Disclosed is a fuel conditioning system (SC) configured to supply an aircraft turbine engine using fuel (Q) from a cryogenic tank (RC), the conditioning system (SC) comprising at least one pumping turbomachine (1), a first heat exchanger (31) configured to heat the fuel (Q) in the fuel circuit (CQ) by circulating an air stream (A), and at least one heating turbomachine (2) configured to supply an air flow (A) to the first heat exchanger (31), the heating turbomachine (2) comprising an air intake compressor (21), a combustion chamber (24) and an air exhaust turbine (22) configured to drive the air intake compressor (21), the combustion chamber (24) being supplied with air taken from the air flow (A) and with the fuel (Q) from the fuel circuit (CQ).
FUEL CONDITIONING SYSTEM AND METHOD CONFIGURED TO POWER AN AIRCRAFT TURBINE ENGINE USING FUEL FROM A CRYOGENIC TANK
2024-02-08
Patent
Electronic Resource
English
European Patent Office | 2024
|European Patent Office | 2024
|CRYOGENIC FUEL TANK SYSTEM AND METHOD FOR CRYOGENIC FUEL TANK SYSTEM OPERATING
European Patent Office | 2024
|CRYOGENIC FUEL TANK SYSTEM AND METHOD FOR OPERATING CRYOGENIC FUEL TANK SYSTEM
European Patent Office | 2024
|