Temat: combustion process - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Combustion process visualisation in rapid compression machine modelling combustion in spark ignition engines
Autorzy:: Leżański, T.
Sęczyk, J.
Wolański, P.
Powiązania:: https://bibliotekanauki.pl/articles/245855.pdf
Data publikacji:: 2013
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: internal combustion engines
spark ignition engines
combustion process
combustion process control
visualization of combustion process
Opis:: Mixture preparation and combustion processes in internal combustion engines are very complex and very difficult to investigate. These processes run very quickly and their parameters are changed quickly and in wide ranges. Therefore, the interpretation of measurement results is very difficult and uncertain. The visualization methods applied in the combustion researches can help to interpret the results. For many years, the visualization methods have been developed at the Aircraft Engine Department of Heat Engineering Institute of Warsaw University of Technology, in the field of combustion in engines, detonation and gas dynamics research. In these researches, different method of registration of very fast changes of combustion were applied. The combustion experiments have been performed in constant volume bomb, rapid compression machines and experimental visualisation engines. In the last case, the electronic digital camera of Photram SA 1.3 has been used. This paper refers to the experiments, which were conducted using rapid compression machine. Their goal was explanation the combustion mechanism in combustion system with semi-open combustion chamber under different parameters of this system. The obtained results show a strong influence of combustion system parameters on combustion mechanism, especially on a compression ratio and ignition timing. The strong swirls were registered at all sharp edges on combustion chamber during compression stroke. These swirls had a strong influence on the combustion system operation.
Źródło:: Journal of KONES; 2013, 20, 4; 219-226
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 2.

Tytuł:: Research of flame propagation in combustion system with semi-open combustion chamber for gasoline SI engines
Autorzy:: Leżański, T.
Sęczyk, J.
Wolański, P.
Powiązania:: https://bibliotekanauki.pl/articles/242275.pdf
Data publikacji:: 2011
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: SI engines
engine combustion systems
combustion process visualization
Opis:: Some results of visualization researches of combustion system with divided, semi - open combustion chamber for SI engines, using rapid compression machine (RPM) and experimental visualization engine (EVE) are presented in his paper. Short description of combustion system operation, description of test stands and research equipment can be found in the paper. The tests were performed at stoichiometric ratio natural gas-air and propane-air mixtures. A few the most characteristic of results are shown; to explain how should be operate the combustion system, to yield the better performance. They are compared the research results (photographs of combustion sequence, diagrams of in-cylinder pressure histories) during visualization testing with using RCM and EVE. During RCM testing we obtained the combustion photographs in the plain pass in cylinder axis but during ECE testing at the plain perpendicular to the cylinder axis. All researches shown that the best performance are yielded when a spark advance angle (ignition timing) is such selected that stream outflow prechamber to main combustion chamber starts when the piston is at TDC and it has adequate energy to travel a main combustion chamber with higher velocity than burning velocity in quiescent chamber. Then the shortest time of combustion, the highest peak pressure in the cycle and bigger useful working are yielded. The impact of spark advance angle on flame propagation process into combustion chamber in extreme cases has been analyzed too.
Źródło:: Journal of KONES; 2011, 18, 2; 251-260
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 3.

Tytuł:: Combustion process control in system with semi-open combustion chamber for spark ignition engines
Kontrola procesu spalania w systemie półotwartej komory spalania dla silników z zapłonem iskrowym
Autorzy:: Leżański, T.
Sęczyk, J.
Wolański, P.
Powiązania:: https://bibliotekanauki.pl/articles/133345.pdf
Data publikacji:: 2013
Wydawca:: Polskie Towarzystwo Naukowe Silników Spalinowych
Tematy:: internal combustion engines
spark ignition engines
combustion process
combustion process control
visualization of combustion process
silniki spalinowe
silniki o zapłonie iskrowym
proces spalania
kontrola procesu spalania
wizualizacja procesu spalania
Opis:: A few operation examples of combustion system with semi open combustion chamber for spark ignitron engines has been presented in this paper. This system has been designed in Aircraft Engine Department of Heat Engineering Institute of Warsaw University of Technology. The principal problem of operation this system is to assure that jet-stream commences to outflow from prechamber to main combustion chamber when the piston is at TDC and that it will have a sufficient energy quickly to displace all main chamber. This is a task for combustion control system. This can be obtained by correct selection of the system operating parameters: the volume ratio of prechamber to total combustion chamber, the hole diameter in partition, the igniter locations, the ignition advance angle. If this system has operate correctly it was obtained the shortening of combustion time about 2.2 time, growth of maximum cycle pressure 1.9 time and increase of combustion efficiency 1.4 time, in comparison to standard combustion chamber. This research results concern the test conducted using rapid compression machine.
W artykule przedstawiono kilka przykładów pracy systemu z półotwartą komora spalania przeznaczonego dla silników o zapłonie iskrowym. System ten został opracowany w Zakładzie Silników Lotniczych Instytutu Techniki Cieplnej Politechniki Warszawskiej. Podstawowym problemem pracy tego systemu jest zapewnienie, że początek wypływu strumienia z komory wstępnej do zasadniczej nastąpi wówczas, kiedy tłok znajduje się w GMP i że energia strugi będzie wystarczająca, aby szybko przebyć całą komorę zasadniczą. Takie jest zadanie układu sterowania. Może to być osiągnięte przez właściwy dobór parametrów pracy systemu: proporcji objętości komory wstępnej do całej objętości komory spalania, średnicy otworu w przegrodzie, miejsca zapłonu oraz kąta wyprzedzenia zapłonu. Jeśli ten system działał prawidłowo, to uzyskiwano: skrócenie czasu spalania około 2.2 razy, zwiększenie ciśnienia maksymalnego cyklu 1,9 razy i wzrost sprawności spalania 1,4 razy, w porównaniu ze standardową komorą spalania. Wyniki te dotyczą badań, które były prowadzone z zastosowaniem maszyny pojedynczego sprężu.
Źródło:: Combustion Engines; 2013, 52, 3; 434-441
2300-9896
2658-1442
Pojawia się w:: Combustion Engines
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 4.

Tytuł:: Influence of chosen parameters of water fuel microemulsion on combustion processes, emission level of nitrogen oxides and fuel consumption of CI engine
Autorzy:: Jankowski, A.
Powiązania:: https://bibliotekanauki.pl/articles/247478.pdf
Data publikacji:: 2011
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: diesel engines
combustion process
ecology
emulsion
microemulsions
Opis:: The microemulsion is the emulsion with dimension of molecules approx. micrometre and smaller. Such microemulsion of water and diesel oil creates new quality and lets on obtainment ecological and economic of effects, as well as eliminates the disadvantageous influence common emulsions, or unprofitable effects of the injection of water to inlet system of the engine, direct to combustion chambers, as well as the sequential injection of water direct to combustion chambers. The essence of apply of the microemulsion is also improve catalytic influence of small molecules of water on combustion process, what, beside decreasing temperature combustion gases, influences both emission level components of toxic combustion gases, as and the level of the specific fuel consumption. The paper presents different ways of microemulsion production, novel way of microemulsion production, which does not demand apply of mixers and suffers obtainment of microemulsion with the volumetric content of water in diesel oil do 40% under conditions of laboratory and stabile the microemulsion with content of water in diesel oil to 25%. Results of laboratory research involving basic parameters of the microemulsion and engine researches with measurements emission ingredients of toxic exhaust gases and fuel consumptions are presented involving basic parameters of the microemulsion and engine researches with measurements emission ingredients (NOx, soot, fuel consumption) of toxic exhaust gases and fuel consumptions are presented in the paper.
Źródło:: Journal of KONES; 2011, 18, 4; 593-600
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 5.

Tytuł:: Employing Optical Measurements for Monitoring and Diagnostics of Combustion Process in Industrial Conditions
Autorzy:: Wójcik, W.
Suleimenov, B.
Junisbekov, M.
Kalizhanova, A.
Smailova, S.
Mussabekov, R.
Powiązania:: https://bibliotekanauki.pl/articles/124530.pdf
Data publikacji:: 2017
Wydawca:: Polskie Towarzystwo Inżynierii Ekologicznej
Tematy:: combustion process
fiber optic probe
signal analysis
Opis:: The paper discusses some practical problems conected with introdction of modern coal combustion technologies as well as biomass co-combustion. In order to ensure that the combustion process runs in a proper way, the multichannel fiber optic monitoring system was applied. The system converts the optical signals coming from several flame zones to electrical that were further transmitted to the control room. The article prsents signal analyses made in time-frequency domain using short-time Fourier transform and wavelet transform and the way of their visualization to power boiler operators.
Źródło:: Journal of Ecological Engineering; 2017, 18, 1; 273-283
2299-8993
Pojawia się w:: Journal of Ecological Engineering
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 6.

Tytuł:: The effect of diesel/ethanol blends on variations of selected combustion parameter
Autorzy:: Lotko, W.
Smigins, R.
Górski, K.
Powiązania:: https://bibliotekanauki.pl/articles/242253.pdf
Data publikacji:: 2009
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: misfire detection
diesel engine
combustion process
ethanol
Opis:: This paper presents and discusses selected research results of the diesel engine fuelled with blends of: diesel oil (DO), synthetic ethanol (ET) as oxygenated additive and small quantity of fatty acid methyl esters (FAME) used as emulsifier. Content of ethanol in diesel oil was changed in wide range (up to 50%). Addition of 5% by vol. Of FAME was constant for each tested mixture. Preliminary tests were focused on influence of fuels blends composition on its combustion process. The main analyzed parameter was mean indicated pressure and its unrepeatability index. Research suggests that diesel oil blended with up to 20% of ethanol can be successfully used for diesel engines feeding. Higher ethanol content in mixture with diesel oil is unfavourable because misfire phenomenon occurs immediately. In this case tested engine works unstable with extremely high toxic gases emission. Some physical properties of tested fuels, measurement system configuration, Values of mean indicated pressure vs. cycle number for AD3.152 engine fuelled with: pure diesel oil, ETIO, ET20, ET30, ET 40, ET50, Variations of unrepeatability index of mean indicated pressure in relationship to kind of tested fuels are presented In the paper. Research shows that tested engine is not possible to operate with using above 40% of ethanol content in diesel oil, as the fuel simply will not ignite.
Źródło:: Journal of KONES; 2009, 16, 2; 279-284
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 7.

Tytuł:: Simulation of injection and combustion processes in 4-stroke spark ignition engine with CNG direct injection
Autorzy:: Sendyka, B.
Mitianiec, W.
Noga, M.
Wachulec, W.
Powiązania:: https://bibliotekanauki.pl/articles/246095.pdf
Data publikacji:: 2010
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: injection process
combustion process
simulation
modelling
alternative fuels
CNG
Opis:: The paper presents results of simulation conducted as afirst step of 4-stroke spark ignition experimental engine testing. The simulations were performed in a KIVA-3Vsoftware, which is intended to carry out a 3-D simulations of engine's processes. The source code of the software has been modified in order to apply it for gas injection. Original version of the software has been designedto simulate liquid fuel injection only. The simulation of direct CNG injection and combustion has been done for stratified and homogenous modes in order to check the assumed injection, ignition and charging parameters. Important assumption is that the injector had only one nozzle with flow area equal to 2 mm2. Two different cases of fuel direct injection for stratified charge have been analysed. In the first case fuel jet was almost vertical. In the other one fuel jet was nearly horizontal. Further testing has been performed using one-cylinder motorcycle 4-stroke SUZUKI DR-Z400S engine adapted to CNG fuelling. Such an engine has a suitable high compression ratio for CNG fuelling. The simulation has confirmed assumed parameters and has shown that one nozzle injector doesn't provide required fuel stream dissipation and piston crown modification is needed to direct fuel stream in spark plug area. However doing simulation requires some effort this example has shown than this is very important step before conducting experimental tests which provides crucial information and helps to avoid expensive mistakes which can be made during experimental engine preparation.
Źródło:: Journal of KONES; 2010, 17, 1; 373-378
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 8.

Tytuł:: Optimizing the shape of a compression-ignition engine combustion chamber by using simulation tests
Autorzy:: Pielecha, Ireneusz
Merkisz, Jerzy
Powiązania:: https://bibliotekanauki.pl/articles/962691.pdf
Data publikacji:: 2019
Wydawca:: Politechnika Gdańska. Wydział Inżynierii Mechanicznej i Okrętownictwa
Tematy:: CI engine combustion system
combustion process thermodynamic analysis
combustion chamber optimization
Opis:: Modern solutions used in compression-ignition internal combustion engines are quite similar to each other. The use of high-pressure, direct fuel injection results in high combustion rates with controlled exhaust emissions. One of the combustion system quality criteria is to obtain adequately high thermodynamic indicators of the combustion process, which are obtained through, among others, the right combustion chamber geometry. Its shape influences the fuel atomization process, turbulence of fuel dose, evaporation and the combustion process. Optimizing the combustion chamber shape is one of the decisive factors proving the correct execution of the combustion process. This article presents the methodology of choosing the combustion chamber shape (changes of three selected combustion chamber dimensions) by using the optimization methods. Generating multidimensional data while maintaining the correlation structure was performed by using the Latin hypercube method. Chamber optimization was carried out by using the Nelder-Mead method. The combustion chamber shape was optimized for three engine load values (determined by the average indicated pressure) at selected engine operating conditions. The presented method of engine combustion chamber optimization can be used in low and high speed diesel propulsion engines (especially in maritime transport applications).
Źródło:: Polish Maritime Research; 2019, 3; 138-146
1233-2585
Pojawia się w:: Polish Maritime Research
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 9.

Tytuł:: Computational modelling of the fuel injection and combustion in a Diesel K6 rotary engine
Autorzy:: Mason, M.
Wyszyński, M. L.
Jordan, O.
Gibson, D.
Powiązania:: https://bibliotekanauki.pl/articles/243793.pdf
Data publikacji:: 2018
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: combustion engine
combustion process
combustion factors
fuel injection
ANSYS Fluent code
Opis:: This paper outlines the methods and results of computations completed using the ANSYS Fluent code modelling the fuel injection and combustion within the K6 engine, a new form of rotary engine in which the fuel is injected in an arc across the top of the cylinder. The model uses the DPM Model in conjunction with a dynamic mesh and non-premixed combustion models to treat the injection as liquid diesel evaporating to C12H23. The outcomes of this model are presented in images displaying the distribution of temperature, and fuel and CO2 concentrations. The limitations pertaining to the maximum injection angles are also studied. The simulation is found to be effective and the results suggestive of successful, clean and complete combustion while presenting some matters, which require further investigation. The article presents temperature within the combustion chamber at various crank angle degrees, ) velocity of fluid within the combustion chamber, effects of impingement with injector offset on temperature and fuel concentration, fuel concentration demonstrating impingement, in cylinder temperature curve.
Źródło:: Journal of KONES; 2018, 25, 4; 263-276
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 10.

Tytuł:: Badanie homogenicznego stałego paliwa rakietowego zawierającego dodatki modyfikujące szybkość spalania
Testing of homogeneous rocket solid propellant including components to modify the rate of burning
Autorzy:: Florczak, B.
Wolszakiewicz, T.
Gawor, T.
Powiązania:: https://bibliotekanauki.pl/articles/236241.pdf
Data publikacji:: 2007
Wydawca:: Wojskowy Instytut Techniczny Uzbrojenia
Tematy:: paliwa rakietowe
proces spalania
rocket propellants
combustion process
Opis:: Przedstawiono wyniki badań homogenicznego stałego paliwa rakietowego składającego się z nitrocelulozy, nitrogliceryny i dodatków modyfikujących szybkość spalania. Zastosowanie dodatków modyfikujących proces spalenia, pozwoliło uzyskać paliwo o właściwych charakterystykach i parametrach eksploatacyjnych wyrażonych odpowiednimi przedziałami wartości kaloryczności, szybkości spalenia, współczynnika wrażliwości temperaturowej i wykładnika potęgowego występującego we wzorze na szybkość palenia paliwa w funkcji zmian ciśnienia. Otrzymanie korzystnych parametrów eksploatacyjnych paliwa okazało się możliwe dzięki synergizmowi zastosowanych komponentów modyfikatora procesu spalenia.
The results are presented in the paper over the testing of a homogeneous rocket solid propellant consisting of nitro-cellulose, nitro-glycerine and other components for modifying the rate of burning. The addition of components modifying the rate of burning resulted in receiving a propellant with desired specifications and characteristics of calorific value limits, burning rate, coefficient of temperature sensitivity and value of the power index in the formula describing the burning rate dependence on the pressure values. The synergism of components used in the propellant is the factor that makes possible to receive the product with good technical characteristics.
Źródło:: Problemy Techniki Uzbrojenia; 2007, R. 36, z. 103; 129-136
1230-3801
Pojawia się w:: Problemy Techniki Uzbrojenia
Dostawca treści:: Biblioteka Nauki

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