scholarly journals Efficiency calculation on 10 MW experimental steam turbine

2018 ◽  
Vol 168 ◽  
pp. 06001
Author(s):  
Michal Hoznedl

The paper deals with defining flow path efficiency of an experimental steam turbine by using measurement of flow, torque, pressures and temperatures. The configuration of the steam turbine flow path is briefly described. Measuring points and devices are defined. The paper indicates the advantages as well as disadvantages of flow path efficiency measurement using enthalpy and torque on the shaft. The efficiency evaluation by the help pressure and temperature measurement is influenced by flow parameter distribution and can provide different values of flow path efficiency. The efficiency determination by using of torque and mass flow measurement is more accurate and it is recommended for using. The disadvantage is relatively very complicated and expensive measuring system.

2018 ◽  
Vol 65 (3) ◽  
pp. 125-135 ◽  
Author(s):  
V. M. Neuimin

Author(s):  
Markus Mu¨ller ◽  
Thomas Streule ◽  
Siegfried Sumser ◽  
Gernot Hertweck ◽  
Arno Nolte ◽  
...  

Current turbocharged diesel engines use exhaust gas recirculation (EGR) to effectively meet emission standards. With exhaust gas recirculation it is possible to keep the nitrogen oxide (NOx) emissions to a minimum, largely by lowering the local peak temperatures in the combustion chamber. Exhaust gas transportation from the exhaust side to the air side can be realized in different ways. All have in common that, a drop of pressure from the exhaust to the air is needed. In this paper the high pressure exhaust gas recirculation concept will be discussed, where the exhaust gases are transported from the upstream side of the turbocharger turbine to the downstream side of the charge air cooler. In this concept a negative pressure difference between turbine inlet and engine intake is needed, leading to inefficient gas exchange and, in the end, increasing fuel consumption. In order to keep the overall fuel consumption increase as low as possible, some of the current 6-cylinder Mercedes-Benz truck engines, that have EGR, are equipped with the so-called asymmetric twin scroll turbine to provide the most efficient exhaust gas transportation. In this design concept the negative pressure difference between engine intake and turbine inlet is generated in just one of the two exhaust branches. Thus, whilst some cylinders are operated with a high exhaust gas backpressure, others are operated with a fuel-saving low exhaust gas back-pressure. The different back-pressures in the two exhaust branches are created by designing each flow path of the twin scroll turbine differently. The exhaust branch with the higher back-pressure needs a turbine scroll with a much smaller flow parameter than the exhaust branch with the lower back-pressure. As both flow paths are coupled to the same turbine wheel, the flow parameter is modified using the design parameters of the scrolls. This produces two totally different turbine concepts in one turbine housing. The turbine path with the higher flow parameter has a classical radial turbine reaction value of 0.5. This flow path can thus be optimized for maximum efficiency in comparison with other radial turbines. In contrast, the turbine path with the lower flow parameter combined with the turbine wheel is operated with a reaction value approaching zero. This flow path tends to need an axial turbine with a high flow direction change like an impulse turbine, even if a radial turbine wheel is used. Operating a radial turbine wheel under this boundary condition needs new development steps to improve the turbine with regard to mechanical feasibility and thermodynamic efficiency. This paper describes the principle mechanism of the asymmetric twin scroll turbine. Detailed engine cycle simulations give a brief introduction into the main advantages of asymmetric turbines in combination with exhaust gas recirculation. Hot gas test stand studies show the principle characteristics of this turbine type and the numerical flow simulations give a detailed insight into the flow phenomena in the turbine. The key design values will be discussed and the future outlook indicates the next development steps that will be required.


Author(s):  
Michal Hoznedl ◽  
Ladislav Tajč ◽  
Lukáš Bednář ◽  
Aleš Macálka ◽  
Antonín Živný

Abstract The paper deals with experimental research of water and steam flow through the grooves in hollow stator blades of the steam turbine last stages with the support of CFD calculations. Also the amount of water sucked by the circumferential groove in the upper limiting wall between the last stage rotor and stator blade was experimentally measured. Measuring took place on a steam turbine with nominal output 1000 MW. With gradual increase of the turbine output it was possible to measure parameters of hollow blades suction for outputs 205, 460, 730, 870 and also 1006 MW. Before starting turbine a complex measuring system was installed consisting of cyclone separator, set of measuring tanks, orifice and pressure sensors and transducers. This measuring system was connected to one hollow stator blade near the horizontal joint. After the measurement the extraction of steam water mixture from this blade was transferred to the condenser via the diffuser chamber in the same way as other non-measured blades. Based on measured data, i.e. the pressure in the hollow stator blade and the flow rate of water captured by the hollow stator blade, it is possible to define the efficiency of suction tract from the viewpoint of total wetness in the inter-stage channel and from the viewpoint of rough liquid phase. The rough liquid phase means water films that flow near the draining grooves and sucked inside to the grooves. The main part of the submitted paper is an analysis of the measured data. Among the analysis results are, besides the flows of rough water phase along the blade surface, the above mentioned efficiency of total wetness suction and of water film suction. For the needs of the analysis there are certain input data, e.g. the value of static pressure and wetness on the blade surface close to the slots that must be defined theoretically using flow path calculations or using CFD methods. In this case, in order to obtain input data, CFD simulations were used when the whole last stage was calculated with the diffuser and exhaust hood. Boundary conditions for CFD were taken from experimental measurements that took place simultaneously with measurement of separated water phase. Numerical simulations were not running for all outputs, but only for three of them — 460, 730 and 1006 MW. For this reason there are no sufficient data for CFD calculations for all outputs and input data of other cases had to be extracted and, based on experience, extrapolated. On the circumferential groove only a part of 30 mm of length was measured, again near the horizontal joint. Due to a short measured groove length it was not possible to obtain the water flow data which would describe suction properties for the whole circumference. The results of experimental measurements provide very important information about the whole suction tract behaviour and its ability to remove liquid water films from the stator blades surface. As very good qualities of the suction tract were confirmed by the measurement, it could be stated that hollow stator blades combined with the circumferential groove on the upper limiting wall is still a suitable technical solution for lowering erosion loading of the last stages. When using a properly dimensioned and correctly working suction system, erosion loading of LSB leading edges on the tip can be lowered by almost a half.


2018 ◽  
Vol 28 (10) ◽  
pp. 2378-2403 ◽  
Author(s):  
Xu Han ◽  
Zhonghe Han ◽  
Wei Zeng ◽  
Peng Li ◽  
Jiangbo Qian

Purpose The purpose of this paper is to study the condensation flow of wet steam in the last stage of a steam turbine and to obtain the distribution of condensation parameters such as nucleation rate, Mach number and wetness. Design/methodology/approach Because of the sensitivity of the condensation parameter distribution, a double fluid numerical model and a realizable k-ε-kd turbulence model were applied in this study, and the numerical solution for the non-equilibrium condensation flow is provided. Findings The simulation results are consistent with the experimental results of the Bakhtar test. The calculation results indicate that the degree of departure from saturation has a significant impact on the wet steam transonic condensation flow. When the inlet steam deviates from the saturation state, shock wave interference and vortex mixing also have a great influence on the distribution of water droplets. Originality/value The research results can provide reference for steam turbine wetness losses evaluation and flow passage structure optimization design.


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