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WO2022208829A1 - Intake structure for internal combustion engine - Google Patents

Intake structure for internal combustion engine Download PDF

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Publication number
WO2022208829A1
WO2022208829A1 PCT/JP2021/014094 JP2021014094W WO2022208829A1 WO 2022208829 A1 WO2022208829 A1 WO 2022208829A1 JP 2021014094 W JP2021014094 W JP 2021014094W WO 2022208829 A1 WO2022208829 A1 WO 2022208829A1
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WO
WIPO (PCT)
Prior art keywords
intake passage
fuel injection
combustion chamber
internal combustion
combustion engine
Prior art date
Application number
PCT/JP2021/014094
Other languages
French (fr)
Japanese (ja)
Inventor
達也 川手
博篤 乾
健吾 富沢
Original Assignee
本田技研工業株式会社
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
Application filed by 本田技研工業株式会社 filed Critical 本田技研工業株式会社
Priority to JP2023510101A priority Critical patent/JP7443622B2/en
Priority to PCT/JP2021/014094 priority patent/WO2022208829A1/en
Publication of WO2022208829A1 publication Critical patent/WO2022208829A1/en

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B31/00Modifying induction systems for imparting a rotation to the charge in the cylinder
    • F02B31/02Modifying induction systems for imparting a rotation to the charge in the cylinder in engines having inlet valves arranged eccentrically to cylinder axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B31/00Modifying induction systems for imparting a rotation to the charge in the cylinder
    • F02B31/04Modifying induction systems for imparting a rotation to the charge in the cylinder by means within the induction channel, e.g. deflectors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M69/00Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M69/00Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • F02M69/04Injectors peculiar thereto
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Definitions

  • the present invention relates to an intake structure for an internal combustion engine.
  • An internal combustion engine has an intake passage leading to a combustion chamber and a fuel injection valve provided in the intake passage.
  • a configuration is disclosed in which a tumble is held near the center of the combustion chamber (for example, Patent Document 1).
  • the intake passage is divided into an upper intake passage and a lower intake passage through a partition wall in order to generate a tumble flow, and the cross-sectional area of the lower intake passage is larger than that of the main intake passage.
  • a configuration with a small value for example, Patent Document 2.
  • the present invention has been made in view of the circumstances described above, and an object of the present invention is to provide an intake structure for an internal combustion engine that facilitates obtaining an air-fuel mixture that is advantageous for improving combustion efficiency.
  • An intake passage leading to a combustion chamber and a fuel injection device provided in the intake passage the intake passage being separated from the combustion chamber in the vertical direction corresponding to the axial direction of the combustion chamber and a main intake passage.
  • an auxiliary intake passage wherein the auxiliary intake passage has a cross-sectional area smaller than that of the main intake passage, wherein the auxiliary intake passage is positioned on either side of the axis of the combustion chamber. and the injection direction of the fuel injection device is oriented in the one direction with respect to the axis of the combustion chamber.
  • downstream side cross-sectional area of the auxiliary intake passage may be smaller than the upstream side cross-sectional area of the auxiliary intake passage.
  • the fuel injection device has a fuel injection valve and a valve mounting member to which the fuel injection valve is mounted, and the valve mounting member is fastened to the main intake passage or the combustion chamber.
  • the fuel injection valve and the fastening portion may be arranged so as to be distributed to one side and the other side with respect to the center of the main intake passage.
  • the fuel injection valve and the fastening portion may at least partially overlap the main intake passage when viewed from above.
  • the internal combustion engine includes a breather hose through which blow-by gas of the internal combustion engine passes, and the breather hose is positioned on the opposite side of the fastening portion with respect to the center of the main intake passage.
  • the fuel injection valve of the fuel injection device is located on the opposite side of the axis of the combustion chamber from the side to which the injection direction is directed, with respect to the center of the main intake passage. good too.
  • the auxiliary intake passage and the injection direction of the fuel injection device may be directed to the opposite side of the ignition plug with respect to the axis of the combustion chamber.
  • An intake passage leading to a combustion chamber and a fuel injection device provided in the intake passage the intake passage being separated from the combustion chamber in the vertical direction corresponding to the axial direction of the combustion chamber and a main intake passage.
  • an auxiliary intake passage wherein the auxiliary intake passage has a cross-sectional area smaller than that of the main intake passage, wherein the auxiliary intake passage is positioned on either side of the axis of the combustion chamber. and the injection direction of the fuel injector is directed to the one-way position with respect to the axis of the combustion chamber.
  • the downstream side cross-sectional area of the auxiliary intake passage may be smaller than the upstream side cross-sectional area of the auxiliary intake passage. According to this configuration, the flow velocity of the air flowing into the combustion chamber from the auxiliary intake passage is increased, and the mixing of the air and the fuel can be further promoted.
  • the fuel injection device has a fuel injection valve and a valve mounting member to which the fuel injection valve is mounted, and the valve mounting member is fastened to the main intake passage or the combustion chamber.
  • the fuel injection valve and the fastening portion may be arranged so as to be distributed to one side and the other side with respect to the center of the main intake passage. According to this configuration, it is easy to prevent the fuel injection valve and the valve mounting member from being arranged to protrude on one side and the other side of the main intake passage.
  • the fuel injection valve and the fastening portion may at least partially overlap the main intake passage when viewed from above. According to this configuration, it becomes easy to arrange the fuel injection valve and the valve mounting member in a compact manner by utilizing the empty space that overlaps with the main intake passage in a top view.
  • the internal combustion engine includes a breather hose through which blow-by gas of the internal combustion engine passes, and the breather hose is positioned on the opposite side of the fastening portion with respect to the center of the main intake passage.
  • the fuel injection valve of the fuel injection device is located on the opposite side of the axis of the combustion chamber from the side to which the injection direction is directed, with respect to the center of the main intake passage. good too. According to this configuration, it is possible to suppress adhesion of fuel to the wall surface of the intake passage and the wall surface of the combustion chamber.
  • the auxiliary intake passage and the injection direction of the fuel injection device may be directed to the opposite side of the ignition plug with respect to the axis of the combustion chamber. According to this configuration, the spark plug hardly obstructs the swirl flow generated in the combustion chamber by the air from the auxiliary intake passage.
  • FIG. 1 is a view showing the left side of a power unit having an air intake structure of the present invention together with its peripheral configuration.
  • FIG. 2 is a diagram showing the top surface of the power unit together with the peripheral configuration.
  • FIG. 3 is a side sectional view of the periphery of the cylinder head of the power unit.
  • FIG. 4 is a diagram showing the inlet pipe and a part of the peripheral structure as viewed from the crankshaft side along the cylinder axis.
  • FIG. 5 is a diagram in which the description related to the fuel injection device is deleted from FIG. 4 and the central axis line LB of the auxiliary intake passage is added.
  • FIG. 6 is a view showing the inlet pipe together with a part of the peripheral structure from the side of the cylinder. 7 is a cross-sectional view taken along line VII-VII of FIG. 5.
  • FIG. 8 is a cross-sectional view taken along line VIII-VIII of FIG. 6.
  • directions such as front, rear, left, right, and up and down are directions based on the vehicle body unless otherwise specified.
  • Symbol FR shown in each figure indicates the front of the vehicle body
  • symbol UP indicates the upper part of the vehicle body
  • symbol LH indicates the left side of the vehicle body.
  • FIG. 1 is a view showing the left side of a power unit 1 having an air intake structure of the present invention together with its peripheral structure
  • FIG. 2 is a view showing the upper surface of the power unit 1 together with its peripheral structure.
  • the power unit 1 is a power unit supported by a body frame of a scooter type motorcycle so as to be vertically swingable, and is also called a swing type power unit.
  • the power unit 1 includes a crankcase 3 that rotatably supports a crankshaft 2 at the front, a cylinder block 4 provided at the front of the crankcase 3, and a It has a mounted cylinder head 5 and a head cover 6 closing an opening of the cylinder head 5.
  • - ⁇ A cylinder portion consisting of a cylinder block 4, a cylinder head 5 and a head cover 6 is tilted forward from the front portion of the crankcase 3 to a state substantially close to water.
  • a portion consisting of the crankcase 3 , the cylinder block 4 , the cylinder head 5 and the head cover 6 constitutes a single-cylinder four-stroke cycle air-cooled internal combustion engine (hereinafter simply referred to as the "internal combustion engine") 10 .
  • a power transmission case portion 11 is connected to the left side of the crankcase 3 .
  • the power transmission case portion 11 accommodates a belt-type continuously variable transmission that changes the speed of the rotation of the crankshaft 2 and transmits it to the rear wheel shaft 12 .
  • the inlet pipe 15 extends from the upper part of the cylinder head 5, curves backward, and is connected to the throttle body 16.
  • An air cleaner device 18 is connected to the rear end of the throttle body 16 via a connecting tube 17 .
  • the air cleaner device 18 is arranged above the power transmission case portion 11 .
  • a throttle valve (not shown) is provided in the throttle body 16, and the amount of intake air to the internal combustion engine 10 is adjusted by the throttle valve.
  • the inlet pipe 15 , throttle body 16 and connecting tube 17 form part of an intake passage 50 that supplies air cleaned by the air cleaner device 18 to the internal combustion engine 10 .
  • an exhaust pipe 19 extends from the bottom of the cylinder head 5. After extending to the right side of the cylinder head 5 , the exhaust pipe 19 extends rearward and is connected to a muffler 20 .
  • Reference numeral LC in FIG. 2 denotes a center line extending linearly in the front-rear direction through the left-right center of the inlet pipe 15, and is hereinafter referred to as an "intake passage center line LC". This intake passage centerline LC also coincides with the left-right centerline of the power unit 1 .
  • the head cover 6 is connected to a breather hose 21 through which blow-by gas passes.
  • the breather hose 21 extends rightward from the upper portion of the head cover 6 and then extends rearward to be connected to the air cleaner device 18 .
  • the breather hose 21 extends rearward through the head cover 6, the cylinder block 4, and the right side of the connecting tube 17 when viewed from above, and extends left rearward along the connecting tube 17. It extends obliquely and is connected to the air cleaner device 18 .
  • FIG. 3 is a side cross-sectional view around the cylinder head 5 of the power unit 1.
  • the cylinder block 4 has a plurality of fins 4F on its outer surface and cylinder bores 22 formed therein.
  • a piston 23 is slidably provided in the cylinder bore 22 .
  • the piston 23 is connected to the crankshaft 2 via a connecting rod, and the piston 23 slides in the cylinder bore 22 to rotate the crankshaft 2 .
  • a space between the top surface of the piston 23 and the ceiling surface of the combustion chamber of the cylinder head 5 facing the top surface constitutes a combustion chamber 24 .
  • reference character L0 denotes an axis that passes through the center of the combustion chamber 24 and coincides with the axis of the cylinder portion.
  • the internal combustion engine of this embodiment employs a SOHC type two-valve system, and a valve mechanism 25 is provided in the space between the cylinder head 5 and the head cover 6 .
  • the valve mechanism 25 includes a camshaft 26 to which the rotation of the crankshaft 2 is transmitted at half the rotation speed via a cam chain (not shown). Rotation of the camshaft 26 operates an intake valve 28 that opens and closes an intake port 27 via an intake cam and an intake rocker arm (not shown). The rotation of the camshaft 26 also operates an exhaust valve 30 that opens and closes the exhaust port 29 via an exhaust cam and an exhaust rocker arm (not shown).
  • the intake port 27 is a passage that communicates the combustion chamber 24 and the inlet pipe 15, and constitutes a part of the intake passage 50.
  • the exhaust port 29 is a passage that allows the combustion chamber 24 and the exhaust pipe 19 to communicate with each other.
  • the valve mechanism 25 opens and closes the intake port 27 and the exhaust port 29 at timings corresponding to four cycles of intake stroke and exhaust stroke.
  • a spark plug 31 is attached to the cylinder head 5 and has a tip facing a position avoiding the intake port 27 and the exhaust port 29 .
  • the intake passage 50 of this embodiment has a structure that generates a tumble flow T (see FIG. 2) in the combustion chamber 24, that is, an intake structure that provides vertical rotation. More specifically, the intake passage 50 is separated from the combustion chamber 24 in the vertical direction corresponding to the direction of the axis L0 of the combustion chamber 24 by the partition wall 32 leading from the inlet pipe 15 to the intake port 27.
  • an intake passage 50A hereinafter referred to as a main intake passage 50A
  • auxiliary intake passage 50B hereinafter referred to as an auxiliary intake passage 50B
  • the auxiliary intake passage 50B is formed as a tumble flow path for generating a tumble flow T within the combustion chamber 24. As shown in FIG.
  • the auxiliary intake passage 50B is formed in a passage having a cross-sectional area (also referred to as a cross-sectional area) smaller than that of the main intake passage 50, and when the intake air amount of the internal combustion engine 10 is relatively small or in an idling state or a low speed rotation state, Air is supplied so that a tumble flow T can be generated. That is, when the opening degree of the throttle valve in the throttle body 16 located upstream of both intake passages 50A and 50B is relatively small, the air cleaned by the air cleaner device 18 mainly passes through the auxiliary intake passage 50B. , to generate a tumble flow T.
  • the main intake passage 50A functions as a passage for sufficiently supplying air when the internal combustion engine 10 has a relatively large amount of intake air and is in a medium/high speed rotation state or an acceleration state. That is, when the opening of the throttle valve in the throttle body 16 becomes relatively large, the air from the air cleaner device 18 passes through both the main intake passage 50A and the auxiliary intake passage 50B, and sufficient air is supplied to the combustion chamber 24. be.
  • the power unit 1 includes a fuel injection device 60 that injects fuel into the air supplied to the internal combustion engine 10 .
  • the fuel injection device 60 includes a fuel injection valve 61 (also called an injector) and a valve mounting member 62 (also called a mount) to which the fuel injection valve 61 is mounted.
  • a fuel injection valve 61 also called an injector
  • a valve mounting member 62 also called a mount
  • the fuel injection valve 61 and the valve mounting member 62 are arranged at a position overlapping at least the inlet pipe 15 when viewed from above.
  • the fuel injection valve 61 and the fastening portion 62T of the valve mounting member 62 which is fastened by the fastening member 63, are aligned with the intake passage center line LC, which is the center of the main intake passage 50A, as a reference in a top view. They are arranged separately on one side (right side) and the other side (left side). Therefore, the fuel injection valve 61 and the fastening portion of the valve mounting member 62 can be arranged by utilizing the space above the main intake passage 50A while suppressing protrusion in the width direction from the main intake passage 50A.
  • valve mounting member 62 is fixed to the portion of the inlet pipe 15 corresponding to the main intake passage 50A with the fastening member 63
  • the present invention is not limited to this.
  • the valve mounting member 62 may be fixed with a fastening member 63 to a portion forming the main intake passage 50A or the combustion chamber 24 in the cylinder head 5 .
  • the fuel injection valve 61 and the fastening portion 62T of the valve mounting member 62 are arranged on one side (right side) and the other side with respect to the intake passage center line LC, which is the center of the main intake passage 50A, as viewed from above. (Left side) and arranged separately.
  • FIG. 4 is a diagram showing the inlet pipe 15 and a part of the peripheral structure as viewed from the crankshaft 2 side along the cylinder axis, and the other structures are omitted.
  • FIG. 5 is a diagram in which the description related to the fuel injection device 60 is deleted from FIG. 4 and the center axis LB of the auxiliary intake passage 50B is added.
  • 6 is a view showing the inlet pipe 15 together with a part of the peripheral structure from the side of the cylinder (left side), omitting the illustration of other structures. As shown in FIG.
  • the main intake passage 50A extends with a substantially constant width and is connected to the inside of the combustion chamber 24, and the central axis line LA of the main intake passage 50A coincides with the intake passage center line LC. ing.
  • the center axis LB of the auxiliary intake passage 50B is either left or right with respect to the axis L0 of the combustion chamber 24 in plan view (the left side opposite to the ignition plug 31 in this configuration). , and is formed in a passage inclined in the left-right direction with respect to the intake passage center line LC.
  • the auxiliary intake passage 50B is formed in a tapered shape in which the width gradually decreases as it approaches the exit of the intake port 27 (combustion chamber 24).
  • the auxiliary intake passage 50B communicates with the main intake passage 50A immediately before the outlet of the intake port 27.
  • the vertical height of the main intake passage 50A is substantially constant, and the vertical height of the sub intake passage 50B is also substantially constant.
  • 7 shows a VII-VII cross-sectional view of FIG. 6, and
  • FIG. 8 shows a VIII-VIII cross-sectional view of FIG.
  • cross-sections of the main intake passage 50A and the auxiliary intake passage 50B are hatched. As shown in FIGS.
  • the main intake passage 50A is formed in a passage extending with a substantially constant cross-sectional area, while the secondary intake passage 50B approaches the exit of the intake port 27.
  • the width of the passage becomes smaller accordingly, and the cross-sectional area of the passage becomes smaller as it approaches the outlet of the intake port 27 .
  • the center axis LA of the main intake passage 50A and the center axis LB of the sub intake passage 50B are aligned. , at the same position as the intake passage centerline LC.
  • the central axis LB of the sub-intake passage 50B is shifted to the left or right by a value d with respect to the central axis LA of the main intake passage 50A. becomes.
  • the vertical direction in FIGS. 7 and 8 coincides with the direction of the axis L0 of the combustion chamber 24. As shown in FIG. In FIGS.
  • the distance along the axis L0 between the central axis LA of the main intake passage 50A and the central axis LB of the auxiliary intake passage 50B is indicated by dL.
  • the distance dL between the center axis LA of the main intake passage 50A and the center axis LB of the sub intake passage 50B becomes shorter as the exit of the intake port 27 is approached. As a result, the intake air from the main intake passage 50A and the auxiliary intake passage 50B can be smoothly merged.
  • Reference character DX in FIGS. 4 and 6 indicates the injection direction of the fuel injection valve 61 .
  • Reference character ArX indicates the range of fuel injected from the fuel injection valve 61 .
  • the injection direction DX of the fuel injection valve 61 is oriented in the same direction (to the left in this configuration) with respect to the axis L0 of the combustion chamber 24 to which the auxiliary intake passage 50B is oriented. .
  • the fuel from the fuel injection valve 61 gradually spreads toward the outlet of the intake port 27, and the range ArX of the fuel expands to the range immediately after the outlet of the auxiliary intake passage 50B.
  • the direction of the air from the auxiliary intake passage 50B and the direction of the fuel injected from the fuel injection valve 61 are aligned, and the mixing of the air from the auxiliary intake passage 50B and the fuel can be promoted.
  • the downstream side cross-sectional area of the auxiliary intake passage 50B is smaller than the upstream side cross-sectional area of the auxiliary intake passage 50B, the flow velocity of the air from the auxiliary intake passage 50B is relatively high. Since the fuel is injected toward the high-velocity air, this also promotes mixing of the fuel and the air. Therefore, it is possible to avoid a situation in which the tumble flow T, in which fuel and air are not sufficiently mixed, is ignited.
  • the fuel injection valve 61 is located on the opposite side (left side) of the injection direction DX with respect to the intake passage center line LC, which is the center of the main intake passage 50A. is located on the right side. Therefore, the injection direction DX of the fuel injection valve 61 is a direction that obliquely intersects the intake passage center line LC in a plan view. According to this configuration, the fuel injected from the fuel injection valve 61 can be prevented from adhering to the wall surface of the main intake passage 50 and the wall surface of the combustion chamber 24 .
  • the angle ⁇ A in FIG. 4 indicates the inclination angle of the injection direction DX with respect to the intake passage centerline LC.
  • the angle ⁇ A shown in FIG. 4 is an example of the angle of the present invention.
  • the angle ⁇ A may be appropriately changed within the range of 0° to 90° so that
  • the injection direction DX of the fuel injection valve 61 prevents the fuel injected from the fuel injection valve 61 from adhering to the wall surface of the main intake passage 50A and the wall surface of the combustion chamber 24. and the range ArX of the fuel is set in a direction that satisfies the condition that the range ArX extends to the range immediately after the outlet of the auxiliary intake passage 50B.
  • the air-fuel mixture in which the fuel and air are properly mixed can be flowed into the combustion chamber 24 as a tumble flow T shown in FIG. 3 and containing components of the swirl flow S shown in FIG. Become.
  • the auxiliary intake passage 50B is oriented in a direction deviated leftward or rightward with respect to the axis L0 of the combustion chamber 24, and fuel injection is performed.
  • the injection direction DX of the device 60 is oriented in the direction deviated from the axis L0 of the combustion chamber 24 to the above one side. According to this configuration, the mixture of air and fuel from the auxiliary intake passage 50B is promoted, and it becomes easier to obtain an air-fuel mixture that is advantageous for improving combustion efficiency.
  • the downstream side cross-sectional area of the auxiliary intake passage 50B is made smaller than the upstream side cross-sectional area of the auxiliary intake passage 50B. According to this configuration, the flow velocity of the air flowing into the combustion chamber 24 from the auxiliary intake passage 50B increases. High velocity air can promote better mixing of air and fuel.
  • the auxiliary intake passage 50B is directed to a position that is shifted to the left or right with respect to the axis L0 of the combustion chamber 24, and the flow velocity of the air flowing into the combustion chamber 24 from the auxiliary intake passage 50B is increased. 4 can be generated in the combustion chamber 24.
  • the effect of the flame growth to the intake side due to the swirl flow S can be expected. This can also be expected to improve combustion efficiency and fuel efficiency.
  • the fuel injection valve 61 and the fastening portion 62T of the valve mounting member 62 to which the fuel injection valve 61 is mounted are connected to the main intake air. They are arranged on one side (right side) and the other side (left side) with reference to the intake passage center line LC, which is the center of the passage 50A. According to this configuration, it is easy to prevent the fuel injection valve 61 and the valve mounting member 62 from being arranged to protrude to the left and right with respect to the main intake passage 50A.
  • the fuel injection valve 61 and the fastening portion 62T of the valve mounting member 62 are at least partially overlapped with the main intake passage 50A when viewed from above. According to this configuration, the fuel injection valve 61 and the valve mounting member 62 can be easily arranged compactly by utilizing the space above the main intake passage 50A.
  • the breather hose 21 through which the blow-by gas of the internal combustion engine 10 passes is positioned relative to the intake passage center line LC, and fuel is injected toward the axis L0 of the combustion chamber 24. It is located on the right side opposite to the side (left side) to which the direction DX points. According to this configuration, the breather hose 21 becomes an obstacle when accessing the fastening portion 62T (the fastening portion of the fastening member 63) of the valve mounting member 62, for example, when performing the work of attaching and detaching the fuel injection valve 61. Easier to avoid situations.
  • the auxiliary intake passage 50B and the injection direction DX of the fuel injection device 60 are directed to the opposite side of the ignition plug 31 with respect to the axis L0 of the combustion chamber 24. , the swirl flow S is less likely to be obstructed by the spark plug 31 .
  • the fuel injection valve 61 is positioned on the side ( left side) is located on the right side. According to this configuration, as shown in FIG. 4, the fuel can be injected in a direction obliquely intersecting with the intake passage center line LC, and the fuel does not adhere to the wall surface of the intake passage 50 and the wall surface of the combustion chamber 24. can be suppressed.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

Provided is an intake structure for an internal combustion engine that makes it easy to obtain an air-fuel mixture that is advantageous for improving combustion efficiency. In the present invention, an intake passage 50 of an internal combustion engine is provided with a main intake passage 50A and a sub intake passage 50B that are separated in the vertical direction with respect to a combustion chamber 24, the sub intake passage 50B being directed toward one direction shifted to either the left or the right from the axis L0 of the combustion chamber 24, and the injection direction DX of a fuel injection device 60 being directed toward the one direction shifted from the axis L0 of the combustion chamber 24.

Description

内燃機関の吸気構造Intake structure of internal combustion engine
 本発明は、内燃機関の吸気構造に関する。 The present invention relates to an intake structure for an internal combustion engine.
 内燃機関には、燃焼室につながる吸気通路と、吸気通路に設けられる燃料噴射弁とを備え、吸気通路の向きと燃料噴射弁の噴射方向の向きが一致し、燃料と空気との混合気がタンブルにより燃焼室中心付近に保持される構成が開示されている(例えば特許文献1)。また、内燃機関には、吸気通路が、タンブル流を発生させるために、仕切り壁を介して上部吸気通路、及び下部吸気通路に区画され、下部吸気通路の断面積が主吸気通路の断面積よりも小さい構成が開示されている(例えば特許文献2)。 An internal combustion engine has an intake passage leading to a combustion chamber and a fuel injection valve provided in the intake passage. A configuration is disclosed in which a tumble is held near the center of the combustion chamber (for example, Patent Document 1). In the internal combustion engine, the intake passage is divided into an upper intake passage and a lower intake passage through a partition wall in order to generate a tumble flow, and the cross-sectional area of the lower intake passage is larger than that of the main intake passage. Also disclosed is a configuration with a small value (for example, Patent Document 2).
特開2003-239479号公報JP-A-2003-239479 特許第6623235号公報Japanese Patent No. 6623235
 近年、内燃機関の燃費性能の更なる向上が望まれている。
 従来の内燃機関では、燃料と空気の混合が十分に行われないまま点火される可能性がある。このような事態をより抑制することができれば、燃焼効率が向上し、燃費性能の向上などに有利となる。
In recent years, there has been a demand for further improvement in fuel efficiency of internal combustion engines.
Conventional internal combustion engines can ignite without sufficient fuel and air mixing. If such a situation can be further suppressed, the combustion efficiency will be improved, which will be advantageous for improving the fuel efficiency and the like.
 本発明は、上述した事情に鑑みてなされたものであり、燃焼効率の向上に有利な混合気を得やすい内燃機関の吸気構造を提供することを目的とする。 The present invention has been made in view of the circumstances described above, and an object of the present invention is to provide an intake structure for an internal combustion engine that facilitates obtaining an air-fuel mixture that is advantageous for improving combustion efficiency.
 燃焼室につながる吸気通路と、前記吸気通路に設けられる燃料噴射装置とを備え、前記吸気通路が、前記燃焼室に対し、その燃焼室の軸線方向に対応する上下方向に離間した主吸気通路と副吸気通路とを備え、前記副吸気通路の断面積が前記主吸気通路の断面積よりも小さい内燃機関の吸気構造において、前記副吸気通路は、前記燃焼室の軸線に対して左右いずれか一方にずれた方向に向けて指向し、前記燃料噴射装置の噴射方向は、前記燃焼室の軸線に対して前記一方にずれた方向に向けて指向していることを特徴とする。 An intake passage leading to a combustion chamber and a fuel injection device provided in the intake passage, the intake passage being separated from the combustion chamber in the vertical direction corresponding to the axial direction of the combustion chamber and a main intake passage. an auxiliary intake passage, wherein the auxiliary intake passage has a cross-sectional area smaller than that of the main intake passage, wherein the auxiliary intake passage is positioned on either side of the axis of the combustion chamber. and the injection direction of the fuel injection device is oriented in the one direction with respect to the axis of the combustion chamber.
 上述の構成において、前記副吸気通路の下流側の断面積は、前記副吸気通路の上流側の断面積よりも小さくしてもよい。 In the above configuration, the downstream side cross-sectional area of the auxiliary intake passage may be smaller than the upstream side cross-sectional area of the auxiliary intake passage.
 また、上述の構成において、前記燃料噴射装置は、燃料噴射弁と、前記燃料噴射弁が装着される弁装着部材とを有し、前記弁装着部材は、前記主吸気通路又は前記燃焼室に締結される締結部分を有し、前記燃料噴射弁と前記締結部分とは、前記主吸気通路の中心を基準とした一方側と他方側とに振り分けて配置してもよい。 Further, in the above configuration, the fuel injection device has a fuel injection valve and a valve mounting member to which the fuel injection valve is mounted, and the valve mounting member is fastened to the main intake passage or the combustion chamber. The fuel injection valve and the fastening portion may be arranged so as to be distributed to one side and the other side with respect to the center of the main intake passage.
 また、上述の構成において、前記燃料噴射弁と前記締結部分とは、上面視で、少なくとも一部が前記主吸気通路に重なってもよい。 Further, in the above configuration, the fuel injection valve and the fastening portion may at least partially overlap the main intake passage when viewed from above.
 また、上述の構成において、前記内燃機関は、当該内燃機関のブローバイガスが通るブリーザホースを備え、前記ブリーザホースは、前記主吸気通路の中心を基準にして、前記締結部分の反対側に位置してもよい。 Further, in the above configuration, the internal combustion engine includes a breather hose through which blow-by gas of the internal combustion engine passes, and the breather hose is positioned on the opposite side of the fastening portion with respect to the center of the main intake passage. may
 また、上述の構成において、前記燃料噴射装置の燃料噴射弁は、前記主吸気通路の中心を基準にして、前記燃焼室の軸線に対して前記噴射方向が指向する側の反対側に位置してもよい。 Further, in the above configuration, the fuel injection valve of the fuel injection device is located on the opposite side of the axis of the combustion chamber from the side to which the injection direction is directed, with respect to the center of the main intake passage. good too.
 また、上述の構成において、前記副吸気通路と、前記燃料噴射装置の噴射方向は、前記燃焼室の軸線に対して点火プラグと反対側を指向してもよい。 Further, in the above configuration, the auxiliary intake passage and the injection direction of the fuel injection device may be directed to the opposite side of the ignition plug with respect to the axis of the combustion chamber.
 燃焼室につながる吸気通路と、前記吸気通路に設けられる燃料噴射装置とを備え、前記吸気通路が、前記燃焼室に対し、その燃焼室の軸線方向に対応する上下方向に離間した主吸気通路と副吸気通路とを備え、前記副吸気通路の断面積が前記主吸気通路の断面積よりも小さい内燃機関の吸気構造において、前記副吸気通路は、前記燃焼室の軸線に対して左右いずれか一方にずれた位置に指向し、前記燃料噴射装置の噴射方向は、前記燃焼室の軸線に対して前記一方にずれた位置に指向している。この構成によれば、副吸気通路からの空気と燃料の混合を促し、燃焼効率の向上に有利な混合気を得やすくなる。 An intake passage leading to a combustion chamber and a fuel injection device provided in the intake passage, the intake passage being separated from the combustion chamber in the vertical direction corresponding to the axial direction of the combustion chamber and a main intake passage. an auxiliary intake passage, wherein the auxiliary intake passage has a cross-sectional area smaller than that of the main intake passage, wherein the auxiliary intake passage is positioned on either side of the axis of the combustion chamber. and the injection direction of the fuel injector is directed to the one-way position with respect to the axis of the combustion chamber. According to this configuration, the mixture of air and fuel from the auxiliary intake passage is promoted, and it becomes easier to obtain an air-fuel mixture that is advantageous for improving combustion efficiency.
 上述の構成において、前記副吸気通路の下流側の断面積は、前記副吸気通路の上流側の断面積よりも小さくしてもよい。この構成によれば、副吸気通路から燃焼室に流入する空気の流速が高まり、空気と燃料の混合をより促すことができる。 In the above configuration, the downstream side cross-sectional area of the auxiliary intake passage may be smaller than the upstream side cross-sectional area of the auxiliary intake passage. According to this configuration, the flow velocity of the air flowing into the combustion chamber from the auxiliary intake passage is increased, and the mixing of the air and the fuel can be further promoted.
 また、上述の構成において、前記燃料噴射装置は、燃料噴射弁と、前記燃料噴射弁が装着される弁装着部材とを有し、前記弁装着部材は、前記主吸気通路又は前記燃焼室に締結される締結部分を有し、前記燃料噴射弁と前記締結部分とは、前記主吸気通路の中心を基準とした一方側と他方側とに振り分けて配置してもよい。この構成によれば、主吸気通路に対し、燃料噴射弁と弁装着部材とが一方側と他方側とに張り出して配置される事態を抑制し易くなる。 Further, in the above configuration, the fuel injection device has a fuel injection valve and a valve mounting member to which the fuel injection valve is mounted, and the valve mounting member is fastened to the main intake passage or the combustion chamber. The fuel injection valve and the fastening portion may be arranged so as to be distributed to one side and the other side with respect to the center of the main intake passage. According to this configuration, it is easy to prevent the fuel injection valve and the valve mounting member from being arranged to protrude on one side and the other side of the main intake passage.
 また、上述の構成において、前記燃料噴射弁と前記締結部分とは、上面視で、少なくとも一部が前記主吸気通路に重なってもよい。この構成によれば、上面視で主吸気通路と重なる空きスペースを利用して、燃料噴射弁と弁装着部材とをコンパクトに配置し易くなる。 Further, in the above configuration, the fuel injection valve and the fastening portion may at least partially overlap the main intake passage when viewed from above. According to this configuration, it becomes easy to arrange the fuel injection valve and the valve mounting member in a compact manner by utilizing the empty space that overlaps with the main intake passage in a top view.
 また、上述の構成において、前記内燃機関は、当該内燃機関のブローバイガスが通るブリーザホースを備え、前記ブリーザホースは、前記主吸気通路の中心を基準にして、前記締結部分の反対側に位置してもよい。この構成によれば、燃料噴射弁にアクセスする際に、ブリーザホースが邪魔になる事態を避けやすくなる。 Further, in the above configuration, the internal combustion engine includes a breather hose through which blow-by gas of the internal combustion engine passes, and the breather hose is positioned on the opposite side of the fastening portion with respect to the center of the main intake passage. may According to this configuration, it becomes easier to avoid the situation where the breather hose becomes an obstacle when accessing the fuel injection valve.
 また、上述の構成において、前記燃料噴射装置の燃料噴射弁は、前記主吸気通路の中心を基準にして、前記燃焼室の軸線に対して前記噴射方向が指向する側の反対側に位置してもよい。この構成によれば、吸気通路の壁面や燃焼室の壁面に燃料が付着することを抑制できる。 Further, in the above configuration, the fuel injection valve of the fuel injection device is located on the opposite side of the axis of the combustion chamber from the side to which the injection direction is directed, with respect to the center of the main intake passage. good too. According to this configuration, it is possible to suppress adhesion of fuel to the wall surface of the intake passage and the wall surface of the combustion chamber.
 また、上述の構成において、前記副吸気通路と、前記燃料噴射装置の噴射方向は、前記燃焼室の軸線に対して点火プラグと反対側を指向してもよい。この構成によれば、副吸気通路からの空気によって燃焼室内に発生するスワール流が点火プラグに阻害され難くなる。 Further, in the above configuration, the auxiliary intake passage and the injection direction of the fuel injection device may be directed to the opposite side of the ignition plug with respect to the axis of the combustion chamber. According to this configuration, the spark plug hardly obstructs the swirl flow generated in the combustion chamber by the air from the auxiliary intake passage.
図1は、本発明の吸気構造を備えたパワーユニットの左側面を周辺構成と共に示す図である。FIG. 1 is a view showing the left side of a power unit having an air intake structure of the present invention together with its peripheral configuration. 図2は、パワーユニットの上面を周辺構成と共に示す図である。FIG. 2 is a diagram showing the top surface of the power unit together with the peripheral configuration. 図3は、パワーユニットのシリンダヘッド周辺の側断面図である。FIG. 3 is a side sectional view of the periphery of the cylinder head of the power unit. 図4は、インレットパイプを周辺構成の一部と共にクランク軸側からのシリンダ軸線視で示した図である。FIG. 4 is a diagram showing the inlet pipe and a part of the peripheral structure as viewed from the crankshaft side along the cylinder axis. 図5は、図4から燃料噴射装置に関わる記載を削除し、副吸気通路の中心軸線LBを追記した図である。FIG. 5 is a diagram in which the description related to the fuel injection device is deleted from FIG. 4 and the central axis line LB of the auxiliary intake passage is added. 図6は、インレットパイプを周辺構成の一部と共にシリンダ側方から示した図である。FIG. 6 is a view showing the inlet pipe together with a part of the peripheral structure from the side of the cylinder. 図7は、図5のVII―VII断面図である。7 is a cross-sectional view taken along line VII-VII of FIG. 5. FIG. 図8は、図6のVIII―VIII断面図である。8 is a cross-sectional view taken along line VIII-VIII of FIG. 6. FIG.
 以下、図面を参照して本発明の一実施形態について説明する。なお、説明中、前後左右、及び上下といった各方向は、特に記載がなければ車体を基準にした方向である。各図に示す符号FRは車体前方を示し、符号UPは車体上方を示し、符号LHは車体左方を示している。 An embodiment of the present invention will be described below with reference to the drawings. In the description, directions such as front, rear, left, right, and up and down are directions based on the vehicle body unless otherwise specified. Symbol FR shown in each figure indicates the front of the vehicle body, symbol UP indicates the upper part of the vehicle body, and symbol LH indicates the left side of the vehicle body.
 図1は、本発明の吸気構造を備えたパワーユニット1の左側面を周辺構成と共に示す図であり、図2は、パワーユニット1の上面を周辺構成と共に示す図である。
 パワーユニット1は、スクータ型自動二輪車の車体フレームに上下に揺動自在に支持されるパワーユニットであり、スイング式パワーユニットとも言う。図1及び図2に示すように、パワーユニット1は、前部にクランク軸2を回転自在に支持するクランクケース3と、クランクケース3の前部に設けられたシリンダブロック4と、シリンダブロック4に取り付けられたシリンダヘッド5と、シリンダヘッド5の開口を塞ぐヘッドカバー6とを備える。シリンダブロック4、シリンダヘッド5及びヘッドカバー6からなるシリンダ部は、クランクケース3の前部から略水に近い状態まで前傾している。
FIG. 1 is a view showing the left side of a power unit 1 having an air intake structure of the present invention together with its peripheral structure, and FIG. 2 is a view showing the upper surface of the power unit 1 together with its peripheral structure.
The power unit 1 is a power unit supported by a body frame of a scooter type motorcycle so as to be vertically swingable, and is also called a swing type power unit. As shown in FIGS. 1 and 2, the power unit 1 includes a crankcase 3 that rotatably supports a crankshaft 2 at the front, a cylinder block 4 provided at the front of the crankcase 3, and a It has a mounted cylinder head 5 and a head cover 6 closing an opening of the cylinder head 5. - 特許庁A cylinder portion consisting of a cylinder block 4, a cylinder head 5 and a head cover 6 is tilted forward from the front portion of the crankcase 3 to a state substantially close to water.
 クランクケース3、シリンダブロック4、シリンダヘッド5及びヘッドカバー6からなる部分は、単気筒4ストロークサイクルの空冷式内燃機関(以下、単に「内燃機関」という。)10を構成する。クランクケース3の左側部には、動力伝動ケース部11が連結される。動力伝動ケース部11には、クランク軸2の回転を変速して後輪軸12に伝達するベルト式無段変速機が収容される。 A portion consisting of the crankcase 3 , the cylinder block 4 , the cylinder head 5 and the head cover 6 constitutes a single-cylinder four-stroke cycle air-cooled internal combustion engine (hereinafter simply referred to as the "internal combustion engine") 10 . A power transmission case portion 11 is connected to the left side of the crankcase 3 . The power transmission case portion 11 accommodates a belt-type continuously variable transmission that changes the speed of the rotation of the crankshaft 2 and transmits it to the rear wheel shaft 12 .
 パワーユニット1の上部では、シリンダヘッド5の上部からインレットパイプ15が延出して後方に湾曲し、スロットルボディ16に連結される。スロットルボディ16の後端には、コネクティングチューブ17を介してエアクリーナ装置18が接続される。エアクリーナ装置18は、動力伝動ケース部11の上方に配置される。スロットルボディ16には、不図示のスロットル弁が設けられ、スロットル弁によって内燃機関10への吸気量を調整する。インレットパイプ15、スロットルボディ16及びコネクティングチューブ17は、エアクリーナ装置18で清浄化された空気を内燃機関10に供給する吸気通路50の一部を形成する。 In the upper part of the power unit 1, the inlet pipe 15 extends from the upper part of the cylinder head 5, curves backward, and is connected to the throttle body 16. An air cleaner device 18 is connected to the rear end of the throttle body 16 via a connecting tube 17 . The air cleaner device 18 is arranged above the power transmission case portion 11 . A throttle valve (not shown) is provided in the throttle body 16, and the amount of intake air to the internal combustion engine 10 is adjusted by the throttle valve. The inlet pipe 15 , throttle body 16 and connecting tube 17 form part of an intake passage 50 that supplies air cleaned by the air cleaner device 18 to the internal combustion engine 10 .
 パワーユニット110の下部では、シリンダヘッド5の下部から排気管19が延出する。排気管19は、シリンダヘッド5の右側方に延出した後、後方に延出し、マフラー20に接続される。図2中の符号LCは、インレットパイプ15の左右中央を前後方向に直線状に延びる中心線であり、以下、「吸気通路中心線LC」と言う。この吸気通路中心線LCは、パワーユニット1の左右中心線とも一致している。 At the bottom of the power unit 110, an exhaust pipe 19 extends from the bottom of the cylinder head 5. After extending to the right side of the cylinder head 5 , the exhaust pipe 19 extends rearward and is connected to a muffler 20 . Reference numeral LC in FIG. 2 denotes a center line extending linearly in the front-rear direction through the left-right center of the inlet pipe 15, and is hereinafter referred to as an "intake passage center line LC". This intake passage centerline LC also coincides with the left-right centerline of the power unit 1 .
 図2に示すように、ヘッドカバー6には、ブローバイガスが通るブリーザホース21が接続される。ブリーザホース21は、ヘッドカバー6の上部から右方に延出した後、後方に延出してエアクリーナ装置18に接続される。本構成では、図2に示すように、ブリーザホース21が、上面視で、ヘッドカバー6、シリンダブロック4及びコネクティングチューブ17の右側方を通って後方に延出し、コネクティングチューブ17に沿って左後方へ斜めに延出してエアクリーナ装置18に接続される。 As shown in FIG. 2, the head cover 6 is connected to a breather hose 21 through which blow-by gas passes. The breather hose 21 extends rightward from the upper portion of the head cover 6 and then extends rearward to be connected to the air cleaner device 18 . In this configuration, as shown in FIG. 2, the breather hose 21 extends rearward through the head cover 6, the cylinder block 4, and the right side of the connecting tube 17 when viewed from above, and extends left rearward along the connecting tube 17. It extends obliquely and is connected to the air cleaner device 18 .
 図3は、パワーユニット1のシリンダヘッド5周辺の側断面図である。
 シリンダブロック4は、外面に複数のフィン4Fを備え、内部にはシリンダボア22が形成されている。シリンダボア22にはピストン23が摺動自在に設けられる。ピストン23はコネクティングロッドを介してクランク軸2に連結され、ピストン23がシリンダボア22を摺動することによってクランク軸2が回転する。ピストン23の頂面と、頂面が対向するシリンダヘッド5の燃焼室天井面との間の空間が燃焼室24を構成する。図3中、符号L0は、燃焼室24の中心を通る軸線であり、シリンダ部の軸線とも一致する。
FIG. 3 is a side cross-sectional view around the cylinder head 5 of the power unit 1. As shown in FIG.
The cylinder block 4 has a plurality of fins 4F on its outer surface and cylinder bores 22 formed therein. A piston 23 is slidably provided in the cylinder bore 22 . The piston 23 is connected to the crankshaft 2 via a connecting rod, and the piston 23 slides in the cylinder bore 22 to rotate the crankshaft 2 . A space between the top surface of the piston 23 and the ceiling surface of the combustion chamber of the cylinder head 5 facing the top surface constitutes a combustion chamber 24 . In FIG. 3, reference character L0 denotes an axis that passes through the center of the combustion chamber 24 and coincides with the axis of the cylinder portion.
 本実施形態の内燃機関は、SOHC型式の2バルブシステムを採用しており、シリンダヘッド5とヘッドカバー6との間の空間に動弁機構25が設けられている。動弁機構25は、不図示のカムチェーンを介してクランク軸2の回転が1/2の回転速度で伝達されるカムシャフト26を備える。カムシャフト26の回転は、不図示の吸気カム及び吸気ロッカーアームを介して、吸気ポート27を開閉する吸気バルブ28を作動させる。また、カムシャフト26の回転は、不図示の排気カム及び排気ロッカーアームを介して、排気ポート29を開閉する排気バルブ30を作動させる。 The internal combustion engine of this embodiment employs a SOHC type two-valve system, and a valve mechanism 25 is provided in the space between the cylinder head 5 and the head cover 6 . The valve mechanism 25 includes a camshaft 26 to which the rotation of the crankshaft 2 is transmitted at half the rotation speed via a cam chain (not shown). Rotation of the camshaft 26 operates an intake valve 28 that opens and closes an intake port 27 via an intake cam and an intake rocker arm (not shown). The rotation of the camshaft 26 also operates an exhaust valve 30 that opens and closes the exhaust port 29 via an exhaust cam and an exhaust rocker arm (not shown).
 吸気ポート27は、燃焼室24とインレットパイプ15とを連通させる通路であり、吸気通路50の一部を構成する。また、排気ポート29は、燃焼室24と排気管19とを連通させる通路である。動弁機構25によって、4サイクルの吸気行程、及び排気行程に対応するタイミングで、吸気ポート27及び排気ポート29がそれぞれ開閉される。また、シリンダヘッド5には、吸気ポート27と排気ポート29とを避けた位置に先端が臨む点火プラグ31が取り付けられている。 The intake port 27 is a passage that communicates the combustion chamber 24 and the inlet pipe 15, and constitutes a part of the intake passage 50. Also, the exhaust port 29 is a passage that allows the combustion chamber 24 and the exhaust pipe 19 to communicate with each other. The valve mechanism 25 opens and closes the intake port 27 and the exhaust port 29 at timings corresponding to four cycles of intake stroke and exhaust stroke. A spark plug 31 is attached to the cylinder head 5 and has a tip facing a position avoiding the intake port 27 and the exhaust port 29 .
 本実施形態の吸気通路50は、燃焼室24内にタンブル流T(図2参照)を発生させる構造、つまり、縦回転を与える吸気構造を備えている。より具体的には、吸気通路50は、インレットパイプ15から吸気ポート27へと続く仕切り壁32によって、燃焼室24に対し、その燃焼室24の軸線L0の方向に対応する上下方向に離間した上側の吸気通路50A(以下、主吸気通路50Aと言う)と、下側の吸気通路50B(以下、副吸気通路50Bと言う)とに区画されている。副吸気通路50Bが、燃焼室24内にタンブル流Tを発生させるタンブル流路に形成されている。 The intake passage 50 of this embodiment has a structure that generates a tumble flow T (see FIG. 2) in the combustion chamber 24, that is, an intake structure that provides vertical rotation. More specifically, the intake passage 50 is separated from the combustion chamber 24 in the vertical direction corresponding to the direction of the axis L0 of the combustion chamber 24 by the partition wall 32 leading from the inlet pipe 15 to the intake port 27. an intake passage 50A (hereinafter referred to as a main intake passage 50A) and a lower intake passage 50B (hereinafter referred to as an auxiliary intake passage 50B). The auxiliary intake passage 50B is formed as a tumble flow path for generating a tumble flow T within the combustion chamber 24. As shown in FIG.
 副吸気通路50Bは、主吸気通路50よりも断面積(横断面積とも言う)が小さい通路に形成され、内燃機関10の吸気量が相対的に少ないアイドリング状態、又は、低速回転状態の場合に、タンブル流Tを発生可能に、空気を供給する。つまり、両吸気通路50A、50Bの上流に位置するスロットルボディ16内のスロットル弁の開度が相対的に小さい場合、エアクリーナ装置18で清浄化された空気が、主に副吸気通路50Bを通過し、タンブル流Tを発生させる。 The auxiliary intake passage 50B is formed in a passage having a cross-sectional area (also referred to as a cross-sectional area) smaller than that of the main intake passage 50, and when the intake air amount of the internal combustion engine 10 is relatively small or in an idling state or a low speed rotation state, Air is supplied so that a tumble flow T can be generated. That is, when the opening degree of the throttle valve in the throttle body 16 located upstream of both intake passages 50A and 50B is relatively small, the air cleaned by the air cleaner device 18 mainly passes through the auxiliary intake passage 50B. , to generate a tumble flow T.
 主吸気通路50Aは、内燃機関10の吸気量が相対的に多い中・高速回転状態、又は加速状態の場合に、空気を十分に供給する通路として機能する。つまり、スロットルボディ16内のスロットル弁の開度が相対的に大きくなると、エアクリーナ装置18からの空気が主吸気通路50A及び副吸気通路50Bの双方を通り、十分な空気が燃焼室24に供給される。 The main intake passage 50A functions as a passage for sufficiently supplying air when the internal combustion engine 10 has a relatively large amount of intake air and is in a medium/high speed rotation state or an acceleration state. That is, when the opening of the throttle valve in the throttle body 16 becomes relatively large, the air from the air cleaner device 18 passes through both the main intake passage 50A and the auxiliary intake passage 50B, and sufficient air is supplied to the combustion chamber 24. be.
 図2及び図3に示すように、パワーユニット1は、内燃機関10に供給される空気に燃料を噴射する燃料噴射装置60を備える。燃料噴射装置60は、燃料噴射弁61(インジェクタとも称する)と、燃料噴射弁61が装着される弁装着部材62(マウントとも称する)とを備える。弁装着部材62が締結部材63を用いてインレットパイプ15に固定されることによって、燃料噴射弁61の先端に設けられた燃料噴射口がインレットパイプ15に設けられた穴から主吸気通路50A内に露出する。 As shown in FIGS. 2 and 3 , the power unit 1 includes a fuel injection device 60 that injects fuel into the air supplied to the internal combustion engine 10 . The fuel injection device 60 includes a fuel injection valve 61 (also called an injector) and a valve mounting member 62 (also called a mount) to which the fuel injection valve 61 is mounted. By fixing the valve mounting member 62 to the inlet pipe 15 using the fastening member 63, the fuel injection port provided at the tip of the fuel injection valve 61 is inserted into the main intake passage 50A from the hole provided in the inlet pipe 15. expose.
 図2に示すように、燃料噴射弁61と弁装着部材62とは、上面視で、少なくともインレットパイプ15に重なる位置に配置される。本構成では、燃料噴射弁61と、弁装着部材62における締結部材63で締結される締結部分62Tとが、上面視で、主吸気通路50Aの中心である吸気通路中心線LCを基準とした一方側(右側)と他方側(左側)とに振り分けて配置されている。このため、燃料噴射弁61と、弁装着部材62の締結部分とを、主吸気通路50Aの上方に空くスペースを利用して主吸気通路50Aから幅方向への突出を抑えて配置できる。 As shown in FIG. 2, the fuel injection valve 61 and the valve mounting member 62 are arranged at a position overlapping at least the inlet pipe 15 when viewed from above. In this configuration, the fuel injection valve 61 and the fastening portion 62T of the valve mounting member 62, which is fastened by the fastening member 63, are aligned with the intake passage center line LC, which is the center of the main intake passage 50A, as a reference in a top view. They are arranged separately on one side (right side) and the other side (left side). Therefore, the fuel injection valve 61 and the fastening portion of the valve mounting member 62 can be arranged by utilizing the space above the main intake passage 50A while suppressing protrusion in the width direction from the main intake passage 50A.
 なお、弁装着部材62を、インレットパイプ15における主吸気通路50Aに対応する箇所に締結部材63で固定する場合を例示したが、これに限定しなくてもよい。例えば、弁装着部材62を、シリンダヘッド5における主吸気通路50A又は燃焼室24を構成する箇所に締結部材63で固定するようにしてもよい。この場合も、燃料噴射弁61と、弁装着部材62の締結部分62Tとを、上面視で、主吸気通路50Aの中心である吸気通路中心線LCを基準とした一方側(右側)と他方側(左側)とに振り分けて配置することが好ましい。 Although the case where the valve mounting member 62 is fixed to the portion of the inlet pipe 15 corresponding to the main intake passage 50A with the fastening member 63 has been exemplified, the present invention is not limited to this. For example, the valve mounting member 62 may be fixed with a fastening member 63 to a portion forming the main intake passage 50A or the combustion chamber 24 in the cylinder head 5 . In this case as well, the fuel injection valve 61 and the fastening portion 62T of the valve mounting member 62 are arranged on one side (right side) and the other side with respect to the intake passage center line LC, which is the center of the main intake passage 50A, as viewed from above. (Left side) and arranged separately.
 図4は、インレットパイプ15を周辺構成の一部と共にクランク軸2側からのシリンダ軸線視で示した図であり、それ以外の構造物の図示は省略している。図5は、図4から燃料噴射装置60に関わる記載を削除し、副吸気通路50Bの中心軸線LBを追記した図である。また、図6は、インレットパイプ15を周辺構成の一部と共にシリンダ側方(左側方)から示し、それ以外の構造物の図示は省略した図である。図4に示すように、平面視で、主吸気通路50Aは略一定の幅で延出して燃焼室24内につながり、かつ、主吸気通路50Aの中心軸線LAは吸気通路中心線LCと一致している。また、図5に示すように、副吸気通路50Bの中心軸線LBは、平面視で、燃焼室24の軸線L0に対し、左右いずれか一方(本構成では点火プラグ31の逆側である左側)にずれた方向に指向し、吸気通路中心線LCに対して左右方向に傾いた通路に形成されている。また、副吸気通路50Bは、吸気ポート27の出口(燃焼室24)に近づくに従って幅が徐々に小さくなる先細形状に形成されている。 FIG. 4 is a diagram showing the inlet pipe 15 and a part of the peripheral structure as viewed from the crankshaft 2 side along the cylinder axis, and the other structures are omitted. FIG. 5 is a diagram in which the description related to the fuel injection device 60 is deleted from FIG. 4 and the center axis LB of the auxiliary intake passage 50B is added. 6 is a view showing the inlet pipe 15 together with a part of the peripheral structure from the side of the cylinder (left side), omitting the illustration of other structures. As shown in FIG. 4, in a plan view, the main intake passage 50A extends with a substantially constant width and is connected to the inside of the combustion chamber 24, and the central axis line LA of the main intake passage 50A coincides with the intake passage center line LC. ing. Further, as shown in FIG. 5, the center axis LB of the auxiliary intake passage 50B is either left or right with respect to the axis L0 of the combustion chamber 24 in plan view (the left side opposite to the ignition plug 31 in this configuration). , and is formed in a passage inclined in the left-right direction with respect to the intake passage center line LC. Further, the auxiliary intake passage 50B is formed in a tapered shape in which the width gradually decreases as it approaches the exit of the intake port 27 (combustion chamber 24).
 図4~図6に示すように、副吸気通路50Bは、吸気ポート27の出口直前で主吸気通路50Aに連通する。この図6に示すように、側面視では、主吸気通路50Aの上下高さはほぼ一定であり、副吸気通路50Bについても上下高さはほぼ一定である。
 図7は、図6のVII―VII断面図を示し、図8は、図6のVIII―VIII断面図を示している。図7及び図8には、主吸気通路50A及び副吸気通路50Bの断面にハッチングを付して示している。
 図7、図8及び図4に示すように、主吸気通路50Aは、ほぼ一定の断面積で延出する通路に形成されるのに対し、副吸気通路50Bは、吸気ポート27の出口に近づくに従って左右の幅が小さくなり、吸気ポート27の出口に近づくに従って断面積が小さくなる通路に形成されている。これにより、燃焼室24内の左右一方に流速を高めた空気を供給でき、燃焼室24内にスワール流S(図4参照)の成分を発生させること、つまり、横回転を与えることができる。
As shown in FIGS. 4 to 6, the auxiliary intake passage 50B communicates with the main intake passage 50A immediately before the outlet of the intake port 27. As shown in FIGS. As shown in FIG. 6, when viewed from the side, the vertical height of the main intake passage 50A is substantially constant, and the vertical height of the sub intake passage 50B is also substantially constant.
7 shows a VII-VII cross-sectional view of FIG. 6, and FIG. 8 shows a VIII-VIII cross-sectional view of FIG. In FIGS. 7 and 8, cross-sections of the main intake passage 50A and the auxiliary intake passage 50B are hatched.
As shown in FIGS. 7, 8 and 4, the main intake passage 50A is formed in a passage extending with a substantially constant cross-sectional area, while the secondary intake passage 50B approaches the exit of the intake port 27. The width of the passage becomes smaller accordingly, and the cross-sectional area of the passage becomes smaller as it approaches the outlet of the intake port 27 . As a result, air having a high flow velocity can be supplied to one of the left and right sides of the combustion chamber 24, and a component of the swirl flow S (see FIG. 4) can be generated in the combustion chamber 24, that is, lateral rotation can be imparted.
 図7に示すように、吸気ポート27の出口から相対的に離れた位置(燃料噴射弁61近傍の位置)では、主吸気通路50Aの中心軸線LAと、副吸気通路50Bの中心軸線LBとが、吸気通路中心線LCと同じ位置に存在する。また、図8に示すように、吸気ポート27の出口に近い位置では、主吸気通路50Aの中心軸線LAに対して、副吸気通路50Bの中心軸線LBが左右一方側に値dだけずれた位置となる。
 なお、図7及び図8の上下方向は、燃焼室24の軸線L0の方向と一致している。図7、図8には、主吸気通路50Aの中心軸線LAと、副吸気通路50Bの中心軸線LBとの間の軸線L0に沿った方向の離間距離を符号dLで示している。図7、図8及び図6に示すように、主吸気通路50Aの中心軸線LAと、副吸気通路50Bの中心軸線LBとの離間距離dLは、吸気ポート27の出口に近づくほど短くなる。これにより、主吸気通路50Aと副吸気通路50Bからの吸気をスムーズに合流させることができる。
As shown in FIG. 7, at a position relatively distant from the outlet of the intake port 27 (a position near the fuel injection valve 61), the center axis LA of the main intake passage 50A and the center axis LB of the sub intake passage 50B are aligned. , at the same position as the intake passage centerline LC. Further, as shown in FIG. 8, at a position near the outlet of the intake port 27, the central axis LB of the sub-intake passage 50B is shifted to the left or right by a value d with respect to the central axis LA of the main intake passage 50A. becomes.
The vertical direction in FIGS. 7 and 8 coincides with the direction of the axis L0 of the combustion chamber 24. As shown in FIG. In FIGS. 7 and 8, the distance along the axis L0 between the central axis LA of the main intake passage 50A and the central axis LB of the auxiliary intake passage 50B is indicated by dL. As shown in FIGS. 7, 8 and 6, the distance dL between the center axis LA of the main intake passage 50A and the center axis LB of the sub intake passage 50B becomes shorter as the exit of the intake port 27 is approached. As a result, the intake air from the main intake passage 50A and the auxiliary intake passage 50B can be smoothly merged.
 図4及び図6中の符号DXは、燃料噴射弁61の噴射方向を示している。また、符号ArXは、燃料噴射弁61から噴射された燃料の範囲を示している。
 図4に示すように、燃料噴射弁61の噴射方向DXは、燃焼室24の軸線L0に対し、副吸気通路50Bが指向する側と同じ側(本構成では左側)にずれた方向に指向する。燃料噴射弁61からの燃料は、吸気ポート27の出口に向かって徐々に拡がり、その燃料の範囲ArXは、副吸気通路50Bの出口直後の範囲にまで拡がる。これらによって、副吸気通路50Bからの空気の向きと、燃料噴射弁61から噴射された燃料の向きとが揃い、副吸気通路50Bからの空気と燃料の混合を促すことができる。
Reference character DX in FIGS. 4 and 6 indicates the injection direction of the fuel injection valve 61 . Reference character ArX indicates the range of fuel injected from the fuel injection valve 61 .
As shown in FIG. 4, the injection direction DX of the fuel injection valve 61 is oriented in the same direction (to the left in this configuration) with respect to the axis L0 of the combustion chamber 24 to which the auxiliary intake passage 50B is oriented. . The fuel from the fuel injection valve 61 gradually spreads toward the outlet of the intake port 27, and the range ArX of the fuel expands to the range immediately after the outlet of the auxiliary intake passage 50B. As a result, the direction of the air from the auxiliary intake passage 50B and the direction of the fuel injected from the fuel injection valve 61 are aligned, and the mixing of the air from the auxiliary intake passage 50B and the fuel can be promoted.
 また、副吸気通路50Bの下流側の断面積は、副吸気通路50Bの上流側の断面積よりも小さいので、副吸気通路50Bからの空気の流速は相対的に高くなる。流速の高い空気に向けて燃料が噴射されるので、これによっても燃料と空気の混合を促すことができる。したがって、燃料と空気の混合が十分に行われないタンブル流Tに点火される事態を回避できる。 Also, since the downstream side cross-sectional area of the auxiliary intake passage 50B is smaller than the upstream side cross-sectional area of the auxiliary intake passage 50B, the flow velocity of the air from the auxiliary intake passage 50B is relatively high. Since the fuel is injected toward the high-velocity air, this also promotes mixing of the fuel and the air. Therefore, it is possible to avoid a situation in which the tumble flow T, in which fuel and air are not sufficiently mixed, is ignited.
 また、図4に示すように、平面視で、燃料噴射弁61は、主吸気通路50Aの中心である吸気通路中心線LCを基準にして、噴射方向DXが指向する側(左側)の反対側である右側に位置している。このため、燃料噴射弁61の噴射方向DXは、平面視で、吸気通路中心線LCに対して斜めに公差する方向となる。この構成によれば、燃料噴射弁61から噴射された燃料が、主吸気通路50の壁面や燃焼室24の壁面に付着することを抑制できる。 Further, as shown in FIG. 4, in a plan view, the fuel injection valve 61 is located on the opposite side (left side) of the injection direction DX with respect to the intake passage center line LC, which is the center of the main intake passage 50A. is located on the right side. Therefore, the injection direction DX of the fuel injection valve 61 is a direction that obliquely intersects the intake passage center line LC in a plan view. According to this configuration, the fuel injected from the fuel injection valve 61 can be prevented from adhering to the wall surface of the main intake passage 50 and the wall surface of the combustion chamber 24 .
 図4中の角度θAは、吸気通路中心線LCに対する噴射方向DXの傾斜角度を示している。図4に示す角度θAは本発明の一例の角度を示したものであり、図3に示すタンブル流T(図4に示すスワール流Sの成分も含む)における空気と燃料の混合度合いなどが適正となるように、角度θAは0°から90°の範囲で適宜に変更してもよい。 The angle θA in FIG. 4 indicates the inclination angle of the injection direction DX with respect to the intake passage centerline LC. The angle θA shown in FIG. 4 is an example of the angle of the present invention. The angle θA may be appropriately changed within the range of 0° to 90° so that
 図6に示すように、側面視でも、燃料噴射弁61の噴射方向DXは、燃料噴射弁61から噴射された燃料が、主吸気通路50Aの壁面や燃焼室24の壁面に付着することが抑制され、かつ、燃料の範囲ArXが副吸気通路50Bの出口直後の範囲にまで拡がる条件を満たす方向に設定される。これらによって、燃料と空気が適切に混合した混合気を、図3に示すタンブル流Tであって、図4に示すスワール流Sの成分を含む混合気として、燃焼室24に流すことが可能になる。 As shown in FIG. 6, even when viewed from the side, the injection direction DX of the fuel injection valve 61 prevents the fuel injected from the fuel injection valve 61 from adhering to the wall surface of the main intake passage 50A and the wall surface of the combustion chamber 24. and the range ArX of the fuel is set in a direction that satisfies the condition that the range ArX extends to the range immediately after the outlet of the auxiliary intake passage 50B. As a result, the air-fuel mixture in which the fuel and air are properly mixed can be flowed into the combustion chamber 24 as a tumble flow T shown in FIG. 3 and containing components of the swirl flow S shown in FIG. Become.
 以上説明したように、本実施形態では、図4に示したように、副吸気通路50Bは、燃焼室24の軸線L0に対して左右いずれか一方にずれた方向に向けて指向し、燃料噴射装置60の噴射方向DXは、燃焼室24の軸線L0に対して上記一方にずれた方向に向けて指向している。この構成によれば、副吸気通路50Bからの空気と燃料の混合を促し、燃焼効率の向上に有利な混合気を得やすくなる。 As described above, in the present embodiment, as shown in FIG. 4, the auxiliary intake passage 50B is oriented in a direction deviated leftward or rightward with respect to the axis L0 of the combustion chamber 24, and fuel injection is performed. The injection direction DX of the device 60 is oriented in the direction deviated from the axis L0 of the combustion chamber 24 to the above one side. According to this configuration, the mixture of air and fuel from the auxiliary intake passage 50B is promoted, and it becomes easier to obtain an air-fuel mixture that is advantageous for improving combustion efficiency.
 また、本実施形態では、副吸気通路50Bの下流側の断面積を、副吸気通路50Bの上流側の断面積よりも小さくしている。この構成によれば、副吸気通路50Bから燃焼室24に流入する空気の流速が高まる。流速の高い空気によって、空気と燃料の混合をより促すことができる。 Further, in the present embodiment, the downstream side cross-sectional area of the auxiliary intake passage 50B is made smaller than the upstream side cross-sectional area of the auxiliary intake passage 50B. According to this configuration, the flow velocity of the air flowing into the combustion chamber 24 from the auxiliary intake passage 50B increases. High velocity air can promote better mixing of air and fuel.
 しかも、上記した副吸気通路50Bが燃焼室24の軸線L0に対して左右いずれか一方にずれた位置に指向する構成、かつ、副吸気通路50Bから燃焼室24に流入する空気の流速を高める構成にすることによって、燃焼室24内に図4に示したスワール流Sを発生させることができる。燃焼室24内で混合気に点火した場合に、スワール流Sによる火炎の吸気側への成長効果を期待できる。これによっても、燃焼効率の向上や燃費向上を期待できる。 Moreover, the auxiliary intake passage 50B is directed to a position that is shifted to the left or right with respect to the axis L0 of the combustion chamber 24, and the flow velocity of the air flowing into the combustion chamber 24 from the auxiliary intake passage 50B is increased. 4 can be generated in the combustion chamber 24. When the air-fuel mixture is ignited in the combustion chamber 24, the effect of the flame growth to the intake side due to the swirl flow S can be expected. This can also be expected to improve combustion efficiency and fuel efficiency.
 また、本実施形態では、図2に示したように、燃料噴射弁61と、燃料噴射弁61が装着される弁装着部材62の締結部分62T(締結部材63の締結箇所)とを、主吸気通路50Aの中心である吸気通路中心線LCを基準とした一方側(右側)と他方側(左側)とに振り分けて配置している。この構成によれば、主吸気通路50Aに対し、燃料噴射弁61と弁装着部材62とが左右に張り出して配置される事態を抑制し易くなる。 Further, in this embodiment, as shown in FIG. 2, the fuel injection valve 61 and the fastening portion 62T of the valve mounting member 62 to which the fuel injection valve 61 is mounted (the fastening portion of the fastening member 63) are connected to the main intake air. They are arranged on one side (right side) and the other side (left side) with reference to the intake passage center line LC, which is the center of the passage 50A. According to this configuration, it is easy to prevent the fuel injection valve 61 and the valve mounting member 62 from being arranged to protrude to the left and right with respect to the main intake passage 50A.
 さらに、本実施形態では、燃料噴射弁61と弁装着部材62の締結部分62Tとを、上面視で、少なくとも一部が主吸気通路50Aに重ねている。この構成によれば、主吸気通路50Aの上方に空くスペースを利用して、燃料噴射弁61と弁装着部材62とをコンパクトに配置し易くなる。 Furthermore, in this embodiment, the fuel injection valve 61 and the fastening portion 62T of the valve mounting member 62 are at least partially overlapped with the main intake passage 50A when viewed from above. According to this configuration, the fuel injection valve 61 and the valve mounting member 62 can be easily arranged compactly by utilizing the space above the main intake passage 50A.
 また、本実施形態では、図2に示したように、内燃機関10のブローバイガスが通るブリーザホース21を、吸気通路中心線LCを基準にして、燃焼室24の軸線L0に対して燃料の噴射方向DXが指向する側(左側)の反対側である右側に位置させている。この構成によれば、燃料噴射弁61を着脱する作業を行う際に、例えば、弁装着部材62の締結部分62T(締結部材63の締結箇所)にアクセスする際に、ブリーザホース21が邪魔になる事態を避けやすくなる。 Further, in the present embodiment, as shown in FIG. 2, the breather hose 21 through which the blow-by gas of the internal combustion engine 10 passes is positioned relative to the intake passage center line LC, and fuel is injected toward the axis L0 of the combustion chamber 24. It is located on the right side opposite to the side (left side) to which the direction DX points. According to this configuration, the breather hose 21 becomes an obstacle when accessing the fastening portion 62T (the fastening portion of the fastening member 63) of the valve mounting member 62, for example, when performing the work of attaching and detaching the fuel injection valve 61. Easier to avoid situations.
 また、本実施形態では、図4に示したように、副吸気通路50Bと、燃料噴射装置60の噴射方向DXは、燃焼室24の軸線L0に対して点火プラグ31の反対側を指向するので、スワール流Sが点火プラグ31に阻害され難くなる。
 また、本実施形態では、図4に示したように、燃料噴射弁61を、吸気通路中心線LCを基準にして、燃焼室24の軸線L0に対して燃料の噴射方向DXが指向する側(左側)の反対側である右側に位置させている。この構成によれば、図4に示したように、吸気通路中心線LCに対して斜めに公差する方向に燃料を噴射でき、吸気通路50の壁面や燃焼室24の壁面に燃料が付着することを抑制できる。
In this embodiment, as shown in FIG. 4, the auxiliary intake passage 50B and the injection direction DX of the fuel injection device 60 are directed to the opposite side of the ignition plug 31 with respect to the axis L0 of the combustion chamber 24. , the swirl flow S is less likely to be obstructed by the spark plug 31 .
Further, in the present embodiment, as shown in FIG. 4, the fuel injection valve 61 is positioned on the side ( left side) is located on the right side. According to this configuration, as shown in FIG. 4, the fuel can be injected in a direction obliquely intersecting with the intake passage center line LC, and the fuel does not adhere to the wall surface of the intake passage 50 and the wall surface of the combustion chamber 24. can be suppressed.
 上記実施形態は、あくまでも本発明の一態様の例示であり、本発明の趣旨を逸脱しない範囲で任意に変形、及び応用が可能である。例えば、本発明をスクータ型自動二輪車の内燃機関10の吸気構造に適用する場合を説明したが、他の二輪タイプ、三輪タイプ、及び四輪タイプなども含む鞍乗り型車両の内燃機関の吸気構造に、本発明を適用してもよい。 The above embodiment is merely an example of one aspect of the present invention, and can be arbitrarily modified and applied without departing from the scope of the present invention. For example, although the case where the present invention is applied to the intake structure of the internal combustion engine 10 of a scooter type motorcycle has been described, the intake structure of the internal combustion engine of other two-wheeled, three-wheeled, and four-wheeled vehicles including saddle-type vehicles. The present invention may be applied to
 1 パワーユニット
 2 クランク軸
 3 クランクケース
 4 シリンダブロック
 5 シリンダヘッド
 6 ヘッドカバー
 10 内燃機関
 15 インレットパイプ
 16 スロットルボディ
 17 コネクティングチューブ
 18 エアクリーナ装置
 21 ブリーザホース
 24 燃焼室
 25 動弁機構
 27 吸気ポート
 29 排気ポート
 31 点火プラグ
 50 吸気通路
 50A 主吸気通路
 50B 副吸気通路
 60 燃料噴射装置
 61 燃料噴射弁
 62 弁装着部材
 63 締結部材
 62T 締結部分(締結部材63の締結箇所)
 T タンブル流
 S スワール流
 LC 吸気通路中心線(主吸気通路の中心)
 L0 燃焼室の軸線
 DX 燃料噴射装置の噴射方向
 ArX 燃料の範囲
Reference Signs List 1 power unit 2 crankshaft 3 crankcase 4 cylinder block 5 cylinder head 6 head cover 10 internal combustion engine 15 inlet pipe 16 throttle body 17 connecting tube 18 air cleaner device 21 breather hose 24 combustion chamber 25 valve mechanism 27 intake port 29 exhaust port 31 spark plug 50 Intake passage 50A Main intake passage 50B Sub-intake passage 60 Fuel injection device 61 Fuel injection valve 62 Valve mounting member 63 Fastening member 62T Fastening portion (fastening portion of fastening member 63)
T Tumble flow S Swirl flow LC Intake passage center line (center of main intake passage)
L0 Axis of combustion chamber DX Direction of injection of fuel injector ArX Range of fuel

Claims (7)

  1.  燃焼室(24)につながる吸気通路(50)と、
     前記吸気通路(50)に設けられる燃料噴射装置(60)とを備え、
     前記吸気通路(50)が、前記燃焼室(24)に対し、その燃焼室(24)の軸線方向に対応する上下方向に離間した主吸気通路(50A)と副吸気通路(50B)とを備え、前記副吸気通路(50B)の断面積が前記主吸気通路(50A)の断面積よりも小さい内燃機関の吸気構造において、
     前記副吸気通路(50B)は、前記燃焼室(24)の軸線(L0)に対して左右いずれか一方にずれた方向に向けて指向し、
     前記燃料噴射装置(60)の噴射方向は、前記燃焼室(24)の軸線(L0)に対して前記一方にずれた方向に向けて指向していることを特徴とする内燃機関の吸気構造。
    an intake passage (50) leading to the combustion chamber (24);
    A fuel injection device (60) provided in the intake passage (50),
    The intake passageway (50) comprises a main intake passageway (50A) and a sub intake passageway (50B) which are vertically separated from the combustion chamber (24) corresponding to the axial direction of the combustion chamber (24). , an intake structure for an internal combustion engine, wherein the cross-sectional area of the auxiliary intake passage (50B) is smaller than the cross-sectional area of the main intake passage (50A),
    the auxiliary intake passage (50B) is oriented in a direction deviated leftward or rightward with respect to the axis (L0) of the combustion chamber (24),
    An intake structure for an internal combustion engine, wherein the injection direction of the fuel injection device (60) is oriented in the direction deviating from the axis (L0) of the combustion chamber (24) to the one side.
  2.  前記副吸気通路(50B)の下流側の断面積は、前記副吸気通路(50B)の上流側の断面積よりも小さいことを特徴とする請求項1に記載の内燃機関の吸気構造。 2. The intake structure for an internal combustion engine according to claim 1, wherein the cross-sectional area of the sub-intake passage (50B) on the downstream side is smaller than the cross-sectional area of the sub-intake passage (50B) on the upstream side.
  3.  前記燃料噴射装置(60)は、燃料噴射弁(61)と、前記燃料噴射弁(61)が装着される弁装着部材(62)とを有し、
     前記弁装着部材は(62)、前記主吸気通路(50A)又は前記燃焼室(24)に締結される締結部分(62T)を有し、
     前記燃料噴射弁(61)と前記締結部分(62T)とは、前記主吸気通路(50A)の中心(LC)を基準とした一方側と他方側とに振り分けて配置されていることを特徴とする請求項1又は2に記載の内燃機関の吸気構造。
    The fuel injection device (60) has a fuel injection valve (61) and a valve mounting member (62) to which the fuel injection valve (61) is mounted,
    The valve mounting member (62) has a fastening portion (62T) that is fastened to the main intake passage (50A) or the combustion chamber (24),
    The fuel injection valve (61) and the fastening portion (62T) are arranged so as to be divided into one side and the other side with respect to the center (LC) of the main intake passage (50A). 3. The intake structure for an internal combustion engine according to claim 1 or 2.
  4.  前記燃料噴射弁(61)と前記締結部分(62T)とは、上面視で、少なくとも一部が前記主吸気通路(50A)に重なることを特徴とする請求項3に記載の内燃機関の吸気構造。 4. An intake structure for an internal combustion engine according to claim 3, wherein said fuel injection valve (61) and said fastening portion (62T) at least partially overlap said main intake passage (50A) when viewed from above. .
  5.  前記内燃機関(10)は、当該内燃機関(10)のブローバイガスが通るブリーザホース(21)を備え、
     前記ブリーザホース(21)は、前記主吸気通路(50A)の中心を基準にして、前記締結部分(62T)の反対側に位置することを特徴とする請求項3又は4に記載の内燃機関の吸気構造。
    The internal combustion engine (10) includes a breather hose (21) through which blow-by gas of the internal combustion engine (10) passes,
    5. The internal combustion engine according to claim 3, wherein the breather hose (21) is located on the opposite side of the fastening portion (62T) with respect to the center of the main intake passage (50A). intake structure.
  6.  前記燃料噴射装置(60)の燃料噴射弁(61)は、前記主吸気通路(50A)の中心(LC)を基準にして、前記燃焼室(24)の軸線(L0)に対して前記噴射方向が指向する側の反対側に位置することを特徴とする請求項1から5のいずれか一項に記載の内燃機関の吸気構造。 The fuel injection valve (61) of the fuel injection device (60) is arranged in the injection direction with respect to the axis (L0) of the combustion chamber (24) with the center (LC) of the main intake passage (50A) as a reference. 6. The intake structure for an internal combustion engine according to any one of claims 1 to 5, characterized in that the air intake structure for an internal combustion engine is located on the side opposite to the side to which the is directed.
  7.  前記副吸気通路(50B)と、前記燃料噴射装置(60)の噴射方向は、前記燃焼室(24)の軸線(L0)に対して点火プラグ(31)と反対側を指向することを特徴とする請求項1から6のいずれか一項に記載の内燃機関の吸気構造。 The injection direction of the auxiliary intake passage (50B) and the fuel injection device (60) is directed to the opposite side of the ignition plug (31) with respect to the axis (L0) of the combustion chamber (24). The intake structure for an internal combustion engine according to any one of claims 1 to 6.
PCT/JP2021/014094 2021-03-31 2021-03-31 Intake structure for internal combustion engine WO2022208829A1 (en)

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