Wyniki wyszukiwania dla: AXIAL TURBINE, BLADE DESIGN, COMPUTATIONAL FLUID DYNAMICS, LAST STAGE OF LOW-PRESSURE TURBINE , TWISTED BLADE - MOST Wiedzy

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Wyniki wyszukiwania dla: AXIAL TURBINE, BLADE DESIGN, COMPUTATIONAL FLUID DYNAMICS, LAST STAGE OF LOW-PRESSURE TURBINE , TWISTED BLADE
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Wyniki wyszukiwania dla: AXIAL TURBINE, BLADE DESIGN, COMPUTATIONAL FLUID DYNAMICS, LAST STAGE OF LOW-PRESSURE TURBINE , TWISTED BLADE

  • Design and computational fluid dynamics analysis of the last stage of innovative gas-steam turbine

    Publikacja

    - Archives of Thermodynamics - Rok 2021

    Research regarding blade design and analysis of flow has been attracting interest for over a century. Meanwhile new concepts and design approaches were created and improved. Advancements in information technologies allowed to introduce computational fluid dynamics and computational flow mechanics. Currently a combination of mentioned methods is used for the design of turbine blades. These methods enabled us to improve flow efficiency...

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  • Revalorisation of the Szewalski’s concept of the law of varying the last-stage blade retraction in a gas-steam turbine

    Publikacja

    - E3S Web of Conferences - Rok 2021

    The article presents the implementations of the free vortex law to the blade of the last stage of a gas-steam turbine. First, a thermodynamic analysis was carried out, determining the parameters at the inlet, then the number of stages of the high and low-pressure part of the turbine was constructed, together with the kinematics and velocity vectors for subsequent stages of the axial turbine. The last step of article was to take...

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  • On design and analysis of flow characteristics of the last stage of gas-steam turbine

    Publikacja

    - Rok 2020

    Research regarding blade design and analysis of flow have been conducted for over a century. Meanwhile new concepts and design approaches were created and improved. Advancements in information technologies allowed to introduce computational fluid dynamics (CFD) and computational flow mechanics (CFM). Currently a combination of mentioned methods is used for design of turbine blades. These methods enabled us to improve flow efficiency...

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  • Updating Finite Element Model of a Wind Turbine Blade Section Using Experimental Modal Analysis Results

    Publikacja
    • M. Łuczak
    • S. Manzato
    • B. Peeters
    • K. Branner
    • P. Berring
    • M. Kahsin

    - SHOCK AND VIBRATION - Rok 2014

    This paper presents selected results and aspects of themultidisciplinary and interdisciplinary research oriented for the experimental and numerical study of the structural dynamics of a bend-twist coupled full scale section of awind turbine blade structure.Themain goal of the conducted research is to validate finite elementmodel of themodified wind turbine blade section mounted in the flexible support structure accordingly to the...

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  • Design and investigations of a micro-turbine flow part

    -generative micro-power plant with the HFE7100 as a working medium was designed and built for experimental investigations. The heat output of the plant was assumed equal to 20 kW, while the electric output amounted to about 3kW.In the paper a multi-stage micro-turbine with partial admission of all the stages is described in detail and the results of the particular experimental investigations and numerical calculations are shown,...

  • OPTIMIZATION OF THE LAST STAGE OF GAS-STEAM TURBINE USING A HYBRID METHOD

    Publikacja

    - Rok 2021

    This paper relates to the CFD calculation of a new turbine type which is in the phase of theoretical analysis, because the working fluid is a mixture of steam and gas generated in wet combustion chamber. At first, this article concentrates on a possibility of streamlining the flow efficiency of a last stage of axial turbine working on gas-steam mixture using a hybrid of the particle swarm optimization algorithm with the Nelder-Mead...

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  • Complex multidisciplinary optimization of turbine blading systems

    Publikacja

    - ARCHIVES OF MECHANICS - Rok 2012

    The paper describes the methods and results of direct optimization of turbine blading systems using a software package Opti_turb. The final shape of the blading is obtained from minimizing the objective function, which is the total energy loss of the stage, including the leaving energy. The current values of the objective function are found from 3D RANS computations (from a code FlowER) of geometries changed during the process...

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  • Rotor Blade Geometry Optimisation in Kaplan Turbine

    Publikacja

    The paper presents the description of method and results of rotor blade shape optimisation. The rotor blading constitutes a part ofturbine flow path. Optimisation consists in selection of the shape that minimises ratio of polytrophic loss. Shape of the blade isdefined by the mean camber line and thickness of the airfoil. Thickness is distributed around the camber line based on the ratio ofdistribution. Global optimisation was done...

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  • TERMODYNAMIC CALCULATIONS OF TURBINE STEAM PARAMETERS

    In this work a heat balance was made for the nominal conditions of a block working with 18K370 turbine. For the parameters obtained, the thermal-flow calculations of the steam turbine were performed, maintaining the actual geometry of its flow system. Based on the nominal values obtained, iterative thermal and flow calculations were made for both the heat cycle of the power plant block and the steam turbine itself, seeking to obtain...

  • Thermal failure of a second rotor stage in heavy duty gas turbine

    Publikacja

    - ENGINEERING FAILURE ANALYSIS - Rok 2020

    The impulse mode of operation and the supply of various types of fuels causes frequent failures even in the heavy duty gas turbines. The paper presents the ravages of second rotor stage failure in a gas turbine. The excessive thermal elongation rise caused by fuel change was indicated as the main cause. We applied nonlinear numerical analysis, preceded by thermodynamic calculations of the turbine and visual inspection of the effects...

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