WO2019044647A1 - Structure de chambre de combustion de moteur - Google Patents

Structure de chambre de combustion de moteur Download PDF

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Publication number
WO2019044647A1
WO2019044647A1 PCT/JP2018/031111 JP2018031111W WO2019044647A1 WO 2019044647 A1 WO2019044647 A1 WO 2019044647A1 JP 2018031111 W JP2018031111 W JP 2018031111W WO 2019044647 A1 WO2019044647 A1 WO 2019044647A1
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WO
WIPO (PCT)
Prior art keywords
cavity
combustion chamber
fuel
injection
engine
Prior art date
Application number
PCT/JP2018/031111
Other languages
English (en)
Japanese (ja)
Inventor
尚奎 金
貴 隅本
大輔 志茂
朋礼 原田
晋太朗 岡田
修治 詫間
Original Assignee
マツダ株式会社
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from JP2017213834A external-priority patent/JP6519633B2/ja
Application filed by マツダ株式会社 filed Critical マツダ株式会社
Priority to EP18851330.3A priority Critical patent/EP3663556B1/fr
Priority to US16/641,758 priority patent/US11092107B2/en
Priority to CN201880055364.6A priority patent/CN111051663B/zh
Publication of WO2019044647A1 publication Critical patent/WO2019044647A1/fr

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    • 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
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0672—Omega-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder center axis
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D41/00—Electrical control of supply of combustible mixture or its constituents
    • F02D41/30—Controlling fuel injection
    • F02D41/38—Controlling fuel injection of the high pressure type
    • F02D41/40—Controlling fuel injection of the high pressure type with means for controlling injection timing or duration
    • F02D41/401—Controlling injection timing
    • 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
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • 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
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0645—Details related to the fuel injector or the fuel spray
    • F02B23/0648—Means or methods to improve the spray dispersion, evaporation or ignition
    • F02B23/0651—Means or methods to improve the spray dispersion, evaporation or ignition the fuel spray impinging on reflecting surfaces or being specially guided throughout the combustion space
    • 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
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0678—Unconventional, complex or non-rotationally symmetrical shapes of the combustion space, e.g. flower like, having special shapes related to the orientation of the fuel spray jets
    • F02B23/0693—Unconventional, complex or non-rotationally symmetrical shapes of the combustion space, e.g. flower like, having special shapes related to the orientation of the fuel spray jets the combustion space consisting of step-wise widened multiple zones of different depth
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D41/00—Electrical control of supply of combustible mixture or its constituents
    • F02D41/30—Controlling fuel injection
    • F02D41/38—Controlling fuel injection of the high pressure type
    • F02D41/3809—Common rail control systems
    • F02D41/3827—Common rail control systems for diesel engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D41/00—Electrical control of supply of combustible mixture or its constituents
    • F02D41/30—Controlling fuel injection
    • F02D41/38—Controlling fuel injection of the high pressure type
    • F02D41/40—Controlling fuel injection of the high pressure type with means for controlling injection timing or duration
    • F02D41/402—Multiple injections
    • F02D41/403—Multiple injections with pilot injections
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00—Cylinders; Cylinder heads 
    • F02F1/24—Cylinder heads
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00—Pistons 
    • F02F3/10—Pistons  having surface coverings
    • F02F3/12—Pistons  having surface coverings on piston heads
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D13/00—Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing
    • F02D13/02—Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing during engine operation
    • F02D13/0203—Variable control of intake and exhaust valves
    • F02D13/0215—Variable control of intake and exhaust valves changing the valve timing only
    • F02D13/0219—Variable control of intake and exhaust valves changing the valve timing only by shifting the phase, i.e. the opening periods of the valves are constant
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00—Pistons 
    • F02F3/26—Pistons  having combustion chamber in piston head
    • 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
    • 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
    • Y02T10/40—Engine management systems

Definitions

  • the present invention relates to a combustion chamber structure of an engine including a cylinder and a piston.
  • the combustion chamber of a vehicle engine such as a car is partitioned by the inner wall surface of the cylinder, the bottom surface of the cylinder head (the combustion chamber ceiling surface), and the crown surface of the piston.
  • Fuel is supplied to the combustion chamber from a fuel injection valve.
  • a combustion chamber structure in which a cavity (recess) is disposed on the crown surface of the piston and fuel is injected from the fuel injection valve toward the cavity.
  • Patent Document 1 discloses a combustion chamber structure in which the cavity has a two-stage structure of an upper cavity and a lower cavity.
  • the object of the present invention is to effectively utilize air in the combustion chamber to form a homogeneous thin air-fuel mixture in a combustion chamber structure of an engine having a cavity on the crown surface of a piston, thereby suppressing generation of soot and the like as much as possible It is to provide a combustion chamber structure of an engine that can be
  • a combustion chamber structure of an engine includes a combustion chamber of the engine formed by a lower surface of a cylinder head, a cylinder and a crown surface of a piston, and a fuel injection valve for injecting fuel into the combustion chamber.
  • the crown surface of the piston is provided with a cavity, and the fuel injection valve injects fuel toward the cavity, and is disposed at or near the radial center of the combustion chamber.
  • the cavity is disposed in a radial center region of the crown surface, and has a first cavity portion provided with a first bottom portion having a first depth in a cylinder axial direction, and an outer periphery of the first cavity portion in the crown surface And a second cavity portion provided with a second bottom portion disposed on the side and having a second depth shallower than the first depth in the cylinder axis direction, and connecting the first cavity portion and the second cavity portion It includes a connecting portion, and a standing wall region disposed radially outward of the second bottom portion of the second cavity portion.
  • the second bottom portion is positioned lower than the upper end portion in the cylinder axial direction of the connecting portion, and the lower portion of the standing wall region is positioned radially inward with respect to the upper end position of the standing wall region. ing.
  • FIG. 1 is a schematic axial sectional view showing an engine to which a combustion chamber structure of an engine according to an embodiment of the present invention is applied.
  • 2 is a perspective view of the crown portion of the piston of the engine shown in FIG. 1;
  • FIG. 3 is a perspective view with a cross section of the piston.
  • FIG. 4A is an enlarged view of a cross section of the piston shown in FIG.
  • FIG. 4B is a view for explaining curved surface shapes of the first and second cavity portions and the connection portion.
  • FIG. 5 is a cross-sectional view of the piston for illustrating the relationship between the crown surface of the piston and the injection axis of fuel by the injector.
  • FIG. 1 is a schematic axial sectional view showing an engine to which a combustion chamber structure of an engine according to an embodiment of the present invention is applied.
  • 2 is a perspective view of the crown portion of the piston of the engine shown in FIG. 1;
  • FIG. 3 is a perspective view with a cross section of the piston.
  • FIG. 6 is a time chart showing the timing of fuel injection and the heat release rate when the cavity according to the embodiment of the present invention is adopted.
  • FIGS. 7A to 7D schematically show the state of generation of air-fuel mixture in the combustion chamber along the crank angle.
  • FIG. 8 is a cross-sectional view showing a cavity structure of Comparative Example 1.
  • FIG. 9 is a time chart in which the timing of fuel injection and the heat generation rate are superimposed on each other when the cavity according to Comparative Example 1 is adopted in the time chart of FIG.
  • FIGS. 10 (A) to 10 (C) are diagrams schematically showing the state of generation of air-fuel mixture in the combustion chamber of Comparative Example 1.
  • FIG. FIG. 11 is a cross-sectional view showing a cavity structure of Comparative Example 2.
  • 12 (A) shows the in-cylinder flow of Comparative Example 2
  • FIG. 12 (B) shows the in-cylinder flow of this embodiment.
  • FIG. 1 is a schematic cross-sectional view showing an engine to which a combustion chamber structure of an engine according to an embodiment of the present invention is applied.
  • the engine according to the present embodiment is a multi-cylinder engine including a cylinder and a piston and mounted on the vehicle as a power source for driving a vehicle such as an automobile.
  • the engine includes an engine body 1 and auxiliary machinery such as an intake manifold (not shown) and various pumps attached thereto.
  • the engine body 1 includes a cylinder block 3, a cylinder head 4 and a piston 5.
  • the cylinder block 3 has a plurality of cylinders or cylinder liners (hereinafter simply referred to as "cylinder 2"; only one of them is shown in the drawing) aligned in a direction perpendicular to the paper surface of FIG.
  • the cylinder head 4 is attached to the upper surface of the cylinder block 3 and closes the upper opening of the cylinder 2.
  • the pistons 5 are slidably accommodated in the respective cylinders 2 and are connected to the crankshaft 7 via the connecting rods 8. In response to the reciprocating motion of the piston 5, the crankshaft 7 rotates about its central axis.
  • the structure of the piston 5 will be described in detail later.
  • a combustion chamber 6 is formed above the piston 5.
  • An intake port 9 and an exhaust port 10 communicating with the combustion chamber 6 are formed in the cylinder head 4.
  • the bottom surface of the cylinder head 4 is a combustion chamber ceiling surface 6U, and the combustion chamber ceiling surface 6U has a flat shape extending in the horizontal direction.
  • an intake side opening 41 that is the downstream end of the intake port 9 and an exhaust side opening 42 that is the upstream end of the exhaust port 10 are formed.
  • the cylinder head 4 is assembled with an intake valve 11 for opening and closing the intake side opening 41 and an exhaust valve 12 for opening and closing the exhaust side opening 42.
  • the intake valve 11 and the exhaust valve 12 are so-called poppet valves.
  • the intake valve 11 includes an umbrella-like valve body for opening and closing the intake side opening 41 and a stem extending perpendicularly from the valve body.
  • the exhaust valve 12 includes an umbrella-like valve body for opening and closing the exhaust side opening 42 and a stem extending vertically from the valve body.
  • Each of the valve bodies of the intake valve 11 and the exhaust valve 12 has a valve surface facing the combustion chamber 6.
  • the combustion chamber wall surface dividing the combustion chamber 6 is a combustion chamber ceiling surface 6 U including the inner wall surface of the cylinder 2, the crown surface 50 which is the upper surface (the + Z side surface) of the piston 5, and the bottom surface of the cylinder head 4 , And each of the intake valve 11 and the exhaust valve 12.
  • the cylinder head 4 is provided with an intake-side valve operating mechanism 13 and an exhaust-side valve operating mechanism 14 for driving the intake valve 11 and the exhaust valve 12 respectively.
  • the intake valve 11 and the exhaust valve 12 are driven by the valve operating mechanisms 13 and 14 in conjunction with the rotation of the crankshaft 7.
  • the valve body of the intake valve 11 opens and closes the intake side opening 41 by driving the intake valve 11 and the exhaust valve 12, and the valve body of the exhaust valve 12 opens and closes the exhaust side opening 42.
  • An intake-side variable valve timing mechanism (intake-side VVT) 15 is incorporated in the intake-side valve operating mechanism 13.
  • the intake side VVT 15 is an electric VVT provided on the intake camshaft, and the opening and closing timing of the intake valve 11 is continuously changed by continuously changing the rotational phase of the intake camshaft relative to the crankshaft 7 within a predetermined angle range.
  • an exhaust-side variable valve timing mechanism (exhaust-side VVT) 16 is incorporated in the exhaust-side valve mechanism 14.
  • the exhaust side VVT 16 is an electric VVT provided on the exhaust camshaft, and the opening and closing timing of the exhaust valve 12 is continuously changed by continuously changing the rotational phase of the exhaust camshaft relative to the crankshaft 7 within a predetermined angular range.
  • One injector 18 for injecting fuel from the tip to the combustion chamber 6 is attached to each cylinder 2 on the cylinder head 4 (combustion chamber ceiling surface 6U).
  • a fuel supply pipe 19 is connected to the injector 18.
  • the injector 18 injects the fuel supplied through the fuel supply pipe 19 into the combustion chamber 6.
  • the injector 18 is assembled to the cylinder head 4 so that the nozzle 181 (FIG. 5) is located at or near the radial center of the combustion chamber 6 and is formed on the crown surface 50 of the piston 5 The fuel is injected toward the cavity 5C (FIGS. 2 to 4B) of FIG.
  • a high pressure fuel pump (not shown) including a plunger type pump and the like interlocked and connected with the crankshaft 7 is connected.
  • a common rail (not shown) for accumulating pressure common to all the cylinders 2 is provided. The fuel accumulated in the common rail is supplied to the injectors 18 of the cylinders 2 so that fuel of high pressure is injected from the injectors 18 into the combustion chamber 6.
  • FIG. 2 is a perspective view mainly showing the upper part of the piston 5.
  • the piston 5 comprises a piston head on the upper side and a skirt located on the lower side, but in FIG. 2 it shows said piston head part having a crown surface 50 on the top surface.
  • FIG. 3 is a perspective view of the piston 5 with a radial cross section
  • FIG. 4A is an enlarged view of the radial cross section shown in FIG.
  • the cylinder axial direction A and the radial direction B of the combustion chamber are indicated by arrows.
  • the piston 5 includes a cavity 5 C, a peripheral flat surface 55 and a side peripheral surface 56.
  • a part (bottom surface) of the combustion chamber wall surface that defines the combustion chamber 6 is formed by the crown surface 50 of the piston 5, and the cavity 5 ⁇ / b> C is provided on the crown surface 50.
  • the cavity 5 ⁇ / b> C is a portion in which the crown surface 50 is recessed downward in the cylinder axial direction A, and is a portion that receives injection of fuel from the injector 18.
  • the peripheral flat portion 55 is an annular flat portion disposed in a region near the outer peripheral edge in the radial direction B in the crown surface 50.
  • the cavity 5 ⁇ / b> C is disposed in the central region in the radial direction B of the crown surface 50 excluding the peripheral flat surface 55.
  • the side peripheral surface 56 is a surface in sliding contact with the inner wall surface of the cylinder 2 and is provided with a plurality of ring grooves into which a piston ring (not shown) is fitted.
  • the cavity 5 ⁇ / b> C includes a first cavity portion 51, a second cavity portion 52, a connecting portion 53 and a peak portion 54.
  • the first cavity portion 51 is a recess disposed in the central region of the crown surface 50 in the radial direction B.
  • the second cavity 52 is an annular recess disposed on the outer circumferential side of the first cavity 51 in the crown surface 50.
  • the connection portion 53 is a portion connecting the first cavity portion 51 and the second cavity portion 52 in the radial direction B.
  • the mountain portion 54 is a mountain-shaped convex portion disposed at the central position in the radial direction B of the crown surface 50 (first cavity portion 51).
  • the peak portion 54 is convexly provided at a position directly below the nozzle 181 of the injector 18 (FIG. 5).
  • the first cavity 51 includes a first upper end 511, a first bottom 512 and a first inner end 513.
  • the first upper end portion 511 is at the highest position in the first cavity portion 51 and is continuous with the connecting portion 53.
  • the first bottom portion 512 is an annular region in a top view that is most recessed in the first cavity portion 51. Even in the entire cavity 5C, the first bottom portion 512 is the deepest portion, and the first cavity portion 51 has a predetermined depth (first depth) in the cylinder axial direction A at the first bottom portion 512. There is. In a top view, the first bottom portion 512 is located closer to the inside in the radial direction B than the coupling portion 53.
  • the first upper end portion 511 and the first bottom portion 512 are connected by a radially recessed portion 514 curved outward in the radial direction B.
  • the radially recessed portion 514 has a portion recessed outward in the radial direction B relative to the connecting portion 53.
  • the first inner end 513 is located at the innermost radial position in the first cavity 51 and is continuous with the lower end of the peak 54.
  • the first inner end portion 513 and the first bottom portion 512 are connected by a curved surface gently curved in a bottom shape.
  • the second cavity 52 includes a second inner end 521, a second bottom 522, a second upper end 523, a tapered region 524 and a rising wall region 525.
  • the second inner end portion 521 is located at the innermost radial position in the second cavity portion 52 and is continuous with the connecting portion 53.
  • the second bottom 522 is the most recessed area in the second cavity 52.
  • the second cavity 52 has a depth (second depth) shallower than the first bottom 512 in the cylinder axial direction A at the second bottom 522. That is, the second cavity portion 52 is a concave portion located on the upper side in the cylinder axial direction A than the first cavity portion 51.
  • the second upper end portion 523 is located at the highest position in the second cavity portion 52 and the outermost side in the radial direction, and is continuous with the peripheral flat portion 55.
  • the tapered region 524 is a portion that extends from the second inner end 521 toward the second bottom 522 and has a surface shape that is inclined radially outward and downward. As shown in FIG. 4A, the tapered region 524 has a slope along a slope line L2 that intersects the horizontal line L1 extending in the radial direction B at a slope angle ⁇ .
  • the standing wall region 525 is a wall surface which is formed so as to rise relatively steeply on the radially outer side of the second bottom 522.
  • the wall surface of the second cavity 52 is curved from the horizontal direction upward from the second bottom 522 to the second upper end 523, and the second upper end In the vicinity of 523, a portion considered as a wall surface close to the vertical wall is a standing wall region 525.
  • the connecting portion 53 has a shape projecting radially inward between the first cavity portion 51 located on the lower side and the second cavity portion 52 located on the upper side in the cross-sectional shape in the radial direction B. doing.
  • the connecting portion 53 has a lower end portion 531 and a third upper end portion 532 (upper end portion in the cylinder axial direction), and a central portion 533 located at the center between them.
  • the lower end portion 531 is a continuous portion with the first upper end portion 511 of the first cavity portion 51.
  • the third upper end 532 is a continuous portion with the second inner end 521 of the second cavity 52.
  • the lower end portion 531 is the lowermost portion of the connecting portion 53, and the third upper end 532 is the uppermost portion.
  • the aforementioned tapered region 524 is also a region extending from the third upper end 532 toward the second bottom 522.
  • the second bottom 522 is located below the third upper end 532. That is, the second cavity 52 of the present embodiment does not have the bottom extending horizontally from the third upper end 532 to the outside in the radial direction B, in other words, the third upper end 532 to the peripheral flat surface 55 is not connected by a horizontal surface, but has a second bottom 522 which is recessed below the third upper end 532.
  • the ridge portion 54 protrudes upward, but the projection height is the same as the height of the third upper end 532 of the connecting portion 53 and is at a position recessed from the peripheral flat portion 55.
  • the ridge portion 54 is located at the center of the circular first cavity portion 51 in a top view, whereby the first cavity portion 51 is in the form of an annular groove formed around the ridge portion 54.
  • FIG. 4B is a cross-sectional view along the cylinder axial direction A for illustrating the curved surface shapes of the first and second cavity portions 51 and 52 and the connecting portion 53.
  • the first cavity portion 51 has a surface shape (hereinafter referred to as an egg shape shape) along a Cartesian oval oval curve in a cross section including the cylinder axis.
  • the first cavity portion 51 has an arc-shaped first portion C1 farthest from the injector 18 (injection hole 182), and a second portion C2 located between the first portion C1 and the connecting portion 53.
  • a third portion C3 extending inward in the radial direction B from the first portion C1.
  • the first portion C1 is in the central region of the radial recess 514, and the second portion C2 is in the region from the radial recess 514 to the first upper end portion 511.
  • the three portions C3 correspond to the area from the radial recess 514 to the first bottom 512, respectively.
  • FIG. 4B shows a state in which the injection axis AX of the fuel injected from the injector 18 intersects with the first portion C1 farthest from the injector 18.
  • the egg shape of the first cavity portion 51 has the smallest radius r1 of the first portion C1 and the direction from the first portion C1 toward the second portion C2 as well as the first portion C1 to the third portion.
  • the radius is continuously increased in the arc shape toward the direction of the portion C3. That is, in the cross section of FIG. 4B, the radius r2 of the second portion C2 becomes larger as the distance from the first portion C1 in the counterclockwise direction.
  • the arc shape in which the radius of the arc decreases from the second portion C2 to the first portion C1 and the radius of the arc increases from the first portion C1 to the third portion C3.
  • the connecting portion 53 has a convex shape formed of a curved surface having a predetermined radius r4 from the lower end portion 531 (first upper end portion 511) to the third upper end portion 532 (second inner end portion 521).
  • the second cavity portion 52 has a concave shape formed of a curved surface having a predetermined radius r5 from the second bottom portion 522 to the upright wall region 525.
  • the second upper end portion 523 has a convex shape formed of a curved surface having a predetermined radius r6.
  • the distance in the cylinder axis direction A between the center point of radius r4 and the center point of radius r5 is a first distance Sv
  • the distance in the radial direction B between the center point of radius r5 and the center point of radius r6 is a second
  • Sh is r4 + r5> Sv r5 + r6 ⁇ Sh
  • the numerical values of the radii r4, r5 and r6 are selected so as to satisfy the following relationship.
  • the portion from the second bottom 522 to the upper end position C4 of the rising wall region 525 is formed by an approximate 1 ⁇ 4 arc of the radius r5.
  • the upper end position C4 of the standing wall region 525 is continued to the lower end position of the second upper end portion 523 which is an approximately 1 ⁇ 4 arc of the radius r6.
  • the upper end of the second upper end portion 523 is continued to the peripheral flat portion 55.
  • the lower portion of the standing wall area 525 is located inside the radial direction B with respect to the upper end position C4 of the standing wall area 525.
  • the air-fuel mixture is inward in the radial direction B of the combustion chamber 6 in cooperation with the egg shape of the first cavity portion 51. It is for preventing combustion too much, and performing the combustion which effectively utilized the space (squish space) of the radial direction B rather than standing wall area 525.
  • FIG. 5 is a simplified cross-sectional view of the combustion chamber 6 and schematically shows the relationship between the crown surface 50 (cavity 5C) and the injection axis AX of the fuel injected from the injector 18 and the flow of the mixture after injection. Arrows F11, F12, F13, F21, F22 and F23 are shown.
  • the injector 18 includes a nozzle 181 disposed to project downward from the combustion chamber ceiling 6U to the combustion chamber 6.
  • the nozzle 181 has an injection hole 182 for injecting fuel into the combustion chamber 6.
  • one injection hole 182 is shown in FIG. 5, a plurality of injection holes 182 are actually arranged at the same pitch in the circumferential direction of the nozzle 181.
  • the fuel injected from the injection holes 182 is injected along the injection axis AX in the figure.
  • the injected fuel diffuses at the spray angle ⁇ .
  • FIG. 5 shows an upper diffusion axis AX1 showing the upward diffusion with respect to the injection axis AX, and a lower diffusion axis AX2 showing the downward diffusion.
  • the spray angle ⁇ is an angle formed by the upper diffusion axis AX1 and the lower diffusion axis AX2.
  • the injection hole 182 can inject fuel toward the connection portion 53 of the cavity 5C. That is, the injection hole 182 is provided in the nozzle 181 so as to have an injection axis AX for injecting the fuel toward the connecting portion 53 at a predetermined crank angle of the piston 5.
  • FIG. 5 shows the positional relationship between the injection axis AX and the cavity 5C at the predetermined crank angle.
  • the fuel injected from the injection hole 182 is mixed with the air of the combustion chamber 6 to form an air-fuel mixture, and is blown to the connecting portion 53.
  • the tapered region 524 of the second cavity portion 52 is a surface having an inclination along the injection axis AX.
  • the inclination along the injection axis AX includes substantially the same inclination as the inclination corresponding to the inclination of the injection axis AX with respect to the horizontal line L1 (FIG. 4A) in the radial direction B.
  • the tapered region 524 may be an inclined surface having an inclination that matches the inclination of the upper diffusion axis AX1 or the lower diffusion axis AX2, or an inclination that substantially matches the upper diffusion axis AX1 or the lower diffusion axis AX2.
  • the fuel injected toward the connection portion 53 along the injection axis AX collides with the connection portion 53 and then travels in the direction (downward direction) of the first cavity portion 51 (arrow It is spatially separated in F11) and in the direction (upward direction) of the second cavity 52 (arrow F21). That is, the fuel injected toward the central portion 533 of the connection portion 53 is separated into upper and lower portions, and thereafter mixed with air present in the first and second cavity portions 51 and 52, respectively. , 52 flow along the surface shape.
  • the air-fuel mixture moving in the direction of the arrow F11 enters the radial recessed portion 514 of the first cavity 51 from the lower end 531 of the connecting portion 53, and flows downward. Thereafter, the air-fuel mixture changes the flow direction from the lower side to the inner side in the radial direction B according to the curved shape of the radial recessed portion 514, and as shown by the arrow F12, the bottom surface of the first cavity portion 51 having the first bottom portion 512. Flow according to the shape. At this time, the mixture is mixed with the air of the first cavity portion 51 to dilute the concentration.
  • the bottom surface of the first cavity portion 51 Due to the presence of the mountain portion 54, the bottom surface of the first cavity portion 51 has a shape that rises in the radial direction center. Therefore, the air-fuel mixture flowing in the direction of the arrow F12 is lifted upward, and eventually flows radially outward from the combustion chamber ceiling surface 6U as indicated by the arrow F13. Even in such a flow, the mixture mixes with the air remaining in the combustion chamber 6 to become a homogeneous thin mixture.
  • the formation of the smooth flow of the arrows F11 to F13 also contributes to the egg shape of the first cavity 51 described above with reference to FIG. 4B.
  • the circular arc shape in which the second portion C2, the first portion C1 and the third portion C3 are sequentially connected allows the air-fuel mixture to flow favorably without staying in the first cavity portion 51. That is, the air-fuel mixture (in-cylinder flow) traveling from the connecting portion 53 through the second portion C2 to the first portion C1 is accelerated because the radius of the arc decreases toward the first portion C1. This promotes the flow of the arrow F11.
  • the radius of the arc increases from the first portion C1 toward the third portion C3. For this reason, the air-fuel mixture is guided radially inward while being decelerated at the third portion C3. That is, the air-fuel mixture does not rapidly disturb the flow upward, and flows upward along the first bottom portion 512 as indicated by the arrow F12.
  • the piston 5 descends, reverse skimish flow toward the outer side in the radial direction B is generated in the peripheral flat portion 55.
  • the mixture is drawn outward in the radial direction B as shown by the arrow F13 in combination with being pulled by the reverse skik flow. . Since such flow is secured, stagnation of the air-fuel mixture in the first cavity portion 51 can be suppressed.
  • the air-fuel mixture moving in the direction of arrow F21 enters the tapered region 524 of the second cavity 52 from the third upper end 532 of the connecting portion 53 and proceeds obliquely downward along the inclination of the tapered region 524. . Then, the air-fuel mixture reaches the second bottom 522, as indicated by an arrow F22.
  • the tapered region 524 is a surface having an inclination along the injection axis AX, the air-fuel mixture can smoothly flow radially outward.
  • the air-fuel mixture reaches a deep position on the radially outer side of the combustion chamber 6 due to the presence of the tapered region 524 and the presence of the second bottom 522 where the third upper end 532 of the connecting portion 53 is also located below.
  • the air-fuel mixture is lifted upward by the rising curved surface between the second bottom 522 and the rising wall area 525, and flows radially inward from the combustion chamber ceiling surface 6U.
  • the air-fuel mixture mixes with the air in the second cavity 52 to become a homogeneous thin air-fuel mixture.
  • a standing wall region 525 extending generally in the vertical direction is provided radially outward of the second bottom 522, so that the injected fuel (air-fuel mixture) is the inner peripheral wall of the cylinder 2 (generally, a liner (not shown)). Is blocked from reaching).
  • the air-fuel mixture can flow to the vicinity of the radially outer side of the combustion chamber 6 by the formation of the second bottom 522, the presence of the standing wall region 525 suppresses the interference with the inner peripheral wall of the cylinder 2. For this reason, it is possible to suppress the occurrence of cooling loss due to the interference.
  • the rising wall area 525 has a shape in which the lower portion is positioned inside in the radial direction B with respect to the upper end position C4. For this reason, the flow indicated by the arrow F22 is not excessively strong, and the mixture can be prevented from returning too much inward in the radial direction B. When the flow of the arrow F22 is too strong, the partially burned mixture collides with the fuel before the newly injected fuel is sufficiently diffused, and inhibits homogeneous combustion to generate soot and the like.
  • the rising wall region 525 of the present embodiment does not have a shape that is turned to the outside in the radial direction, and the flow of the arrow F22 is suppressed, and the flow toward the outside of the radial direction B indicated by the arrow F23 is also generated Do.
  • the flow may be pulled by the reverse flow and the flow of the arrow F23 is likely to occur. Therefore, it is possible to perform combustion effectively utilizing the space radially outside the standing wall region 252 (the squish space on the peripheral flat portion 55). Therefore, the occurrence of soot and the like can be suppressed, and combustion can be realized by effectively utilizing the entire combustion chamber space.
  • the fuel injected toward the connection portion 53 along the injection axis AX collides with the connection portion 53 and is spatially separated, and exists in the spaces of the first and second cavity portions 51 and 52, respectively. Air to produce a mixture.
  • the space of the combustion chamber 6 can be widely used to form a homogeneous thin air-fuel mixture, and generation of soot and the like can be suppressed at the time of combustion.
  • FIG. 6 is a time chart showing an example of the timing of fuel injection from the injector 18 to the cavity 5C and the heat release rate characteristic E1 at that time. Note that FIG. 6 also shows the ideal characteristic E0 of the heat release rate.
  • the ideal characteristic E0 is a heat release rate characteristic having a high degree of equivalence and a short combustion period (about crank angle CA10).
  • the above-described spatial separation of the fuel injection and the temporal separation of the fuel injection described here are devices for obtaining the heat release rate characteristic E1 as close as possible to the ideal characteristic E0.
  • the operation of fuel injection by the injector 18 is controlled by a fuel injection control unit 18A (see FIG. 1).
  • the fuel injection control unit 18A causes the injector 18 to perform three fuel injections of the pilot injection P1, the main injection P2, and the pre-injection P3 per cycle.
  • the main injection P2 is a fuel injection that is performed at a timing when the piston 5 is located near the compression top dead center (TDC).
  • FIG. 6 shows an example in which the main injection P2 is performed at a timing slightly delayed from TDC.
  • the pilot injection P1 is a fuel injection that is performed earlier than the main injection P2 and earlier than TDC.
  • FIG. 6 shows an example in which pilot injection P1 is performed in a period of crank angle -CA16 to -CA12.
  • the injection rate peak value of the fuel is the same for the pilot injection P1 and the main injection P2, but the fuel injection period is set to be longer in the former.
  • the pre-injection P3 is a small amount of fuel injection performed between the pilot injection P1 and the main injection P2.
  • the pre-injection P3 is executed for the purpose of reducing noise as much as possible by making the valley between peaks in the heat release rate characteristic E1 (the valley near the crank angle CA2 to 3) as small as possible. May be omitted.
  • the fuel injection directed to the connection portion 53 described above is performed at the time of the pilot injection P1. That is, the injection hole 182 of the injector 18 is an injection hole having an injection axis AX for injecting fuel toward the connecting portion 53 at a crank angle at which the pilot injection P1 is performed.
  • Main injection P2 forms a flow in which the fuel (air-fuel mixture) injected in pilot injection P1 is spatially separated up and down as shown in FIG.
  • the fuel injection which is executed to utilize the air remaining in the space to form a new mixture. That is, the fuel injection control unit 18A moves up and down at timing when the fuel supplied in the first fuel injection (pilot injection P1) enters the space of the first and second cavity portions 51 and 52 and is spatially separated.
  • the second fuel injection (main injection P2) that utilizes the air existing in the mixture of (1) is temporally separated and executed (temporal separation of fuel injection).
  • FIGS. 7A to 7D schematically show the state of generation of air-fuel mixture in the combustion chamber 6 of the present embodiment along the crank angle CA.
  • the darkly colored portions indicate that the mixture has a high fuel concentration.
  • pilot injection P1 fuel is injected toward the connecting portion 53 of the cavity 5C.
  • the injection fuel of the pilot injection P1 is mixed with the air in the combustion chamber 6 and blows to the connecting portion 53 while becoming the first mixture M1.
  • the first mixture M1 has not progressed in diffusion yet, and the fuel concentration is high.
  • the first air-fuel mixture M1 is separated into the lower air-fuel mixture M11 directed to the first cavity 51 and the upper air-fuel mixture M12 directed to the second cavity 52 by blowing into the connecting portion 53. This is the spatial separation of the mixture described above.
  • the piston 5 is at a position of approximately TDC, fuel is injected toward the slightly lower position of the connecting portion 53 in the main injection P2.
  • the lower mixture M11 and the upper mixture M12 of the pilot injection P1 injected earlier enter the first cavity 51 and the second cavity 52, respectively, and are mixed with the air in the respective spaces to proceed with dilution. ing.
  • unused air air not mixed with fuel
  • the egg shape of the first cavity 51 contributes to the formation of such an unused air layer.
  • the injection fuel of the main injection P2 is in the form of entering between the lower mixture M11 and the upper mixture M12, and mixed with the unused air to form a second mixture M2.
  • FIG. 7C shows the state of the combustion chamber 6 in which the crank angle has advanced by 1 degree from the state of FIG. 7B.
  • the diffusion of the lower mixture M11 and the upper mixture M12 is increased to increase the area. It can be seen that the mixing of the second mixture M2 with the unused air proceeds between the lower mixture M11 and the upper mixture M12 to form a mixture M21 having a reduced concentration. This is the temporal separation of fuel injection.
  • the fuel injected from the pilot injection P1 and the fuel injected from the main injection P2 each generate an air-fuel mixture without interference in the combustion chamber 6. That is, fuel is not injected by the main injection P2 in a superimposed manner in the space where the lower mixture M11 and the upper mixture M12 already exist, but the fuel is in the space between the two mixtures M11 and M12. It is injected. Therefore, the mixture M21 is generated in the form of effectively utilizing the space (air) of the combustion chamber 6.
  • the second point is that the upper mixture M12 does not reach the inner peripheral wall of the cylinder 2. This originates in the geometrical feature of the 2nd cavity part 52 that penetration of upper part mixture M12 to peripheral flat part 55 does not occur easily by existence of above-mentioned standing wall field 525. This contributes to the suppression of cold loss.
  • the lower air-fuel mixture M11 and the upper air-fuel mixture M12 by the pilot injection P1 and the air-fuel mixture M21 by the main injection P2 are well mixed because the flow is promoted by the jet generated by the main injection P2. Together, they form a synthetic mixture M3. That is, it can be seen that a homogeneous thin synthetic mixture M3 is widely generated, which widely uses the space in the combustion chamber 6. Therefore, it is possible to realize the combustion which hardly generates soot.
  • Comparative example 1 and comparative example 2 are shown for evaluation of piston 5 provided with cavity 5C concerning this embodiment.
  • FIG. 8 is a cross-sectional view of a piston 500 provided with a cavity 50C according to the first comparative example.
  • the cross-sectional shape of the cavity 5C of the present embodiment is indicated by a dotted line.
  • the cavity 50C of the first comparative example has a cavity portion 510 recessed in the radial center region of the piston 500, a flat portion 571 provided in the radially outer region, and a lip between the cavity portion 510 and the flat portion 571.
  • a unit 572 is provided.
  • the cavity 50C of Comparative Example 1 is an aspect in which the second cavity portion 52 in the present embodiment does not exist. That is, in the cavity 50C, there is no portion located below the lip 572 in the radial direction outside the lip 572 (the portion corresponding to the connecting portion 53 in this embodiment). This is different from the cavity 5C of the present embodiment.
  • FIG. 9 is a time chart in which the timing of fuel injection and the heat release rate are superimposed on each other when the cavity 50C according to Comparative Example 1 is adopted in the time chart of FIG. Also in Comparative Example 1, three fuel injections of pilot injection Q1, main injection Q2 and pre-injection Q3 are performed per cycle, as in the present embodiment.
  • the position of the lip portion 572 is higher than the position of the connecting portion 53 of the present embodiment by the absence of the second cavity portion 52. Therefore, the start timing of the pilot injection Q1 is set approximately 8 degrees earlier in crank angle CA than the pilot injection P1 of the present embodiment, and the injection axis AX is directed to the lip portion 572.
  • the start timing of the main injection Q2 is also set slightly later than the main injection P2.
  • FIGS. 10A to 10C schematically show the state of generation of air-fuel mixture in the combustion chamber 6 when the cavity 50C of Comparative Example 1 is employed.
  • FIG. 10A shows the state of the combustion chamber at the time of execution of the pilot injection Q1.
  • fuel is injected toward the lip 572 of the cavity 50C.
  • the fuel injected from the pilot injection Q1 is mixed with the air in the combustion chamber to form the first mixture N1, and is blown to the lip portion 572.
  • the first mixture N1 is separated into the lower mixture N11 directed to the cavity portion 510 and the upper mixture N12 directed upward.
  • FIG. 10B shows the state of the combustion chamber at the timing when the main injection Q2 ends.
  • the piston 5 is approximately at TDC, so that in the main injection Q2, the fuel is injected toward the cavity portion 510 located below the lip 572.
  • the injection fuel of the main injection Q2 is the second mixture N2.
  • the upper mixture N12 of the pilot injection Q1 injected earlier does not generate the flow as shown by the arrow F22 in FIG. 5 because the second cavity 52 of the present embodiment does not exist, and the flat portion 571 Deep into the area between the chamber and the ceiling surface of the combustion chamber (squish area). Therefore, the upper air-fuel mixture N12 interferes with the inner peripheral wall of the cylinder 2 and a cold loss occurs.
  • FIG. 10C shows the state of the combustion chamber at a timing corresponding to the timing at which the combustion ends.
  • the second mixture N2 by the main injection Q2 and the lower mixture N11 by the pilot injection Q1 are mixed to form a combined mixture N3.
  • the upper mixture N12 is not sufficiently mixed with the composite mixture N3, and an air layer N0 (or a mixture whose fuel concentration is considerably low) is interposed between the two. For this reason, it is difficult to say that a sufficiently homogeneous thin air-fuel mixture is generated in the combustion chamber.
  • the fuel spray period (period from the start of pilot injection P1 to the end of main injection P2) is the spray period of comparative example 1 (the start of pilot injection Q1 to main injection Q2).
  • Period of termination can be shorter than As a result, although the 10-90% combustion period also required 20.3 deg in terms of crank angle in Comparative Example 1, according to this embodiment, it could be shortened to 15.9 deg. Thereby, it was confirmed that the fuel consumption performance is improved by the application of the cavity 5C of the present embodiment.
  • FIG. 11 is a cross-sectional view showing the structure of the cavity 500C of Comparative Example 2. As shown in FIG. In FIG. 11, the cross-sectional shape of the cavity 5C of the present embodiment is indicated by a dotted line.
  • the cavity 500C of Comparative Example 2 includes a first cavity portion 51A recessed in a radial center region of the piston 500A, and a second cavity portion 52A provided in an outer region of the first cavity portion 51A in the radial direction B; And a connecting portion 53A connecting the two cavity portions 51A and 52A.
  • a standing wall region 525A is provided outside the bottom of the second cavity 52A in the radial direction B. That is, the components of the cavity 500C of Comparative Example 2 are the same as the cavity 5C of the present embodiment.
  • the difference between the cavity 500C and the cavity 5C of the present embodiment is the shape of the standing wall region 525A.
  • the lower portion of the standing wall area 525A is located outside in the radial direction B with respect to the upper end position C4 of the standing wall area 525A. That is, the standing wall region 525A has a shape that is turned to the outside in the radial direction B with respect to the perpendicular e in contact with the upper end position C4.
  • FIG. 12 (A) shows the in-cylinder flow when the cavity 500C of Comparative Example 2 is adopted
  • FIG. 12 (B) shows the in-cylinder flow when the cavity 5C of this embodiment is adopted.
  • the timings shown in FIGS. 12A and 12B correspond to the timing at which the main injection P2 shown in FIG. 7B is performed.
  • the air-fuel mixture is the lower side mixture M110 toward the first cavity portion 51A, and the second cavity portion 52A. It is separated into the upper mixture M 120 toward the
  • the lower air-fuel mixture M110 proceeds inward in the radial direction B along the surface shape of the first cavity portion 51A.
  • the upper air-fuel mixture M120 also travels outward in the radial direction B along the surface shape of the second cavity portion 52A, and then travels in the forward wall region 525A by hitting it.
  • the standing wall region 525A has an arc shape turned to the outside in the radial direction B, the upper mixture M 120 is vigorously folded back in the radial direction B by the arc-shaped portion. Even with the assistance of the reverse squish flow RSQ generated when the piston 5 descends, this flow tendency of the upper mixture M 120 does not change much.
  • the upper air-fuel mixture M120 collides with the fuel injected by the main injection P2. That is, the injected fuel of the main injection P2 collides with the upper air-fuel mixture M120 before it is sufficiently diffused in the combustion chamber 6. At this stage, the upper mixture M 120 partially burns and is flamed, and the collision causes the injected fuel to burn before it becomes a homogeneous mixture. Therefore, wrinkles may be generated.
  • the air-fuel mixture includes the lower mixture M11 toward the first cavity 51 and the upper mixture M12 toward the second cavity 52. Separated into The lower and upper mixture gases M11 and M12 flow along the surface shapes of the first and second cavity portions 51 and 52, respectively.
  • the standing wall area 525 has a shape in which the lower portion of the standing wall area 525 is positioned inside in the radial direction B with respect to the upper end position C4. More specifically, from the second bottom portion 522 of the second cavity portion 52 to the upper end position C4, a curved surface of approximately 1 ⁇ 4 arc having a radius r5 is provided.
  • the upper air-fuel mixture M12 is lifted in the cylinder axial direction A instead of being vigorously folded back inward in the radial direction B as in the comparative example 2. Thereafter, the upper air-fuel mixture M12 is divided into an inner component M12A directed inward in the radial direction B and an outer component M12B directed outward in the radial direction B.
  • the reverse squish flow RSQ contributes to the formation of the outer component M12B.
  • the inner component M12A does not have the force to collide with the injected fuel of the main injection P2, and the circulating flow of the lower mixture M11 brought about by the egg shape shape of the first cavity 51 and the reverse squish flow RSQ (FIG.
  • the fuel injection control by the fuel injection control unit 18A shown in FIG. 6 is useful when the engine body 1 is a diesel engine and partially performs homogeneous charge compression ignition (PCI) combustion.
  • PCI charge compression ignition
  • the above-mentioned medium load is, for example, an operating range where the engine speed is 2000 rpm and the BMEP is approximately 600 kPa.
  • the effect of the above-described spatial separation of the mixture tends to be insufficient when the amount of fuel injected from the injector 18 is large (high load) and small (low load).
  • the volume of the first cavity 51 is not sufficient for the amount of fuel, that is, the first cavity 51 has a small volume by dividing the cavity 5C into the two cavities 51 and 52.
  • the fuel-rich mixture tends to be formed.
  • the load is low, the fuel concentration of the air-fuel mixture in the space of the first and second cavity portions 51 and 52 becomes too thin, and the ignitability tends to decrease. Therefore, it is desirable to execute the fuel injection control including the pilot injection P1 in the above-mentioned medium load operation scene where these tendencies do not easily occur.
  • the cavity 5C formed on the crown surface 50 of the piston 5 is the first cavity portion 51 in the central region in the radial direction B, and the first cavity portion 51
  • the depth of the cylinder axial direction A is shallower than that of the second cavity portion 52 disposed on the outer peripheral side in the radial direction B to form a two-stage structure.
  • the second bottom 522 of the second cavity 52 is positioned lower than the third upper end 532 of the connecting portion 53 connecting the two cavities 51 and 52.
  • the second cavity portion 52 is provided with a standing wall region 525.
  • the standing wall region 525 makes it difficult for the air-fuel mixture to easily reach the inner peripheral wall of the cylinder 2, but it can be structured such that it can be directed to the outside in the radial direction B to some extent.
  • the lower portion of the upright wall region 525 has a structure located inside in the radial direction B with respect to the upper end position C4 of the upright wall region 525. In this way, combustion is performed so as to prevent the air-fuel mixture from being excessively returned to the inside in the radial direction B of the combustion chamber 6 while reducing the cooling loss, and effectively utilizing the space (squish space) radially outside the standing wall region 525. Can be done.
  • the flow provided by the egg shape shape of the first cavity portion 51 also contributes to the effective use of the squish space.
  • the air-fuel mixture can be generated by utilizing the air present in the space of the first and second cavity portions 51 and 52, respectively.
  • the fuel injection control unit 18A causes the injector 18 to execute the main injection P2 for performing the fuel injection near TDC and the pilot injection P1 for performing the fuel injection at a timing earlier than the main injection P2.
  • the fuel is injected toward the connecting portion 53 in the pilot injection P1.
  • the fuel injected by the main injection P2 exists between the lower mixture M11 and the upper mixture M12 spatially separated so as to enter the space of the first and second cavity portions 51 and 52.
  • Air can be used to form a new second mixture M2. That is, the main injection P2 separates from the pilot injection P1 in time, and an air-fuel mixture is formed using the air present in the combustion chamber 6 by the main injection P2. Therefore, a more homogeneous and thin mixture can be formed in the combustion chamber 6.
  • a combustion chamber structure of an engine includes a combustion chamber of the engine formed by a lower surface of a cylinder head, a cylinder and a crown surface of a piston, and a fuel injection valve for injecting fuel into the combustion chamber.
  • a cavity is provided on a crown surface of the piston, and the fuel injection valve injects fuel toward the cavity, and a radial center of the combustion chamber or the fuel injection valve
  • a first cavity portion disposed in the vicinity, the cavity being disposed in a radial center region of the crown surface, and having a first bottom portion having a first depth in a cylinder axial direction;
  • a second cavity portion disposed on an outer peripheral side of the first cavity portion and having a second bottom portion having a second depth shallower than the first depth in the cylinder axial direction; the first cavity and the first cavity A connecting portion connecting the cavity portion, and a rising wall region disposed radially outward of the second bottom portion of the second cavity portion, the second bottom portion in the axial direction of the cylinder in the connecting portion
  • the lower portion of the standing wall area is located radially inward with respect to the upper end position of the standing wall area.
  • the cavity formed on the crown surface of the piston has a first cavity portion in the radial center region of the crown surface and a diameter smaller in depth in the cylinder axial direction than the first cavity portion. It has a two-stage structure with a second cavity portion disposed on the outer peripheral side in the direction. Furthermore, the second bottom portion of the second cavity portion is located below the upper end portion of the connecting portion connecting the two cavities. Therefore, when fuel is injected from the fuel injection valve disposed at or near the radial center of the combustion chamber toward the cavity, an air-fuel mixture of the fuel and air in the combustion chamber is mixed in the second bottom portion. As a result, the air-fuel mixture can be easily directed outward in the radial direction of the combustion chamber. Therefore, according to the above combustion chamber structure, the air in the combustion chamber can be effectively used to form a homogeneous thin air-fuel mixture, and the generation of soot and the like can be suppressed.
  • a standing wall region is provided radially outside the second bottom portion of the second cavity portion.
  • this standing wall region it is possible to make the air-fuel mixture difficult to reach the cylinder inner peripheral wall easily, and it is possible to reduce the cold loss.
  • the lower portion of the standing wall area has a structure located radially inward with respect to the upper end position of the standing wall area. As a result, the mixture can be prevented from returning excessively inward in the radial direction of the combustion chamber, and combustion can be performed effectively utilizing the space (squish space) radially outward of the standing wall region.
  • the flow in the cylinder directed radially inward is not too strong, and the flow in the cylinder directed radially outward from the standing wall region is also assisted by the reverse squish flow generated when the piston descends. Can be generated to some extent. Therefore, the occurrence of soot and the like can be suppressed, and combustion can be realized by effectively utilizing the entire combustion chamber space.
  • the first cavity portion is located between a first portion in a circular arc shape farthest from the fuel injection valve, the first portion, and the connection portion in a cross section including a cylinder axis.
  • a second portion and a third portion extending radially inward from the first portion, wherein the radius of the arc decreases from the second portion to the first portion, and the arc from the first portion to the third portion It is desirable to have an arc shape in which the radius of.
  • the mixture can be favorably flowed without staying in the first cavity portion. That is, the in-cylinder flow from the connecting portion to the first portion through the second portion is accelerated because the radius of the arc decreases toward the first portion. Thereafter, the in-cylinder flow is guided radially inward while being decelerated at the third portion. When the reverse squish flow is present, the in-cylinder flow is pulled by this and is directed radially outward again. Since such flow is secured, stagnation of the air-fuel mixture in the first cavity portion can be suppressed.
  • the fuel injection valve has an injection hole for injecting fuel, and the injection hole is an injection hole having an injection shaft for injecting fuel toward the connecting portion at a predetermined crank angle. It is desirable to have.
  • the fuel injected toward the connecting portion collides with the connecting portion, whereby the fuel is directed toward the first cavity portion (downward), the second cavity portion (the upper portion) Separated in direction towards the direction). For this reason, the air-fuel mixture can be generated by utilizing the air respectively present in the space of the first and second cavity portions.
  • the fuel injection control unit controls an operation of fuel injection by the fuel injection valve, and the fuel injection control unit is configured to perform the fuel injection at a timing when at least the piston is positioned near a compression top dead center. And a pilot injection for causing the fuel injection to be performed at a timing earlier than the main injection, the fuel injection valve performing a crank injection in which the pilot injection is performed. It is desirable that the injection hole has an injection shaft for injecting fuel toward the connecting portion at a corner.
  • the fuel injected in the pilot injection becomes the above-described spatially separated fuel.
  • the fuel injected by the main injection utilizes the air existing between the air-fuel mixture spatially separated to enter the space of the first and second cavity portions to form a new air-fuel mixture It will be done. That is, the air-fuel mixture is formed using air present in the combustion chamber separately from the pilot injection in time. Therefore, it is possible to form a more homogeneous and thin mixture in the combustion chamber.
  • the fuel injection control unit execute the pilot injection in an operating region in which the load of the engine is a medium load.
  • the benefits of the above-described spatial separation of fuels tend to not be fully realized when the amount of fuel injected is too high (high load) and too low (low load).
  • the volume of the first cavity located at the lower side in the cylinder axial direction is not sufficient for the amount of fuel, that is, the first cavity is formed by dividing the cavity into two cavities. Due to the small volume, an air-fuel mixture having a high fuel concentration tends to be formed and soot to be generated.
  • the fuel concentration of the air-fuel mixture in the space of the first and second cavity portions becomes too thin, and the ignitability tends to be reduced. Therefore, it is desirable to carry out the pilot injection in the medium load operating region where these tendencies do not easily occur.
  • the cavity includes a tapered region extending from the upper end of the connection portion toward the second bottom of the second cavity portion, and the tapered region has an inclination along the injection axis. It is desirable to have a face.
  • the cavity includes a tapered region having an inclination along the injection axis of the fuel injection valve, the injected fuel is not inhibited and the radial direction of the combustion chamber along the tapered region. You can go smoothly to the outside. Therefore, it contributes to the formation of a more homogeneous and thin mixture.
  • the air in the combustion chamber is effectively used to form a homogeneous thin air-fuel mixture, generating soot and the like
  • An engine combustion chamber structure that can be suppressed as much as possible can be provided.

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Abstract

L'invention concerne une structure de chambre de combustion d'un moteur comprenant une chambre de combustion de moteur et une soupape de pulvérisation de carburant. La soupape de pulvérisation de carburant pulvérise du carburant en direction d'une cavité d'une surface de tête de piston. La cavité comprend : une première partie cavité disposée dans une région radialement centrale sur la surface de tête et pourvue d'un premier fond ayant une première profondeur dans une direction axiale de cylindre ; une seconde partie cavité disposée, sur la surface de tête, sur un côté circonférentiel externe de la première partie cavité, et pourvue d'un second fond ayant une seconde profondeur inférieure à la première profondeur dans la direction axiale du cylindre ; une partie de raccordement destinée à relier la première partie cavité et la seconde partie cavité ; et une région paroi verticale disposée davantage à l'extérieur dans la direction radiale que le second fond de la seconde partie cavité. Le second fond est positionné plus bas dans la direction axiale du cylindre qu'une extrémité supérieure de la partie de raccordement, et une partie côté inférieur de la région de paroi verticale est positionnée sur l'intérieur dans une direction horizontale par rapport à une position d'extrémité supérieure de la région de paroi verticale.
PCT/JP2018/031111 2017-08-28 2018-08-23 Structure de chambre de combustion de moteur WO2019044647A1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP18851330.3A EP3663556B1 (fr) 2017-08-28 2018-08-23 Structure de chambre de combustion de moteur
US16/641,758 US11092107B2 (en) 2017-08-28 2018-08-23 Combustion chamber structure of engine
CN201880055364.6A CN111051663B (zh) 2017-08-28 2018-08-23 发动机的燃烧室结构

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JP2021181765A (ja) * 2020-05-19 2021-11-25 株式会社小松製作所 ディーゼルエンジン用のピストン及びディーゼルエンジン
CN114412652B (zh) * 2022-03-29 2022-06-24 潍柴动力股份有限公司 一种发动机燃烧系统控制方法及发动机燃烧系统

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