Linked, non-plugging cooling microcircuits

摘要

A linked microcircuit (7) for providing coolant gas flow through an aircraft part, comprises at least one inlet through which a coolant gas may enter, a circuit channel (29) extending from the at least one inlet through which the coolant gas may flow. The circuit channel (29) is formed from the superimposition of a plurality of alternating serpentine circuits. At least one outlet (30) is appended to the circuit channel 29 through which the coolant gas may exit the circuit channel.