HEATING TURBOMACHINE FOR A FUEL-CONDITIONING SYSTEM CONFIGURED TO SUPPLY AN AIRCRAFT TURBOSHAFT ENGINE WITH FUEL FROM A CRYOGENIC TANK

Abstract: a heating turbomachine for a fuel-conditioning system, which is configured to supply an aircraft turboshaft engine with fuel from a cryogenic tank. the heating turbomachine comprising: compressor; a turbine; a combustion chamber which is configured to discharge a flow of exhaust air loaded with heat energy and to rotate the turbine; at least one fluid circuit in which a heat-transfer fluid circulates in the downstream direction; and at least one post-combustion heat exchanger which is mounted in the fluid circuit and is configured to extract heat energy from the exhaust air chamber flow between the combustion and the turbine.

Inventor(s): Nicolas Claude PARMENTIER, Samer MAALOUF

CPC Classification: F02C7/224 (Heating fuel before feeding to the burner)

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