Temat: piston combustion engine - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Analysis of the wear of piston rings prototype in terms of team endurance test
Autorzy:: Kaźmierczak, A.
Dudziński, W.
Kaźmierczak, Ł.
Powiązania:: https://bibliotekanauki.pl/articles/245677.pdf
Data publikacji:: 2013
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: combustion engine
piston ring
wear
Opis:: The article discusses the results of the wear of piston rings for internal combustion engines with self ignition. The research was a prototype multilayer ring sealing of the porous coating and the so-called chromium embankment diamonds [2]. Technology of the rings is the deposition of multilayer coatings in the process of chromium plating. In times of chromium deposited from the bath particles are technical diamond's shape, and granulation. This technology is a response to domestic factory piston rings to the needs of the automotive market and is an innovative development. Conducted engine tests consisted of a 50-hour cycle and to hour break-in team life cycle, which was repeated 150 times. Thus the total duration of sample equal to 200 hours. Cycle life is a team containing a phase-hour cycle engine traffic load at maximum speed and maximum torque and maximum power of the tween partial load and idling. This cycle is repeated in the 200-hour test 150 times. During the measurement of key indicators were measured at the engine, the fuel consumption, coolant temperature and pressure of the lubricating oil. In order to calculate the wear of piston rings, the difference was calculated to measure the thickness and height before and after sample of 200 hours. In a similar way as the use of thickness and height of the rings was calculated by weight loss.
Źródło:: Journal of KONES; 2013, 20, 2; 181-187
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 2.

Tytuł:: Analysis of the wear of piston ring prototype of an embankment of diamond in terms endurance test
Autorzy:: Kaźmierczak, A.
Kaźmierczak, Ł.
Powiązania:: https://bibliotekanauki.pl/articles/242911.pdf
Data publikacji:: 2012
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: combustion engine
piston ring
wear
Opis:: The article discusses the results of the wear of piston rings for internal combustion engines with spark ignition. The research was a prototype multilayer ring sealing of the porous coating and the so-called chromium embankment diamonds. Technology of the rings is the deposition of multilayer coatings in the process of chromium plating. In times of chromium deposited from the bath, particles are technical diamond's shape, and granulation. This technology is a response to domestic factory piston rings to the needs of the automotive market and is an innovative development. Conducted engine tests consisted of a 50-hour cycle and to hour break-in team life cycle, which was repeated 150 times. Thus, the total duration of sample equal to 200 hours. Cycle life is a team containing a phase-hour cycle engine traffic load at maximum speed and maximum torque and maximum power of the tween partial load and idling. This cycle is repeated in the 200-hour test 150 times. During the measurement of key indicators were measured at the engine, the fuel consumption, coolant temperature and pressure of the lubricating oil. In order to calculate the wear of piston rings, the difference was calculated to measure the thickness and height before and after sample of 200 hours. In a similar way as the use of thickness and height of the rings was calculated by weight loss.
Źródło:: Journal of KONES; 2012, 19, 4; 283-289
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 3.

Tytuł:: Geometric shape of the support surface of the piston
Autorzy:: Iskra, A.
Babiak, M.
Wróblewski, E.
Powiązania:: https://bibliotekanauki.pl/articles/243151.pdf
Data publikacji:: 2015
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: combustion engine
piston
friction losses
Opis:: Geometry of the slot between piston bearing surface and cylinder bore affects the friction losses of the IC engine to the far extent. It appears that these losses depend more on the area covered with oil than the thickness of oil layer separating collaborating parts. Barrel-shaped or stepwise piston bearing surface is the way to reduce the oil-covered area. The first concept has been used for years while the stepwise profile has not been applied for various reasons, although this idea providing higher load capacity of oil layer in stepwise slot was published in literature in the fifties of twentieth century. The stepwise profile can be obtained covering the cylindrical or tapered piston-bearing surface with a thin layer graphite. This paper presents the results of simulation leading to the reduction in friction losses and abrasive wear of piston bearing surface and cylinder bore. Covering the piston bearing surface with a thin layer of graphite one can get an extremely advantageous tribological properties of the piston assembly which means the expected parameters of oil film and in a case of film rupture – an ignorable abrasive wear of the graphite layer and/or cylinder bore.
Źródło:: Journal of KONES; 2015, 22, 4; 95-101
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 4.

Tytuł:: The impact of microgeometry bearing surface of the piston on the parameters of oil film
Autorzy:: Wróblewski, E.
Iskra, A.
Babiak, M.
Powiązania:: https://bibliotekanauki.pl/articles/242986.pdf
Data publikacji:: 2016
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: combustion engine
piston
friction losses
Opis:: The formation of oil film is possible under certain parameters of microgeometry cooperating components the main node of the internal combustion engine, which is a piston-pin-piston rings. In addition, this node is primarily responsible for the formation of mechanical losses. It is advisable to reduce friction losses in the piston-cylinder group lead to an increase in the overall efficiency of the engine and thus reduce the fuel consumption. One way of achieving these objectives is modification of microgeometry of the piston-bearing surface, which cooperates with the cylinder wall. The geometry of the gap between the piston skirt and the cylinder liner greatly affects the friction loss inside the engine. This means that the friction loss is much more affected by the area covered by the oil film separating the mating elements than its thickness. The method to reduce the area covered by the oil film is a modification of the bearing surface of the piston by adjusting the profile. The supporting surface, which performs a reciprocating motion relative to the strokes of the cylinder liner ensure the continuity of the oil film with the smallest possible value of the friction losses at the node piston-cylinder. This paper presents the results of simulation leading which aim to determining the parameters oil film on the friction loss for the modified bearing surface of the piston.
Źródło:: Journal of KONES; 2016, 23, 2; 431-436
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 5.

Tytuł:: Engine researches on the influence of the piston ring insert on temperature distribution in piston
Autorzy:: Stężycki, P.
Kowalski, M.
Jankowski, A.
Powiązania:: https://bibliotekanauki.pl/articles/949512.pdf
Data publikacji:: 2018
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: combustion engine
engine piston
piston ring insert
electromagnetic induction
temperature measurement
thermistor
Opis:: The article presents a method of piston temperature measurement on a running engine using electromagnetic induction for transferring measurement results from a moving measuring system placed in a piston to a stationary system attached to the engine crankcase and to measuring system located outside the engine. Selected test results that were carried out on a single-cylinder Diesel engine are presented. A system consisting of a thermistor and a secondary coil was mounted in the piston. The primary coil was mounted in the crankcase under the cylinder liner of the engine. Engine tests were aimed at determining the influence of the piston ring insert on the temperature distribution in the piston. Temperature measurements in the piston without the ring insert were carried out for comparison. In both cases, the pistons had the same geometrical dimensions. The tests were carried out in conditions of external characteristics (the maximum load as a function of engine speed) and load characteristics (load changes at constant engine speed). The test results in the form of the temperature difference between the temperature of piston top and the temperature under the top compression ring indicate that the ring insert is a barrier to the heat flow from the piston to the engine cooling system. In addition, the results of the piston temperature measurements during the step change of the engine speed and its load to the nominal value are presented.
Źródło:: Journal of KONES; 2018, 25, 4; 563-570
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 6.

Tytuł:: Investigation of friction loss in internal combustion engine of experimental microgeometry piston bearing surface
Autorzy:: Wróblewski, E.
Finke, S.
Babiak, M.
Powiązania:: https://bibliotekanauki.pl/articles/244305.pdf
Data publikacji:: 2017
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: combustion engine
friction
lubrication
piston
microgeometry bearing surface
Opis:: The piston is the most mechanically and thermally loaded engine component. The energy required to overcome the mechanical losses in the combustion engine is approx. 10% of the energy supplied to the engine in a fuel. The main node piston-pin-piston rings are most responsible for the formation of mechanical losses. It is advisable to reduce friction losses in the piston-cylinder group lead to an increase in the overall efficiency of the engine and thus reduce the fuel consumption. The way of achieving these objectives is modification of microgeometry of the pistonbearing surface, which cooperates with the cylinder wall. The geometry of the gap between the piston skirt and the cylinder liner greatly affects the friction loss inside combustion engine. A way to reduce the area covered by the oil film is the application of a stepped profile of the piston skirt. The stepwise profile can be obtained covering the cylindrical or tapered piston-bearing surface with a thin layer graphite. Covering the piston bearing surface with a thin layer of graphite one can get an extremely advantageous tribological properties of the piston assembly which means the expected parameters of oil film and reduction friction loss. In this article, the results of research on experimental pistons on friction loss in combustion engine are presented.
Źródło:: Journal of KONES; 2017, 24, 2; 307-313
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 7.

Tytuł:: How the wear of cylinder liner affects the cooperation of piston - cylinder assembly of IC engine
Autorzy:: Serdecki, W.
Krzymień, P.
Powiązania:: https://bibliotekanauki.pl/articles/248040.pdf
Data publikacji:: 2012
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: combustion engine
piston ring
blow-by
torque instability
Opis:: A ring pack of modern IC engine consists of at least one compression ring that should guarantee secure a necessary tightness of combustion chamber. A circumferential wall pressure of correctly designed compression ring should be sufficient to achieve a full contact between wall and ring, which means light tightness preventing gas blowby. Lack of tightness is being considered as a principal cause of deterioration of engine performance data including torque instability, and a rapid grow in ring and cylinder wear within the area of blow-by. During engine design process mathematical models are applied which implement analytical and numerical methods of calculation. Analytical methods that were used earlier presented a limited range of application and lower accuracy in comparison to the numerical methods but they allowed achieving approximate results quicker. Taking this into consideration the presented study describes the most important relations between ring geometry and its wall pressure, which were obtained using the analytical methods. Presented formulas facilitate the evaluation of cylinder wear effect on the ring circumferential pressure distribution, especially the change in liner diameter. An attempt of light slits evaluation has been performed as well. The study was supplemented with graphs and calculative example.
Źródło:: Journal of KONES; 2012, 19, 1; 357-363
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 8.

Tytuł:: Effect of friction force determination method on results obtained from model of gas flow from combustion chamber to the crankcase
Autorzy:: Koszałka, G.
Niewczas, A.
Guzik, M.
Powiązania:: https://bibliotekanauki.pl/articles/245664.pdf
Data publikacji:: 2009
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: combustion engine
blowby
piston ring
friction force
mathematical model
Opis:: The paper presents investigation of the influence of the friction force calculation method on the results of simulations run with the use of the model ofgas flow from the combustion chamber to the crankcase and piston rings motion in the grooves. The first series of simulations was run using the gas flow and ring motion model in which the friction force was calculated from the empirical equation. The second series was run with the use of the gas flow and ring motion model fully integrated with the ring lubrication model. In that case the friction force was derived from the hydrodynamic model of ring lubrication. Comparison of the results obtained in the first and second series of simulations indicated that despite the fact that the friction forces calculated with these two methods differed considerably, the method of friction force calculation had insignificant effect. This refers to the ąuantities determined in the simulations which are most important from practical point of view - i.e. displacements of the rings in the grooves, pressure courses in inter-ring regions and blowby rate. It is not necessary to integrate the gas flow and ring motion model with the model of ring lubrication, and doing so to complicate it very much, if the aim of the calculations is simulation of blowby and rings behaviour in the grooves.
Źródło:: Journal of KONES; 2009, 16, 4; 223-239
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 9.

Tytuł:: Dependence of piston ring parameters determination accuracy on the method of calculation
Autorzy:: Serdecki, W.
Krzymień, P.
Powiązania:: https://bibliotekanauki.pl/articles/247098.pdf
Data publikacji:: 2011
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: combustion engine
piston ring
ring geometry
ring pressure
simulation
Opis:: Mathematical models are commonly used at the stage of piston ring design and during examination of ring collaboration with liner surface. Both analytical and numerical methods are used for development of such models. In the case of models based on analytical methods the range of their application is usually limited only to selected cases while the use of numerical methods allow to widen the range of their applications but their accuracy depends on increment used. The paper presents a procedure of verification of the piston ring mathematical model constructed by the authors using numerical methods. Conformity between the results obtained using this program and the results of analytical calculations concerning the displacement of ring free ends brought about by the acting loads was the aim of the analysis. Exemplary computations were carried out for three compression rings of different geometry. Regarding the conformity of achieved results as satisfactory for practical use probable causes of observed discrepancies were pointed out. Relations between energy accumulated in curved bar and loading force (according to the Castiliano's theorem) were used in a course of calculations. Exemplary calculations were carried out for compression rings of three types engine, i.e. automotive, bulldozer and marine ones. A probable cause of differences between results of calculations carried out according to various analytical methods have been pointed out assuming their accuracy as satisfactory for practical purposes.
Źródło:: Journal of KONES; 2011, 18, 4; 435-441
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 10.

Tytuł:: Geometry of the improved layer over a piston skirt
Geometria warstwy uszlachetniającej na powierzchni bocznej tłoka
Autorzy:: Iskra, A.
Krzymień, P.
Wróblewski, E.
Powiązania:: https://bibliotekanauki.pl/articles/134069.pdf
Data publikacji:: 2015
Wydawca:: Polskie Towarzystwo Naukowe Silników Spalinowych
Tematy:: combustion engine
piston
CNT
silnik spalinowy
tłok
nanorurki węglowe
Opis:: Geometry of the slot between piston skirt and cylinder bore affects the friction losses of the IC engine to the far extent. It appears that these losses depend more on the area covered with oil than the thickness of oil layer separating collaborating parts. Barrel-shaped or stepwise piston skirt is the way to reduce the oil covered area. The first concept has been used for years while the stepwise profile has not been applied for various reasons, although this idea providing higher load capacity of oil layer in stepwise slot was published in literature in the fifties of twentieth century. The stepwise profile can be obtained covering the cylindrical or taper piston skirt with a thin layer of carbon nanotubes (CNT). This paper presents the results of simulation and test stand investigations leading to the reduction in friction losses and abrasive wear of piston skirt and cylinder bore. Covering the piston skirt with a thin layer of CNT one can get an extremely advantageous tribological properties of the piston assembly which means the expected parameters of oil film and in a case of film rupture – an ignorable abrasive wear of the CNT layer and/or cylinder bore.
Geometria szczeliny między powierzchnią boczną tłoka a cylindrem w bardzo dużym stopniu wpływa na straty tarcia w silniku spalinowym. Okazuje się, że na wymienione straty w większym stopniu wpływa obszar pokryty filmem olejowym niż grubość filmu olejowego rozdzielającego współpracujące elementy. Drogą do zmniejszenia obszaru pokrytego filmem olejowym jest baryłkowy lub schodkowy kształt powierzchni bocznej tłoka. Pierwszy sposób stosowany jest od dawna, natomiast kształt schodkowy z różnych powodów nie był dotychczas stosowany, chociaż publikacje o największej nośności filmu olejowego utworzonego w szczelinie schodkowej ukazały się jeszcze w latach pięćdziesiątych dwudziestego wieku. Kształt schodkowy szczeliny można uzyskać nanosząc cienką warstwę nanorurek węglowych (CNT) na cylindryczną lub stożkową powierzchnię boczną tłoka. W artykule przedstawiono wyniki badań stanowiskowych i symulacyjnych zmierzających do redukcji strat tarcia i zużycia ściernego powierzchni bocznej tłoka i gładzi cylindra. Syntetyzując na powierzchni bocznej tłoka cienką warstwę CNT uzyskuje się bardzo dobre właściwości trybologiczne pary kinematycznej, jaką stanowi zespół tłok – cylinder, co oznacza oczekiwane parametry filmu olejowego, a w przypadku jego braku, prowadzącego do bezpośredniego kontaktu mikro-nierówności tłoka i cylindra - pomijalne zużycie ścierne warstwy CNT i/lub gładzi cylindra.
Źródło:: Combustion Engines; 2015, 54, 3; 192-196
2300-9896
2658-1442
Pojawia się w:: Combustion Engines
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 11.

Tytuł:: Analysis and research of piston working conditions of combustion engine in high thermal load conditions
Autorzy:: Jankowska-Sieminska, B.
Jankowski, A.
Slezak, M.
Powiązania:: https://bibliotekanauki.pl/articles/243400.pdf
Data publikacji:: 2007
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: combustion engine
piston
thermal load
thermal expansion
thermal shock
Opis:: Explanation of phenomena occurring in pistons of combustion engines which appear during heating and cooling processes in reference to standard materials and composite materials of high material proprieties is aim of the paper. Bring over researches were mostly directed on measurements of difference dimensions which appear during the piston work in the combustion engine. The paper concentrates on phenomenon of different proprieties of materials. The thermal stresses and shocks differ. In the thermal shock, thermal stresses are caused by instantaneous temperature gradients which appear at high engine speed. These stresses are determined thro temperature distribution and they do not differ from stresses in steady-state conditions. Researches concerning thermal expansions were performed by means of sensitive dilatometer which can work in simple and differential system. Changes of dimensions versus temperature function were measured with inductive sensor and the sensitive Pt-ptrh thermocouple, and results were referred to reference material-Platinum. Research results are illustrated on diagrams of different courses of changes of the of thermal expansion coefficient during heating and cooling of standard and composite materials. Values of the thermal expansion coefficient a for the heating and cooling are smaller for composite alloys. The course of the coefficient â during cooling can be higher or lower from the coefficient a during heating. Similar values were also received. Maximum differences were of 10%. Smaller values of the coefficient a for composite alloys cause that for such the same thermal loads temperature gradients will be smaller for composite alloys. Courses of changes of the coefficient â have a different characteristics suited from chemical composition of alloy, granularity of the composite component and thermal treatment.
Źródło:: Journal of KONES; 2007, 14, 3; 233-243
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 12.

Tytuł:: O możliwości pomiaru temperatur tłoka
Possibilities of piston temperature measurements
Autorzy:: Mitukiewicz, G.
Sygniewicz, J.
Powiązania:: https://bibliotekanauki.pl/articles/263398.pdf
Data publikacji:: 2007
Wydawca:: Sieć Badawcza Łukasiewicz. Przemysłowy Instytut Motoryzacji
Tematy:: pomiar
silnik spalinowy
temperatura
tłok
combustion engine
measurements
piston
temperature
Opis:: spalinowego jest bardzo istotna. Można go uzyskać, między innymi, na drodze eksperymentalnej. Pole temperatur tłoka, ze względu na warunki jego pracy jest bardzo zróżnicowane. W warunkach ustalonej pracy silnika temperatura maksymalna tłoka sięga 670K od strony komory spalania i spada aż do 390K od strony skrzyni korbowej. Ponieważ pomiar temperatury tłoka jest dokonywany w ograniczonej liczbie punktów pomiarowych, w których temperatura nie musi osiągać wartości ekstremalnych, otrzymuje się przybliżony obraz rozkładu temperatur i jej gradientów. Dobór aparatury badawczej, jak również sposobu przekazywania sygnału jest niezwykle ważny do precyzyjnego wykonania pomiarów. W artykule tym przedstawiono rodzaje czujników pomiarowych, które stosowane są w doświadczalnym wyznaczaniu temperatury tłoka. Należą do nich: (możliwości) wyprowadzania sygnału pomiarowego na zewnątrz silnika, z podziałem na mechaniczne (ciągłe i stykowe) i telemetryczne.
Estimation of temperature distribution of piston, one of the most important parts of the internal combustion engine is of fundamental importance. It can be done in an experimental way. Piston temperature depends on the engine operation conditions and varies significantly. At the stationary conditions, piston temperature reaches 670K on the combustion chamber side and drops down to 390K on the inner side of piston body. Because the measurement of piston temperature is done in limited measurement points, we get only an approximate field of temperature distribution and its gradients. Selection of research equipment and the way of signal transmission are very important to get the right results. The paper describes types of measurement sensors, which can be used to determine the piston temperature in an experimental way: termoelements, thermistors, pyrometers and others. In the second part, transmission of measurement signal outside the engine is shown. There are described mechanical continuous and periodical) and telemetrical methods.
Źródło:: Archiwum Motoryzacji; 2007, 4; 331-348
1234-754X
2084-476X
Pojawia się w:: Archiwum Motoryzacji
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 13.

Tytuł:: Thermal deformations of the SW680 engine piston depending on the applied combustion chamber shape
Odkształcenia cieplne tłoka silnika sw680 w zależności od kształtu zastosowanej komory spalania
Autorzy:: Mitukiewicz, G.
Sygniewicz, J.
Powiązania:: https://bibliotekanauki.pl/articles/243030.pdf
Data publikacji:: 2007
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: silnik spalinowy
tłok
odkształcenia termiczne
komora spalania
combustion engine
piston
thermal deformations
combustion chamber
Opis:: The paper describes simulation model of thermal deformations of piston of Diesel engine with combustion chamber placed in piston crown. Results for different shapes of combustion chamber are presented and analyzed. For calculations assumed that thermal deformation of piston do not vary within engine 's cycle if it works in constant conditions. An hand of pressure and temperature charts of SW680 engine, heat transfer coefficient on piston crown surface was defined. Heat transfer coefficient on the rest piston surfaces was defined based on the literature. Using finite element method (FEM) code, piston shape was created, and then the piston body was meshed and loaded according to Fourier conditions. Nodes displacements let describe piston deformation. The simulation results allow to find the optimal shape of combustion chamber, in respect of piston deformation, and also can be the base to create the method of fast verify combustion chamber shape. Results simulation research of piston deformations showed that piston deformations were considerably dependent from combustion chamber shape . The biggest deformations came out for the chamber of small depth and the high diameter. Differences of thermal deformations of piston skirt reach to 50 mi m
W artykule przedstawiono model obliczeniowy odkształceń cieplnych tłoka silnika o zapłonie samoczynnym z komorą spalania umieszczoną w jego denku, oraz wyniki obliczeń dla różnych kształtów komory spalania wraz z ich analizą. Do obliczeń przyjęto, że odkształcenia cieplne tłoka są stałe w całym cyklu pracy silnika jeżeli pracuje on w ustalonych warunkach. Na podstawie wykresu indykatorowego silnika SW680 określono współczynnik przejmowania ciepła na powierzchni denka tłoka ALFA 0. Współczynniki przejmowania ciepła na pozostałych powierzchniach tłoka zostały przyjęte na podstawie zależności podanych w literaturze. Za pomocą programu komputerowego wykorzystującego metodę elementów skończonych (MES) zamodelowano tłok, a następnie dyskretyzowano jego objętość elementami przestrzennymi obciążonymi cieplnie przy wykorzystaniu warunków brzegowych trzeciego rodzaju (Fouriera). Wyznaczenie przesunięcia węzłów siatki pozwoliło na określenie odkształceń tłoka. Uzyskane wyniki obliczeń mogą stanowić punkt wyjścia do wyznaczenia optymalnego pod względem odkształceń cieplnych kształtu komory spalania a także być podstawą do stworzenia metody umożliwiającej szybką weryfikację przyjętego kształtu komory spalania. Wyniki badań symulacyjnych odkształceń tłoka, wskazały, że odkształcenia tłoka są w znacznym stopniu zależne od kształtu komory spalania. Największe odkształcenia wystąpiły dla komory o małej głębokości i dużej średnicy. Różnice odkształceń cieplnych części prowadzącej tłoka sięgają do 50mi m.
Źródło:: Journal of KONES; 2007, 14, 2; 327-334
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 14.

Tytuł:: Analiza ruchów pierścieni uszczelniających w aspekcie zachowania szczelności złożenia tłok : pierścienie : cylinder
Analysis of the movement of the sealing rings in terms of preserving the tightness of the piston : ring : cylinder assembly
Autorzy:: Abramek, K. F.
Klyus, O.
Powiązania:: https://bibliotekanauki.pl/articles/314856.pdf
Data publikacji:: 2017
Wydawca:: Instytut Naukowo-Wydawniczy "SPATIUM"
Tematy:: tłok
pierścienie
przedmuchy gazów
silnik spalinowy
piston
rings
blow-by
combustion engine
Opis:: Tematyka publikacji dotyczy zagadnień i badań związanych ze zjawiskiem strat ładunku w postaci przedmuchów gazów do skrzyni korbowej przez układ tłok – pierścienie – cylinder (TPC) silników spalinowych. Analizowany problem dotyczy oceny możliwości ruchów i przemieszczeń pierścieni uszczelniających, co w największym stopniu wpływa na wartość natężenia przedmuchów. W wyniku przeprowadzonych badań silników zauważono, że zjawisko przedmuchów zależy od wielu parametrów konstrukcyjnych, jak i eksploatacyjnych tłokowego silnika spaliowego. Przeprowadzony zakres badań potwierdził wpływ tych parametrów na ruchy pierścieni i na zjawisko przedmuchów.
The subject of the publication concerns issues and research related to the phenomenon of cargo losses in the form of gusts of crankcase gases through the piston-ring-cylinder (PRC) of internal combustion engines. The analyzed problem concerns the evaluation of the movement and displacement of the sealing rings, which has the greatest effect on the purge rate. As a result of engine tests, it has been observed that the blow-by phenomenon is influenced by many constructional and operational parameters of the piston-type combustion engine. The scope of the study confirmed the influence of these parameters on the ring motions and on the blow-by phenomenon.
Źródło:: Autobusy : technika, eksploatacja, systemy transportowe; 2017, 18, 7-8; 143-147
1509-5878
2450-7725
Pojawia się w:: Autobusy : technika, eksploatacja, systemy transportowe
Dostawca treści:: Biblioteka Nauki

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Tytuł:: Finite element analysis of a composite piston for a diesel aircraft engine
Autorzy:: Pietrykowski, Konrad
Magryta, Paweł
Skiba, Krzysztof
Powiązania:: https://bibliotekanauki.pl/articles/133234.pdf
Data publikacji:: 2019
Wydawca:: Polskie Towarzystwo Naukowe Silników Spalinowych
Tematy:: piston
combustion engine
FEM
thermal
mechanical loads
tłok
silnik spalinowy
obciążenia mechaniczne
Opis:: The article presents calculations of thermal and mechanical loads of the piston, consisting of two parts: steel and aluminum. The calculations were made using FEM in the Abaqus software. The piston is characterized by a split construction and was equipped with a cooling oil channel. The piston will be used in an aircraft diesel engine characterized by opposite piston movement. The presented geometry of the piston is the next of the ones being developed earlier and contains preliminary assumptions as to the size and main geometrical dimensions. The thermal boundary conditions of the simulation tests assumed defined areas of heat reception surface and heating of the piston by defining a temperature map on its crown. The results of these studies were presented in the form of temperature distribution and heat flux on the surface of the tested element. The strength boundary conditions assumed a mechanical load in the form of pressure resulting from the pressure in the combustion chamber applied to the piston crown surface and the opposite pressure defined on the support at the surface of contact between the piston and the piston pin. The results of these tests were presented in the form of stress distribution on the surface of the tested element. As a result of the analyses carried out, the results constituting the basis for further modernization of the piston geometry were obtained.
Źródło:: Combustion Engines; 2019, 58, 4; 107-111
2300-9896
2658-1442
Pojawia się w:: Combustion Engines
Dostawca treści:: Biblioteka Nauki

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