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Y. M. Choi, N. D. Trang, W. Kang, Y. Terao, N. Kurihara, A. Iwai, T. Funaki, S. H. Bak, C. S. Yoo, Y. T. Kwon
The inter-comparison of air speed from 2 m/s to 40 m/s by Pitot static tubes

The Mutual Recognition Arrangement (MRA) is framed by the International Committee of Weights and Measures in order to establish the degree of equivalence of national measurement standards via the key comparisons as well as the inter-comparisons of measurements. Based on this objective, the current work was performed in order to determine the degrees of equivalence among three laboratories in Korea Research Institute of Standards and Science (KRISS), National Metrology Institute of Japan (NMIJ) and HCT company for air speed over the range from 2 m/s to 40 m/s. In this inter-comparison of air speed, two AMCA type Pitot static tubes were considered as artifacts. The reference value (RV) and its uncertainty was calculated from all measurement results reported by the participants. The normalized deviations, En-number, were mostly smaller than 1. Consequently, the results of participants were mutually consistent.

E. Audrito, F. Bertiglia, M. Bisi, C. Francese, G. La Piana, A. Piccato, M. Santiano, P. G. Spazzini
A novel calibration of the Large Piston Prover at INRIM

INRIM realizes its flow rate standard using three distinct facilities, aimed at measuring different flow rate ranges; in particular, for the larger flow range (10-2600 L/min) a piston of 1000 mm nominal diameter and 1200 mm nominal stroke is used. The traceability of the standard is obtained through dimensional calibration of the piston, regarding both the piston size and its stroke.
The first calibration of the machine was performed at its initial installation. Even if most of the relevant documentation about this first calibration is not available, INRIM realized a procedure similar to the old one and performed measurements to renovate the first facility calibration. The present paper will dedicate special attention to the description of the measurement chain used for the calibration of the piston in its own siege. Moreover, the method for the transfer of traceability from the length standard to the measurement of the piston diameter will be discussed; it should be noted that the dimensional study is not completed yet, because the first set of measurements described in the present work, evidenced the criticalities of the procedure adopted in the past. For this aim, a further measurement campaign will be carried out in order to minimize the uncertainty associated to the dimensional measurement of the piston and of its displacement. Finally, the results of first dimensional evaluation will be presented alongside.

S. Oertel, M. Eggert, C. Gutsmuths, P. Wilhelm, H. Müller, H. Többen
Bistatic wind lidar system for traceable wind vector measurements with high spatial and temporal resolution

Wind lidar systems have become a cost-efficient alternative to wind met masts in the recent years to measure and monitor the wind velocity in many applications in the fields of wind energy and meteorology. Conventional wind lidar systems work according to the monostatic measurement principle that is inherently accompanied by a spatial and temporal averaging procedure. This averaging procedure complicates the traceability of such systems as the uncertainty of the measured wind velocity depends on the homogeneity of the investigated wind fields. In contrast, the wind lidar system presented here works according to a bistatic measurement principle that measures the velocity vector of single aerosols in a spatially highly resolved measurement volume in heights from 5 m to 250 m with a resolution of about 0.1 m/s. The novel system has the potential for traceable wind speed measurements in homogeneous as well as in inhomogeneous wind fields as was proven by comparison measurements with a wind met mast. At PTB, the aim is to use the bistatic wind lidar as a traceable reference standard to calibrate other remote sensing devices, necessitating an in-depth validation of the bistatic lidar system and its measurement uncertainty. To this end, a new, specially designed wind tunnel with a laser Doppler anemometer (LDA) as flow velocity reference has been built up to validate the bistatic lidar in detail. First validation measurements in the velocity range from 4 m/s to 16 m/s are presented, showing an average deviation between the bistatic lidar and the LDA of 0.37 %.

O. Büker, K. Stolt
Investigations on pressure dependence of Coriolis Mass Flow Meters used at Hydrogen Refuelling Stations

In the framework of the ongoing EMPIR JRP 16ENG01 “Metrology for Hydrogen Vehicles” a main task is to investigate the influence of pressure on the measurement accuracy of Coriolis Mass Flow Meters (CFM) used at Hydrogen Refueling Stations (HRS). At HRS hydrogen is transferred at very high and changing pressures with simultaneously varying flow rates and temperatures. It is clearly very difficult for CMFs to achieve the later expected legal requirements in relation to the demand for accurate mass flow measurement at the measurement conditions at HRS. It was observed, mainly due to the very dynamic filling process, that the accuracy of mass flow measurement at different pressure ranges is too inaccurate. Particularly at higher pressures it was found out that especially short refuelling time causes significant measurement deviations. On this background it can be concluded that the medium pressure has a great impact on the mass flow measurement accuracy. To gain a deeper understanding of this matter RISE has built a unique high-pressure test facility. With the aid of this newly developed test rig it is possible to calibrate CFMs over a wide pressure and flow range with water and base oils as test medium. The test rig allows calibration measurements under the conditions prevailing at 70 MPa HRS regarding mass flows (up to 3.6 kg min-1) and pressures (up to 87.5 MPa).

R. Maury, C. Auclercq, C. Devilliers
Hydrogen refuelling station calibration with a traceable gravimetric standard

Of all alternatives to gasoline fuels, hydrogen offers the greatest long-term potential to radically reduce many problems inherent in transportation fuel use. Hydrogen vehicles have zero tailpipe emissions and are very efficient. If it is made from renewable sources, nuclear power, or fossil sources with carbon emissions captured and sequestered, hydrogen use on a global scale could produce nearly zero greenhouse gas emissions and greatly reduce emissions of air pollutants.The aim of this work is to realise a traceability chain for hydrogen flow metering in the range typical for fuelling application in a wide pressure range with pressures up to 875 bar (for Hydrogen Refuelling Station HRS with Nominal Working Pressure of 700 bar) and temperature changes from - 40 °C (pre-cooling) to 85 °C (maximum allowed vehicle tank temperature) in accordance with the worldwide accepted standard SAE J2601.Several HRS have been tested in Europe (France, Netherlands and Germany) and the results show a good repeatability for all tests. This demonstrates that the testing equipment works well in real conditions. Depending on the configuration of installation, some systematic errors have been detected and explained. Errors observed for the stations of Configuration 1 can be explained by the difference of pressure, at beginning and end of the fueling, in the piping between the CFM and the dispenser: the longer the distance, the bigger the errors. For Configuration 2, as this distance is very short, the error is negligible.

A. K. Niemann, S. Haack, J. Frederiksen
Novel calibration facility for water flow with large temperature span

Danish Technological Institute (DTI) is extending the flowrate of the existing flow rig up to 1.000 m³/h in the temperature span from 4 – 85 °C and pipe dimension up to DN400, and thereby become a unique calibration facility. The new test rig will serve as the national primary standard for the field of water flow measurement and thereby replacing the current at DTI.
From 0.5 – 500 m³/h the test rig is based on gravimetric principle using a diverter principle. From 500 – 1000 m³/h the test rig is based on reference flow metering. The reference flow meters will consist of two high precision Coriolis flowmeters mounted in parallel. The reference flowmeters are placed in the same circuit as the gravimetric system. This setup allows for calibration of each reference flowmeter against the gravimetric method without dismounting the meters. This ensures low uncertainties and traceability to a primary standard and possibility to participate in international intercomparisons.
The new flow rig will be highly digitalized with a high degree of automation. Communication with flowmeters under test will be flexible with both conventional analogue interfaces but also through industrial communication standards.

T. Meng, C. Xing, B. Wu, C. Wang, H. C. Shi, X. P. Li
Experimental Analysis of Influencing Factors on Flow Stability of Water Flow Facilities

Because the flow fluctuation can cause the deviation of flow measurement, flow stabilizing methods are used, in the most of the flow metering facilities. Two common flow stabilizing methods of water flow facilities are tested by a new flow stability measurement system which is consisted by a flowmeter and a pressure sensor.
The amplitude of fluctuation can be measured by flowmeter, and the frequency of fluctuation can be obtained by FFT (Fast Fourier Transform) analysis of the pressure signal. The direction of fluctuation source can be distinguished by correlation analysis of pressure and flow signals. Based on this method, the characteristics of the fluctuation source can be obtained by experiments under different flow rate and pipe pressure. An obvious fluctuation signal with a frequency of about 1.5Hz had been found in a test for a flow facility with a buffer tank. The amplitude of fluctuation increases with the decrease of flow rate. When the flow rate is less than 1/10 of the rated flow rate of the pump, the amplitude of fluctuation is about 1%. It is shown that the high frequency fluctuation produced by the pump can be effectively isolated by the buffer tank, but the low frequency fluctuation can be caused by the pump when it worked in a low efficiency range.
In another set of experiments, a flow facility with a constant head water tank and a buffer tank was tested, and two flow stabilizing methods were directly compared and analysed. The test results of the two methods are close under the similar working flow rate and pressure. And if it is under different operating conditions, the amplitude of fluctuation is closely related to the opening of the regulating valve which is installed downstream of the test bench. The fluctuation amplitude increases with the decrease of the valve opening. When the valve opening is less than 30%, the fluctuation amplitude is about 0.5%. Further, it is obtained that the cavitation is caused by the excessive local pressure loss of the regulating valve is the main reason of the facility with constant head water tank.
In summary, the buffer tank and the constant head water tank are both effective methods for stabilizing flow, and the optimal stabilization effect can be obtained by setting a reasonable range of operation for the pump and the regulating valve.

J. Geršl, P. Busche, M. de Huu, D. Pachinger, H. Müller, K. Hölper, A. Bertašienė, M. Vilbaste, I. Care, H. Kaykısızlı, L. Maar, S. Haack
Comparison of calibrations of wind speed meters with a large blockage effect

In this paper we report on the first results of EURAMET project no. 1431 which was initiated in 2017 with a goal to experimentally determine systematic deviations of calibration results of vane and cup anemometers due to various boundary conditions in different wind tunnels especially in wind tunnels with open test section where theoretical models are missing. For that purpose 3 vane anemometers and 2 cup anemometers of various dimensions have been calibrated in 14 wind tunnels with various types and sizes of test sections ranging from 15 cm to 100 cm in diameter. This paper provides the first look to calibration data from the recently completed measurements. On top of that, velocity disturbance fields in front of the 5 tested anemometers have been measured in order to avoid mixing of the effect of boundary conditions with other source of deviations due to placing a reference meter to an area influenced by a meter under test. The velocity disturbance fields reported in this paper can be useful for all air speed calibration laboratories giving an idea how large these deviations can be and what is the optimal position and distance of a reference meter.

D. T. Nguyen, W. Kang, Y. M. Choi, S. H. Lee, Y. M. Choi
Uncertainty Evaluation of Stack Flowrate Measurement with S-Type Pitot Tube by Monte Carlo Method

In order to attempt to mitigate the climate change, efforts to reduce the quantity of carbon emissions by actively seeking CO2 trading and carefully control the liability of the emission test monitoring system from the industrial factories are a current issue. Therefore, the quality of greenhouse gas (GHG) emissions measurement with a proper uncertainty needs to be firstly considered. Currently, GHG emissions are estimated by a continuous emission measurement (CEM). The U.S Environmental Protection Agency (EPA), has classified the measurement of GHG emissions by the CEM as the highest quality Tier IV with lowest uncertainty level. Relating to accuracy of the CEM, both knowledge of the uncertainty contributions on GHG concentrations and volumetric flow rates are necessary for achieving a credible result. In order to accurately evaluate the uncertainty of the CEM method, flow rate measurements in the stack as well as GHGs concentration measurements by gas analyzer are crucial due to various uncertainty factors. In this study, we concentrate on finding measurand inputs and their uncertainty estimates that affect volumetric flow rates in a heat and power generation plant. Both the law of propagation method and Monte Carlo method (MCM) are used to evaluate the uncertainty of the flow rate measurement in order to minimize the numerical approximation of the partial derivatives of the complex model with respect to the every input. Consequently, the result of MCM is consistent with the result that by the law of propagation of uncertainty. The relative expanded uncertainties at 95% confidence level with coverage factor k = 2 are 528.1 m³ and 527.2 m³, respectively.

S. H. Lee, M. Link, B.-R. Yoon, E. Frahm
Measurement of hydrocarbon liquid flow rate using volumetric and gravimetric methods: comparison between KRISS and PTB hydrocarbon standard systems

In this study, the hydrocarbon liquid flow rate was measured using both volumetric and gravimetric methods. Both methods are representative reference techniques for measuring the hydrocarbon flow rate. The volumetric method uses a calibrated volume tank, while the gravimetric method is based on a calibrated balance. Using these two methods, which have different traceability systems, a Coriolis flowmeter was calibrated under comparable flow conditions. The deviation and uncertainty of the flow measurement results obtained from the volumetric and gravimetric methods were analyzed.
The study included the calibration of a 1000 L reference volumetric tank at the PTB hydrocarbon facility by using two different approaches: a filling method and a gravimetric method. For the filling method, a 100 L reference volume pipette was installed above the volume tank. A balance system under the 1000 L tank was used to calibrate the tank based on the gravimetric method. The uncertainties of the filling and gravimetric methods were 325.18 ml and 171.39 ml (k = 2), respectively, and the maximum difference between these methods was 78.06 ml. Thus, the calibration values of both methods were found to agree with each other within the estimated uncertainties.
For the final comparison, a Coriolis flowmeter was calibrated using the 1000 L volume tank at the PTB flow facility. The diameter of the pipeline was 80 mm and the flow rate ranged from 13.68 t/h to 54.81 t/h. A balance reference was used at the hydrocarbon flow systems of KRISS. Since the fluid properties (density and viscosity) used at the two institutes are different, the flow measurements were compared based on the Reynolds number to compensate for these fluid properties. The calibration values of the Coriolis flowmeter at KRISS and PTB were 0.21–0.23% (U=0.08%, k = 2) and 0.18–0.24% (U=0.05%, k = 2), respectively, for an Re number range between 35,000 and 145,000. The results from the gravimetric method in KRISS matched very well with the results from the volumetric at PTB, within the estimated uncertainties. Thus, we confirmed that the hydrocarbon flow standard systems of KRISS and PTB have traceability when using the volumetric and gravimetric methods in the given range of Re number. The procedure and results of the volume tank calibration at the PTB hydrocarbon facility will be given during the presentation. In addition, the results of the flow comparison between PTB and KRISS will be presented to demonstrate the traceability of both hydrocarbon laboratories.

Page 180 of 977 Results 1791 - 1800 of 9762