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Tytuł:
Creating a ranking of diagnostic parameters for the dynamic process of marine combustion engine in the aspect of multi-criteria evaluations
Autorzy:
Zadrąg, R.
Powiązania:
https://bibliotekanauki.pl/articles/2073645.pdf
Data publikacji:
2016
Wydawca:
Politechnika Gdańska. Wydział Inżynierii Mechanicznej i Okrętownictwa
Tematy:
diagnostic
marine diesel engine
exhaust gas toxicity
multi-equation models
diagnostyka
silnik Diesla
toksyczność spalin
modele wielorównaniowe
Opis:
The change of some of the engine’s structural parameters affects the change of toxic compound emission in exhaust gases. It mainly applies to the damage sustained by the charge exchange system as well as the fuel system and the engine supercharging system. These changes are definitely higher during dynamic states and the related transient states. As such, it is possible to speak of a diverse sensitivity of the diagnostic parameters on the exact same excitations which come from the structure of the engine but are realized in other states of load. In the paper presented is the diagnostic model of an engine, based on the theory of multi-equation models, in which the diagnostic symptoms are the indices and characteristics of exhaust gas compound emissions. For the sake of this paper, the modal value of the structure parameters was assumed to be the change in the angle of advance of the fuel injection. The diagnostic model of the engine was supplemented with the results of research conducted on a station equipped with a single cylinder CI test engine. In previous works of the author, the information capacity index method (the Hellwig method) was suggested for the measurement of the sensitivity of a diagnostic parameter. Based on this method, a ranking of diagnostic parameters can be created, which divides the collection of diagnostic transients into stimulators, destimulators and nominants. This normalization of the collection seems to be helpful during making a diagnostic decision.
Źródło:
Journal of Polish CIMEEAC; 2016, 11, 1; 211--218
1231-3998
Pojawia się w:
Journal of Polish CIMEEAC
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
The identification of toxic compound emission sensitivity as a diagnostic parameter during dynamic processes of the marine engine
Autorzy:
Zadrąg, R.
Kniaziewicz, T.
Powiązania:
https://bibliotekanauki.pl/articles/2073657.pdf
Data publikacji:
2015
Wydawca:
Politechnika Gdańska. Wydział Inżynierii Mechanicznej i Okrętownictwa
Tematy:
diagnostic
theory of experiments
marine diesel engine
exhaust gas toxicity
multi-equation models
Opis:
Changing some parameters of the engine structure alters the emission of harmful components in the exhaust gas. This applies in particular to the damage of charge exchange system as well as fuel system and engine supercharger. These changes are much greater during the dynamic states and their accompanying transitional processes. The different sensitivity of diagnostic parameters to the same force, coming from the engine structure, but realized in other loading conditions can be discussed. Presented in the paper is a model of the engine diagnostic, in which symptoms are indicators of diagnostic and emission characteristics of gaseous exhaust components. For the purpose of the paper the parameters were taken as the dominant structure in the change of fuel injection timing. The diagnostic engine model, based on the theory of multi-equation models, was supplemented by the results of the tests on the single-cylinder research engine ZS. Also proposed is a measure of the sensitivity of the diagnostic parameter during dynamic processes. The following paper is building on the problem previously published by the authors in [X].
Źródło:
Journal of Polish CIMEEAC; 2015, 10, 1; 161--170
1231-3998
Pojawia się w:
Journal of Polish CIMEEAC
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Utilization of the zero unitarization method for the building of a ranking for diagnostic marine engine parameters
Autorzy:
Zadrąg, R.
Kniaziewicz, T.
Powiązania:
https://bibliotekanauki.pl/articles/133246.pdf
Data publikacji:
2017
Wydawca:
Polskie Towarzystwo Naukowe Silników Spalinowych
Tematy:
diagnostic
theory of experiments
marine diesel engine
exhaust gas toxicity
multi-equation models
diagnostyka
teoria eksperymentów
silnik okrętowy
toksyczność spalin
modele wielorównaniowe
Opis:
Changing some of the parameters of the engine structure affects the emission of harmful components in the exhaust gases. This primarily concerns damage in the cargo exchange system as well as in the fuel system and engine boost system. Changes in emissions of harmful compounds are often ambiguous, depending largely on the parameters that shape the combustion process. An additional problem is that often simple but undesired interactions occur with the interaction of these parameters. It is therefore possible to speak of different diagnostic parameters' sensitivity to the same extractions from the engine structure, but implemented in other load states. In cases where the set of parameters is numerous and the values of these parameters are similar, there is a real problem with their proper classification, often based on the discretion of the researcher. In the paper the authors propose a methodology for classification of acquired diagnostic parameters. In previous papers [4, 5], Hellwig's method of information capacity index was proposed as a measure of diagnostic parameter sensitivity. This method can be used to build a diagnostic parameter ranking that divides the set of diagnostic variables into stimulators, destimulators and nominators. This normalization of the set seems to be helpful in making a diagnostic decision not influenced by the discretion of the researcher. The zero unitary method can also be helpful in creating diagnostic tests.
Źródło:
Combustion Engines; 2017, 56, 4; 44-50
2300-9896
2658-1442
Pojawia się w:
Combustion Engines
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Criteria for the assessment of the engine efficiency of the multi-purpose aircraft missions
Autorzy:
Wygonik, P.
Powiązania:
https://bibliotekanauki.pl/articles/245198.pdf
Data publikacji:
2014
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
multi-purpose aircraft
turbine engines
airframe and engine integration
thermal cycle
Opis:
The problem of design parameters selection of the turbine engine is the most important task at the preliminary design stage of the multi-purpose aircraft. A special feature of the multi-purpose aircraft mission is a sudden (even pulse) weight change, especially its decrease as a result of discharge of cargo bombing or rockets due to the ammunition consumption during air combat manoeuvring. In this article the attempt to use economic and mass criteria to assess the impact of the type of air missions on the choice of the design parameters of the engine was done. As the design, parameters there were selected the following measures: compression ratio, the turbine temperature and the bypass ratio. A mathematical model of the engine – aircraft – air task system was built (taking into account the flight conditions, the mission elements – the subsonic and supersonic flight, flight time, thermo-gas-dynamic and mass model of the engine). The model enables to conduct the simulation research of the complex flight missions and their assessment on the basis of the constructed criteria. The model includes a parametric description of physical processes in the turbofan engine, thereby allowing a direct assessment of the impact of the selection of engine parameters on the effectiveness of the mission. The paper presents the results of calculations according to the classical criteria (e.g. kilometre fuel consumption, specific fuel consumption of the engine). New criteria for evaluation were presented; they are the energy efficiency of complex mission of an aircraft and the relative total and specific fuel consumption. The values of circuit parameters that need to be taken as design constraints for the engine to allow the implementation of the aviation missions were determined. The results are shown in an illustrative way on the number of graphs.
Źródło:
Journal of KONES; 2014, 21, 3; 301-307
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Criteria of aircraft engine parameters evaluation for multi-purpose aircraft
Kryteria oceny parametrów silnika turbinowego stanowiącego napęd samolotu wielozadaniowego
Autorzy:
Wygonik, P.
Powiązania:
https://bibliotekanauki.pl/articles/243118.pdf
Data publikacji:
2007
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
samolot wielozadaniowy
silniki turbinowe
integracja samolotu i silnika
multi-purpose aircraft
turbine engines
airframe and engine integration
Opis:
At the stage of a power unit selection for a multi-purpose aircraft the problem of mutual relations between the dimension of an aircraft and an engine should be solved. Starting from the motion equation of an aircraft and the theory of similarity the criteria and performance were determined which connect in a geometrical and power way the engine and the aircraft. The analysis of the influence of flight conditions and the parameters of an engine comparative cycle on the geometrical dimensions was conducted. In the paper it was shown that the fundamental flight stage which determines the relations between the geometrical parameters of the aircraft and the engine is the take-off or supersonic flight on the big altitude. Usually the parameters selection of the turbine engine thermal cycle is done on the basis of the internal characteristics of the engine, such as specific thrust and specific fuel usage. In case of the turbofan engine model with the mixer, afterburner, and the aircraft model (with simplified aerodynamic and mass characteristics) the influence of the cycle parameters on the performance and aerodynamic lift/drag ratio, the agreed range and the theoretical range was described. The next problem is to find those thermodynamics parameters (compression ratio, turbine inlet total temperature, bypass ratio) which give minimum of total mass of engine and consumed fuel for different airplane missions gamma Z. For long-lasting mission minimum gamma Z is occurs for compression ratio near his economic value (for specific fuel consumption). For short missions minimum of gamma Z occurs for smaller compression ratio (near 20-30), but greater than for those giving maximum specific thrust. A little change in minimum value of gamma Z gives a big difference in compression ratio. The most important conclusion is that the best thermodynamics parameters from minimum mass criterion are less than for minimum specific fuel consumption.
Na etapie wyboru zespołu napędowego do samolotu wielozadaniowego należy rozwiązać problem wzajemnych relacji między wymiarami samolotu i silnika. Wychodząc z równań ruchu samolotu i teorii podobieństwa wyznaczono kryteria i wskaźniki wiążące geometrycznie i energetycznie silnik oraz samolot. Przeprowadzono analizę wpływu warunków lotu samolotu i parametrów obiegu porównawczego silnika na wybrane wymiary geometryczne. W pracy wykazano, że zasadniczym stanem lotu determinującym relacje między parametrami geometrycznymi samolotu i silnika jest start samolotu lub przelot naddźwiękowy na dużej wysokości. Zwykle doboru parametrów obiegu cieplnego silnika turbinowego dokonuje się w oparciu o charakterystyki wewnętrzne silnika- ciąg jednostkowy, jednostkowe zużycie paliwa. W oparciu o model silnika dwuprzepływowewgo, z mieszalnikiem strumieni, dopalaczem oraz model samolotu (przyjęto uproszczone charakterystyki aerodynamiczne i masowe) określono wpływ parametrów obiegu na podstawowe wskaźniki samolotu jak doskonałość aerodynamiczna, zasięg umowny i zasięg teoretyczny. Kolejnym problemem jest określenie parametrów termogazodynamicznych, które pozwalają minimalizować masę silnika i zużytego w trakcie misji samolotu paliwa. W trakcie misji tzw. długich parametr jednostkowej masy względnej silnika gamma Z osiąga minimum dla sprężu całkowitego sprężarki rzędu (20-30), ale większych niż wartości sprężu optymalnego. Niewielka zmiana w wartości minimum gamma Z powoduje znaczną zmianę w wartości sprężu sprężarki. Parametry termogazodynamiczne, które pozwalają minimalizować masę sumaryczną paliwa i silnika są mniejsze niż dla minimum jednostkowego zużycia paliwa i zbliżone do wartości charakterystycznych dla współczesnych silników lotniczych.
Źródło:
Journal of KONES; 2007, 14, 2; 571-578
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Selection criteria of internal parameters of turbofan engine for the type of multi-task aircraft mission
Kryteria doboru parametrów wewnetrznych silnika dwuprzepływowego do rodzaju misji samolotu wielozadaniowego
Autorzy:
Wygonik, P.
Powiązania:
https://bibliotekanauki.pl/articles/133911.pdf
Data publikacji:
2013
Wydawca:
Polskie Towarzystwo Naukowe Silników Spalinowych
Tematy:
multi-task airplane
turbofan engine
engine parameters optimization
samolot wielozadaniowy
silnik przepływowy
optymalizacja parametrów silnika
Opis:
The problem described in the paper concerns the selection strategy of the so-called calculation point of the turbofan engine of the multi-task aircraft already at the stage of preliminary design of the aircraft and aircraft engine as a system. A multi-task airplane during each mission needs to perform a series of tasks with different levels of power utilization, while changing the mass, at different altitudes and flight velocities. There was defined the criterion of the LoLoLo mission based on an assessment of mission energy consumption. The calculation results were presented from the point of view of the influence of thermo-gas-dynamic parameters of the comparative cycle circulation (such as compression, turbine inlet temperature, the degree of streams distribution) on the criterion of energy resources usage. The presented criterion allows to make a correct selection of parameters of thermodynamic cycle from the viewpoint of energy possibilities of an aircraft and a mission.
Problem przedstawiony w artykule dotyczy strategii wyboru tzw. punktu obliczeniowego silnika systemu lotniczego. Samolot wielozadaniowy podczas każdej misji musi wykonać cały szereg zadań, różniących się poziomem wykorzystania mocy, przy zmieniającej się masie własnej, na różnych wysokościach i prędkościach lotu. Zdefiniowano kryterium oceny misji typu LoLoLo w oparciu o ocenę energochłonności misji. Wyniki obliczeń przedstawiono z punktu widzenia wpływu parametrów termogazodynamicznych obiegu porównawczego (jak spręż, temperatura przed turbiną, stopień podziału strumieni) na kryterium wykorzystania zasobów energetycznych. Przedstawione kryterium pozwala dokonac prawidłowości wyboru parametrów obiegu termodynamicznego z punktu widzenia możliwości energetycznych samolotu i misji.
Źródło:
Combustion Engines; 2013, 52, 3; 483-488
2300-9896
2658-1442
Pojawia się w:
Combustion Engines
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Thermodynamics and mass selection criterions of low bypass turbine engine parameters for multi-purpose
Autorzy:
Wygonik, P.
Powiązania:
https://bibliotekanauki.pl/articles/244019.pdf
Data publikacji:
2008
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
multi-purpose aircraft
turbine engines
airframe and engine integration
thermal cycle
Opis:
Parameters of the turbofan engine comparative cycle (turbine inlet temperature, compression of compressors), by-pass ratio, fan compressor, (or low pressure compressor) are the most important engine parameters which determine their characteristics and construction. In order to fulfill the task there is a necessity for searching the optimum parameters for the system. The most important equation that binds airplane and engine characteristics is mass balance equation. The sum of engine mass and fuel mass was called total engine-fuel mass. In the paper specific total engine mass index was introduced (gamma 2). This index is equal to total engine-fuel mass divided by thrust in design point. Impact of the choice of the design point on the total mass index of the engine and the fuel used up was presented for different airplane mission. The next problem is to find those thermodynamics parameters (compression ratio, turbine inlet total temperature, bypass ratio) which give minimum of total mass of engine and consumed fuel for different airplane missions. A very important parameter that plays the part in fuel consumption is airplane flight time. The most important conclusion is that the best thermodynamics parameters from minimum mass criterion are less than for minimum specific fuel consumption.
Parametry obiegu porównawczego dwuprzeplywowego turbinowego silnika odrzutowego determinują jego charakterystyki i schemat konstrukcyjny. W pracy przedstawiono problem poszukiwania optymalnych wartości parametrów termogazodynamicznych obiegu porównawczego silnika turbinowego. Do tych parametrów zaliczono: spręż całkowity sprężarki, temperaturę przed turbiną, stopień podziału strumieni. Przedstawiono wpływ wybranych warunków lotu, sprężu sprężarki i temperatury przed turbiną na zmianę ciągu jednostkowego i jednostkowego zużycia paliwa. Jako kryterium optymalizacji wybrano sumaryczną masę silnika i paliwa, wymaganą do wykonania zadania lotniczego. Wykorzystano, zbudowany na potrzeby innych prac, model silnika, który jest funkcją parametrów termogazodynamicznych. Wyprowadzono zależności pozwalające na optymalizację jednostkowej masy sumarycznej (jako kryterium bezwymiarowego). Przeprowadzono szereg obliczeń, których wyniki przedstawiono na wykresach. Wykazano, że na podstawie wybranego kryterium optymalizacji, jakim jest sumaryczna masa silnika i paliwa, można wyznaczyć wartości sprężu sprężarki, dla których wskazane kryteria oceny masy osiągają swoje minimum.
Źródło:
Journal of KONES; 2008, 15, 2; 543-551
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Fault diagnosis of me marine diesel engine fuel injector with novel IRCMDE method
Autorzy:
Shi, Qingguo
Hu, Yihuai
Yan, Guohua
Powiązania:
https://bibliotekanauki.pl/articles/34608122.pdf
Data publikacji:
2023
Wydawca:
Politechnika Gdańska. Wydział Inżynierii Mechanicznej i Okrętownictwa
Tematy:
marine diesel engine
fuel injector
improved refined composite multi-scale dispersion entropy
fault diagnosis
Opis:
As an important component of the fuel injection system, the fuel injector is crucial for ensuring the power, economy, and emissions for a whole ME (machine electronically-controlled) marine diesel engine. However, injectors are most prone to failures such as reduced pressure at the opening valve, clogged spray holes and worn needle valves, because of the harsh working conditions. The failure characteristics are non-stationary and non-linear. Therefore, to efficiently extract fault features, an improved refined composite multi-scale dispersion entropy (IRCMDE) is proposed, which uses the energy distribution of sampling points as weights for coarse-grained calculation, then fast correlation-based filter (FCBF) and support vector machine (SVM) are used for feature selection and fault classification, respectively. The experimental results from a MAN B&W 6S35ME-B9 marine diesel engine show that the proposed algorithm can achieve 92.12% fault accuracy for injector faults, which is higher than multiscale dispersion entropy (MDE), refined composite multiscale dispersion entropy (RCMDE) and multiscale permutation entropy (MPE). Moreover, the experiment has also proved that, due to the double-walled structure of the high-pressure fuel pipe, the fuel injection pressure signal is more accurate than the vibration signal in reflecting the injector operating conditions.
Źródło:
Polish Maritime Research; 2023, 3; 96-110
1233-2585
Pojawia się w:
Polish Maritime Research
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Analysis of the pre-injection system of a marine diesel engine through multiple-criteria decision-making and artificial neural networks
Autorzy:
Rodriguez, C. G.
Lamas, M. I.
Rodriguez, J. D.
Abbas, A.
Powiązania:
https://bibliotekanauki.pl/articles/2033205.pdf
Data publikacji:
2021
Wydawca:
Politechnika Gdańska. Wydział Inżynierii Mechanicznej i Okrętownictwa
Tematy:
marine engine
emissions
consumption
artificial neural networks
multi-criteria decision making
computational fluid dynamics
Opis:
The present work proposes several pre-injection patterns to reduce nitrogen oxides in the Wartsila 6L 46 marine engine. A numerical model was carried out to characterise the emissions and consumption of the engine. Several pre-injection quantities, durations, and starting instants were analysed. It was found that oxides of nitrogen can be noticeably reduced but at the expense of increasing consumption as well as other emissions such as carbon monoxide and hydrocarbons. According to this, a multiple-criteria decision-making (MCDM) model was established to select the most appropriate parameters. Besides, an artificial neural network (ANN) was developed to complement the results and analyse a huge quantity of alternatives. This hybrid MCDM-ANN methodology proposed in the present work constitutes a useful tool to design new marine engines.
Źródło:
Polish Maritime Research; 2021, 4; 88-96
1233-2585
Pojawia się w:
Polish Maritime Research
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Effects of mixture formation strategies on combustion in dual-fuel engines - a review
Autorzy:
Pielecha, Ireneusz
Sidorowicz, Maciej
Powiązania:
https://bibliotekanauki.pl/articles/2097496.pdf
Data publikacji:
2021
Wydawca:
Polskie Towarzystwo Naukowe Silników Spalinowych
Tematy:
dual fuel engine
excess air coefficient
multi-fuel mixture forming
silnik dwupaliwowy
współczynnik nadmiaru powietrza
formowanie mieszanki wielopaliwowej
Opis:
The article presents an overview of technical solutions for dual fuel systems used in internal combustion engines. It covers the historical and contemporary genesis of using two fuels simultaneously in the combustion process. The authors pay attention to the value of the excess air coefficient in the cylinder, as the ignitability of the fuel dose near the spark plug is a critical factor. The mixture formation of compression ignition based systems are also analyzed. The results of research on indirect and direct injection systems (and their combinations) have been presented. Research sections were separated based to the use of gasoline with other fuels or diesel oil with other fuels. It was found that the use of two fuels in different configurations of the fuel supply systems extends the conditions for the use of modern combustion systems (jet controlled compression ignition, reactivity controlled compression ignition, intelligent charge compression ignition, premixed charge compression ignition), which will enable further improvement of combustion efficiency.
Źródło:
Combustion Engines; 2021, 60, 1; 30--40
2300-9896
2658-1442
Pojawia się w:
Combustion Engines
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Badanie wtryskiwaczy paliwa w silnikach o zapłonie iskrowym
Spark ignition fuel injectors research
Autorzy:
Osipowicz, T.
Powiązania:
https://bibliotekanauki.pl/articles/312471.pdf
Data publikacji:
2017
Wydawca:
Instytut Naukowo-Wydawniczy "SPATIUM"
Tematy:
silnik o zapłonie iskrowym jednopunktowy wtrysk paliwa
wielopunktowy wtrysk paliwa
diagnozowanie układu wtryskowego
spark ignition engine
single point ignition system
multi point ignition system
injection system diagnosing
Opis:
Artykuł przedstawia możliwości badawcze wtryskiwaczy paliwa zastosowanych w silnikach o zapłonie iskrowym. W referacie opisano rodzaje układów zasilania silników o zapłonie wymuszonym, ich budowę i działanie. Zostały opisane również sposoby tworzenia się mieszaniny palnej i spalanie w omawianych silnikach. Przedstawiono w jaki sposób można testować i ewentualnie przywracać parametry robocze wtryskiwaczy paliwa silników ZI.
Article presents the research possibilities of spark ignition fuel injectors. Paper describes types of spark ignition systems, construction and work. There has been presented the methods of rising combustible mixture and combustion process in spark ignition engines. There has been dicussed the test and work parameters reset methods spark ignition engines fuel injectors.
Źródło:
Autobusy : technika, eksploatacja, systemy transportowe; 2017, 18, 7-8; 196-198
1509-5878
2450-7725
Pojawia się w:
Autobusy : technika, eksploatacja, systemy transportowe
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Multiparameter approximation model of temperature conditions of marine diiesel generator sets, based on Markov chain Monte Carlo
Autorzy:
Myrhorod, V.
Hvozdeva, I.
Budashko, V.
Powiązania:
https://bibliotekanauki.pl/articles/24201416.pdf
Data publikacji:
2022
Wydawca:
Uniwersytet Morski w Gdyni. Wydział Nawigacyjny
Tematy:
marine diesel engine
Markov chain Monte Carlo
temperature condition
multi-parameter approximation model
marine diesel generator
markov model
diagnostics
technical diagnostics
Opis:
In the article we propose a multi-parameter approximation model, based on Markov chain Monte Carlo, which describes the relationship between the temperature regime, operating conditions and electromechanical parameters of marine diesel generator sets. The approximation model is constructed on the basis of the analysis of experimental data of the exhaust gases temperature of marine diesel generator sets in their long-term operation. As a statistical model of random processes of temperature deviations from the approximation model, a Markov process model is proposed that takes into account the possible correlation of the initial data. Since the measuring channels of modern diagnostic systems are digital, due to discretization in time and level, the studied processes form a Markov chain, which makes it possible to establish the important features of such processes. The use of approximation models ensures the stationarity conditions and the correctness of the proposed Markov model in the conditions of multi-mode operation of marine diesel generator sets. The proposed multi-parameter approximation model, based on Markov chain Monte Carlo, allows you to take into account random perturbations that lead to a random change in the output coordinates of the diagnostic object. The proposed improvement of the model makes it possible to ensure its adequacy to real processes of changing the parameters of the temperature regimes of marine diesel generator sets. The proposed multi-parameter approximation model, based on Markov chain Monte Carlo, can be used in the systems of technical diagnostics of marine diesel generator sets in order to increase the reliability of diagnostic conclusions.
Źródło:
TransNav : International Journal on Marine Navigation and Safety of Sea Transportation; 2022, 16, 4; 779--784
2083-6473
2083-6481
Pojawia się w:
TransNav : International Journal on Marine Navigation and Safety of Sea Transportation
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Optimisation of the topping-up process of lubricating oil in medium-speed marine engines
Autorzy:
Młynarczak, Andrzej
Krzysztof, Rudzki
Powiązania:
https://bibliotekanauki.pl/articles/1573592.pdf
Data publikacji:
2021
Wydawca:
Politechnika Gdańska. Wydział Inżynierii Mechanicznej i Okrętownictwa
Tematy:
multi-objective optimisation
medium-speed marine engine
lubricating oil
soild impurities
alkalinity
topping-up process
Opis:
In this paper, we examine the problem of optimising the process of topping up lubricating oil in medium-speed marine engines. This process is one of the methods that can be applied to improve the properties of lubricating oil. The amount of fresh oil added to lubricating oil system always balances its consumption, but the method used to top up depends on the marine engineer. Small amounts of fresh oil can be added at short intervals, or large ones at long intervals, and the element of randomness often plays a significant role here. It would therefore be valuable to find a method that can help the mechanical engineer to choose the right strategy. We apply a multi-criteria optimisation method for this purpose, and assume that the criterion functions depend on the concentration of solid impurities and the alkalinity, which are among the most important aspects of the quality and properties of lubricating oil. These criterion functions form the basis for multi-objective optimisation carried out with the use of the MATLAB computer program.
Źródło:
Polish Maritime Research; 2021, 2; 78-84
1233-2585
Pojawia się w:
Polish Maritime Research
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
The concept and construction of the engine test bed for experiments with a multi - fuel CI engine FED with cng and liquid fuel as an ignition dose
Autorzy:
Mikulski, M.
Wierzbicki, S.
Powiązania:
https://bibliotekanauki.pl/articles/246758.pdf
Data publikacji:
2012
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
combustion engines
CI engines
engine test bed
multi-fuel engine
CNG
Opis:
The experiments described in the article aimed at adjusting the engine test bed, its equipment and software to perform comprehensive tests on a dual-fuel spontaneous combustion engine with the main gas dose (methane or biogas) and a liquid fuel ignition dose. The steps undertook during the tests included installing a new engine on the engine test bed, installing its equipment and preparing a dual-fuel feed system. The toxic emissions analysis system was also modified, thanks to which a thorough research based on current test methods was possible. All measurement devices were integrated and are governed by one system of data acquisition and controlling, which ensures repeatable testing conditions. In order to exercise better control over the oil pilot dose injection, the previously used engine was replaced with a Common Rail one, which facilitates better control over the pilot dose injection and ensures controlling the system through an external driver. Providing the engine with a set of measurement systems makes it possible to test it not only with reference to its power and toxic emissions into the atmosphere, but also to the heat absorbed by the cooling system, which enables testing engines for cogeneration units.
Źródło:
Journal of KONES; 2012, 19, 3; 289-296
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Exhaust emissions evaluation for multi-role fighter aircraft operation
Autorzy:
Merkisz, J.
Markowski, J.
Pielecha, J.
Jasinski, R.
Wirkowski, P.
Slusarz, G.
Powiązania:
https://bibliotekanauki.pl/articles/2073639.pdf
Data publikacji:
2016
Wydawca:
Politechnika Gdańska. Wydział Inżynierii Mechanicznej i Okrętownictwa
Tematy:
exhaust emissions
harmful compounds
aircraft operation
turbine engine
multi-role aircraft
emisje spalin
związki szkodliwe
silnik turbinowy
samolot wielozadaniowy
Opis:
Multi-role aircraft as a technical object of a certain functional purpose and operating characteristics resulting from its construction, affects the operating environment mechanically, as a source of disturbance of the medium in which it moves and chemically, by generating the emission of harmful substances resulting from the need to use consumable fuels. Operation of multi-role aircraft, in contrast to civil aircraft, is characterized by high volatility of flight data resulting from the diversity of performed tasks. Therefore it seems desirable to attempt the ecological evaluation of the drive in terms of emissions on the basis of a dedicated test for a particular group of aircraft. An attempt at such an assessment is presented in this article.
Źródło:
Journal of Polish CIMEEAC; 2016, 11, 1; 117--130
1231-3998
Pojawia się w:
Journal of Polish CIMEEAC
Dostawca treści:
Biblioteka Nauki
Artykuł
Wyświetlanie 1-15 z 23

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