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Wyszukujesz frazę "high-pressure turbine" wg kryterium: Temat


Wyświetlanie 1-7 z 7
Tytuł:
Review of loss models for high pressure turbines
Autorzy:
Back da Trindade, D.
Bugała, P.
Simone, D.
Powiązania:
https://bibliotekanauki.pl/articles/244992.pdf
Data publikacji:
2018
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
turbomachinery
gas turbines
high-pressure turbine
HPT
loss model
Opis:
This article presents a literature review about the physical analysis of the loss models, which are used in offdesign procedure for high-pressure turbines. A high-pressure turbine is designed to have maximum performance at design point. However, engines are operating in different conditions, and the comprehension of off-design conditions is very important. The loss mechanisms are very complex and predictions considering empirical methods are a good approach to have preliminary results. Based on these results, different researches have proposed theories about the loss mechanisms, and over the time, these models have been modified to describe better the phenomena involved between blades and flow. Once the physical mechanisms behind the loss models are known, it is possible to compare them and understand the reason why the results given for some methods present a higher agreement to experimental or numerical data. In this framework, 2D numerical simulations of the flow around the blades of an axial high pressure turbine with different off design conditions have been realized, by using ANSYS FLUENT® code, to show the losses described by some of these models. Using these simulations a loss model has been selected and implemented in Matlab® to compare its results with the experimental data found in literature.
Źródło:
Journal of KONES; 2018, 25, 2; 38-44
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Deviation angle models in off-design high-pressure turbines
Autorzy:
Bugała, P.
Powiązania:
https://bibliotekanauki.pl/articles/247825.pdf
Data publikacji:
2018
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
turbomachinery
gas turbines
high-pressure turbine
HPT
deviation angle
Opis:
In the article, a set of deviation angle models, which are used to predict the off-design performance high-pressure turbines, has been presented, basing on a literature study. The deviation angle is a deviation between the actual flow angle and the blade inclination angle. It is an essential parameter in turbine performance evaluation. This angle shall be obtained accurately in 1-D design and evaluation, so as to ensure the validity of blade profiling and calculation results. If deviation angle is ignored, the turbine will produce a lower change of tangential velocity, and consequently a lower torque, output work and enthalpy drop than intended by the designer. For this reason, the deviation angle model needs to be established. There exist a number of different deviation models, resulting in varying degrees of flow deviation when applied. In the article, correlations for gas outlet angle, dependent on the Mach number at outlet and determined by the blade loading towards the trailing edge has been presented. The main difficulty in establishing the deviation model is a continuity in defining the angle for all speed ranges (both subcritical and supercritical). Each of the models presented in the article deals with this problem in a different way. A few deviation models, briefly discussed in the article, are based on experimental data and one is based on analytical approach.
Źródło:
Journal of KONES; 2018, 25, 2; 69-74
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Influence of cooling air mass flux variation on the convective heat transfer coefficient of HPT rotor disk
Autorzy:
Domański, R.
Jedliński, K.
Powiązania:
https://bibliotekanauki.pl/articles/243193.pdf
Data publikacji:
2007
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
CFD
Fluent
High Pressure Turbine
Rotor Disk
convective heat transfer coefficient
Opis:
The paper is focused on the convective heat transfer phenomena on the High Pressure Turbine (HPT) rotor disk wall. The disk is a part of PW6000 turbojet engine (designed by Pratt & Whitney Company) and is a base of the 1st stage of HPT blades having very high temperature (combustion gases leaving combustion chamber have temperature around 1800 K). The analyzed disk is cooled by the air taken from one of the compressor's stages. The air gets to the gap between HPT disk and mini disk through discrete pump holes and then divides into two streams. One of them is used to decrease temperature of turbine blades and the second one is directed to the sequent turbine stages. Numerical analysis (made in Fluent) is based on the two dimensional aerodynamic model (in steady state) which is the cross section of the real geometry. There are three different sets of boundary conditions analyzed. Each of them has the same flow splits (40% of air is used to cool turbine blades and 60% gets to the next turbine stage) and all settings except cooling air mass flow on the inlet. Convective heat transfer coefficients are calculated using different method then proposed by Fluent (WFHTC and SHTC options give wrong results in this case). Coefficients are presented along disk wall and are compared with Fluent calculation methods.
Źródło:
Journal of KONES; 2007, 14, 2; 107-114
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Review of design of high-pressure turbine
Autorzy:
Bugała, P.
Powiązania:
https://bibliotekanauki.pl/articles/246988.pdf
Data publikacji:
2017
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
preliminary design
turbomachinery
gas turbine
high-pressure turbine
HPT
projekt wstępny
turbo mechanizm
turbina gazowa
turbina wysokociśnieniowa
Opis:
The engine manufacturers adopt new measures in order to further improve the characteristics of a turbine engine. They pose new challenges to reduce a fuel consumption and an emission of pollution to the environment (including noise), but also keeping the highest level of reliability. Based on those considerations, current research in propulsion is conducted. Modern turbines are characterised by high inlet temperature. This has implications for engine efficiency, which is expressed with a change of mass, cross-section and fuel consumption. In this article, main trends in the development of turbine engines are presented. This analysis was carried out on the basis of Rolls-Royce engine data. The article presents literature review concerning the analytical methods of high-pressure turbines preliminary design. The aerodynamic design process is highly iterative, multidisciplinary and complex. Due to this, modern gas turbines need sophisticated tools in terms of aerodynamics, mechanical properties and materials. The article depicts simplified model of real turbine engine. As showed in the article, this model gives only a 10% error level in engine thrust value. The calculations may be used for preliminary engine analyses.
Źródło:
Journal of KONES; 2017, 24, 1; 67-76
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
The influence of stator-rotor interspace overlap of meridional contours on the efficiency of high-pressure steam turbine stages
Autorzy:
Rusanov, Andrii
Rusanov, Roman
Powiązania:
https://bibliotekanauki.pl/articles/1845496.pdf
Data publikacji:
2021
Wydawca:
Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:
high-pressure steam turbine
cavern
overlap
impulse type stage
reactive type stage
Opis:
The results of a systematic study of the influence of meridional contours overlap in the stator-rotor axial interspace of the impulse and reactive type stages of a high-pressure steam turbine on the flow structure and gas-dynamic efficiency of the flow part are introduced. The studied flow parts of the impulse and reactive stages are typical for high-power high-pressure steam turbines. It is shown that the stages that have no overlaps and/or have a smooth shape of meridional contours have the best gasdynamic efficiency, and the most negative effect on the flow part is caused by the presence of caverns in the stator-rotor interspace. For cases where, due to technological limitations, it is impossible to avoid the presence of caverns and overlaps with a sharp (step-wise) change in the shape of the meridional contours, it is recommended to perform overlaps with positive size of overlap values near the rotor blades.
Źródło:
Archives of Thermodynamics; 2021, 42, 1; 97-114
1231-0956
2083-6023
Pojawia się w:
Archives of Thermodynamics
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Wzorcowanie wysokociśnieniowe gazomierzy – stanowisko z pętlą zamkniętą
Gas meters high pressure calibration – closed-loop test stand
Autorzy:
Kułaga, P.
Powiązania:
https://bibliotekanauki.pl/articles/1835442.pdf
Data publikacji:
2017
Wydawca:
Instytut Nafty i Gazu - Państwowy Instytut Badawczy
Tematy:
gazomierze
gazomierze turbinowe
wzorcowanie
wzorcowanie wysokociśnieniowe
pętla zamknięta
gas meters
turbine gas meters
calibration
high pressure calibration
closed-loop test stand
Opis:
W artykule przedstawiono stosowane obecnie zasady badania i wzorcowania gazomierzy przy ciśnieniu roboczym. Poprawne wzorcowanie gazomierza jest kluczem do zapewnienia właściwej dokładności pomiaru. Omówiono zasady badania i weryfikacji gazomierzy w zależności od ciśnienia roboczego według norm europejskich EN 12480, EN 12261 oraz zaleceń OIML. Przybliżono również zagadnienie wzorcowania gazomierzy przy użyciu alternatywnych gazów – jako medium roboczego w instalacjach wysokociśnieniowych. Przedstawiono ogólny zarys stanowiska pomiarowego z zamkniętą pętlą wraz z opisem podstawowych elementów stanowiska.
The article presents the rules currently applicable, for testing and calibration of gas meters at operating pressure. The proper calibration of gas meters is key to ensuring accuracy of the reading. The principles of testing and verification of meters, depending on the pressure according to European standards EN 12480, EN 12261 and OIML requirements are presented. Also the issue of the calibration of gas meters using alternative gases as the working medium in high-pressure closed-loops is presented. The overview of a measuring stand with a closed-loop and description of its basic elements are presented.
Źródło:
Nafta-Gaz; 2017, 73, 5; 332-339
0867-8871
Pojawia się w:
Nafta-Gaz
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Approach to Impact Assessment of the Rated Power Uprate of NPP Unit on the Service Life of the Turbine Critical Elements
Autorzy:
Chernousenko, Olga
Nikulenkova, Tetyana
Peshko, Vitaliy
Nikulenkov, Anatolii
Powiązania:
https://bibliotekanauki.pl/articles/1811575.pdf
Data publikacji:
2020
Wydawca:
Politechnika Koszalińska. Wydawnictwo Uczelniane
Tematy:
nuclear power plant
reliability
turbine
steam flow
computational fluid dynamics
high pressure rotor
service life
long-term strength
low cycle fatigue
Opis:
Nuclear power plants play an important role in power systems of many countries. Ability to reasonable increase installed capacity of nuclear power units allow to reduce the cost for building of new power plants. When increasing NPP capacity to 104% there is a need to estimate the residual life of plant’s typical elements and continue their operation. The mathematical model of estimation of service life indicators of steam turbine K-1000-60/3000 is developed. The effect of increasing the capacity of a nuclear reactor on the heat transfer coefficients of a steam in the nozzle segments of high-pressure cylinder was established by using CFD modeling. The thermal and stress-strain state of the high-pressure rotor for the most typical operating modes are calculated. Using the correlation dependences of low-cycle fatigue, the rate of accumulation of cyclic damage of the base metal is established. The resistance of the metal to the exhaustion of long-term strength is also determined. On the example of the high pressure rotor of the 3rd power unit of Rivne NPP the service life indicators are calculated. The validity of increasing the installed capacity of the power unit was also confirmed.
Źródło:
Rocznik Ochrona Środowiska; 2020, Tom 22, cz. 1; 105-116
1506-218X
Pojawia się w:
Rocznik Ochrona Środowiska
Dostawca treści:
Biblioteka Nauki
Artykuł
    Wyświetlanie 1-7 z 7

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