Heat exchanger incorporated into a wall of an aircraft

摘要

An aircraft includes at least one wall delimiting a first zone (I) of the aircraft which is thermally insulated from the outside of the aircraft and a second zone (E) contained within the aircraft which is not thermally insulated with respect to the outside of the aircraft and a heat exchanger inside which a heat transfer fluid circulates, wherein the wall includes at least one duct inside which the heat transfer fluid circulates so as to act as a heat exchanger.

主权项

1. An aircraft comprising:
a first zone thermally insulated from outside of the aircraft; a second zone contained with the aircraft and not thermally insulated with respect to the outside of the aircraft; at least one wall delimiting the first zone of the aircraft and the second zone; and a first heat exchanger wherein a heat transfer fluid is configured to circulate to remove heat from a heat source in the aircraft, wherein said at least one wall comprises at least one duct wherein the heat transfer fluid is configured to circulates so as to act as a second heat exchanger to dissipate heat to air present in the second zone.