发明名称 Pressurizer for a rocket engine
摘要 The present invention provides for a pressurizer for pressurizing a fluid, comprising a pressurant entrance for the introduction of a pressurant, a fluid entrance for the fluid, a fluid exit for the fluid, and a transfer chamber movable in a cycle with respect to the fluid exit, where for a portion of a cycle the pressurant exerts a force on the fluid inside the transfer chamber. In a preferred aspect of the present invention, the pressurizer further comprises a spindle housing more than one transfer chamber, rotatable about an axis between the fluid entrance and the fluid exit. In another preferred aspect, the transfer chamber comprises either a flexible membrane or a movable piston to separate the pressurant and the fluid.
申请公布号 US6499288(B1) 申请公布日期 2002.12.31
申请号 US20010878293 申请日期 2001.06.12
申请人 KNIGHT ANDREW F. 发明人 KNIGHT ANDREW F.
分类号 F02K9/50;F02K9/56;(IPC1-7):F02K9/46 主分类号 F02K9/50
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