发明名称 CRYOGENIC TANK AND SPACE LAUNCHER INCLUDING SUCH A TANK
摘要 The invention relates to a cryogenic tank for a space launcher, including a partition (2) defining upper (VS) and lower (VI) spaces for the fluid in the tank, said upper and lower spaces communicating via at least one free central opening (3) formed in the partition so as to enable a flow of the liquid from the upper space to the lower space by gravity and via the central opening(s) and so as to prevent the backflow of fluid from the lower space to the upper space via said central opening(s) due to acceleration forces, the tank further including at least one vent (5) separate from the central opening(s) and ensuring the fluid communication between the upper and lower spaces, the vent being shaped so as to facilitate the transit of vapour from the lower space to the upper space and for preventing a liquid backflow from the lower space to the upper space.
申请公布号 WO2010089493(A1) 申请公布日期 2010.08.12
申请号 WO2010FR50130 申请日期 2010.01.28
申请人 L'AIR LIQUIDE SOCIETE ANONYME POUR L'ETUDE ET L'EXPLOITATION DES PROCEDES GEORGES CLAUDE;LACAPERE, JEROME;BUTTERWORTH, JAMES 发明人 LACAPERE, JEROME;BUTTERWORTH, JAMES
分类号 B64G1/40;F17C13/00 主分类号 B64G1/40
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