Research Article  Open Access
Improvement of the Efficiency of the AxialFlow Pump at Part Loads due to Installing Outlet Guide Vanes Mechanism
Abstract
In order to investigate the influence of adjustable outlet guide vane on the hydraulic performance of axialflow pump at part loads, the axialflow pump with 7 different outlet guide vane adjustable angles was simulated based on the RNG turbulent model and Reynolds timeaveraged equations. The Vector graphs of airfoil flow were analyzed in the different operating conditions for different adjustable angles of guide vane. BPANN prediction model was established about the effect of adjustable outlet guide vane on the hydraulic performance of axialflow pump based on the numerical results. The effectiveness of prediction model was verified by theoretical analysis and numerical simulation. The results show that, with the adjustable angle of guide vane increasing along clockwise, the high efficiency area moves to the large flow rate direction; otherwise, that moves to the small flow rate direction. The internal flow field of guide vane is improved by adjusting angle, and the flow separation of tail and guide vane inlet ledge are decreased or eliminated, so that the hydraulic efficiency of pumping system will be improved. The prediction accuracy of BPANN model is 1%, which can meet the requirement of practical engineering.
1. Introduction
With the increasing application of an axialflow pump, the improvement of its efficiency continues to become more and more important. One of the most useful methods to increase its efficiency is the installation of a guide vane behind the pump impeller [1]. Out guide vane (OGV) can improve the head and the efficiency of the pump by transforming the kinetic energy of the rotating flow, which has a tangential velocity component, into pressure energy. When the axialflow pump is working under offdesign condition, the attack angle, which causes hydraulic loss, will always exist at the leading edge of the guide vane. This is because the traditional guide vane is fixed on the guide vane hub with a fixed angle for the design condition and cannot be adjustable with the change in working conditions. The literature on OGV investigations for aircraft engine mainly falls into the following categories: effects of OGV on aircraft engine’s noise [2–4], unsteady interaction between the stationary OGVs and the rotor [5], and flow characteristics of OGVs [6–9]. The flow in a compressor OGV blade row downstream of a singlestate rotor was carried out by Carrotte et al. [10]. Many researchers studied the internal flow characteristics of OGV based on the whole passage of pump [11–14]. Compared with aircraft engine and compressor, the usage of adjustable OGVs is extremely rare for axialflow pump. The paper investigates the influence of OGVs setting angles on the hydraulic performance of axialflow pump by CFD. The internal flow of OGVs is analyzed in different setting angles. The BPANN prediction model will be built about the influence of OGVs setting angles on the pump performance based on the resulting data.
2. Numerical Calculations
2.1. Numerical Model and Calculation Method
The numerical model and method for simulating the flow field in the axialflow pump can be found in previous work by Yang and Liu [15] and Jafarzadeh et al. [16]. The governing equations for the turbulent incompressible flow encountered in this research are the steadystate RANS equations for the conservation of mass and momentum, given aswhere is the averaged pressure, is the molecular viscosity, and is the Reynolds stress. To correctly account for turbulence, the Reynolds stresses are modeled in order to achieve the closure of (2). The modeling is based on the Boussinesq hypothesis to relate the Reynolds stresses to the mean velocity gradients within the flow. The Reynolds stresses are given bywhere is the turbulent viscosity and is the turbulent kinetic energy.
The renormalization group (RNG) turbulent model is widely applied in turbo machines, which is suitable for simulating the complex flow in rotating and high curvature computational domain. A more comprehensive description of RNG theory and its applications to turbulence computation can be found in [17].
The turbulence kinetic energy and its rate dissipation are obtained from the following transport equations:
The production term in (4) is given bywhere is the modulus of the mean rateofstrain tensor, defined by
The effective viscosity is calculated by
with , , , and
In the present calculation work, the commercial CFD code ANSYS CFX14.0 is employed. ANSYS CFX uses the element based finite volume method and an algebraic multigrid approach. The equations solved in the calculation are the NavierStokes equations coupled with the RNG turbulence model. A uniform axial velocity based on the massflow rate is specified at the inlet for each computation run, and the static pressure at the outlet is set to 1.2 atm. The turbulence intensity at the inlet totally depends on the upstream history of flow. Since the fluid in the suction tank is undisturbed, the turbulence intensity for all conditions is considered 1%. Scalable wall functions are used to simulate the boundary layers. Adiabatic and hydraulically smooth walls with no slip condition were considered at solid boundaries. Periodic boundaries are set at the blade passage interfaces. Water was used as a working fluid in ambient condition.
2.2. Computational Domain and Mesh
Figure 1 shows 3D geometry of axialflow pump model, with the specific speed of 1200 and impeller diameter of 300 mm, which is used to simulate and measure its entire flow field. The specific speed is defined below:
The impeller has 3 blades and the outlet guide vane has 5 blades. The rotating speed is 1450 r/min. The average tip clearance of impeller is 0.2 mm at blade angle , which are the same as those of the experimental model. The computational domain is the flow passage from the inlet to outlet, including the inlet passage, outlet passage, impeller, and guide vane.
The grid quality in the impeller and guide vane will affect the accuracy of axialflow pump simulation. Accordingly, H/J/Ltype topology structure is applied to the impeller, and Htype topology structure is applied to the outlet guide vane. Otype grid is used at the blade surface region to control boundary layer distribution. Prior to step for analysis of axialflow pump, in order to determine the optimal number of grids, a preliminary grid dependency test with numbers of nodes ranging from 500000 to 1600000 is carried out. The computations have shown that grid convergence has been obtained for the performance of the axialflow pump at , as shown in Figure 2. With the increase of grid numbers, the head coefficient and efficiency change greatly at first and then change very little gradually. Finally, the appropriate grid number for the simulation was determined by the preliminary simulation results. In the present study, grid number 1272707 was selected for the final simulation.
The nondimensional head and power coefficients are defined as follows.
Head coefficient is as follows:where is head coefficient, is the head of the axialflow pump, is rotation speed, and is the impeller diameter.
Flow coefficient is as follows:where the efficiency of the pump is defined as follows:where is volume flow rate and is the measured torque.
3. Performance Prediction Results and Experimental Validation
3.1. Test Device and Method
Physical model of axialflow pump was tested in the Hydrodynamic Engineering Laboratory of Jiangsu Province. Figure 3 shows the rig for the experimental measurements. The test apparatus consists of three sections: ① water supply section: the inlet water tank, the outlet water tank, the surge water tank, mixedflow pump, and regulating value; ② outlet section: pressure gauge, electromagnetic flowmeter, and regulating value; and ③ pump section: axialflow pump, composite torque detector, and motor. Axialflow pump head is measured by differential pressure transmitter EJA110A with ±0.113%, and measuring sections are closed in the tanks with the inlet and outlet passages for concluding hydraulic loss of inlet and outlet sections. Torque is measured by TS3100B digital torque and speed sensor with ±0.0203%, which is transmitted by pump shaft. Flow rate is measured by Emag DN400 electromagnetic flowmeter with ±0.197%.
3.2. Results Comparison
According to test data, the highest efficiency of axialflow pump is 80.39% at blade angle , with flow rate coefficient of 0.511 and head coefficient of 0.604. The prediction data agree with the experimental head and efficiency, as shown in Figure 4. There is a good quantitative agreement at the flow rate coefficient of 0.36~0.60, with the maximum relative errors smaller than 4.0%, which demonstrates that numerical calculations simulate the pump performance accurately.
4. Results and Discussion
4.1. Influence of OGV on the Hydraulic Performance of AxialFlow Pump
The hydraulic performances of axialflow pump with seven different OGV setting angles were predicted. The OGV setting angle is in the range of −10°~+10°. The 3D models of OGV with three different setting angles are shown in Figure 5.
The hydraulic performances of axialflow pump with seven different OGV setting angles were predicted. The OGV setting angle is in the range of −10°~+10°. Figure 6 shows the numerical results of pump head coefficient and efficiency for different flow rates. The change law of pump efficiency, head coefficient , and OGV setting angle is not the same in the same flow rate coefficient . The OGV setting angle has great influence on the inner flow pattern of OGV and hydraulic performance of pump, and the rotorstator interaction is complex. The OGV setting angle has great influence on the hydraulic performance of outlet passage. When the OGVs are regulated to the positive angle, the hydraulic performance will be improved in the large flow rate condition. When the OGVs are regulated to the negative angle, the hydraulic performance will be improved in the small flow rate condition. If the OGVs are regulated to the positive angle, the high efficiency area will be closed to the large flow rate condition; otherwise, the high efficiency area will be closed to the small flow rate condition. In order to eliminate the inlet incidence angle and tail flow separation of blade, the OGV setting angle should be regulated according to axialflow pump operating conditions.
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4.2. Internal Flow Pattern of AxialFlow Pump
The flow patterns in the OGV channel at low flow rate condition (), high efficiency flow rate condition (), and large flow rate condition () are shown in Figures 7–9. These figures show the flow patterns of OGV channel in different OGV setting angles.
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In the low flow rate condition (), the vortices appeared in the OGV suction surface from the 1/4 length of inlet edge, the backflow is in the inlet edge of blade, but the flow pattern of trailing edge is good for OGV. The hydraulic loss increases because of vortices appearing, and it is 21.41% of the pump head in . With the increase of OGV setting angles to positive, the hydraulic loss increases gradually. Compared with the OGV setting angle , the hydraulic loss increases by 38.66% and the hydraulic efficiency dropped by 3.93% in the OGV setting angle . From Figure 7, flow separation occurs in the trailing edge of OGV blade, and it influences the flow field of the inlet region of OGV blade. The hydraulic loss increases because the flow hits the pressure surface of OGV blades. With the increase of OGV setting angles to negative, the hydraulic loss decreases firstly and then increases. Compared with the OGV setting angle , the hydraulic loss decreases by 6.41% and the hydraulic efficiency improves by 0.74%. With the increase of OGV setting angles to negative from , the area of vortex region increases gradually in the OGV suction surface, and the hydraulic loss increases and the hydraulic efficiency decreases gradually. The vortex region accounts approximately for 33.3% of the OGV suction surface area at OGV setting angle .
In the high efficiency flow rate condition (), the vortices appeared in the OGV suction surface from the 1/2 length of inlet edge, and the hydraulic loss of OGV accounts for 8.22% of axialflow pump head. Compared with the OGV setting angle , the hydraulic loss of OGV increases approximately by 55%, the hydraulic efficiency of pump decreases approximately by 1% at and , and the hydraulic loss of OGV increases by 118.55%, and the hydraulic efficiency of pump decreases by 4.86% at . The vortex region is in the middle of OGV suction surface at and , and the vortex region extends to the inlet region of OGV blade at from Figure 8. With the increase of OGV setting angle to negative, the hydraulic loss decreases firstly and then increases. Compared with the OGV setting angle , the hydraulic loss decreases by 14.55% and the hydraulic efficiency improved by 1.59% at . With the increase of OGV setting angle to negative from , the hydraulic loss increases and the hydraulic efficiency decreases gradually. The vortex is in the trailing edge of OGV blade suction surface at . The hydraulic loss increases because flow separation is in the trailing edge of OGV blade.
In the large flow rate condition (), with the increase of OGV setting angles to negative, the vortex region increases gradually in the OGV pressure surface. The hydraulic loss of OGV increases gradually. Compared with the OGV setting angle , the hydraulic loss increases by 297%, and the hydraulic efficiency of pump decreases by 17.87%. From Figure 9, the vortex region is in the OGV pressure surface from the 1/4 and the 3/4 length of inlet edge. The vortex causes the hydraulic efficiency to drop significantly. There are no vortex and flow separation around the airfoil of OGV blades at the OGV setting angles , , and . The flow separation is in the trailing edge of OGV blade, so the hydraulic loss increases at . The coupling effects of impeller, OGV, and outlet passage are considered in the numerical simulation of axialflow pump. Compared with the OGV setting angle , the hydraulic loss decreases by 14.65%, and the hydraulic efficiency of pump improved by 5.29% at the OGV setting angle .
4.3. Artificial Neural Networks
In this paper, a computational tool, known as back propagation artificial neural networks (BPANN), is used to predict the hydraulic performance of axialflow pump with OGVs. The network usually consists of input layer, hidden layer, and output layer. A schematic diagram of the typical threelayer feedforward neural network architecture is shown in Figure 10. The prediction mathematical model is constructed based on the modified BPANN. The modified BPANN consists of two layers of back propagation network structure. The hyperbolic tangent Stype function tansig( ) is used in the input layer and hidden layer. The pure linear function purelin( ) is used in the output layer. The neurons numbers of input layer are assumed as the samples index . The repeated training of node number was carried out in the hidden layer [18], and the node numbers are assumed as . The neurons numbers of output layer are assumed as , so the network structure model is . The BP elastic algorithm trainrp( ) was adopted for training function, and it can be used in the bulk mode training. It has fast convergence speed and calculation with small storage space. The topology structure of BPANN network is shown in Figure 10.
The impeller torque , the pump flow rate coefficient , the pump head coefficient , and the OGVs setting angle are assumed as input variables, the neurons number of input layer is 4 and the neurons number of output layer is 1 for BPANN network. The neurons number of hidden layer is calculated bywhere . The neurons number of hidden layer is 1 by using the comparative method and cutandtry method. The network structure model is .
The seven groups of OGVs setting angles were used to train and test the BPANN prediction model, and each group includes seven pump operating conditions and 49 groups of pump performance data. The 49 groups were divided into two parts: one part was used as training samples, and the other part was used to exam the BPANN prediction model. In order to ensure the learning precision of BPANN prediction model, more training samples were needed, 42 groups were chosen randomly, and the rest of data were used to test the prediction model. Normalization processing was carried out for samples firstly, and then the prediction model was trained. Function premnmx( ) was used to recode the normalization processing of input value and output value in Matlab software, so that training samples were in the range of −1 to 1.
The function newff( ) was used to construct the BPANN prediction model by using the commercial mathematical software Matrix & Laboratory; it can be expressed by where net is mesh object of BPANN, is the number of input groups, is the number of output groups, is unit number of hidden layers, is the transfer function of each layer, is the training function of BPANN, BLF is learning function of weight, is objective performance function, is row unit array of input proceeding function, is row unit array of output proceeding function, and is data decomposition function.
The prediction model was trained by using 42 groups of pump performances data. The trained prediction model has a good stability and satisfies the precision demands for prediction assessment. The error curve is shown in Figure 11.
In order to validate the effectiveness of prediction model, numerical results of 7 operating conditions were assumed as testing sample at the OGVs setting angle . The comparison of predicted results and simulated results is shown in Table 1. The maximum deviation is 0.98%, the minimum deviation is 0.03%, and the average deviation is 0.35%. The prediction accuracy of BPANN model is below 1%, which can meet the requirement of practical engineering.

The pump performance is predicted by using BPANN model, which needs to give 4 parameters, including setting angle, flow rate coefficient, torque, and head coefficient. The functional relation surface of flow rate coefficient , head coefficient , and the OGVs setting angles with a determination coefficient of 0.997, and the functional relation surface of flow rate coefficient , the OGVs setting angles , and torque with a determination coefficient of 0.998 are shown in Figure 12 by using binary nonlinear regression analysis method.
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The suitable OGVs setting angle can be predicted firstly according to flow rate coefficient and head coefficient based on the fitting surface of binary nonlinear function about ; then, the torque can be predicted according to flow rate coefficient and OGVs setting angle based on the fitting surface of binary nonlinear function about , and the pump hydraulic efficiency can be predicted by using BPANN model according to different OGVs setting angles.
As shown in Figure 13, if the guide vane inlet attack angle , the OGVs suitable angle will be calculated bywhere is the crowding coefficient at the entrance of OGVs, is the axial velocity at the entrance of OGVs, is the circumferential component of absolute velocity at the entrance of OGVs, and is the circulation thickness of blade at the OGVs inlet.
The OGVs suitable angles are intended to maintain the shock free flow pattern. The schematic diagram of OGV is shown in Figure 13. The basic idea of the OGV is that the guide vane inlet flow angle should be adjusted according to the impeller outlet flow angle to reduce hydraulic loss. The impeller outlet flow angle can be derived from the velocity triangle when the blade angle and flow rate are known, as shown in Figure 13. According to theorem of moment of momentum about impeller outlet flow and guide vane inlet flow , if the radius of OGV calculation flow surface is relative to impeller calculation flow surface, will be equal to . The formula of can be derived from the velocity triangle and discharge as follows [19]:where is the radius of pump case at the impeller outlet, is the radius of hub at the impeller outlet, and is the impeller rotation speed.
If the hydraulic loss is minimum, the OGVs suitable angle will be equal to and . The OGVs suitable angle can be written as follows:where is the blade thickness at the impeller inlet.
The OGVs setting angle is calculated by where is the OGVs suitable angle and is OGVs fixed angle.
The OGVs setting angle can be calculated based on the flow rate coefficient and head coefficient ; then, the torque is calculated based on the OGVs setting angle and the flow rate coefficient . The three operating conditions (, 0.552, and 0.664) were chosen for verifying the BPANN model. The calculation results are shown in Table 2 based on the OGV fixed angle formula given in [19] and binary nonlinear function.

The predicted efficiency is closer to calculated efficiency by CFD at the OGV setting angle , and the absolute deviation is less than 1%. The difference is because the rotorstator interaction is not considered in the OGV setting angle formulae (17)–(19).
In order to verify the feasibility of predication method, the internal flow of axialflow pump was simulated by ANSYS CFX at for the OGV setting angle . The Vector graph of airfoil flow of OGV is shown in Figure 14. There are no vortex and flow separation around the airfoil. The pump efficiency is 81.12% based on the simulated results; the difference value is 0.41%, compared with predicted results in Table 2. The pump efficiency , and the OGV setting angle in the flow rate coefficient .
5. Conclusion
Simulations of the threedimensional steady flow in an axialflow pump with OGV were conducted using the commercial CFD software ANSYS CFX, and the BPANN prediction model was established firstly about the effect of adjustable outlet guide vane on the hydraulic performance of axialflow pump. The results show the following:(1)The mathematical model used in this paper can accurately simulate the flow field inside the axialflow pump. The computational curves agree well with the experimental ones.(2)The internal flow field of guide vane is improved by adjusting angle, and the flow separation of tail and guide vane inlet ledge are decreased or eliminated, so that the hydraulic efficiency of pumping system will be improved.(3)The adjustable outlet guide vane can significantly improve the head and efficiency of the pump at offdesign conditions. If the OGVs are regulated to the positive angle, the high efficiency area will be closed to the large flow rate condition; otherwise, the high efficiency area will be closed to the small flow rate condition.(4)BPANN prediction model is established firstly about the effect of adjustable outlet guide vane on the hydraulic performance of axialflow pump. The prediction accuracy of BPANN model is 1%, which can meet the requirement of practical engineering.
Conflict of Interests
The authors declare that there is no conflict of interests regarding the publication of this paper.
Acknowledgments
This work was supported by the National Natural Science Foundation of China (Grant no. 51376155), the Natural Science Foundation of Jiangsu Province (Grant no. BK20150457), the Natural Science Foundation of Jiangsu Higher Education Institutions of China (Grant no. 14KJB570003), and the Priority Academic Program Development of Jiangsu Higher Education Institutions (PAPD).
References
 B. Nesbitt, Handbook of Pumps and Pumping, Elsevier Science & Technology Books, 2006.
 Y. D. Khaletskiy and Y. S. Pochkin, “Fan noise reduction of an aircraft engine by inclining the outlet guide vanes,” Acoustical Physics, vol. 61, no. 1, pp. 101–108, 2015. View at: Publisher Site  Google Scholar
 D. Giacché, L. Xu, and J.P. Coupland, “Optimization of bypass outlet guide vane for low interaction noise,” AIAA Journal, vol. 52, no. 6, pp. 1145–1158, 2014. View at: Publisher Site  Google Scholar
 X. Sun, Z. Yang, and X. Wang, “Effect of fan outlet guide vane on the acoustic treatment design in aeroengine nacelle,” Journal of Sound and Vibration, vol. 302, no. 12, pp. 287–312, 2007. View at: Publisher Site  Google Scholar
 A. R. Wadia, P. N. Szucs, and K. L. GundyBurlet, “Design and testing of swept and leaned outlet guide vanes to reduce statorstrutsplitter aerodynamic flow interactions,” Journal of Turbomachinery, vol. 121, no. 3, pp. 416–427, 1999. View at: Publisher Site  Google Scholar
 J. Li, G. Page, and J. McGuirk, “Coupled reynoldsaveraged navierstokes/largeeddy simulation for outlet guide vane and prediffuser flows,” AIAA Journal, vol. 53, no. 3, pp. 678–691, 2015. View at: Publisher Site  Google Scholar
 C. A'Barrow, J. F. Carrotte, A. D. Walker, and A. M. Rolt, “Aerodynamic performance of a coolant flow offtake downstream of an outlet guide vane,” Journal of Turbomachinery, vol. 135, no. 1, Article ID 011006, 2012. View at: Publisher Site  Google Scholar
 J. Hjärne, J. Larsson, V. Chernoray, and L. Löfdahl, “An experimental investigation of secondary flows and loss development downstream of a highly loaded low pressure turbine outlet guide vane cascade,” in Proceedings of the ASME Turbo Expo, pp. 681–690, Barcelona, Spain, May 2006. View at: Publisher Site  Google Scholar
 T. Sonoda and H.A. Schreiber, “Aerodynamic characteristics of supercritical outlet guide vanes at low Reynolds number conditions,” Journal of Turbomachinery, vol. 129, no. 4, pp. 694–704, 2007. View at: Publisher Site  Google Scholar
 J. F. Carrotte, K. F. Young, and S. J. Stevens, “Measurements of the flow field within a compressor outlet guide vane passage,” Journal of Turbomachinery, vol. 117, no. 1, pp. 29–37, 1995. View at: Publisher Site  Google Scholar
 F.P. Tang and G.Q. Wang, “Influence of outlet guide vanes upon performances of water jet axialflow pump,” Journal of Ship Mechanics, vol. 10, no. 6, pp. 19–26, 2006. View at: Google Scholar
 H. Zhu and R. Zhang, “Numerical analysis on the distribution features of velocity circulation of axialflow pump,” Revista Tecnica de la Facultad de Ingenieria Universidad del Zulia, vol. 37, no. 3, pp. 14–21, 2014. View at: Google Scholar
 D. Kaya, “Experimental study on regaining the tangential velocity energy of axial flow pump,” Energy Conversion and Management, vol. 44, no. 11, pp. 1817–1829, 2003. View at: Publisher Site  Google Scholar
 H. Zhang, W.D. Shi, B. Chen, Q.H. Zhang, and W.D. Cao, “Experimental study of flow field in interface area between impeller and guide vane of axial flow pump,” Journal of Hydrodynamics, vol. 26, no. 6, pp. 894–901, 2015. View at: Publisher Site  Google Scholar
 F. Yang and C. Liu, “Pressure pulsations of the blade region in Sshaped shaftextension tubular pumping system,” Mathematical Problems in Engineering, vol. 2014, Article ID 820135, 10 pages, 2014. View at: Publisher Site  Google Scholar
 B. Jafarzadeh, A. Hajari, M. M. Alishahi, and M. H. Akbari, “The flow simulation of a lowspecificspeed highspeed centrifugal pump,” Applied Mathematical Modelling, vol. 35, no. 1, pp. 242–249, 2011. View at: Publisher Site  Google Scholar  Zentralblatt MATH
 V. Yakhot and S. A. Orszag, “Renormalization group analysis of turbulence. I. Basic theory,” Journal of Scientific Computing, vol. 1, no. 1, pp. 3–51, 1986. View at: Publisher Site  Google Scholar
 S. Rajakarunakaran, P. Venkumar, D. Devaraj, and K. S. P. Rao, “Artificial neural network approach for fault detection in rotary system,” Applied Soft Computing Journal, vol. 8, no. 1, pp. 740–748, 2008. View at: Publisher Site  Google Scholar
 Z.D. Qian, Y. Wang, W.X. Huai, and Y. H. Lee, “Numerical simulation of water flow in an axial flow pump with adjustable guide vanes,” Journal of Mechanical Science and Technology, vol. 24, no. 4, pp. 971–976, 2010. View at: Publisher Site  Google Scholar
Copyright
Copyright © 2016 Fan Yang et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.