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Adaptable system for storing liquid under pressure and spacecraft propellant storage applications thereof

机译:用于在压力下存储液体的自适应系统及其航天器推进剂存储应用

摘要

A system for storing liquid under pressure is adapted to contain any of various quantities of liquid determined in advance with approximately the same filling ratio in an environment in which the temperature varies. It comprises a main storage tank adapted to contain at least the largest of these quantities of liquid in such a way as to leave a residual volume of pressurized gas and a reserve gas storage capacity mechanically independent of the main storage tank and in permanent communication with the residual volume of pressurized gas via a liquid non-return device. The reserve capacity is chosen so that the quantity of liquid actually introduced into the system divided by the sum of the volumes of the main storage tank and reserve capacity is at least approximately equal to the filling ratio.
机译:用于在压力下存储液体的系统适于在温度变化的环境中以近似相同的填充率容纳预先确定的各种液体中的任何一种。它包括一个主储罐,该储罐适于以这种方式容纳至少这些液体中的最大量,以便保留机械上独立于主储罐并与储罐永久连通的剩余量的加压气体和储备气体储罐。通过液体单向装置的加压气体的残余量。选择储备容量,以使实际引入系统的液体量除以主储罐容积和储备容量的总和至少近似等于填充率。

著录项

  • 公开/公告号US5116000A

    专利类型

  • 公开/公告日1992-05-26

    原文格式PDF

  • 申请/专利权人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE;

    申请/专利号US19900629764

  • 发明设计人 ALAIN GIRARD;

    申请日1990-12-18

  • 分类号B64D37/00;

  • 国家 US

  • 入库时间 2022-08-22 05:22:53

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