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公开(公告)号:US11808204B2
公开(公告)日:2023-11-07
申请号:US18007082
申请日:2021-07-21
申请人: SAFRAN , ARIANEGROUP SAS
发明人: Pierre-Alain Lambert , Hugo Pierre Mohamed Jouan , Samer Maalouf , Louis-Vianney Mabille De La Paumeliere , Carlos Alberto Cruz , Davide Duri
摘要: A fuel supply circuit for an aeronautical cryogenic turbomachine including: at least one cryogenic reservoir containing a liquid fuel topped with a boil-off gas and including a high-pressure liquid pump to supply at least one main propulsion device of the turbomachine with liquid fuel, an auxiliary turbomachine including an electric generator, a gas compressor to supply the auxiliary turbomachine with gaseous fuel, and a buffer gas reservoir connecting the gas compressor to the cryogenic reservoir to reinject gas into the cryogenic reservoir in order to maintain the pressure in the cryogenic reservoir above a predefined value, the electric generator supplying the high-pressure liquid pump and the gas compressor.