An electronics cooling system (100) for an aircraft includes a heat exchanger (101) comprising a coolant circuit (103), an air circuit (105) and a fuel circuit (107) such that each of the circuits is in thermal communication with the other circuit. The coolant circuit (103) is in thermal communication with one or more aircraft electronics. The air circuit (105) is fluidly connectable with at least one air source,.The fuel circuit (107) is fluidly connectable with a fuel tank (111) between the fuel tank (111) and an engine of the aircraft and/or fluidly connectable with a fuel loop that returns to the fuel tank (111).
AIRCRAFT ELECTRONICS THERMAL REGULATION SYSTEM
THERMISCHES REGELUNGSSYSTEM FÜR DIE ELEKTRONIK EINES FLUGZEUGS
SYSTÈME DE RÉGULATION THERMIQUE DE L'ÉLECTRONIQUE D'UN AÉRONEF
2020-02-12
Patent
Elektronische Ressource
Englisch
IPC: | 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 |
Engineering Index Backfile | 1967