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介绍我站燃油流量标准装置在校准美国EG&G公司生产的液体涡轮流量传感器时,其检测结果与美国EG&G公司油流量标准装置的检测结果相一致,平均仪表系数两者相差Kmax=0.065%,进行了一次油流量标准装置间的量值比对工作。为今后进行同类流量标准装置间的比对积累了经验。 相似文献
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介绍一种高精度低温介质稳态质量流量、液位自动测量系统,该系统包括液面计、密度计、二次仪表、采集系统、微机系统等,可通过计算机对低温介质贮箱中的液位进行实时监测,并能计算低温介质的稳态质量流量。该系统对液氧液位实时监测的精度可达到3%,对液氧稳态质量流量测量的精度可达到0.473%。 相似文献
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为提高谐振式MEMS压力传感器的品质因数,且同时降低温度漂移,设计了一种传感器的单芯片级真空封装和低应力组装方法,选用非光敏苯并环丁烯(BCB)材料在真空加热、加压条件下实现PYREX7740玻璃空腔与传感器芯片的黏合键合,在可伐合金管座上加工出与传感器尺寸相匹配的方形空腔,实现传感器芯片的低应力组装.实验结果表明:传感器具有较高的品质因数(9455),检测范围为500—1100hPa,灵敏度为9.6Hz/,hPa,满量程最大非线性度为0.08%,-40℃-50℃内温度系数为0.9Hz/℃,温度总漂移为传感器满量程变化的1.3%,传感器在开机加电稳定后长时漂移为0.086%F.S. 相似文献
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《工业计量》2017,(1)
为了研究高精度电磁流量计在不同温度下的特性变化,以山东省计量院的DN50~DN400热水流量标准装置为实验平台,对横河DN40、科隆DN80、西门子DN100三块0.2级电磁流量计进行研究。采用热水流量标准装置质量法测试电磁流量计在不同温度及流速下的仪表系数和重复性。通过实验分析得出:电磁流量计的仪表系数随介质温度的升高逐渐降低;仪表系数在高温以及低温处受影响明显,DN40电磁流量计的仪表系数本次实验高低温处最大变化量约为0.7%;在电磁流量计对应的流量范围内,仪表系数受介质流速变化的影响不超过±0.2%等。通过实验分析,对电磁流量计的特性有了深入的了解,对流量计量器具的标定以及相关的实验工作有着积极的作用。 相似文献
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脉冲型流量传感器仪表系数准确性研究 总被引:3,自引:0,他引:3
本文介绍了脉冲型流量传感器仪表系数的设置方法,提出了线性仪表系数的概念和使用线性仪表系数带来的好处,尤其对气体流量测量领域中,线性仪表系数具有很大的实用意义。 相似文献
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利用γ射线的指数衰减规律,研制放射性的燃油密度传感器,在不同的环境条件下测量燃油密度。本文主要从放射性燃油密度测量传感器的工作原理,数学建模,测量数据分析等方面来论述放射性燃油密度测量技术在飞机燃油系统中的应用。 相似文献
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水中运动体高速下会发生空化而改变流场结构,研究测速涡轮装置空化特性对提升运动体自主环境感知能力具有重要意义。该文基于内置测速涡轮的防空化结构设计,针对水流速度为10 m/s下的不同空化数、有无偏角情况,利用空化水洞实验和数值仿真模拟对测速涡轮装置的空化情况、涡轮转动情况和涡轮装置的空化特性进行了研究。结果表明:与无涡轮装置样机相比,空化区域发生了明显变化,云状空化团脱落明显加快,云状脱落范围更小。同时,该涡轮装置具有隔离外部空化的能力,在外界空化数高于临界空化数(σCr=0.4)的情况下,能够保证涡轮装置位于线性测量范围。 相似文献
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A new method is considered for measuring the mass flow rate of a substance in pipelines using restricting apertures, without the use of instruments for measuring the density and temperature of the flow. A structural measurement scheme is given and analytical expressions are obtained for determining the mass flow rate and the density of the substance under working conditions. A calculation is given of the errors of the flow parameters. 相似文献
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本文介绍了一种基于分子流传感元件的真空腔体漏率测量方法,该方法通过分子流传感元件测量真空腔体整体漏率,采用的测量装置由气体流量测量系统、真空抽气系统、恒温系统等部分组成。在测量系统中,流经传感元件的气流处于分子流状态,通过测量传感元件两端的差压,计算质量流量,可以得到真空腔体的整体漏率。实验中对多个真空腔体漏率的测量结果表明,该方法可以实现对10-5-10-3 Pa·m3/s量级真空腔体漏率的准确测量。除去本底漏率之后,测量结果与理论结果高度拟合,测量结果显示最小偏差为0.05%,最大仅为0.62%。且通过改变分子流传感元件流导值和差压变送器量程可以进一步扩展该方法可测真空腔体整体漏率范围。 相似文献
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Ultrasonic density sensor for liquids 总被引:1,自引:0,他引:1
Puttmer A Hauptmann P Henning B 《IEEE transactions on ultrasonics, ferroelectrics, and frequency control》2000,47(1):85-92
This paper presents an ultrasonic density sensor for liquids that unifies high accuracy with high durability and is suitable for on-line measurements in a wide range of tube diameters. The sensor consists of a transducer with a piezoceramic disk mounted between two reference rods of quartz glass. Additionally, a second transducer is used as a sound receiver. The density is obtained from the reflection coefficient of ultrasound at the interface between the quartz glass rod and the liquid and the transit time of sound between this interface and the second transducer. Parameters, such as high long-term stability and accuracy of +/-0.1% of full scale, were obtained by an internal acoustic reference measurement. The reference signal is generated using the sound radiated from the rear side of the piezoceramic disk. Design aspects such as sensor materials and signal-to-noise ratio are discussed, and experimental results are given in this paper. Applications of the sensor include concentration measurement, and ultrasonic mass flow measurement. 相似文献
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《低温学》2015
A cryogenic liquid turbine expander is developed as a replacement for traditional Joule–Thomson valves used in the cryogenic systems for the purpose of energy saving. An experimental study was conducted to evaluate the performance of the turbine expander and is the subject of this paper. The test rig comprises a closed-loop liquefied nitrogen system, cryogenic liquid turbine expander unit, and its auxiliary and measuring systems. The test operating parameters of the turbine expander are determined on the basis of flow similarity rules. Pre-cooling of the liquid nitrogen system is first performed, and then the tests are conducted at different flow rates and speed ratios. The turbine expander flow rate, inlet and outlet pressure and temperature, rotational speed and shaft torque were measured. Experimental results and their uncertainties were analyzed and discussed. The following are demonstrated: (1) For both test cases, turbine expander peak isentropic efficiency is respectively 78.8% and 68.4% obtained at 89.6% and 92% of the design flow rate. The large uncertainties in isentropic efficiency are caused by the large enthalpy variations subjected to small measurement uncertainties in temperature and pressure. (2) Total efficiency and hydraulic efficiency of the turbine expander are obtained. They are essentially the same, since both include flow-related effects and also bearing losses. Comparisons of total efficiency and hydraulic efficiency were used to justify measurement uncertainties of different quantities, since the former involves the measured mass flow rate and enthalpy drop (being dependant on inlet and outlet temperature and pressure), while the latter involves the actual shaft power, volume flow rate, and inlet and outlet pressure. (3) Losses in flow passages and the shaft-bearing system have been inferred based on the measured turbine expander total efficiency, isentropic efficiency, and mechanical efficiency, which are respectively 57.6–74.8%, 62.1–78.8% and 89.5–96.4%. Uncertainty analysis is conducted for experimental isentropic efficiency, hydraulic efficiency, and total efficiency. The hydraulic efficiency seems to be the best measure for assessing the performance of cryogenic liquid turbine expander. (4) Isentropic efficiency versus speed ratio is obtained from the experimental data. The experimental isentropic efficiency increases with the speed ratio, and it reaches 78.8% at the largest experimental speed ratio. A higher efficiency would be achieved if the speed ratio could reach a larger value. This provides some guidance for an optimal operation of the turbine expander in the future. 相似文献
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水下常规弹药引信可利用外置涡轮获得其自身运动速度,研究高速旋转涡轮的空化特性对引信测速、测距误差的分析具有重要意义。该文从空化的发生和发展机理出发,针对水流速度为10m/s和8m/s下的不同空化数,分别利用数值仿真和空化水洞实验对涡轮空化形态和动力学特性进行了研究,并分析了空化条件下的涡轮转动。根据仿真和实验的结果,对涡轮空化发展的各阶段特征进行了分析比较。结果表明,数值方法能较好的预测涡轮空化的发展规律和空化下的涡轮动力特性;在一定的水流速度下,涡轮的转动速度随空化数的降低先略有升高然后降低;在一些水流速度和空化数下,涡轮转速信号具有明显的低频周期性变化。 相似文献