THERMAL ASSEMBLY FOR A PROPULSION SYSTEM OF AN AIRCRAFT

Abstract: a thermal assembly including a heat exchanger including a central matrix including a first assembly, an inlet module configured to cause a first fluid to enter the central matrix, and an outlet module configured to evacuate the first fluid from the central matrix, and a support including a base to be fixed to the propulsion system and rails rigidly fastened to the base including a second assembly cooperating with the first assembly to form a sliding connection. also an aircraft with such a heat exchanger.

Inventor(s): Szymon FULARA, Sébastien DARGEIN

CPC Classification: B64D33/10 (EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT)

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