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Method for determining real gas effects in critical flow nozzles

机译:确定临界流量喷嘴中实际气体影响的方法

摘要

A method and apparatus for determining the gas flow rate in a high pressure critical flow nozzle is disclosed. A high pressure gas flows through a first critical flow nozzle. Upstream of the first critical flow nozzle a small slip-stream of gas is removed and flows through a smaller second critical flow nozzle. The small second critical flow nozzle drops the pressure of the gas to a low level. This flow rate of this low pressure gas stream is measured in a highly accurate low pressure gas flow rate measuring device. Since the flow rate in this device must be the same as that of the second critical flow nozzle, a correction factor can be calculated for the second critical flow nozzle. This flow rate correction factor will be the same for the first critical flow nozzle.
机译:公开了一种用于确定高压临界流量喷嘴中的气体流速的方法和设备。高压气体流过第一临界流量喷嘴。在第一临界流量喷嘴的上游,一小部分气流被除去并流过较小的第二临界流量喷嘴。小的第二临界流量喷嘴将气体压力降低到较低水平。在高精度的低压气体流量测量装置中测量该低压气体流的流量。由于此设备中的流量必须与第二临界流量喷嘴的流量相同,因此可以为第二临界流量喷嘴计算校正系数。对于第一临界流量喷嘴,该流量校正因子将是相同的。

著录项

  • 公开/公告号US4753095A

    专利类型

  • 公开/公告日1988-06-28

    原文格式PDF

  • 申请/专利权人 CHEVRON RESEARCH COMPANY;

    申请/专利号US19870065195

  • 发明设计人 EMRYS H. JONES JR.;ROBERT E. JACKSON;

    申请日1987-06-22

  • 分类号G01F25/00;

  • 国家 US

  • 入库时间 2022-08-22 06:48:57

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