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Wyszukujesz frazę "silnik Wankla" wg kryterium: Temat


Wyświetlanie 1-5 z 5
Tytuł:
Modelling and simulation of working processes in Wankel engine with direct hydrogen injection system
Modelowanie i symulacja procesów roboczych w silniku Wankla z bezpośrednim wtryskiem wodoru
Autorzy:
Mitianiec, W.
Powiązania:
https://bibliotekanauki.pl/articles/133875.pdf
Data publikacji:
2015
Wydawca:
Polskie Towarzystwo Naukowe Silników Spalinowych
Tematy:
combustion engines
Wankel engine
scavenging process
hydrogen combustion
silniki spalinowe
silnik Wankla
przepłukanie
spalanie wodoru
Opis:
Wankel engines were very attractive in automotive sector almost forty years ago because of small dimensions, compactness, simple design, smoothness of engine work and lack of vibration caused by inertia forces. The disadvantage of such engine was very high pollution, especially of hydrocarbons and carbon monoxide and high fuel consumption. These disadvantages can be eliminated by applying of direct injection of hydrogen and in the aviation sector by applying of fuel with high octane number also at a direct injection system. The main objective of the work is modelling of the thermodynamic process taking place during the scavenge process in such engine. At assumed geometry of the engine, initial and boundary conditions the change of engine parameters such as pressure, temperature, density, heat exchange and volume are calculated on the base of zero-dimensional model as a function of rotation angle of the piston. Forming of the mixture during fuel injection process in compression process gives information about the air excess ratio. The presented model is applicable for different sort of fuels. This work is introduction to a broader analysis of the processes in spatial system. Application of hydrogen reduces of toxic components emission from such engine, but decreases also engine power.
Silnik Wankla byl bardzo interesujący dla przemysłu samochodowego prawie czterdzieści lat temu ze względu na małe wymiary, kompaktowość, prostą konstrukcję, równomierność pracy silnika i brak drgań wywołanych siłami bezwładności. Wadą tego silnika była duża toksyczność emitowanych spalin, szczególnie węglowodorów i tlenków azotu oraz duże zużycie paliwa. Te niedoskonałości silnika mogą być wyeliminowane dzięki zastosowaniu bezpośredniego wtrysku paliwa o dużej liczbie oktanowej lub wodoru. Głównym celem pracy jest modelowanie parametrów termodynamicznych procesów zachodzących w czasie przepłukania w tym silniku. Przy założonych parametrach geometrycznych silnika, warunkach brzegowych i początkowych obliczono zmiany parametrów takich, jak: ciśnienie, temperatura, gęstość, prędkości wlotu i wylotu za pomocą własnego programu komputerowego opartego na modelu 0-D w funkcji kąta obrotu wału korbowego. Tworzenie mieszanki podczas wtrysku paliwa daje informację o współczynniku nadmiaru powietrza. Zaprezentowany model obliczeniowy jest dostosowany do różnego rodzaju paliwa. Praca jest wstępem do szerszej analizy procesów przestrzennych w komorze spalania. Zastosowanie wodoru zmniejsza emisję szkodliwych składników spalin, lecz zmniejsza również moc silnika.
Źródło:
Combustion Engines; 2015, 54, 2; 42-52
2300-9896
2658-1442
Pojawia się w:
Combustion Engines
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
A rotating piston engine with electric generator in serial hybrid propulsion system for use in light aircraft
Autorzy:
Kalwara, Maciej
Kuźniar, Michał
Orkisz, Marek
Powiązania:
https://bibliotekanauki.pl/articles/2097559.pdf
Data publikacji:
2021
Wydawca:
Polskie Towarzystwo Naukowe Silników Spalinowych
Tematy:
hybrid
combustion engines
motor glider
rotary engine
Wankel engine
hybrid propulsion
hybryda
silniki spalinowe
motoszybowiec
silnik rotacyjny
silnik Wankla
napęd hybrydowy
Opis:
Analysis of the possibility of using a rotary engine based electric generator to propell a powered sailplane. The paper presents analysis of utilising Wankel type enine as a power input for an electric generator in the motor glider propulsion system. This generator would be a part of the propulsion system of a hybrid motor glider using the AOS 71 motor glider airframe. In the research, the rotational characteristics of the LCR 407ti wankel engine were determined experimentally. Driving torque run, power and fuel consumption were determined as a function of engine speed. The obtained results are presented in diagrams. The conceptual diagram of the hybrid drive is presented. The electric generator was selected and its effectiveness, as well as the effectiveness of entire propulsion system was assessed from the motor glider's performance point of view. Basing on the research conducted, conclusions were drawn and there were indicated the objectives and directions of further research on hybrid propulsion with specific aerodynamic and mass limitations of the aircraft.
Źródło:
Combustion Engines; 2021, 60, 4; 42--45
2300-9896
2658-1442
Pojawia się w:
Combustion Engines
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Analysis of the possibility of using an engine with a rotating piston as the propulsion of an electric generator in application to a motor glider propulsion
Autorzy:
Orkisz, Marek
Wygonik, Piotr
Kuźniar, Michał
Kalwara, Maciej
Powiązania:
https://bibliotekanauki.pl/articles/134090.pdf
Data publikacji:
2019
Wydawca:
Polskie Towarzystwo Naukowe Silników Spalinowych
Tematy:
hybrid
combustion engines
motor glider
rotary engine
Wankel engine
hybrid propulsion
hybryda
silniki spalinowe
motoszybowiec
silnik rotacyjny
silnik Wankla
napęd hybrydowy
Opis:
Analysis of the possibility of using an engine with a rotating piston as the propulsion of an electric generator in application to a motor glider propulsion The paper presents an analysis of the possibilities of application of a rotating piston engine (Wankel type) as a propulsion for an electric generator in the motor glider propulsion system. This generator would be a part of the propulsion system of a hybrid motor glider using the AOS 71 motor glider airframe. In the research, the rotational characteristics of the LCR 407ti engine were determined experimentally. Driving torque run, power and fuel consumption were determined as a function of engine speed. The obtained results are presented in diagrams. The conceptual diagram of the hybrid drive is presented. The current generator was selected and the effectiveness of the generator and the entire propulsion were assessed from the motor glider's performance point of view. On the basis of the conducted research, conclusions were drawn and there were indicated the objectives and directions of further research on hybrid propulsion with specific aerodynamic and mass limitations of the aircraft.
Źródło:
Combustion Engines; 2019, 58, 3; 264-268
2300-9896
2658-1442
Pojawia się w:
Combustion Engines
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Comparative analysis of pollutants emission by classical and distributed propulsions applied on the AOS motor glider
Autorzy:
Orkisz, Marek
Wygonik, Piotr
Kuźniar, Michał
Kalwara, Maciej
Powiązania:
https://bibliotekanauki.pl/articles/133089.pdf
Data publikacji:
2019
Wydawca:
Polskie Towarzystwo Naukowe Silników Spalinowych
Tematy:
distributed propulsion
hybrid
motor glider
rotary engine
Wankel engine
hybrid propulsion
emission
exhaust gases
napęd rozproszony
hybryda
motoszybowiec
silnik rotacyjny
silnik Wankla
napęd hybrydowy
emisja spalin
Opis:
Comparative analysis of harmful compounds emission of classical and distributed propulsions applied on the AOS motor glider, taking into account the perspective of the development of hybrid propulsions. A novel path is indicated by so-called distributed aircraft propulsion. The advantages and disadvantages of this type of solutions are presented, as well as the conceptual design of the distributed propulsion for the AOS 71 motor glider. In the paper there were compared the emissions of harmful compounds generated by a hybrid power unit developed for the airframe of AOS 71 motor glider - traditional propulsion, so-called focused (one-propeller) and dispersed propulsion (multi-propelled). Functional diagrams of both types of propulsions solutions are presented. Construction and aerodynamic constraints of both propulsions are discussed and comparative analysis is made. In the traditional version of the propulsion (so-called focused propulsion). the propeller is driven by an Emrax 228 electric engine with effective parameters: N = 55 kW, M = 120 Nm. The power source is a battery set with a capacity of 16 Ah and a range extender powered by a LCR 407ti rotating piston engine with maximum power of 28 kW. In the variant of the distributed propulsion. Ten electric engines of AXI 8120 type were used to drive small propellers arranged along the wingspan. The power source in this variant is analogous to the variant with the Emrax electric engine. For the adopted variant of the flight mission of the motor glider. a flight trajectory model was developed, which was used to determine the load of the power unit. In laboratory conditions. emission tests of both propulsions were conducted. The results are summarized in charts and discussed in the conclusions.
Źródło:
Combustion Engines; 2019, 58, 4; 102-106
2300-9896
2658-1442
Pojawia się w:
Combustion Engines
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Comparative analysis of combustion engine and hybrid propulsion unit in aviation application in terms of emission of harmful compounds in the exhausts emitted to the atmosphere
Autorzy:
Orkisz, Marek
Wygonik, Piotr
Kuźniar, Michał
Kalwara, Maciej
Powiązania:
https://bibliotekanauki.pl/articles/133727.pdf
Data publikacji:
2019
Wydawca:
Polskie Towarzystwo Naukowe Silników Spalinowych
Tematy:
hybrid
combustion engines
motor glider
rotary engine
Wankel engine
hybrid propulsion
emission
exhaust gases
hybryda
silniki spalinowe
motoszybowiec
silnik rotacyjny
silnik Wankla
napęd hybrydowy
emisja spalin
Opis:
Comparative analysis of combustion and hybrid propulsion unit in aviation application in terms of emission of harmful compounds in the exhausts emitted to the atmosphere. For the propulsion of the AOS 71 motor glider, two types of propulsion were planned as development versions. The first analysed propulsion is based on a combustion engine, but of the Wankel type (LCR 814 engine with the power of 55 kW). The second designed propulsion is an hybrid based on a LCR 407 combustion engine with a power of 28 kW, which is connected in series with an electric generator propelling the engine (Emrax 228 engine), total power of the propulsion is 55 kW. The comparison of emissions of harmful compounds emitted to the atmosphere generated by the combustion and hybrid power unit intended for assembly in the AOS 71 motor glider, assuming various loads and methods of hybrid propulsion control, was made. The tests were conducted in laboratory conditions. Several different programs were designed to simulate different energy management methods in a hybrid system, depending on the predicted mission and load of the motor glider. On the basis of laboratory tests, exhaust emission was determined from both propulsions as a function of rotational speed and load. Then, based on the assumed flight trajectory and collected test data, the emission for both propulsions variants was determined. The values of emission parameters were compared and the results were presented in diagrams and discussed in the conclusions.
Źródło:
Combustion Engines; 2019, 58, 3; 213-217
2300-9896
2658-1442
Pojawia się w:
Combustion Engines
Dostawca treści:
Biblioteka Nauki
Artykuł
    Wyświetlanie 1-5 z 5

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