WO2012120037A2 - Zweitaktmotor mit einem schalldämpfer - Google Patents
Zweitaktmotor mit einem schalldämpfer Download PDFInfo
- Publication number
- WO2012120037A2 WO2012120037A2 PCT/EP2012/053901 EP2012053901W WO2012120037A2 WO 2012120037 A2 WO2012120037 A2 WO 2012120037A2 EP 2012053901 W EP2012053901 W EP 2012053901W WO 2012120037 A2 WO2012120037 A2 WO 2012120037A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- chamber
- combustion chamber
- muffler
- exhaust gas
- flow channel
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 claims abstract description 167
- 239000000203 mixture Substances 0.000 claims abstract description 61
- 238000012423 maintenance Methods 0.000 claims abstract description 6
- 230000003584 silencer Effects 0.000 claims description 44
- 230000015572 biosynthetic process Effects 0.000 claims description 8
- 238000013461 design Methods 0.000 claims description 8
- 238000011017 operating method Methods 0.000 claims description 5
- 238000006073 displacement reaction Methods 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 4
- 229910001220 stainless steel Inorganic materials 0.000 claims description 2
- 239000010935 stainless steel Substances 0.000 claims description 2
- 238000012546 transfer Methods 0.000 abstract description 2
- 239000000446 fuel Substances 0.000 description 10
- 230000009467 reduction Effects 0.000 description 9
- 238000010586 diagram Methods 0.000 description 4
- 230000004888 barrier function Effects 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- 230000002349 favourable effect Effects 0.000 description 3
- 230000010355 oscillation Effects 0.000 description 3
- 230000001419 dependent effect Effects 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005284 excitation Effects 0.000 description 2
- 230000003993 interaction Effects 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 238000005457 optimization Methods 0.000 description 2
- 230000010349 pulsation Effects 0.000 description 2
- 238000012549 training Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N5/00—Exhaust or silencing apparatus combined or associated with devices profiting by exhaust energy
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N1/00—Silencing apparatus characterised by method of silencing
- F01N1/08—Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling
- F01N1/089—Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling using two or more expansion chambers in series
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B27/00—Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
- F02B27/04—Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues in exhaust systems only, e.g. for sucking-off combustion gases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2490/00—Structure, disposition or shape of gas-chambers
- F01N2490/02—Two or more expansion chambers in series connected by means of tubes
- F01N2490/04—Two or more expansion chambers in series connected by means of tubes the gases flowing longitudinally from inlet to outlet only in one direction
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2490/00—Structure, disposition or shape of gas-chambers
- F01N2490/16—Chambers with particular shapes, e.g. spherical
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2590/00—Exhaust or silencing apparatus adapted to particular use, e.g. for military applications, airplanes, submarines
- F01N2590/06—Exhaust or silencing apparatus adapted to particular use, e.g. for military applications, airplanes, submarines for hand-held tools or portables devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B2700/00—Measures relating to the combustion process without indication of the kind of fuel or with more than one fuel
- F02B2700/03—Two stroke engines
- F02B2700/037—Scavenging or charging channels or openings
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the present invention relates to a two-stroke engine with a silencer for an engine working device, in particular for a hand-operated engine tool, such as a garden and green area maintenance device, a hand tool such as a chainsaw, a circular saw or a power cutter or for a moped, a boat engine and the like, wherein the muffler a silencer inlet, to which a flow channel connects, so that the flow channel can be attached by means of the silencer inlet to an outlet of a combustion chamber of the two-stroke engine, and wherein at least one overflow opens into the combustion chamber, enters via the fuel-air mixture into the combustion chamber, if a piston movably bounding the combustion chamber is located in the area of bottom dead center, wherein the flow channel opens into a first chamber at the end opposite the silencer inlet, wherein a second chamber is further provided, into which Exhaust gas flows through a branched off from the flow channel main outlet and from the exhaust gas flows through an outlet, wherein the flow channel between the silence
- the two-stroke engine is shown in simplified form and arranged at the outlet of the two-stroke engine, so that the burned in the combustion chamber of the two-stroke engine air-fuel mixture can enter the muffler.
- the exhaust gas enters a flow channel of the muffler, via which the muffler is mounted by means of the muffler inlet on the cylinder of the two-stroke engine.
- the flow channel connects as a straight pipe formed, which opens into a first chamber via a channel end.
- a main outlet is arranged on the flow channel, and exhaust gas can pass through the main outlet from the flow channel into a second chamber, and leave the second chamber via an outlet and go outside.
- the flow channel is currently running, so that the exhaust gas flowing into the flow channel via the muffler inlet initially favors at least predominantly into the first chamber and forms an overpressure in the first chamber. Due to its overpressure, a large part of the exhaust gas flows back toward the muffler inlet or even into the combustion chamber and forms a gas barrier which prevents the fuel-air mixture, which has been reloaded through the overflow channel into the combustion chamber of the cylinder, from entering the muffler unburnt or already in the muffler the muffler entered fuel-air mixture can be returned by the backflowing exhaust gas back into the combustion chamber.
- the geometric design of the flow channel and the volume of the first chamber are determined such that a flow behavior of the exhaust gas in the flow channel and the first chamber is formed, which corresponds to the stroke of the piston and the opening of the outlet of the combustion chamber in the region of the bottom dead center of the piston.
- a flow behavior of the exhaust gas in the flow channel and the first chamber is formed, which corresponds to the stroke of the piston and the opening of the outlet of the combustion chamber in the region of the bottom dead center of the piston.
- the muffler of interest here allows a backflow of the exhaust gas in the direction of the outlet of the combustion chamber.
- the objective is pursued that the exhaust gas from the first chamber in the direction of the silencer inlet forms the back pressure at a time while the outlet of the combustion chamber is open, namely when the piston passes through the area of bottom dead center. Only then can be pushed back into the combustion chamber of the two-stroke engine already entered into the flow channel fuel-air mixture, so briefly after emptying of the combustion chamber by outflow of exhaust gas into the muffler again a pressure increase is generated in the combustion chamber, which is generated by the flowing back into the combustion chamber exhaust gas.
- the fuel-air mixture first passes through an inlet into the crankcase of the two-stroke engine, and in the crankcase, the fuel-air mixture is pre-compressed by the downward movement of the piston.
- the piston of the overflow which opens into the combustion chamber, released, and the fuel-air mixture flows through the overflow from the crankcase into the combustion chamber.
- a flow behavior of the fuel-air mixture through the overflow into the combustion chamber occur, which can enter an excessive amount of fuel-air mixture in the combustion chamber of the two-stroke engine.
- the amount of fuel-air mixture that passes through the overflow into the combustion chamber in addition to the pressure of the fuel-air mixture in the crankcase of the two-stroke engine and the geometric design of the flow channel further determined by the timing, opened by the overflow by the movement of the piston and closed.
- the overflow channel can be open over a crank angle of up to 100 ° crank angle, and the overflow is open at the bottom dead center of the piston maximum.
- the overflow channel can open into the combustion chamber with a relatively large cross-sectional area, which in particular has an advantageous flow behavior of the Fuel-air mixture in the combustion chamber favors.
- the disadvantage of an excessive amount of fuel / air mixture introduced into the combustion chamber can arise.
- the flow channel is currently running, so that the exhaust gas flowing into the flow channel via the muffler inlet initially favors at least predominantly into the first chamber and forms an overpressure in the first chamber. Due to this overpressure, a large part of the exhaust gas flows back towards the muffler inlet and forms a gas barrier, which prevents that in the combustion chamber of the cylinder recharged fuel-air mixture unburned enters the muffler or already entered into the muffler fuel-air mixture can through the backflowing exhaust gas are transported back into the combustion chamber.
- the geometric design of the flow channel and the volume of the first chamber are determined such that a flow behavior of the exhaust gas in the flow channel and the first chamber is formed with the stroke of the piston and the opening of the outlet of the combustion chamber when passing through the range of the bottom dead center of the piston corresponds.
- a flow behavior of the exhaust gas in the flow channel and the first chamber is formed with the stroke of the piston and the opening of the outlet of the combustion chamber when passing through the range of the bottom dead center of the piston corresponds.
- the aim is basically that the exhaust gas forms a counter-pressure from the first chamber in the direction of the silencer inlet at the correct time, while the outlet of the combustion chamber is in the area of the bottom dead center the piston is still open. Furthermore, the objective is pursued that the backflowing exhaust gas forms a pressure at the correct level so that the exhaust gas does not return back into the combustion chamber, however, the pressure should be determined such that the escape of unburned fuel-air mixture from the combustion chamber in the muffler is effectively avoided. It is known that this optimization with the Length of the flow channel and the first chamber, but also by the volume of the first chamber, can be achieved.
- a muffler has the task of effectively attenuating the noise arising from the combustion chamber when the exhaust gas exits.
- a particularly good damping is achieved when the exhaust gas has the lowest possible pressure fluctuations at the outlet of the muffler.
- This optimization goes hand in hand with the desire for a particular sound image of the engine tool, but also the goal is to be able to use certain materials for the construction of silencers.
- a large total volume of the muffler affects the two-stroke engine rather at low speeds, a smaller total volume of the muffler affects the two-stroke engine rather at higher speeds.
- the muffler noise is thereby influenced by the prevailing in the muffler pressure oscillations.
- Another object of the present invention is to influence the pressure fluctuations of the exhaust gas on leaving the muffler by adapting the volumes involved in the muffler accordingly. In particular, it is the object of the present invention to achieve the greatest possible noise reduction of the operation of the two-stroke engine.
- the invention includes the technical teaching that the formation of the back pressure of the exhaust gas takes place in a time range in which the outlet is released by the piston and the fuel-air mixture has at least predominantly passed through the at least one overflow into the combustion chamber.
- the invention is based on the idea that the outflow behavior of the fuel-air mixture from the transfer ports into the combustion chamber is influenced by the backpressure of the exhaust gas, which exhaust gas from the muffler in the direction of the combustion chamber, that is also partially into the combustion chamber, flows back.
- the geometric design of the at least one overflow channel can be such that the formation of the back pressure of the exhaust gas takes place in the required time range, in which the or the overflow to the combustion chamber is still released by the piston.
- the geometric design of the or overflow channels determines the timing to the opening, and the overflow forms with the piston a kind sliding valve, and the overflow is released when the piston passes through the area of the bottom dead center.
- the cross-sectional height of the or the overflow window, with which the overflow channel opens into the combustion chamber and which corresponds to the piston stroke direction, forms the appropriate size for determining the timing.
- a large cross-sectional height of the overflow window causes a long opening time of the overflow window, and according to the invention the overflow window of the overflow is designed so that the overflow at least partially or already open when the back pressure of the exhaust gas from the muffler before or even forms in the combustion chamber.
- At least the flow channel and the first chamber may be formed such that the formation of the back pressure by the exhaust gas takes place in the required time range in which the overflow is released to the combustion chamber through the piston.
- the exhaust gas Will the outlet of the Open combustion chamber toward the muffler by the downward movement of the piston, the exhaust gas enters the flow channel and at least predominantly in the first chamber, and flows after filling the first chamber through the flow channel back to the outlet of the combustion chamber or even into the combustion chamber.
- the flow time is influenced in particular by the length, but also by the cross-sectional area of the flow channel, furthermore, the flow duration is influenced by the volume of the first chamber, so that at least the flow channel and / or the first chamber can be designed so that the necessary flow duration is reached becomes.
- the ratio of the volume of the first chamber to the displacement of the two-stroke engine can be 1/4 to 2.
- the volume of the first chamber to the total volume of the muffler, formed by the absolute volume of the second chamber be 1/40 to 1/2. With even greater advantage, the ratio of the volume of the second chamber to the displacement volume can be 4 to 10.
- the ratio of the numerical value of the total length of the flow channel and the depth of the first chamber in centimeters to the numerical value of the stroke volume of the two-stroke engine in cubic centimeters can be 0.15 to 0.35, in particular less than 0.15 to 0.35.
- the backpressure of the exhaust gas at the time and / or in its height can be determined such that the outflow behavior, in particular the amount of the fuel-air mixture entering through the overflow channel into the combustion chamber can be influenced, in particular reduced.
- the fuel-air mixture can shoot into the combustion chamber in a preferred direction, wherein it should be avoided that this preferred direction points in the direction of the outlet of the combustion chamber in the muffler.
- the outlet can be arranged in a position opposite to the overflow channel on the cylinder.
- the counterpressure of the exhaust gas from the muffler influences the amount of fuel / air mixture which is injected into the combustion chamber, in particular it can be reduced. If the exhaust gas escaped through the outlet from the combustion chamber into the muffler, the pressure in the combustion chamber may drop after the exhaust gas has escaped and rise again after the flow time of the exhaust gas flow in the flow channel and the first chamber back into the combustion chamber, whereby the amount of fuel Air mixture can be reduced, which passes through the overflow from the crankcase into the combustion chamber, since the pressure of the exhaust gas forms a back pressure against the fuel-air mixture.
- both the outflow behavior of the fuel-air mixture can be positively influenced by the back pressure of the exhaust gas, and the amount of fuel-air mixture passing through the overflow channel into the combustion chamber can be influenced.
- the outlet of the combustion chamber can open at about 110 ° crank angle, wherein the flow channel and / or the first chamber may be formed such that adjusts a pressure maximum at 140 ° to 160 ° crank angle in the first chamber.
- the exhaust pressure in the combustion chamber initially reaches a minimum, so that then forms an intermediate pressure maximum again by the back pressure of the exhaust gas in the combustion chamber, when the piston is at bottom dead center, which is reached at 180 ° crank angle. Consequently, the maximum pressure in the first chamber is preferably reached at about 30 ° to 40 ° crank angle before the bottom dead center of the piston of the two-stroke engine, and by the backflow of the exhaust gas, this forms a back pressure in the combustion chamber with an intermediate pressure maximum at 180 ° crank angle.
- the object of the present invention is further achieved by an operating method for operating a two-stroke engine of an engine operating unit with a silencer, in particular for a hand-operated engine work tool such as a garden and green area maintenance device, a hand tool such as a chainsaw, a circular saw or a power grinder or for a moped a boat engine and the like, wherein the silencer has a silencer inlet, to which a flow channel adjoins, so that the flow channel is attached by means of the silencer inlet to an outlet of the combustion chamber of the two-stroke engine, and wherein at least one overflow channel opens into the combustion chamber, enters the combustion chamber via the fuel-air mixture when a piston movably bounding the combustion chamber is in the region of the bottom dead center, wherein the flow channel at the end opposite the silencer inlet into a first comb
- a second chamber is provided, in which exhaust gas flows through a branched off from the flow passage main outlet and from which the exhaust gas flows through an outlet, wherein the flow channel between the silence
- the back pressure of the exhaust gas can be formed in a time range in which the piston passes through the bottom dead center, in particular it can be provided that the intermediate pressure of the exhaust gas in the combustion chamber an intermediate pressure maximum is formed when the piston is at bottom dead center. Furthermore, it can be provided that the outflow behavior of the fuel-air mixture from the overflow channel into the combustion chamber is influenced by the backpressure of the exhaust gas, in particular that the amount of the fuel-air mixture entering from the overflow duct into the combustion chamber is reduced by the backpressure of the exhaust gas.
- the invention further includes the technical teaching that the ratio of the volume of the first chamber to the total volume of the muffler is 1/40 to 1/2.
- the invention is based on the idea of optimizing the volumes involved in the muffler such that the best possible noise reduction is achieved during operation of the engine working device. It has been shown that at a volume of the first chamber in relation to the total volume of the muffler from 1/40 to 1/2, the pressure oscillations at the outlet of the muffler particularly strong decrease, so that the noise during operation of the engine working device can be made quieter.
- the ratio of the volume of the first chamber to the total volume of the muffler can be 1/20 to 1/8, whereby particularly good results for noise reduction were achieved.
- the ratio of the volume of the first chamber to the total volume of the muffler may be 1/16 to 1/10, with best results being achieved when the ratio of the volume of the first chamber to the total volume of the muffler is about 1/12.
- the total volume of the muffler may be formed from the volumes of the first chamber, the second chamber and the flow channel.
- the first chamber may be enclosed by the second chamber, further, the second chamber may be formed such that it also encloses at least a part of the flow channel, the first chamber also outside the second chamber may be arranged. Therefore, the total volume of the muffler can be approximated by the volume of the second chamber, and the outlet where the pressure oscillations are to be minimized to achieve the lowest possible level of noise in the operation of the two-stroke engine concerns the outlet through which the exhaust gas the second chamber leaves to the outside.
- the ratio of the volume of the flow channel to the total volume of the muffler may be 1/50 to 1/10.
- To the volume of the flow channel may also be added to the volume of the main outlet.
- the first chamber may also have a secondary outlet through which exhaust gas from the first chamber can flow directly into the second chamber without at least partially flowing through the flow channel again.
- the volume of the secondary outlet can be assigned to the volume of the first chamber, but preferably to the volume of the second chamber and thus to the total volume of the silencer.
- the ratios of the volumes of the first chamber to the total volume of the muffler, but also the volume of the flow channel to the total volume of the muffler leads primarily to lower pressure fluctuations at the main outlet, which is arranged on the flow channel, and enter through the exhaust gas from the flow channel into the second chamber can.
- a reduction in the overall noise level of the muffler is achieved when the pressure fluctuations of the exhaust gas at the outlet from the second chamber are minimized, through which the exhaust gas can escape into the open.
- the effect is achieved that the frequency of the pressure fluctuations with which the exhaust gas passes through the main outlet into the second chamber does not coincide with the resonance frequency of the second chamber. It is important that the excitation frequency of the second chamber as far as possible a large distance from the pulsation frequency of the pressure fluctuations of the exhaust gas, with which the exhaust gas through the main outlet in the second Kam- flows in. Only then can a particularly effective reduction of the overall noise level of the muffler be achieved.
- the objective is pursued that inside the muffler, formed by the interaction of the first chamber, the flow channel and the combustion chamber, a flow principle is used to create the pulsating pressure barrier at the outlet of the combustion chamber, and thereby the To optimize emission levels.
- the target is tracked, letting no resonance arise, so that the frequency of the pressure fluctuations, with which the Exhaust gas enters the second chamber through the main outlet, if possible not coincident with the excitation frequency of the second chamber. Consequently, a particularly good acoustic attenuation result of the silencer results, so that on the one hand very good emission results are achieved, on the other hand a very good reduction of the operating noise of the engine working device can be achieved.
- the two-stroke engine may have a stroke volume, and the ratio of the volume of the first chamber to the stroke volume is 1/4 to 2.
- the exhaust flow principle to form an exhaust backpressure can be particularly effectively implemented to optimize the emission levels, but also the fuel consumption of the two-stroke engine.
- the ratio of the volume of the second chamber to the displacement volume can be 4 to 10. By this ratio, a particularly good noise reduction is achieved in the operation of the two-stroke engine.
- the muffler may preferably be made of a stainless steel, for example with the material number 1.4301, and the E-modulus of the material may preferably be 200,000 N / mm 2 .
- FIG. 1 shows a schematic representation of an exemplary embodiment of a two-stroke engine with a silencer
- FIG. 2 shows a diagram of the pressures over the crank angle of the two-stroke engine in the first chamber and in the combustion chamber
- FIG. 3 shows a schematic view of a silencer of the type of interest here in arrangement with a two-stroke engine
- Figure 4 is a graph of the pressure over the crank angle of the two-stroke engine with different pressure gradients at a speed of 7000 1 / min and
- Figure 5 is a diagram of the pressure over the crank angle of the two-stroke engine with different pressure gradients at a speed of 10,000 1 / min.
- the two-stroke engine 100 has a cylinder 18 in which a combustion chamber 13 is formed.
- the combustion chamber 13 is movably bounded by a piston 21, which is connected via a connecting rod 23 with a crankshaft 22 to form a crank mechanism, and the crankshaft 22 is mounted in a crankcase 24.
- an outlet is arranged, on which the muffler 10 is flanged via a muffler inlet 11 in a manner not shown in detail ter.
- the piston 21 releases the outlet of the combustion chamber 13 in this area, and exhaust gas can pass from the combustion chamber 13 through the muffler inlet 11 into the muffler 10.
- the silencer inlet 11 is adjoined by a flow channel 12, which opens into a first chamber 15 with a channel end opposite the silencer inlet 11.
- the muffler 10 has a second chamber 16, which is formed by way of example larger than the first chamber 15 and the first Chamber 15 preferably completely and also a part of the flow channel 12 encloses.
- the exhaust gas entering the muffler inlet 11 can first at least for the most part reach the first chamber 15, wherein a main outlet 17 is arranged on the flow channel 12, and the exhaust gas can pass from the flow channel 12 through the main outlet 17 into the second chamber 16. Furthermore, the first chamber 15 has a secondary outlet 20, so that exhaust gas can flow from the first chamber 15 directly into the second chamber 16. The exhaust gas can leave the muffler 10 through an outlet 19, which is introduced in the wall of the second chamber 16 and reach the outside.
- the flow channel 12 extends in a straight training between the first chamber 15 and the muffler inlet 11, and is designed so aerodynamically favorable that the exhaust gas flowing into the muffler inlet 11 due to its inertia mainly flows into the first chamber 15 and in this an overpressure generated.
- the exhaust gas can again flow back in the direction of the muffler inlet 11, and thereby form a back pressure against the combustion chamber 13. This avoids that fuel-air mixture passes unburned in the muffler 10 or already in the muffler 10 occurred fuel-air mixture is forced back into the combustion chamber 13. Only after backflow of the exhaust gas against the outlet of the combustion chamber 13, the exhaust gas can leave the flow channel 12 and the first chamber 15 through a main outlet 17 and enter the second chamber 16 and pass through the outlet 19 into the open.
- an overflow channel 25 is shown, which forms a flow connection between the crankcase 24 and the combustion chamber 13.
- the fuel-air mixture is first sucked in a manner not shown in detail through an inlet in the crankcase 24 when the piston 21 makes an upward movement, and increases the volume of the crankcase 24.
- the aspirated fuel-air mixture is then compressed by a downward movement of the piston 21 in the crankcase 24, so that the fuel-air mixture has an overpressure.
- Moves the piston 21 in his Lifting movement towards the bottom dead center the piston 21 releases a overflow window 26 in the wall of the cylinder 18, and the overflow window 26 forms the inlet of the overflow 25 into the combustion chamber 13.
- the overflow channel 25 opens in the overflow window 26 at a position in the combustion chamber 13, although the combustion chamber 13 has a flow connection with the muffler inlet 11.
- the flowing back from the first chamber 15 through the flow channel 12 exhaust gas in the direction of the combustion chamber 13 form a back pressure or even flow into the combustion chamber 13 and form an overpressure in this, and there may be an interaction between the backflowing exhaust gas and the take place through the overflow channel 25 into the combustion chamber 13 incoming air-fuel mixture.
- the backflowing exhaust gas still form a temporary overpressure in the combustion chamber 13 during the opening time of the outlet, and the overpressure can influence the amount of fuel-air mixture and the outflow behavior of the fuel-air mixture are taken through the overflow 25 in the Combustion chamber 13 flows. Consequently, the flowing back exhaust gas in the combustion chamber 13 can form a temporary pressure surge, can be taken by the influence on the flowing into the combustion chamber 13 fuel-air mixture.
- FIG. 2 shows in a diagram a pressure which is plotted in degrees over a crank angle ° KW.
- the diagram shows two pressure curves A and B, and the pressure curve A gives the pressure profile in the combustion chamber 13, and the pressure curve B is the pressure curve in the first chamber 15 again.
- a crank angle of about 110 ° opens the outlet of the combustion chamber 13, characterized by EO, approximately at about 130 ° opens the overflow 25 into the combustion chamber 13, characterized by TPO, wherein the closing of the overflow Strömkanals 25 is characterized by TPC, and takes place at 230 °.
- the outlet of the combustion chamber 13 is closed at about 250 °, characterized by EC. This makes it clear that the outlet window in the cylinder 18 has a greater extent in the piston stroke direction than the overflow channel 25. However, both the outlet and the overflow channel 25 between 130 ° crank angle and 230 ° crank angle are both open.
- the pressure profile A in the combustion chamber 13 shows that after opening the outlet of the combustion chamber 13, the pressure in the combustion chamber 13 drops until the pressure A reaches a value of about 1.3 bar.
- the exhaust gas flows from the combustion chamber 13 into the muffler 10, so that the pressure curve B measured in the first chamber 15 records an increase.
- the exhaust gas flows from the combustion chamber 13 into the first chamber 15, and at drop in the pressure curve A is an increase in the pressure curve B recorded.
- the maximum pressure in the first chamber 15 is reached approximately at 145 ° crank angle and flows through the flow channel 12 back into the combustion chamber 13.
- the pressure in the combustion chamber 13 shows an increase up to an intermediate maximum pressure, denoted by X.
- the intermediate pressure maximum X is reached approximately at bottom dead center BDC, and the intermediate pressure in the combustion chamber 13 can be influenced on the fuel-air mixture, which at the same time by the overflow channel 25 also flows into the combustion chamber 13.
- the pressure curve B in the first chamber 15 subsequently shows a further intermediate maximum pressure since part of the exhaust gas flows back toward the first chamber 15 before the exhaust gas leaves the flow channel 12 or the first chamber 15 through the main outlet 17.
- the pressure curve A in the combustion chamber 13 illustrates an exhaust gas recirculation flow which takes place at a point in time which lies between the opening TPO of the overflow channel 25 and the closing TPC of the overflow channel 25.
- FIG. 3 shows a two-stroke engine 110 in a schematic, cross-sectional view, and a two-stroke engine 110 has a muffler 200 mounted thereon.
- the two-stroke engine 110 has a cylinder 118 in which a combustion chamber 113 is formed.
- the combustion chamber 113 is movably limited by a piston 121, which is connected via a connecting rod 123 with a crankshaft 122 for forming a crank mechanism, and the crankshaft 122 is mounted in a crankcase 124.
- an outlet is arranged, on which the muffler 200 is flanged via a muffler inlet 111 in a manner not shown in detail.
- the piston 121 When the piston 121 is in the illustrated position of the bottom dead center, the piston 121 releases the outlet of the combustion chamber 113, and exhaust gas can pass from the combustion chamber 113 through the muffler inlet 111 into the muffler 200.
- the silencer inlet 111 is adjoined by a flow channel 112, which opens into a first chamber 115 with a channel end 114 opposite the silencer inlet 111.
- the muffler 110 has a second chamber 116, which is formed larger than the first chamber 115 and the first chamber 115 completely and also encloses a part of the flow channel 112.
- the exhaust gas entering the muffler inlet 111 can first at least for the most part reach the first chamber 115, wherein a main outlet 117 is arranged on the flow channel 112, and the exhaust gas can pass from the flow channel 112 through the main outlet 117 into the second chamber 116. Furthermore, the first chamber 115 has a secondary outlet 120, so that exhaust gas can also flow from the first chamber 115 directly into the second chamber 116.
- the exhaust gas may exit the muffler 200 through an outlet 119 formed in the wall of the second chamber 116.
- the flow channel 112 extends in a straight training between the first chamber 115 and the muffler inlet 111, and is designed so aerodynamically favorable that the inflowing into the muffler inlet 111 exhaust gas due to its inertia predominantly flows into the first chamber 115 and generates an overpressure in this. After filling the first chamber 115, the exhaust gas can again flow back in the direction of the silencer inlet 111, and thereby form a back pressure against the combustion chamber 113. This avoids that fuel-air mixture unburned enters the muffler 200 or already in the muffler 200 occurred fuel-air mixture is pushed back into the combustion chamber 113.
- the illustration shows the first chamber 115 having dimensions that are significantly smaller than the dimensions of the second chamber 116, and the second chamber 116 enclosing the first chamber 115 by way of example as well as a part of the flow channel 112.
- the ratio of the volume of the first chamber 115 to the total volume of the muffler 1/40 to 1/2, and the total volume of the muffler 200 is formed by the absolute volume of the second chamber 116.
- Figures 4 and 5 show for different speeds the pressure curve p in bar over the crank angle of the crankshaft 122 in degrees
- the crank angle at which the outlet of the combustion chamber 113 opens and closes is indicated for a plurality of charge changes.
- the indication EO indicates that the outlet of the combustion chamber 113 is opened
- the indication EC indicates that the outlet of the combustion chamber 113 is closed again.
- two opening cycles of the outlet are shown, and the pressure curve in the combustion chamber 113 is indicated by C. 5 shows due to the higher speed three opening cycles of the combustion chamber 113, indicated by the pressure curves C.
- the pressure profile A shows the curve of the pressure of the exhaust gas mass flow at the outlet for a muffler 200 with the features of the present invention
- B shows the pressure curve of the exhaust gas mass flow at the outlet of a conventional muffler, which has a ratio of the volumes of an antechamber to the total volume of a muffler that is not within the claimed range.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE112012001120.1T DE112012001120A5 (de) | 2011-03-09 | 2012-03-07 | Zweitaktmotor mit einem Schalldämpfer |
US13/985,651 US8844672B2 (en) | 2011-03-09 | 2012-03-07 | Two-stroke engine comprising a muffler |
CN201280012466.2A CN103415682B (zh) | 2011-03-09 | 2012-03-07 | 包括消声器的二冲程发动机 |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE202011000531.3 | 2011-03-09 | ||
DE202011000531U DE202011000531U1 (de) | 2011-03-09 | 2011-03-09 | Schalldämpfer für ein Motorgerät |
DE202011000535U DE202011000535U1 (de) | 2011-03-09 | 2011-03-09 | Zweitaktmotor mit einem Schalldämpfer |
DE202011000535.6 | 2011-03-09 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2012120037A2 true WO2012120037A2 (de) | 2012-09-13 |
WO2012120037A3 WO2012120037A3 (de) | 2013-03-21 |
Family
ID=45808962
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2012/053901 WO2012120037A2 (de) | 2011-03-09 | 2012-03-07 | Zweitaktmotor mit einem schalldämpfer |
Country Status (4)
Country | Link |
---|---|
US (1) | US8844672B2 (de) |
CN (1) | CN103415682B (de) |
DE (1) | DE112012001120A5 (de) |
WO (1) | WO2012120037A2 (de) |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE202008005168U1 (de) | 2008-04-14 | 2009-08-27 | Dolmar Gmbh | Schalldämpfer für ein Motorgerät |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
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US1804321A (en) | 1928-06-22 | 1931-05-05 | Lloyd L E Crowe | Pulsation control |
US2542756A (en) | 1946-05-02 | 1951-02-20 | Draminsky Per | Two-stroke engine |
JPS5815708A (ja) | 1981-07-22 | 1983-01-29 | Nissan Motor Co Ltd | 消音器 |
JPS60142009A (ja) | 1983-12-28 | 1985-07-27 | Ishikawajima Shibaura Kikai Kk | 2サイクルエンジンの排気装置 |
CA1232550A (en) | 1984-04-09 | 1988-02-09 | Orbital Engine Company (Australia) Pty. Limited | Internal combustion engines |
US4848279A (en) * | 1988-02-03 | 1989-07-18 | Industrial Technology Research Institute | Air-injection device for two-stroke engines |
AT404391B (de) | 1989-11-10 | 1998-11-25 | Pischinger Rudolf Dipl Ing Dr | Auspuffanlage für eine zweitakt-brennkraftmaschine |
JP3038763B2 (ja) | 1990-03-14 | 2000-05-08 | スズキ株式会社 | 内燃機関のマフラ |
DE4203507A1 (de) | 1992-02-07 | 1993-08-12 | Fichtel & Sachs Ag | Auspuffsystem fuer zweitakt-verbrennungsmotoren |
US5245824A (en) | 1992-03-03 | 1993-09-21 | Nouis Randy G | Method and apparatus for optimizing the exhaust system of a two cycle engine |
JP3816581B2 (ja) | 1996-06-21 | 2006-08-30 | 株式会社共立 | 内燃エンジンのマフラー |
SE516698C2 (sv) * | 1996-11-15 | 2002-02-12 | Electrolux Ab | Förbränningsmotor |
WO2000065209A1 (fr) * | 1999-04-23 | 2000-11-02 | Komatsu Zenoah, Co. | Moteur a deux temps de balayage a charges stratifiees |
SE9903403L (sv) | 1999-09-22 | 2001-03-23 | Electrolux Ab | Tvåtakts förbränningsmotor |
AUPR853401A0 (en) | 2001-10-29 | 2001-11-29 | Arnold, Phillip John | Harmonic synchroniser system |
US20040144081A1 (en) | 2003-01-21 | 2004-07-29 | Lacy James W. | Engine exhaust system |
ITRN20050003A1 (it) | 2005-01-27 | 2006-07-28 | Ct Ricerche Tecnologiche Srl | Barriera fluida a getto di gas per motori a due tempi |
DE202005005328U1 (de) | 2005-04-04 | 2006-08-10 | Dolmar Gmbh | Zweitaktmotor |
AT505406B1 (de) | 2007-08-07 | 2009-01-15 | Hans Leeb Zweirad Handel Gmbh | Auspuffanlage für eine zweitakt-brennkraftmaschine |
AT507634B1 (de) | 2008-12-12 | 2011-01-15 | Forschungsgesellschaft Fuer Verbrennungskraftmaschinen Und Thermodynamik Mbh | Auspuffanlage für eine verbrennungskraftmaschine |
DE202011000528U1 (de) * | 2011-03-09 | 2012-06-12 | Makita Corporation | Zweitaktmotor mit einem Schalldämpfer |
DE202011000534U1 (de) * | 2011-03-09 | 2012-06-11 | Makita Corporation | Schalldämpfer für einen Zweitaktmotor eines Motorarbeitsgerätes |
-
2012
- 2012-03-07 CN CN201280012466.2A patent/CN103415682B/zh active Active
- 2012-03-07 DE DE112012001120.1T patent/DE112012001120A5/de not_active Withdrawn
- 2012-03-07 US US13/985,651 patent/US8844672B2/en active Active
- 2012-03-07 WO PCT/EP2012/053901 patent/WO2012120037A2/de active Application Filing
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE202008005168U1 (de) | 2008-04-14 | 2009-08-27 | Dolmar Gmbh | Schalldämpfer für ein Motorgerät |
Also Published As
Publication number | Publication date |
---|---|
DE112012001120A5 (de) | 2014-01-02 |
US8844672B2 (en) | 2014-09-30 |
WO2012120037A3 (de) | 2013-03-21 |
US20130319789A1 (en) | 2013-12-05 |
CN103415682B (zh) | 2016-06-01 |
CN103415682A (zh) | 2013-11-27 |
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