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公开(公告)号:EP4348138A1
公开(公告)日:2024-04-10
申请号:EP22732602.2
申请日:2022-05-27
申请人: ENGIE , ArianeGroup SAS
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公开(公告)号:EP4355985A1
公开(公告)日:2024-04-24
申请号:EP22735215.0
申请日:2022-06-13
申请人: ArianeGroup SAS
发明人: DURI, Davide , PENIN, Loïc , PALISSAT, Géraldine , MABILLE DE LA PAUMELIERE, Louis-Vianney , CHABERNAUD, Pierre
CPC分类号: F25J1/0007 , F25J1/001 , F25J1/0015 , F25J1/0022 , F25J2230/3020130101 , F25J2230/0420130101 , F25J1/0242 , F25J1/0296 , F01K25/10
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公开(公告)号:EP4302031A1
公开(公告)日:2024-01-10
申请号:EP22713436.8
申请日:2022-03-03
申请人: ArianeGroup SAS
发明人: DURI, Davide , NOMERANGE, Philippe , PENIN, Loïc , PALISSAT, Géraldine , MABILLE DE LA PAUMELIERE, Louis-Vianney
IPC分类号: F25J1/00
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公开(公告)号:EP3519689A1
公开(公告)日:2019-08-07
申请号:EP17787497.1
申请日:2017-09-28
申请人: ArianeGroup SAS
发明人: DURI, Davide
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公开(公告)号:EP3436671A1
公开(公告)日:2019-02-06
申请号:EP17717786.2
申请日:2017-03-27
申请人: ArianeGroup SAS
发明人: DURI, Davide
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公开(公告)号:EP4302030A1
公开(公告)日:2024-01-10
申请号:EP22713435.0
申请日:2022-03-03
申请人: ArianeGroup SAS
发明人: DURI, Davide , NOMERANGE, Philippe , PENIN, Loïc , PALISSAT, Géraldine , MABILLE DE LA PAUMELIERE, Louis-Vianney
IPC分类号: F25J1/00
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8.
公开(公告)号:EP4189224A1
公开(公告)日:2023-06-07
申请号:EP21752090.7
申请日:2021-07-21
申请人: SAFRAN , ArianeGroup SAS
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公开(公告)号:EP3973170A1
公开(公告)日:2022-03-30
申请号:EP20737259.0
申请日:2020-05-20
申请人: ArianeGroup SAS
发明人: DURI, Davide , BRANDELY, Anaïs , PENIN, Loïc
IPC分类号: F02K9/48
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公开(公告)号:EP3311070A1
公开(公告)日:2018-04-25
申请号:EP16734433.2
申请日:2016-06-09
申请人: ArianeGroup SAS
发明人: DURI, Davide
摘要: System (100) for supplying an igniter with propellant, comprising - a reservoir (10) having an intake (11) and a discharge (12), - a liquid propellant supply line connected to the intake (11) of the reservoir (10), - a propellant discharge line connecting a discharge (12) of the reservoir (10) to an igniter (40), characterized in that said reservoir (10) has an internal volume filled with heat storage spheres (20), said storage spheres (20) being designed to store heat and to transmit it to a fluid passing through said reservoir (10) so as to evaporate a liquid propellant passing through said reservoir (10).
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