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    • 3. 发明授权
    • Method and device for acoustic length testing of compressor
    • 压缩机声学长度试验方法及装置
    • US08306765B2
    • 2012-11-06
    • US12338086
    • 2008-12-18
    • William C. Egan
    • William C. Egan
    • G06F17/40G06F17/00
    • F04C29/061F04C18/16
    • Computer system and method for determining frequencies of various components of a volume choke volume dampener to be attached to a compressor. The method includes determining a sound spectrum of a cavity of the compressor without attaching the dampener to the compressor; calculating an acoustic wavelength of the cavity; receiving a length of a proximal nozzle of the dampener; and calculating, based on the acoustic wavelength of the cavity and the length of the proximal nozzle of the dampener, multiple order frequencies associated with the proximal nozzle of the dampener and the cavity of the compressor, wherein the proximal nozzle of the dampener is proximal to the cavity of the compressor when the dampener is attached to the compressor.
    • 用于确定要连接到压缩机的体积扼流体积阻尼器的各种部件的频率的计算机系统和方法。 该方法包括确定压缩机空腔的声谱,而不将阻尼器连接到压缩机; 计算腔的声波长; 接收所述阻尼器的近端喷嘴的长度; 并且基于所述腔的声波波长和所述阻尼器的近侧喷嘴的长度,计算与所述阻尼器的近侧喷嘴和所述压缩机的空腔相关联的多个次级频率,其中所述阻尼器的近侧喷嘴接近 压缩机的空腔,当减振器连接到压缩机时。
    • 4. 发明授权
    • Fatigue resistant thermowell and methods
    • 耐疲劳耐热套管及方法
    • US08770837B2
    • 2014-07-08
    • US12643533
    • 2009-12-21
    • William C. EganRobert Schultz
    • William C. EganRobert Schultz
    • G01K7/00G01K1/00G01K13/00G01K1/14G01K13/02G01K1/08
    • G01K1/08G01K1/14G01K13/02
    • Methods and thermowell systems that can be uses in high dynamic pressure environments. A thermocouple system includes a thermowell configured to enter a structure through which a medium flows; an elongated probe provided partially inside the thermowell and configured to measure a temperature; at least one o-ring disposed around the elongated probe at a first end, the o-ring being configured to dampen a vibration for the elongated probe by contacting the thermowell; and an elastomer disposed around the elongated probe section at a second end, the elastomer being configured to dampen the vibration for the elongated probe by contacting the thermowell.
    • 可在高动态压力环境中使用的方法和热套管系统。 热电偶系统包括配置成进入介质流过的结构的热套管; 细长的探针部分地设置在热套管内并被配置成测量温度; 至少一个O形环在第一端处设置在所述细长探针周围,所述O形环被配置为通过接触所述热套管来衰减所述细长探针的振动; 以及弹性体,其在第二端处围绕所述细长探针部分设置,所述弹性体构造成通过接触所述热套管来抑制所述细长探针的振动。
    • 5. 发明申请
    • Fatigue Resistant Thermowell and Methods
    • 耐疲劳耐热套管及方法
    • US20110150033A1
    • 2011-06-23
    • US12643533
    • 2009-12-21
    • William C. EganRobert Schultz
    • William C. EganRobert Schultz
    • G01K7/02G01K13/00G01K1/14
    • G01K1/08G01K1/14G01K13/02
    • Methods and thermowell systems that can be uses in high dynamic pressure environments. A thermocouple system includes a thermowell configured to enter a structure through which a medium flows; an elongated probe provided partially inside the thermowell and configured to measure a temperature; at least one o-ring disposed around the elongated probe at a first end, the o-ring being configured to dampen a vibration for the elongated probe by contacting the thermowell; and an elastomer disposed around the elongated probe section at a second end, the elastomer being configured to dampen the vibration for the elongated probe by contacting the thermowell.
    • 可在高动态压力环境中使用的方法和热套管系统。 热电偶系统包括配置成进入介质流过的结构的热套管; 细长的探针部分地设置在热套管内并被配置成测量温度; 至少一个O形环在第一端处设置在所述细长探针周围,所述O形环被配置成通过接触所述热套管来衰减所述细长探针的振动; 以及弹性体,其在第二端处围绕所述细长探针部分设置,所述弹性体构造成通过接触所述热套管来抑制所述细长探针的振动。