scholarly journals An Axial-Flow Cyclone for Aircraft-Based Cloud Water Sampling

2004 ◽  
Vol 21 (12) ◽  
pp. 1825-1839 ◽  
Author(s):  
Derek J. Straub ◽  
Jeffrey L. Collett

Abstract A new aircraft-based cloud water collection system has been developed to provide samples of cloud water for chemical analysis. The collection system makes use of centrifugal separation in an axial-flow cyclone to remove cloud drops from the airstream. An automated sample storage system allows up to seven independent samples to be obtained during a single research flight. The entire collection system is housed in a Particle Measurement Systems (PMS) canister to permit the collector to be used on a range of research aircraft without extensive modification to the collector or the aircraft structure. Computational fluid dynamics (CFD) analysis was used extensively throughout the development of the new collector for component design and to predict internal flow dynamics. CFD-based cloud drop trajectory simulations provided an estimate of collection efficiency as a function of drop size. Based on the numerical modeling, the 50% cut diameter was predicted to be 8 μm. Through a quantitative laboratory calibration using fluorescein-tagged monodisperse drops, CFD predictions of drop deposition patterns in the interior of the axial-flow cyclone were verified. The numerical and experimental evaluations were performed to ensure that the population of collected cloud drops is well characterized. Initial flight testing of the system occurred during the Dynamics and Chemistry of Marine Stratocumulus, Phase II (DYCOMS-II) field project in July 2001. Although the major components of the prototype collection system operated as expected during flight testing, sample collection rates were lower than expected because of the inefficient removal and storage of cloud water collected in the axial-flow cyclone. Actual sample collection rates ranged between 0.1 and 1.2 mL min−1.

2011 ◽  
Vol 27 (3) ◽  
pp. 272-280 ◽  
Author(s):  
Se-Young Kim ◽  
Soon-Bark Kwon ◽  
Duck-Shin Park ◽  
Young-Min Cho ◽  
Jin-Ho Kim ◽  
...  

Author(s):  
Yigang Luan ◽  
Lianfeng Yang ◽  
Tao Sun

Axial flow cyclone separator with guide blade has been widely used, due to its low resistance, huge gas processing and small volume. Although its structure is simple, three-dimension strong rotating turbulent flow forms which involves many complex interactions such as dual-phase separation, adsorption and electrostatic interference. This paper is focused on studying the resistance performance of the axial flow cyclone separator. Numerical simulation methods are carried out to acquire the internal flow field characteristics under different operating pressure and temperature conditions. The result shows that the pressure drop decreases under the same operating pressure, as the operating temperature increases. When the operating temperature is the same, the higher operating pressure enhances the value of the pressure drop. Velocity distribution, pressure contours and turbulent viscosity contours have been presented, to analyze the characteristics of the internal airflow, so as to help optimize the design. Experiments are intended to verify the results of numerical simulation and explore the internal flow field of the cyclone separator further. The cyclone separator has 8 rotary blades which are split into 8 parts, namely one blade is 45° in the tangential direction. 0° and 22.5° are chosen in the experiment. The dimensionless pressure distribution is shown. A comparison of the CFD results and the experimental results is made to prove that the numerical simulation methods are correct and accurate. The curve of the numerical simulation results is very close to that of the experimental results with the similar trend. It is concluded that the methods can predict the internal flow field characteristics of the axial flow cyclone separator.


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