehen, in denen die Wärmetauschmittel nicht in direkte Berührung miteinander kommen , HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT |