Selecting the optimum pressure drop per unit length of district heating piping network based on operating strategies

2016 ◽  
Vol 177 ◽  
pp. 341-353 ◽  
Author(s):  
Pengfei Jie ◽  
Xiangfei Kong ◽  
Xian Rong ◽  
Shangqun Xie
Energy ◽  
2020 ◽  
Vol 202 ◽  
pp. 117681
Author(s):  
Pengfei Jie ◽  
Wanyue Zhao ◽  
Fating Li ◽  
Fengjun Wei ◽  
Jing Li

Author(s):  
Y. Haseli

Optimum pressure ratios of a regenerative gas turbine (RGT) power plant with and without a solid oxide fuel cell are investigated. It is shown that assuming a constant specific heat ratio throughout the RGT plant, explicit expressions can be derived for the optimum pressure ratios leading to maximum thermal efficiency and maximum net work output. It would be analytically complicated to apply the same method for the hybrid system due to the dependence of electrochemical parameters such as cell voltage on thermodynamic parameters like pressure and temperature. So, the thermodynamic optimization of this system is numerically studied using models of RGT plant and solid oxide fuel cell. Irreversibilities in terms of component efficiencies and total pressure drop within each configuration are taken into account. The main results for the RGT plant include maximization of the work output at the expenses of 2–4% lower thermal efficiency and higher capital costs of turbo-compressor compared to a design based on maximum thermal efficiency. On the other hand, the hybrid system is studied for a turbine inlet temperature (TIT) of 1 250–1 450 K and 10–20% total pressure drop in the system. The maximum thermal efficiency is found to be at a pressure ratio of 3–4, which is consistent with past studies. A higher TIT leads to a higher pressure ratio; however, no significant effect of pressure drop on the optimum pressure ratio is observed. The maximum work output of the hybrid system may take place at a pressure ratio at which the compressor outlet temperature is equal to the turbine downstream temperature. The work output increases with increasing the pressure ratio up to a point after which it starts to vary slightly. The pressure ratio at this point is suggested to be the optimal because the work output is very close to its maximum and the thermal efficiency is as high as a littler less than 60%.


2019 ◽  
Vol 15 (1) ◽  
Author(s):  
M. Vivekanandan ◽  
N. Anantharaman ◽  
M. Premalatha

Abstract In a circulating fluidized bed (CFB), the loop seal is an important component which recirculates the solids captured by the cyclone to the bottom of the riser and avoids the direct flow of gas from high-pressure riser to the low-pressure cyclone. Most of the CFBC systems employ a Non-Mechanical valve, and its function has been investigated by many researchers. In this work, the flow of solid particle within the loop seal has been studied elaborately, and various design and operating parameters of the loop seal were analyzed in detail using Computational Fluid Dynamics (CFD). The CFD study has handled a loop-seal of dimension 110 mm × 430 mm × 400 mm high. This analysis has been done with a 200 µm sand particle and it is checked for its flow ability through various sizes and by altering the L/H ratio for three solid mass fluxes and for three L/H ratios of loop seal. The rate of solid mass flux depends on the length of the horizontal passage connecting the recycle cycle compartment of the loop seal with the supply chamber and hence the solid flow rate and the pressure difference per unit length are directly proportional to the length of the chamber or passage. Hence, L/H ratio is taken as a driving variable for the optimum performance of loop seal. The CFD analysis results reveal that the aeration of the solid to be used within the loop-seal should be higher than the Minimum Fluidization velocity. Also, keeping the length of the horizontal passage constant and varying the height of the passage will reduce the pressure drop. The pressure drop across the horizontal passage decreases up to a certain L/H ratio after which it increases. By comparing the three L/H ratios, L/H ratio of 2.62 is having a lesser pressure drop for the three mass fluxes. L/H ratio of 2.62 is having a good fluidization phenomenon and also the flow from the recycle chamber is more in comparison to the other L/H ratios. Experimental data from the literature is in good agreement with the CFD results.


1985 ◽  
Vol 25 (02) ◽  
pp. 176-190 ◽  
Author(s):  
G.J. Hirasaki ◽  
J.B. Lawson

Abstract The apparent viscosity of foam flowing through smooth capillaries was measured experimentally, and a mathematical model was developed. Foam texture (a measure of bubble volume) is a key parameter in determining the following properties of foam flowing through a capillary:whether the foam exists as bulk foam or as a chain of bubbles where each pair of bubbles is separated by an individual lamella,the number of lamellae per unit length of the capillary, andthe radius of curvature of the gas-liquid interface. The apparent viscosity is the sum of three contributions:that from slugs of liquid between bubbles,the resistance to deformation of the interface of a bubble passing through a capillary, andthe surface tension gradient that results when surface active material is swept from the front of a bubble and accumulates at the back of it. The sensitivity of both measured and calculated apparent viscosity is presented as a function of bubble size, capillary radius, ratio of bubble radius to capillary radius, velocity, quality, and surface tension gradient. Introduction An early conceptual model for the relative permeability of two-phase flow was the bundle of capillary tubes model. In this model, the wetting phase flowed in the smaller capillaries and the nonwetting phase flowed in the larger capillaries. The relationship between the flow rate and pressure drop in a capillary was described by the pressure drop in a capillary was described by the Hagen-Poiseuille law. The flow of a discontinuous nonwetting phase, such as a foam, cannot be described by the Hagen-Poiseuille law. The purpose of this investigation was to determine the relationship between flow rate and pressure drop for the flow of foam through a capillary. This relationship is described by an apparent viscosity that is required to modify the Hagen-Poiseuille law for the flow of foam. Our previous observations of flow of foam lamellae in transparent porous models showed that lamellae move from pore to pore by translation. Breaking and re-forming of lamellae were rare; so was bubble coalescence. These observations suggest that the apparent viscosity of foam or lamellae in uniform, smooth capillaries is related to and, indeed, is one component of the mobility of foam in porous media. A reasonable conceptual model of a natural porous medium is a bundle of interconnected capillaries of different sizes and containing constrictions. All capillary sections, or pores, near to one another have the same capillary pressure. Thus, phase saturations may differ from pore to pore, but the radii of curvature of the gas/ liquid interfaces are equal. When flow in such an array of capillaries is modeled, resistance to flow in parallel channels of both the same and different sizes is conceived to be in parallel. Flow in smooth, uniform pore sections is in series with flow through constrictions. The component of resistance owing to smooth, uniform pore sections is approximated by resistance to flow in smooth, uniform capillaries. Measurements and theory presented here show that the most important variable affecting foam viscosity in uniform, smooth capillaries is foam texture (bubble size). Foam of finer texture has more lamellae per unit length and, as a result, greater resistance to flow. This is true both for flow of bulk foam and series of lamellae. The principal factors affecting apparent viscosity of foam in uniform capillaries are dynamic changes at gas/liquid interfaces. These are illustrated in Fig. 1.Slugs of liquid between gas bubbles resist flow.Viscous and capillary forces result in interfaces that are deformed against the restoring force of surface tension. The extent of this deformation and the resulting bubble shape partially determine apparent viscosity as a function of flow rate.Another factor determining apparent viscosity as a function of velocity is expansion of the interface at the leading end of a bubble, accompanied by compression at the trailing end. This sweeping action causes surface active material to be depleted at the front and to accumulate at the back of the bubble. The result is a surface tension gradient that resists flow. Scaling of Foam Texture and Capillary Radius Since foam texture is a measure of the average volume or equivalent radius of its bubbles, one would expect that an important scale factor is the ratio of this equivalent radius to the equivalent radius of a porous medium or the radius of a capillary. This ratio can be expressed either as the wetted perimeter per unit area of the solid or as the number of lamellae per unit length of capillary. These quantities are denoted as nL and are referred to as the number of equivalent lamellae per unit length. This concept is illustrated in Fig. 2. SPEJ P. 176


2014 ◽  
Vol 953-954 ◽  
pp. 871-875
Author(s):  
Hong Bo Ren ◽  
Qiong Wu ◽  
Jian Yang ◽  
Yin Yin Ban

In this paper, a distributed energy resource (DER) system plan and evaluation model is extended to include the design of district heating network. In the model, production and consumption of electric power and heat, power transmissions, transport of fuels to the production plants, transport of water in the district heating pipelines and storage of heat are taken into account. The problem is formulated as a mixed integer linear programming (MILP) model where the objective is to minimize the overall cost of the DER system. The solution gives the DER structure, i.e., which production units, heat transport lines and storages should be built as well as their locations, together with design parameters for plants and pipelines.


2018 ◽  
Vol 40 (2) ◽  
pp. 237-255 ◽  
Author(s):  
Oliver Martin-Du Pan ◽  
Paul Woods ◽  
Richard Hanson-Graville

Reducing heat losses is an important factor in improving the performance of district heating networks. High heat losses are sometimes experienced in UK district heating networks and this is often as a result of poor design, partly due to oversized pipes. To provide additional guidance to designers on this issue, this paper proposes a set of maximum pipe diameters to be used for a given maximum flow rate to reduce the risk of oversizing and high heat losses. It was found that the optimised velocities are higher than those given in CIBSE CP1 Heat Networks Code of Practice and adopting these will result in smaller pipe diameters and lower operational and capital costs. The methodology used in this paper is based on minimising the total operational energy. The flow and return optimised pipe diameters are calculated for different scenarios which include variations in the pipe material, insulation thickness, water temperature and ambient environment. It was found that the optimised velocity in every scenario remains relatively constant with a varying pipe diameter. This paper shows that the operational cost of a DH network can be reduced when selecting the recommended maximum pipe diameter, compared to commonly used sizing criteria. Further savings can be achieved if the flow and return pipe are sized separately; to minimise operational energy of both flow and return pipes, the return pipe should be sized for a lower velocity. This paper also explores particular questions of interest: A range of insulation thicknesses. Benefit from using a variable flow temperature and to supply the flow at 90℃ at peak times instead of a constant temperature at 70℃. A comparison between steel and plastic pipes which have different roughness coefficients. Optimised differential pressure drop per unit length in both flow and return pipes. Maximum distance occurring before measuring a temperature loss and pressure drop of 1℃ and 1 bar, respectively, at peak load. However, this paper does not take into account any potential benefits that a lower flow temperature might have in reducing heat production costs or a lower return temperature might have in enhanced heat recovery, or that lower temperatures may enable use of plastic carrier pipes. Such matters are site specific but should be included in any similar pipe sizing analysis and operating temperature optimisation carried out for an actual scheme. Practical application: Optimising maximum pipe diameters is necessary to improve the viability of district heating systems. The current guidance for designers is not considered optimal and this paper suggests a new methodology to size pipes to reduce both the heat losses and the operational cost. This paper also gives guidance to sustainability engineers to assess the performance of 90/40℃, 70/40℃ and 60/30℃ district heating networks; 70℃ was assumed to be the minimum acceptable flow temperature in the network to enable domestic hot water to be heated to a safe temperature of 60℃ for storage; 40℃ was the used return temperature to be in line with the CIBSE Code of Practice CP1 stating in Objective 3.5 that best practice should achieve return temperatures below 40℃ for a scheme supplying heat to new buildings. A 90/40℃ DH network performance when increasing the flow temperature was then compared to the performance of a 70/40℃ system. Finally, a 60/30℃ system was also analysed to investigate the benefit from operating a DH network complying with the 4th generation of DH network temperatures that encourages minimal exergy destruction from the network to the end user.


Author(s):  
Jaime Moreu ◽  
Ricardo García-Morato ◽  
Jesús Valle ◽  
Santiago de Guzmán ◽  
Miriam Terceño

Kinetic turbines harnessing tidal and ocean currents make use, in some designs, of nozzles and/or diffusers. Nozzles come at a cost, but they can help from the structural, hydrodynamic or positioning points of view. In those cases, they might make sense as long as they drive the LCoE (Levelized Cost of Energy) down, which is the ultimate objective of energy-harnessing devices. The design must then optimize the combined performance of both blades and nozzle. However, the interaction between turbine blades and nozzle is not always fully clear, and even less its optimization. A relevant amount of efficiency can be lost if the design spiral is not appropriate. The authors have suggested in [1] an approach for the optimization of turbines within nozzles. This approach was followed in [2] and validated with model tests. In the approach, the turbine is initially substituted by an actuator disc that applies a radially constant pressure drop. But in these references, the optimum pressure drop in the actuator disc was the same as if there was no nozzle at all, i.e., 4/9ρv2. This is equivalent to considering the nozzle coefficient does not depend on the pressure drop, and thus, on the induced velocity field. Hence it is a somewhat arbitrary assumption. This paper describes, using actuator disc theory, how nozzles affect the disc optimum pressure drop in uniform flow conditions. The effect of a hub is also analyzed. Then, using a viscous FVM CFD code, the variation of the pressure drop is quantified for two different acceleration nozzles, one suffering flow separation and the other one not. As the pressure drop increases, so does the flow expansion downstream. This rises the average radial component of velocity at the nozzle, increasing the thrust and nozzle coefficient. Therefore the optimum pressure drop goes up compared to that without nozzle. The increment in efficiency that can be obtained with this approach is quantified for the studied nozzles. Finally, the integration of this effect into the blade design is discussed.


Clean Energy ◽  
2020 ◽  
Vol 4 (2) ◽  
pp. 142-157 ◽  
Author(s):  
Hossein Piri ◽  
Xiaotao T Bi ◽  
Hui Li ◽  
Haijiang Wang

Abstract In the last decade, many researchers have focused on developing fuel-cell flow-field designs that homogeneously distribute reactants with an optimum pressure drop. Most of the previous studies are numerical simulations and the few experimental studies conducted have used very simple flow-field geometries due to the limitations of the conventional fabrication techniques. 3D printing is an excellent rapid prototyping method for prototyping bipolar plates (BPPs) to perform experiments on new flow-field designs. The present research investigates the applicability of different 3D-printed BPPs for studying fluid-dynamic behaviour. State-of-the-art flow-field designs are fabricated using PolyJet 3D printing, stereolithographic apparatus (SLA) 3D printing and laser-cutter technologies, and the pressure-drop and velocity profiles are measured for each plate. The results demonstrate that SLA BPPs have great promise in serving as a screening tool in modifying flow-field design with a small feature size.


2021 ◽  
Vol 1192 (1) ◽  
pp. 012008
Author(s):  
F Abd Lahin ◽  
R Sarbatly ◽  
C Chel-Ken

Abstract A simple, small scale upflow sand filter was fabricated using a locally obtained sands at three different rivers in Sabah, Malaysia: Liwagu River (SL), Tamparuli River (ST), and Kaingaran River (SK). The grain size, porosity, bulk density, particle density and sphericity of the sands were characterized to associate with the corresponding pressure drop across the sand bed. The highest pressure drop per unit length for SK, PT, and SL are 15.85 kPa m-1 at 0.747 m s-1 vs, 10.18 kPa m-1 at 0.352 m s-1 vs, and 9.24 kPa m-1 at 0.747 m s-1 vs, respectively. The pressure drop per unit length at different filter bed depth were plotted, and compared against three theoretical models of Ergun, Kozeny-Carman, and Fair and Hatch. By analyzing the experimental-theoretical comparison using RMSE and Chi-Test, prediction of pressure drop in an upflow sand filter is able to be predicted using the Kozeny-Carman equation preceding filter bed fluidization and subsequently Fair and Hatch’s equation after bed is fluidized.


Sign in / Sign up

Export Citation Format

Share Document