EP0704017B1 - Luft-brennstoff-gemischzufuhrvorrichtung für eine zweitaktbrennkraftmaschine - Google Patents

Luft-brennstoff-gemischzufuhrvorrichtung für eine zweitaktbrennkraftmaschine Download PDF

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Publication number
EP0704017B1
EP0704017B1 EP94923771A EP94923771A EP0704017B1 EP 0704017 B1 EP0704017 B1 EP 0704017B1 EP 94923771 A EP94923771 A EP 94923771A EP 94923771 A EP94923771 A EP 94923771A EP 0704017 B1 EP0704017 B1 EP 0704017B1
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EP
European Patent Office
Prior art keywords
air
combustion chamber
port
cylinder
fuel mixture
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
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EP94923771A
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English (en)
French (fr)
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EP0704017A1 (de
Inventor
Jean-Marc Masse
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Individual
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Individual
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Classifications

    • 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
    • F02B25/00—Engines characterised by using fresh charge for scavenging cylinders
    • F02B25/14—Engines characterised by using fresh charge for scavenging cylinders using reverse-flow scavenging, e.g. with both outlet and inlet ports arranged near bottom of piston stroke
    • 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
    • F02B75/00—Other engines
    • F02B75/02—Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
    • 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
    • F02B33/00—Engines characterised by provision of pumps for charging or scavenging
    • F02B33/02—Engines with reciprocating-piston pumps; Engines with crankcase pumps
    • F02B33/04—Engines with reciprocating-piston pumps; Engines with crankcase pumps with simple crankcase pumps, i.e. with the rear face of a non-stepped working piston acting as sole pumping member in co-operation with the crankcase
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D9/00—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
    • F02D9/02—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits concerning induction conduits
    • F02D2009/0201—Arrangements; Control features; Details thereof
    • F02D2009/0291—Throttle control device for throttle being disposed in a two-stroke engine transfer passage

Definitions

  • the present invention relates to a device for supplying the air-fuel mixture to a two-stroke internal combustion engine of the type swept by compressed air in the casing, comprising at least one cylinder, a piston moving in back and forth in said cylinder to delimit a combustion chamber and a purge air compression housing provided with an air intake orifice, the cylinder comprising at least one exhaust port, at least one port transfer communicating through a transfer channel with the housing, and a light for introducing an air-fuel mixture into the combustion chamber, towards the end of the sweep.
  • document WO-A-91 02 144 describes a two-stroke internal combustion engine in which the air flow from the compression housing to the combustion chamber takes place through two passages.
  • a first passage controlled by the piston is traversed by the major part of the air flow.
  • a second passage traversed by a reduced part of the air flow contains a rotary shutter driven in synchronism with the rotation of the engine, a fuel introduction taking place in said reduced part of the air flow, downstream of the rotary shutter, in such a way that an air-fuel mixture is admitted into the combustion chamber through an air-fuel mixture introduction port, during a limited angle of rotation of the engine.
  • the present invention aims to eliminate or at least reduce to a large extent the drawbacks of the solutions already proposed with a view to reducing the consumption and pollution of two-stroke engines.
  • the subject of the invention is a device for supplying the air-fuel mixture to a two-stroke internal combustion engine of the type swept by compressed air in the casing, this engine comprising at least one cylinder, a movable piston. back and forth in the cylinder to define a combustion chamber and a purge air compression housing provided with an air intake orifice.
  • the cylinder comprises at least one exhaust port, at least one transfer port communicating via a transfer channel with the casing, and a port for introducing an air-fuel mixture into the combustion chamber towards the end of the sweep. .
  • the supply device comprises an air reservoir supplied with air at a pressure higher than the pressure prevailing in the combustion chamber after opening of the exhaust port, and a rotary shutter member driven in synchronism with the rotation of the engine, associated with the light for introducing the air-fuel mixture into the combustion chamber.
  • a venturi is placed between said tank and the rotary shutter and a fuel inlet from a constant level tank opens into the divergent portion of said venturi
  • the rotary shutter is preferably placed inside said tank.
  • the rotary obturator can preferably be a cylindrical plug obturator whose axis is parallel to the axis of the cylinder and which has in its cylindrical wall a window controlling the communication of the tank by the introduction light with the combustion chamber .
  • the air tank can be supplied with pressurized air by a system external to the engine, or by a system internal to the engine.
  • the reservoir is advantageously supplied with air from the casing by a conduit also controlled by a rotary shutter driven in synchronism with the rotation of the engine.
  • the upper edge of the light for introducing the air-fuel mixture into the combustion chamber may be at the same level as the upper edge of the exhaust light, but according to a preferred embodiment, the upper edge of the introduction light is located closer to the cylinder head than the upper edge of the exhaust light, so that when the piston rises, the combustion chamber still communicates with the air tank and the increasing the pressure in the combustion chamber leads to an increase in the air pressure in the tank for the introduction of the air-fuel mixture during the next cycle.
  • the air-fuel jet of the air-fuel mixture supply device is oriented towards the cylinder head so that said jet does not meet the exhaust lumen.
  • the engine as illustrated in the drawing is an internal combustion engine operating on a two-stroke cycle, of the type scanned by compressed air in the casing.
  • a cylinder 1 defined in a cylinder block 2 surmounted by a cylinder head 3 carrying a spark plug 4.
  • the cylinder block 2 is attached to a casing 5 provided with an air intake opening 6 and a non-flap valve represented.
  • a crankshaft 7 In the casing 5 rotates a crankshaft 7 to which is coupled by a connecting rod 8 a piston 9 which is movable back and forth in the cylinder 1 and delimits in the latter a combustion chamber 10 with the cylinder head 3.
  • the cylinder 1 also comprises an exhaust light 11 as well as a transfer light 12 communicating via a transfer channel not shown with the casing 5, the two lights 11 and 12 being formed in the cylinder 1 so as to open into the combustion chamber 10 at a height such that they are completely cleared only when the piston 9 is in bottom dead center, as shown.
  • the engine as described above also comprises a device 13 for supplying the air-fuel mixture to the combustion chamber 10.
  • This device 13 comprises an air reservoir 14 communicating through a passage 15 with the casing 5 as well as by a light 16 with the cylinder 1, the light 16 being substantially at the same height as the exhaust light 11.
  • a rotary shutter 19 rotating around an axis parallel to the axis of the cylinder 1 is rotatably mounted at the inside the chamber 14 so as to control the communication between the inside of the chamber 14 and the cylinder 1.
  • the shutter 19 is a plug valve with a cylindrical wall located between the ve nturi 17 and the light 16 has a window 21.
  • the shaft 20 of the shutter 19 also carries another rotary shutter 22 whose light 23 controls the communication between the chamber 14 and the casing 5 via the conduit 15, as well as 'a drive pinion 24 consisting of a bevel gear engaged with a not shown bevel gear of a shaft which is parallel to the crankshaft 7 and is driven by the latter.
  • the insertion light 16 is arranged in such a way that its lower edge is located at the height of the top of the piston 9 when the latter is in bottom dead center and that its upper edge is located at a level slightly above the upper edge of the exhaust lumen 11. Furthermore, the introductory lumen 16 is opposite the exhaust lumen 11 and the venturi 17 is oriented obliquely upwards towards the cylinder head 3 so as to produce a jet which crosses the axis of the cylinder 1 and passes over the exhaust port 11.
  • the piston 9 moves towards the cylinder head 3 in the direction of the top dead center. During this piston rise stroke, the volume of the casing 5 increases and air is drawn into the casing 5 through the inlet port 6 and the valve not shown.
  • the spark plug 4 triggers the combustion of the air-fuel mixture contained in the combustion chamber 10 and under the thrust of the gases resulting from this combustion, the piston 9 moves away from cylinder head 3 towards bottom dead center. During this descent of the piston 9, the air previously sucked into the casing 5 is compressed, the valve not shown preventing any discharge of air through the intake orifice 6.
  • the piston 9 successively discovers the introduction light 16, the exhaust light 11 and the transfer light 12.
  • the introduction light 16 is still closed by the shutter 19, the gases of exhaust are evacuated by the exhaust port 11, this movement being assisted by the introduction, via the transfer orifice 12, of fresh air previously compressed in the casing 5.
  • the window 21 and the light 16 still allow, for a short time, a communication of the combustion chamber 10 with the tank 14, so that the pressure which increases in the chamber combustion 10 due to the upward movement of the piston 9 increases the pressure of the air contained in the tank 14, for the introduction of fuel during the next cycle.
  • the piston 9 then continues its upward movement in the direction of the cylinder head 3, compressing the air-fuel mixture in the combustion chamber 10 and sucking air into the casing 5 through the intake port 6 and the valve not shown.
  • pressurized air into the reservoir 14 instead of being done by a system internal to the engine (transfer in the reservoir 14 of part of the compressed air in the casing 5), could also be done by a system external to the engine.
  • the shutter 19 could be a rotary shutter other than in the form of a plug, rotating around an axis other than parallel to the axis of the cylinder 1, although the arrangement described and shown is particularly favorable in the measurement. where it makes it possible to place the shutter as close as possible to the insertion lumen 16 and to produce the insertion device 13 as a whole in a particularly compact form.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Claims (9)

  1. Einrichtung, um einen Zweitaktverbrennungsmotors, der in der Bauart mit Spülung durch aus dem Gehäuse kommende komprimierte Luft ausgeführt ist, mit einem Kraftstoff-Luft-Gemisch zu versorgen, mit wenigstens einem Zylinder, mit einem in dem Zylinder hin- und hergehenden beweglichen Kolben, der darin eine Brennkammer begrenzt, mit einem Gehäuse für unter Druck stehende Spülluft, das mit einer Lufteinlassöffnung versehen ist, wobei der Zylinder wenigstens einen Auslass-Schlitz, wenigstens einen Überstromschlitz, der über einen Überströmkanal mit dem Gehäuse strömungsmäßig in Verbindung steht, und wenigstens einen Einlass-Schlitz zum Einlassen des Kraftstoff-Luft-Gemischs in die Brennkammer gegen Ende der Spülung aufweist, mit einem Drehschieber (19), der synchron mit der Drehbewegung des Motors angetrieben und dem Einlass-Schlitz (16) für das Kraftstoff-Luft-Gemisch zugeordnet ist und mit einem Luftvorratsbehälter (14), der mit Luft gespeist wird, die unter einem höheren Druck steht als der Druck in der Brennkammer vor dem Öffnen des Auslass-Schlitzes (11), dadurch gekennzeichnet, dass sie unter anderem eine Venturi-Düse (17) aufweist, die zwischen dem Vorratsbehälter (14) und dem Drehschieber (19) angeordnet ist, und dass eine Kraftstoffeinlassöffnung (18) vorhanden ist, die aus einer Kammer mit konstantem Füllstand gespeist wird und die in den divergierenden Teil der Venturi-Düse mündet.
  2. Einrichtung nach Anspruch 1, dadurch gekennzeichnet, dass der Drehschieber (18) innerhalb des Behälters (14) angeordnet ist.
  3. Einrichtung nach Anspruch 2, dadurch gekennzeichnet, dass der Drehschieber (19) ein zylindrischer becherförmiger Drehschieber ist, dessen Achse parallel zu der Achse des Zylinders (1) verläuft und der in seinem zylindrischen Kragen ein Fenster (21) enthält, das die strömungsmäßige Verbindung über den Einlass-Schlitz (16) des Vorratsbehälters (14) mit der Brennkammer (10) steuert.
  4. Einrichtung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Luftvorratsbehälter (14) durch ein von dem Motor getrenntes System mit Druckluft versorgt wird.
  5. Einrichtung nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass der Luftvorratsbehälter (14) durch ein in dem Motor befindliches System mit Druckluft versorgt wird.
  6. Einrichtung nach Anspruch 5, dadurch gekennzeichnet, dass der Luftvorratsbehälter (14) mit unter Druck stehender Luft versorgt wird, die von der Kurbelkammer (5) durch einen Kanal (15) kommt, der durch einen Drehschieber (22) gesteuert wird, der synchron mit der Drehbewegung des Motors angetrieben ist.
  7. Einrichtung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die obere Kante des Einlass-Schlitzes (16) für das Kraftstoff-Luft-Gemisch sich in der Brennkammer (10) auf derselben Höhe befindet wie die obere Kante des Auslass-Schlitzes (11).
  8. Einrichtung nach einem der vorhergehenden Ansprüche 1 bis 6, dadurch gekennzeichnet, dass die obere Kante des Einlass-Schlitzes (16) für das Kraftstoff-Luft-Gemisch in der Brennkammer (10) sich auf einer Höhe befindet, die näher an dem Zylinderkopf (3) liegt als die obere Kante des Auslass-Schlitzes (11).
  9. Einrichtung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Kraftstoff-Luft-Gemischstrahl der Kraftstoff-Luft-Gemischzufuhreinrichtung in Richtung auf den Zylinderkopf (3) gerichtet ist, in der Weise, dass der Strahl nicht auf den Auslass-Schlitz (11) trifft.
EP94923771A 1993-08-03 1994-08-02 Luft-brennstoff-gemischzufuhrvorrichtung für eine zweitaktbrennkraftmaschine Expired - Lifetime EP0704017B1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR9309556 1993-08-03
FR9309556A FR2708666B1 (fr) 1993-08-03 1993-08-03 Dispositif d'alimentation en mélange air-carburant d'un moteur à explosion à deux temps.
PCT/FR1994/000972 WO1995004212A1 (fr) 1993-08-03 1994-08-02 Dispositif d'alimentation en melange air-carburant d'un moteur a explosion a deux temps

Publications (2)

Publication Number Publication Date
EP0704017A1 EP0704017A1 (de) 1996-04-03
EP0704017B1 true EP0704017B1 (de) 1997-07-09

Family

ID=9449898

Family Applications (1)

Application Number Title Priority Date Filing Date
EP94923771A Expired - Lifetime EP0704017B1 (de) 1993-08-03 1994-08-02 Luft-brennstoff-gemischzufuhrvorrichtung für eine zweitaktbrennkraftmaschine

Country Status (9)

Country Link
US (1) US5586525A (de)
EP (1) EP0704017B1 (de)
JP (1) JPH09500943A (de)
CN (1) CN1049948C (de)
AT (1) ATE155208T1 (de)
DE (1) DE69404148T2 (de)
ES (1) ES2105739T3 (de)
FR (1) FR2708666B1 (de)
WO (1) WO1995004212A1 (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU704849B2 (en) * 1995-09-19 1999-05-06 Honda Giken Kogyo Kabushiki Kaisha Two-cycle internal combustion engine
US5769040A (en) * 1997-04-18 1998-06-23 Christner; Oval F. Two cycle internal combustion engine
JP3778319B2 (ja) * 1997-05-24 2006-05-24 本田技研工業株式会社 ２サイクル内燃機関
FR2780099B1 (fr) * 1998-06-22 2001-01-05 Daniel Drecq Moteur a combustion interne a deux temps muni d'un dispositif de suralimentation et de recirculation partielle de gaz d'echappement
US6367432B1 (en) * 1999-05-14 2002-04-09 Kioritz Corporation Two-stroke cycle internal combustion engine
US6427646B2 (en) * 2000-01-27 2002-08-06 Walbro Corporation Small engine fuel injection system
DE102005002275B4 (de) * 2005-01-18 2015-02-05 Andreas Stihl Ag & Co. Kg Verfahren zum Betrieb eines Einzylinder-Zweitaktmotors
AU2005248964A1 (en) * 2005-02-23 2006-09-07 Techtronic Industries Co., Ltd Two-stroke engine with fuel injection

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DE666717C (de) * 1934-02-21 1938-11-18 Triumph Werke Nuernberg Akt Ge Drehschiebersteuerung fuer Brennkraftmaschinen
US2115525A (en) * 1934-07-26 1938-04-26 Hocke Enrico Diesel type locomotive with direct transmission and with automatically supercharged motor when decreasing the velocity
US2113979A (en) * 1934-12-01 1938-04-12 Whitworth & Co Scavenging of two-stroke internal combustion engines
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US2214047A (en) * 1938-11-14 1940-09-10 John F Tulloch Throttle control in internal combustion engine
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GB1538852A (en) * 1975-04-25 1979-01-24 Hooper B Multi-cylinder stepped piston two stroke engines
JPS6235019A (ja) * 1985-08-06 1987-02-16 Yamaha Motor Co Ltd ２サイクルエンジンの吸気装置
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JPH02169818A (ja) * 1988-12-21 1990-06-29 Fuji Heavy Ind Ltd ２サイクルエンジン
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GB9412181D0 (en) * 1994-06-17 1994-08-10 Ricardo Consulting Eng Crankcase scavenged two-stroke engines

Also Published As

Publication number Publication date
ATE155208T1 (de) 1997-07-15
ES2105739T3 (es) 1997-10-16
DE69404148T2 (de) 1998-01-15
FR2708666A1 (fr) 1995-02-10
WO1995004212A1 (fr) 1995-02-09
EP0704017A1 (de) 1996-04-03
JPH09500943A (ja) 1997-01-28
CN1049948C (zh) 2000-03-01
DE69404148D1 (de) 1997-08-14
CN1128555A (zh) 1996-08-07
FR2708666B1 (fr) 1995-10-13
US5586525A (en) 1996-12-24

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