WO2023174003A1 - Piston and engine - Google Patents

Piston and engine Download PDF

Info

Publication number
WO2023174003A1
WO2023174003A1 PCT/CN2023/077047 CN2023077047W WO2023174003A1 WO 2023174003 A1 WO2023174003 A1 WO 2023174003A1 CN 2023077047 W CN2023077047 W CN 2023077047W WO 2023174003 A1 WO2023174003 A1 WO 2023174003A1
Authority
WO
WIPO (PCT)
Prior art keywords
piston body
annular groove
arc
piston
wall
Prior art date
Application number
PCT/CN2023/077047
Other languages
French (fr)
Chinese (zh)
Inventor
窦站成
崔京朋
梁伟
刘近报
李志杰
王德成
Original Assignee
潍柴动力股份有限公司
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 潍柴动力股份有限公司 filed Critical 潍柴动力股份有限公司
Publication of WO2023174003A1 publication Critical patent/WO2023174003A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00Pistons 
    • F02F3/26Pistons  having combustion chamber in piston head
    • 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

  • This application relates to the field of engine technology, for example, to a piston and an engine.
  • the engine is an important part of power devices such as vehicles, and the combustion chamber is one of the core components of the engine.
  • the structure of the combustion chamber plays an important role in the thermal efficiency of the engine and the fuel economy of the engine.
  • the present application provides a piston and an engine that can improve the problem of unsatisfactory thermal efficiency of the engine and unsatisfactory fuel economy of the engine due to the structure of the combustion chamber.
  • One embodiment provides a piston, including:
  • the piston body is provided with a combustion chamber at the top of the piston body, and a convex portion is provided at the bottom of the combustion chamber; the combustion chambers are arranged sequentially in a direction from the bottom of the piston body to the top of the piston body.
  • the first annular groove, the second annular groove and the third annular groove, the diameters of the first annular groove, the second annular groove and the third annular groove increase in sequence, the first annular groove, the The second annular groove and the third annular groove are coaxial and connected with each other, and the first annular groove, the second annular groove and the third annular groove are all arranged around the protrusion;
  • the second annular groove includes an annular outer wall and is located inside the outer wall and connected with The bottom wall is connected to the outer side wall, and a boss extending in the direction of the axis of the piston body is formed between the bottom wall and the first annular groove;
  • the third annular groove includes an arc-shaped concave portion, the inner end of the arc-shaped concave portion is connected to an end of the outer wall away from the bottom wall, and the outer end of the arc-shaped concave portion is connected to an end of the piston body.
  • the top surface is connected; during engine operation, the arc-shaped concave surface can form an air interlayer between the mixture and the air mixture.
  • the piston provided by this application includes a piston body with a combustion chamber on the top, and a convex portion is provided on the bottom of the combustion chamber.
  • the combustion chamber includes a third piston body with a caliber that is sequentially arranged in a direction from the bottom of the piston body to the top of the piston body and whose caliber increases sequentially.
  • the first annular groove, the second annular groove and the third annular groove are coaxial and connected with each other, and are all arranged around the protrusion.
  • the second annular groove includes an annular outer wall and a bottom wall located inside the outer wall and connected to the outer wall. A boss extending in the direction of the axis of the piston body is formed between the bottom wall and the first annular groove.
  • the third ring groove includes an arc-shaped concave portion.
  • the inner end of the arc-shaped concave portion is connected to an end of the outer wall of the second ring groove away from the bottom wall of the second ring groove.
  • the outer end of the arc-shaped concave portion is connected to the top surface of the piston body. connect.
  • the fuel flows to the center of the combustion chamber, and finally forms a relatively uniform mixture in the upper space of the second and third annular grooves.
  • the turbulence in the combustion chamber is fully utilized to form a mixture in the upper space of the second and third annular grooves.
  • Combustion enables the piston provided by this application to make full use of the combustion chamber space and form a uniform mixture inside the entire combustion chamber.
  • Making full use of the combustion chamber space for mixing and combustion can fully increase the heat release rate of the entire combustion process, especially the heat release rate when the crankshaft angle is 8° to 30°, thereby improving engine thermal efficiency and engine fuel economy.
  • an air interlayer is formed between the arc-shaped concave portion of the third ring groove and the mixture.
  • the air interlayer can reduce heat loss and effectively reduce the piston's wear and tear. Reduce heat transfer loss, improve thermal efficiency, and further reduce engine fuel consumption.
  • the piston provided by this application makes full use of the space of the entire combustion chamber to form a uniform mixture.
  • the fuel-rich area is reduced during the combustion process, and the high-temperature combustion area inside the combustion chamber is reduced. Therefore, nitrogen can be significantly reduced. Formation of oxygen compounds while fuel mixes with space Sufficient can significantly reduce the formation of particulate matter.
  • the diameter of the portion of the boss closest to the axis of the piston body is 50% to 55% of the outer diameter of the piston body.
  • the boss is an arcuate boss.
  • the center of the circle where the arc surface of the arcuate boss is located coincides with the third
  • the distance between the lowest parts of an annular groove is H1, and H1 is 7% to 8% of the outer diameter of the piston body.
  • the third annular groove includes a planar portion and an arc-shaped convex portion, the inner end of the planar portion is connected to the second annular groove, and the outer end of the planar portion is connected to the arc-shaped concave portion.
  • the inner end is connected; the inner end of the arc-shaped convex portion is connected to the outer end of the arc-shaped concave portion, and the outer end of the arc-shaped convex portion is connected to the top surface of the piston body.
  • the outer wall of the second annular groove is perpendicular to the top surface of the piston body
  • the distance between the outer end of the flat part and the outer wall of the second ring groove is W3, and the outer end of the arc-shaped convex part and the second ring groove
  • the distance between the outer side walls of the groove is W4, and the value of W4/W3 is 3 to 4.
  • the radius of the arc-shaped concave portion is 2 to 3 times the radius of the arc-shaped convex portion
  • the depth of the third annular groove is 2.5% to 4.5% of the thickness of the piston body
  • the diameter of the third annular groove is 80% to 90% of the outer diameter of the piston body.
  • the part with the smallest inner diameter of the arc boss is the throat.
  • the part of the first annular groove farthest from the axis of the piston body is between the corresponding part of the throat. The distance is d.
  • the distance between the center of the circle where the arc surface of the arc surface boss is located and the lowest part of the first annular groove in the axial direction of the piston body is 9 to 10 times d. times.
  • the distance between the part of the boss closest to the axis of the piston body and the outer wall is 4% to 5% of the outer diameter of the piston body;
  • the outer side wall of the second ring groove is connected to the third ring groove through a first fillet, and the outer wall of the second ring groove is connected to the third ring groove through a first fillet.
  • the fillet is connected to the bottom wall; the distance between the flat part and the center of the second fillet in the axial direction of the piston body is 1.1% to 1.3% of the outer diameter of the piston body;
  • the caliber at the outer wall of the second annular groove is 55% to 65% of the outer diameter of the piston body
  • the bottom wall of the second annular groove includes a tapered surface, and an included angle between the tapered surface and the top surface of the piston body is 8° to 25°.
  • the distance between the lowest part of the first annular groove and the top surface of the piston body is 13% to 20% of the outer diameter of the piston body.
  • the first annular groove includes a first arc segment and a second arc segment that are smoothly connected, the first arc segment is located at the bottom of the first annular groove, and the second arc segment Connect the first arc segment and the second annular groove;
  • the circle where the first arc segment is located is the first circle
  • the circle where the second arc segment is located is the second circle
  • the second circle is located in the first circle and is connected with the first circle.
  • the circles are tangent, and the center of the first circle is closer to the axis of the piston body than the center of the second circle; the part of the first circle closest to the axis of the piston body is in contact with the second circle.
  • the distance between the parts farthest from the axis of the piston body is W1, and the value of W1/H1 is 1.65-1.9.
  • the raised portion includes a truncated cone portion disposed at the bottom of the combustion chamber and located in the combustion chamber, and a spherical portion disposed on a side of the truncated cone portion facing the top surface of the piston body, wherein,
  • the cone angle of the truncated cone portion is 92° to 96°, and the radius of the spherical portion is 15 to 20 mm.
  • This application also provides an engine, including any piston provided in the above technical solutions.
  • the engine provided by this application can reduce heat loss, effectively reduce the heat transfer loss of the piston, improve thermal efficiency, and reduce engine fuel consumption.
  • the piston makes full use of the entire combustion chamber space to form a uniform mixture. This reduces the excessively rich fuel area during the combustion process and reduces the high-temperature combustion area inside the combustion chamber. Therefore, the formation of nitrogen oxide compounds can be significantly reduced. , and at the same time, sufficient mixing of fuel and space can significantly reduce the formation of particulate matter.
  • Figure 1 is a schematic structural diagram of a piston provided by an embodiment of the present application.
  • Figure 2 is a schematic structural diagram of the partial structure of the piston shown in Figure 1 when marked;
  • Figure 3 is an enlarged view of E in Figure 1;
  • Figure 4 is a schematic structural diagram of another part of the structure of the piston shown in Figure 1;
  • Figure 5 is a schematic diagram of the path of fuel in a piston provided by an embodiment of the present application (the arrow drawn from the axis of the piston body in the figure represents the fuel sprayed by the injector, and other arrows represent the fuel injected into the side wall of the combustion chamber and then burned through the The path of the fuel after being guided by the side wall of the chamber);
  • Figure 6 is a simulation cloud diagram of the mixture distribution in the combustion chamber when the engine uses the piston provided by this application;
  • Figure 7 is a simulation cloud diagram of the mixture distribution in the combustion chamber when the engine uses a piston other than that of this embodiment.
  • Icon 1-piston body; 2-combustion chamber; 3-convex portion; 21-first ring groove; 22-second ring groove; 221-outside wall; 222-bottom wall; 23-third ring groove; 231 -Arc-shaped concave portion; 232-Planar portion; 233-Arc-shaped convex portion; 24-Boss; 4-First circle; 5-Second circle.
  • the existing combustion chamber can effectively organize the mixing of oil and gas inside it, but the utilization rate of the air in the peripheral area of the combustion chamber is very low. If the diameter of the existing combustion chamber at the top surface of the piston is increased to bring the outer edge of the combustion chamber as close as possible to the outer edge of the piston, a large amount of oil-gas mixture will inevitably burn close to the inner wall of the cylinder liner, resulting in oil burning and piston enlargement.
  • the wear of the ring and cylinder liner, the increase in soot (soot) emissions from the engine increase the collection pressure of the after-treatment, increase the exhaust back pressure of the engine, and increase the cost of the after-treatment. At the same time, the increase in engine exhaust back pressure in turn reduces the engine's fuel economy. Since the existing combustion chamber cannot fully utilize the air near the edge of the combustion chamber, the heat release rate is relatively low when the diesel engine is working (when the crankshaft angle is about 8° to 30°), resulting in a relatively low thermal efficiency of the engine.
  • a piston provided in this embodiment includes a piston body 1, a combustion chamber 2 is provided at the top of the piston body 1, and a boss 3 is provided at the bottom of the combustion chamber 2; the combustion chamber 2 is included in the piston body 1
  • the bottom of the first annular groove 21, the second annular groove 22 and the third annular groove 23 are arranged sequentially in the direction of the top of the piston body 1.
  • the first annular groove 21, the second annular groove 22 and the third annular groove 23 are The caliber increases sequentially, the first annular groove 21, the second annular groove 22 and the third annular groove 23 are coaxial and connected with each other, and the first annular groove 21, the second annular groove 22 and the third annular groove 23 all surround the bulge Part 3 settings;
  • the second annular groove 22 includes an annular outer wall 221 and an outer There is a bottom wall 222 inside the wall 221 and connected to the outer wall 221. A boss 24 extending in the direction of the axis of the piston body 1 is formed between the bottom wall 222 and the first annular groove 21;
  • the third ring groove 23 includes an arc-shaped concave portion 231.
  • the inner end of the arc-shaped concave portion 231 is connected to an end of the outer wall 221 away from the bottom wall 222.
  • the outer end of the arc-shaped concave portion 231 is connected to the top surface of the piston body 1; engine During operation, the arc-shaped concave portion 231 can form an air interlayer F between the mixed gas (as shown in Figures 5 and 6, where the air interlayer is not numbered in Figure 6).
  • the piston provided in this embodiment includes a piston body 1 with a combustion chamber 2 at the top.
  • the combustion chamber 2 is provided with a protrusion 3 at the bottom.
  • the combustion chamber 2 is included in the direction from the bottom of the piston body 1 to the top of the piston body 1.
  • the first annular groove 21, the second annular groove 22 and the third annular groove 23 are arranged and have their diameters increased sequentially.
  • the first annular groove 21, the second annular groove 22 and the third annular groove 23 are coaxial and connected with each other, and are evenly spaced.
  • the second annular groove 22 includes an annular outer wall 221 and a bottom wall 222 located inside the outer wall 221 and connected to the outer wall 221 .
  • the third ring groove 23 includes an arc-shaped concave portion 231.
  • the inner end of the arc-shaped concave portion 231 is connected to an end of the outer wall 221 of the second ring groove 22 away from the bottom wall 222 of the second ring groove 22.
  • the outer end is connected to the top surface of the piston body 1.
  • the upper space of the annular groove 23 forms a mixture for combustion, so that the piston provided in this embodiment can fully utilize the space of the combustion chamber 2 and form a uniform mixture inside the entire combustion chamber 2 .
  • Making full use of the space of the combustion chamber 2 for mixing and combustion can fully increase the heat release rate of the entire combustion process, especially the heat release rate when the crankshaft angle is 8° to 30°, thus improving the engine thermal efficiency and engine fuel economy.
  • an air interlayer will be formed between the arc-shaped concave portion 231 of the third annular groove 23 and the mixture (as shown in Figures 5 and 6 (shown), the air interlayer can reduce heat loss, effectively reduce the heat transfer loss of the piston, improve thermal efficiency, and further reduce engine fuel consumption.
  • the piston provided in this embodiment fully utilizes the space of the entire combustion chamber 2 to form a uniform mixture.
  • the fuel-rich area is reduced during the combustion process, and the high-temperature combustion area inside the combustion chamber 2 is reduced. Therefore, it is possible to The formation of nitrogen oxides is significantly reduced, and sufficient mixing of fuel and space can significantly reduce the formation of particulate matter.
  • the air interlayer in this embodiment cannot be formed. , that is, the effects of reducing heat loss, reducing piston heat transfer loss, and improving thermal efficiency cannot be achieved.
  • the distance H0 between the top of the protrusion 3 and the top surface of the piston body 1 is related to the protrusion amount of the injector and can be set according to actual needs. Moreover, those skilled in the art know that the protrusion The top of the rising portion 3 is lower than the top surface of the piston body 1 .
  • the bottom of the combustion chamber 2 is provided with a protruding portion 3.
  • the protruding portion 3 is provided at the center of the bottom of the combustion chamber 2.
  • the first annular groove 21, the second annular groove 22, and the third annular groove 23 and the axis of the protrusion 3 can be coincident with the axis of the piston body 1 .
  • the raised portion 3 includes a truncated cone portion disposed at the bottom of the combustion chamber 2 and located in the combustion chamber 2, and a truncated cone portion disposed on the truncated cone portion facing the top surface of the piston body 1.
  • the cone angle ⁇ of the truncated cone portion is 92° to 96°
  • the radius R0 of the spherical portion is 15 to 20 mm.
  • the diameter of the first annular groove 21 mentioned in this embodiment refers to the diameter of the end of the first annular groove 21 away from the bottom of the piston body 1
  • the diameter of the second annular groove 22 refers to the diameter of the second annular groove 22
  • 22 is the diameter of the end of the third annular groove 23 away from the first annular groove 21
  • the diameter of the third annular groove 23 refers to the diameter of the end of the third annular groove 23 away from the second annular groove 22 .
  • a boss 24 extending in the direction of the axis of the piston body 1 is formed between the bottom wall 222 of the second ring groove 22 and the first ring groove 21. In order to facilitate processing, it can also play a role in controlling the fuel injected onto the boss 24. For better guiding effect, when specifically setting the above-mentioned boss 24, in an optional implementation manner, the boss 24 is a curved boss.
  • the diameter D1 of the portion of the boss 24 closest to the axis of the piston body 1 is 50% to 55% of the outer diameter of the piston body 1 .
  • the boss 24 is an arcuate boss.
  • the arcuate boss is The distance between the center of the circle where the arc surface is located and the lowest part of the first ring groove 21 is H1, H1 It is 7% to 8% of the outer diameter of the piston body 1 , so that the first annular groove 21 can utilize the air in the combustion chamber 2 more effectively.
  • the radius R1 of the arcuate boss may be 2.5-3.5 mm, for example, 3 mm.
  • the third annular groove 23 includes a flat portion 232 and an arc-shaped convex portion. 233, the inner end of the flat part 232 is connected with the second annular groove 22, the outer end of the flat part 232 is connected with the inner end of the arc concave part 231; the inner end of the arc convex part 233 is connected with the outer end of the arc concave part 231 The outer end of the arc-shaped convex portion 233 is connected to the top surface of the piston body 1 .
  • the outer side wall 221 of the second annular groove 22 is perpendicular to the top surface of the piston body 1;
  • the third annular groove 23 includes a flat portion 232 and an arc-shaped convex portion 233.
  • the radius R4 of the arc-shaped concave portion 231 is 2 to 3 times the radius R5 of the arc-shaped convex portion 233, for example: R4 is 2.5 times that of R5.
  • the depth H4 of the third ring groove 23 is 2.5% to 4.5% of the thickness of the piston body 1;
  • the diameter D3 of the third annular groove 23 (that is, the diameter of the third annular groove 23 at the connection point between the arc-shaped convex portion 233 and the top surface of the piston body 1) is 80% to 90% of the outer diameter of the piston body 1.
  • the above-mentioned radius R4 is 2 to 3 times the radius R5 of the arc-shaped convex portion 233 , the depth H4 is 2.5% to 4.5% of the thickness of the piston body 1 , and the diameter D3 is 80% of the outer diameter of the piston body 1
  • the above arrangement of the third ring groove 23 is more conducive to the formation of an air interlayer between the arc-shaped concave portion 231 and the mixture.
  • boss 24 formed between the bottom wall 222 of the second ring groove 22 and the first ring groove 21 is an arc boss
  • the part with the smallest inner diameter of the arc boss is the throat; on the same radius of the piston body 1, the first The distance between the farthest part of the annular groove 21 from the axis of the piston body 1 and the corresponding part of the throat is d.
  • d is 0.5% ⁇ of the outer diameter of the piston body 1 1%;
  • the distance f between the center of the circle where the arc surface of the arcuate boss is located and the lowest part of the first annular groove 21 in the axial direction of the piston body 1 is 9 to 10 times d.
  • d is 0.5% to 1% of the outer diameter of the piston body 1 and the distance f is 9 to 10 times d, which can also be used together in the same embodiment.
  • the above arrangement of the first annular groove 21 makes it difficult for the oil jet ejected from the injector to overlap with the air-fuel mixture rolled back by the first annular groove 21 , thereby improving the uniformity of the oil-air mixture inside the first annular groove 21 .
  • the outer wall 221 of the second annular groove 22 is perpendicular to the top surface of the piston body 1.
  • the part of the boss 24 closest to the axis of the piston body 1 is in contact with the second ring groove 22.
  • the distance W2 (as shown in Figure 4) between the outer side walls 221 of the annular groove 22 is 4% to 5% of the outer diameter of the piston body 1, so as to better guide the fuel injected onto the boss 24. .
  • the outer side wall 221 of the second ring groove 22 is connected to the third ring groove 23 through the first fillet R3, and is connected to the bottom wall 222 through the second fillet R2.
  • the third ring groove 23 includes Planar portion 232, the inner end of the planar portion 232 is connected to the second annular groove 22, and the outer end of the planar portion 232 is connected to the inner end of the arc concave portion 231; along the axis direction of the piston body 1, the planar portion 232 is connected to the second annular groove 22.
  • the diameter D2 at the outer side wall 221 of the second annular groove 22 is 55% to 65% of the outer diameter of the piston body 1;
  • the bottom wall 222 of the second annular groove 22 includes a tapered surface, and the angle b between the tapered surface and the top surface of the piston body 1 is 8° to 25°.
  • the bottom wall 222 of the second annular groove 22 has an inclined structure, which is beneficial to fuel guidance.
  • the above-mentioned arrangement of the second annular groove 22 is more conducive to guiding the oil-air mixture injected onto it upward, and is conducive to improving the mixing uniformity of the oil-air mixture.
  • the distance H2 between the lowest part of the first annular groove 21 and the top surface of the piston body 1 is the outer diameter of the piston body 1 13% to 20%.
  • the first annular groove 21 includes a first circular arc segment and a second circular arc segment that are smoothly connected.
  • the first circular arc segment is located at the bottom of the first annular groove 21 and the second circular arc segment is located at the bottom of the first annular groove 21 .
  • the arc segment connects the first arc segment and the second annular groove 22;
  • the circle where the first arc segment is located is the first circle 4, the circle where the second arc segment is located is the second circle 5, the second circle 5 is located in the first circle 4 and is tangent to the first circle 4, and
  • the center of the first circle 4 is closer to the axis of the piston body 1 than the center of the second circle 5; between the part of the first circle 4 closest to the axis of the piston body 1 and the part of the second circle 5 farthest from the axis of the piston body 1
  • the distance is W1
  • the value of W1/H1 is 1.65 ⁇ 1.9.
  • the value of W1/H1 is 1.65 ⁇ 1.9, which makes it difficult for the oil jet ejected from the injector in the early stage of combustion of the engine to overlap with the mixed gas recirculated from the first annular groove 21, which can improve the mixing of oil and gas inside the first annular groove 21. Uniformity can effectively improve the heat release rate in the early stage of combustion, improve thermal efficiency, and reduce fuel consumption rate; at the same time, the oil and gas are evenly mixed in the first ring groove 21, which can effectively reduce soot emissions.
  • the combustion chamber 2 includes three annular grooves, which improves the full utilization of air in each area inside the combustion chamber 2 by forcibly dividing the oil-air mixture into different circulation paths (as shown in Figure 5).
  • the design of multiple ring grooves can form multiple oil jets through steps between ring grooves, which is conducive to the complete mixing of oil and gas.
  • the outermost ring groove (the third ring groove 23 in this embodiment) in the multi-ring groove design can make full use of the air near the outer edge of the combustion chamber 2 close to the inner wall of the cylinder liner; improving the uniformity of the oil-gas mixture inside the combustion chamber 2 sex.
  • the three-ring groove design of the piston can make full use of the squeezing flow generated when the piston is compressed to make the oil-air mixture flow more easily toward the center of the combustion chamber 2, avoiding oil burning and wear caused by the mixture burning close to the inner wall of the cylinder liner.
  • Reliability problems such as aggravation
  • the optimized annular groove design can take advantage of the squeezing flow at the edge of the piston and the interaction of the oil beam to form an air interlayer between the mixture and the third annular groove 23 of the piston.
  • the air interlayer can effectively reduce the piston heat transfer loss, further reducing engine fuel consumption.
  • the design of the annular groove of the combustion chamber 2 in this embodiment makes it easier for the combustion chamber 2 to match the air passage. Regardless of the arrangement of the air passage, the swirl ratio intensity can be easily optimally matched to the combustion chamber 2.
  • This embodiment provides an engine including the above-mentioned piston.
  • the engine provided by this embodiment includes the above-mentioned piston. Therefore, it can at least achieve the technical effects that the above-mentioned piston can achieve, and the technical effects will not be described again here.
  • the engine provided in this embodiment can further improve the thermal efficiency of the diesel engine and reduce the engine fuel consumption on the premise of meeting the National VI emissions.
  • the engine mentioned in this embodiment may be a diesel engine or a gasoline engine.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)

Abstract

A piston and an engine. The piston comprises a piston body (1), the top of which is provided with a combustion chamber (2). The combustion chamber comprises a first ring groove (21), a second ring groove (22) and a third ring groove (23) sequentially arranged in a direction from the bottom of the piston body to the top of the piston body and having sequentially increasing diameters; the bottom of the combustion chamber is provided with a protruding part (3); the first ring groove, the second ring groove and the third ring groove are coaxial and communicated with each other, and are all arranged around the protruding part; the second ring groove comprises an annular outer side wall (221) and a bottom wall (222) located on the inner side of the outer side wall and connected to the outer side wall, and a boss (24) is formed between the bottom wall and the first ring groove; the third ring groove comprises an arc-shaped concave part (231), the inner end of the arc-shaped concave part is connected to the end of the outer side wall distant from the bottom wall, and the outer end of the arc-shaped concave part is connected to the top surface of the piston body.

Description

活塞及发动机Pistons and engines
本申请要求2022年03月17日提交中国专利局、申请号为202210260961.0、发明名称为“一种活塞及发动机”的发明专利的优先权,其全部内容通过引用结合在本申请中。This application claims the priority of the invention patent filed with the China Patent Office on March 17, 2022, with the application number 202210260961.0 and the invention title "A piston and an engine", the entire content of which is incorporated into this application by reference.
技术领域Technical field
本申请涉及发动机技术领域,例如涉及一种活塞及发动机。This application relates to the field of engine technology, for example, to a piston and an engine.
背景技术Background technique
发动机是车辆等动力装置的重要组成部分,燃烧室则是发动机的核心部件之一。燃烧室的结构对发动机的热效率以及发动机的燃油经济性起到重要作用。The engine is an important part of power devices such as vehicles, and the combustion chamber is one of the core components of the engine. The structure of the combustion chamber plays an important role in the thermal efficiency of the engine and the fuel economy of the engine.
近年来,随着人们环保意识的增强,各车企对发动机的热效率以及发动机的燃油经济性越来越重视,然而,相关技术中,受限于燃烧室的结构,发动机的热效率以及发动机的燃油经济性还并不理想。In recent years, as people's awareness of environmental protection has increased, various car companies have paid more and more attention to the thermal efficiency of the engine and the fuel economy of the engine. However, related technologies are limited by the structure of the combustion chamber, the thermal efficiency of the engine and the fuel economy of the engine. The economics are not ideal yet.
因而,亟待设计一种新的燃烧室结构来改善上述问题。Therefore, there is an urgent need to design a new combustion chamber structure to improve the above problems.
发明内容Contents of the invention
本申请提供了一种活塞及发动机,能够改善由于燃烧室的结构致使发动机的热效率以及发动机的燃油经济性不理想的问题。The present application provides a piston and an engine that can improve the problem of unsatisfactory thermal efficiency of the engine and unsatisfactory fuel economy of the engine due to the structure of the combustion chamber.
一实施例提供一种活塞,包括:One embodiment provides a piston, including:
活塞本体,所述活塞本体的顶部设有燃烧室,所述燃烧室的底部设有凸起部;所述燃烧室包括在所述活塞本体的底部指向所述活塞本体的顶部的方向上依次设置的第一环槽、第二环槽和第三环槽,所述第一环槽、所述第二环槽和所述第三环槽的口径依次增大,所述第一环槽、所述第二环槽和所述第三环槽同轴并相互连通,且所述第一环槽、所述第二环槽和所述第三环槽均环绕所述凸起部设置;The piston body is provided with a combustion chamber at the top of the piston body, and a convex portion is provided at the bottom of the combustion chamber; the combustion chambers are arranged sequentially in a direction from the bottom of the piston body to the top of the piston body. The first annular groove, the second annular groove and the third annular groove, the diameters of the first annular groove, the second annular groove and the third annular groove increase in sequence, the first annular groove, the The second annular groove and the third annular groove are coaxial and connected with each other, and the first annular groove, the second annular groove and the third annular groove are all arranged around the protrusion;
其中,所述第二环槽包括环状的外侧壁以及位于所述外侧壁内侧并与 所述外侧壁连接的底壁,所述底壁与所述第一环槽之间形成有向所述活塞本体的轴线所在方向延伸的凸台;Wherein, the second annular groove includes an annular outer wall and is located inside the outer wall and connected with The bottom wall is connected to the outer side wall, and a boss extending in the direction of the axis of the piston body is formed between the bottom wall and the first annular groove;
所述第三环槽包括弧形凹面部,所述弧形凹面部的内端与所述外侧壁远离所述底壁的一端连接,所述弧形凹面部的外端与所述活塞本体的顶面连接;发动机运行过程中,所述弧形凹面部能够与混合气之间形成空气夹层。The third annular groove includes an arc-shaped concave portion, the inner end of the arc-shaped concave portion is connected to an end of the outer wall away from the bottom wall, and the outer end of the arc-shaped concave portion is connected to an end of the piston body. The top surface is connected; during engine operation, the arc-shaped concave surface can form an air interlayer between the mixture and the air mixture.
本申请提供的活塞包括顶部设有燃烧室的活塞本体,燃烧室的底部设有凸起部,燃烧室包括在活塞本体的底部指向活塞本体的顶部的方向上依次设置且口径依次增大的第一环槽、第二环槽和第三环槽,第一环槽、第二环槽和第三环槽同轴并相互连通,且均环绕凸起部设置。其中,第二环槽包括环状的外侧壁以及位于外侧壁内侧并与外侧壁连接的底壁,底壁与第一环槽之间形成有向活塞本体的轴线所在方向延伸的凸台。借助燃油本身的动能和第二环槽可以有效引导喷射到燃烧室壁面上的燃油,进而引导油束射向第三环槽的空间中。而第三环槽包括弧形凹面部,弧形凹面部的内端与第二环槽的外侧壁远离第二环槽底壁的一端连接,弧形凹面部的外端与活塞本体的顶面连接。活塞运行过程中,到达预定位置(例如:活塞运行到发动机上止点附近)时,会形成由外缘向燃烧室中心的强挤流,该强挤流使从第二环槽导流过来的燃油向燃烧室中心流动,最终在第二环槽和第三环槽上部空间形成相对均匀的混合气,充分利用燃烧室内的湍流,在第二环槽和第三环槽上部空间形成混合气进行燃烧,使得本申请提供的活塞可以充分利用燃烧室空间,在整个燃烧室内部形成均匀混合气。而充分利用燃烧室空间进行混合及燃烧,可以充分提高整个燃烧过程的放热率,特别是曲轴转角8°~30°时的放热率,进而提升发动机热效率,提高发动机燃油经济性。The piston provided by this application includes a piston body with a combustion chamber on the top, and a convex portion is provided on the bottom of the combustion chamber. The combustion chamber includes a third piston body with a caliber that is sequentially arranged in a direction from the bottom of the piston body to the top of the piston body and whose caliber increases sequentially. The first annular groove, the second annular groove and the third annular groove are coaxial and connected with each other, and are all arranged around the protrusion. The second annular groove includes an annular outer wall and a bottom wall located inside the outer wall and connected to the outer wall. A boss extending in the direction of the axis of the piston body is formed between the bottom wall and the first annular groove. With the help of the kinetic energy of the fuel itself and the second annular groove, the fuel injected onto the combustion chamber wall can be effectively guided, and then the fuel beam is directed to the space of the third annular groove. The third ring groove includes an arc-shaped concave portion. The inner end of the arc-shaped concave portion is connected to an end of the outer wall of the second ring groove away from the bottom wall of the second ring groove. The outer end of the arc-shaped concave portion is connected to the top surface of the piston body. connect. During the operation of the piston, when it reaches a predetermined position (for example, when the piston moves to near the top dead center of the engine), a strong squeezing flow will be formed from the outer edge to the center of the combustion chamber. The fuel flows to the center of the combustion chamber, and finally forms a relatively uniform mixture in the upper space of the second and third annular grooves. The turbulence in the combustion chamber is fully utilized to form a mixture in the upper space of the second and third annular grooves. Combustion enables the piston provided by this application to make full use of the combustion chamber space and form a uniform mixture inside the entire combustion chamber. Making full use of the combustion chamber space for mixing and combustion can fully increase the heat release rate of the entire combustion process, especially the heat release rate when the crankshaft angle is 8° to 30°, thereby improving engine thermal efficiency and engine fuel economy.
发动机运行过程中,在活塞边缘的强挤流和油束的相互作用下,第三环槽的弧形凹面部与混合气之间形成的空气夹层,空气夹层能够减少热损失、有效降低活塞的传热损失、提高热效率,进一步降低发动机油耗。During engine operation, under the interaction of the strong squeeze flow at the edge of the piston and the oil jet, an air interlayer is formed between the arc-shaped concave portion of the third ring groove and the mixture. The air interlayer can reduce heat loss and effectively reduce the piston's wear and tear. Reduce heat transfer loss, improve thermal efficiency, and further reduce engine fuel consumption.
此外,本申请提供的活塞充分利用了整个燃烧室的空间形成均匀混合气,如此一来,在燃烧过程中减少了燃油过浓区域,减少了燃烧室内部高温燃烧区域,因而,可明显降低氮氧化合物的形成,同时燃油与空间混合 充分可以明显降低颗粒物的形成。In addition, the piston provided by this application makes full use of the space of the entire combustion chamber to form a uniform mixture. In this way, the fuel-rich area is reduced during the combustion process, and the high-temperature combustion area inside the combustion chamber is reduced. Therefore, nitrogen can be significantly reduced. Formation of oxygen compounds while fuel mixes with space Sufficient can significantly reduce the formation of particulate matter.
可选地,所述凸台最靠近所述活塞本体轴线的部位的直径为所述活塞本体的外径的50%~55%。Optionally, the diameter of the portion of the boss closest to the axis of the piston body is 50% to 55% of the outer diameter of the piston body.
可选地,所述凸台为弧面凸台,沿所述活塞本体的轴线方向,在所述活塞本体的纵向截面上,所述弧面凸台的弧面所在圆的圆心与所述第一环槽的最低部位之间的距离为H1,H1为所述活塞本体的外径的7%~8%。Optionally, the boss is an arcuate boss. Along the axis direction of the piston body, in the longitudinal section of the piston body, the center of the circle where the arc surface of the arcuate boss is located coincides with the third The distance between the lowest parts of an annular groove is H1, and H1 is 7% to 8% of the outer diameter of the piston body.
可选地,所述第三环槽包括平面部和弧形凸面部,所述平面部的内端与所述第二环槽连接,所述平面部的外端与所述弧形凹面部的内端连接;所述弧形凸面部的内端与所述弧形凹面部的外端连接,所述弧形凸面部的外端与所述活塞本体的顶面连接。Optionally, the third annular groove includes a planar portion and an arc-shaped convex portion, the inner end of the planar portion is connected to the second annular groove, and the outer end of the planar portion is connected to the arc-shaped concave portion. The inner end is connected; the inner end of the arc-shaped convex portion is connected to the outer end of the arc-shaped concave portion, and the outer end of the arc-shaped convex portion is connected to the top surface of the piston body.
可选地,所述第二环槽的外侧壁垂直于所述活塞本体的顶面;Optionally, the outer wall of the second annular groove is perpendicular to the top surface of the piston body;
在所述活塞本体的径向方向上,所述平面部的外端与所述第二环槽的外侧壁之间的距离为W3,所述弧形凸面部的外端和所述第二环槽的外侧壁之间的距离为W4,W4/W3的值为3~4。In the radial direction of the piston body, the distance between the outer end of the flat part and the outer wall of the second ring groove is W3, and the outer end of the arc-shaped convex part and the second ring groove The distance between the outer side walls of the groove is W4, and the value of W4/W3 is 3 to 4.
可选地,还包括以下方案中的至少一种:Optionally, at least one of the following solutions is also included:
所述弧形凹面部的半径是所述弧形凸面部的半径的2~3倍;The radius of the arc-shaped concave portion is 2 to 3 times the radius of the arc-shaped convex portion;
所述第三环槽的深度为所述活塞本体的厚度的2.5%~4.5%;The depth of the third annular groove is 2.5% to 4.5% of the thickness of the piston body;
所述第三环槽的口径为所述活塞本体的外径的80%~90%。The diameter of the third annular groove is 80% to 90% of the outer diameter of the piston body.
可选地,还包括以下方案中的至少一种:Optionally, at least one of the following solutions is also included:
所述弧面凸台内径最小的部位为喉口,在所述活塞本体的同一半径上,所述第一环槽距离所述活塞本体轴线最远的部位与所述喉口的相应部位之间的距离为d,当所述活塞本体的外径小于等于150毫米时,d为所述活塞本体的外径的0.5%~1%;The part with the smallest inner diameter of the arc boss is the throat. On the same radius of the piston body, the part of the first annular groove farthest from the axis of the piston body is between the corresponding part of the throat. The distance is d. When the outer diameter of the piston body is less than or equal to 150 mm, d is 0.5% to 1% of the outer diameter of the piston body;
所述活塞本体的纵向截面上,所述弧面凸台的弧面所在的圆的圆心与所述第一环槽的最低部位在所述活塞本体的轴线方向上的距离为d的9~10倍。In the longitudinal section of the piston body, the distance between the center of the circle where the arc surface of the arc surface boss is located and the lowest part of the first annular groove in the axial direction of the piston body is 9 to 10 times d. times.
可选地,还包括以下方案中的至少一种:Optionally, at least one of the following solutions is also included:
在所述活塞本体的同一半径上,所述凸台最靠近所述活塞本体轴线的部位与所述外侧壁之间的距离为所述活塞本体的外径的4%~5%;On the same radius of the piston body, the distance between the part of the boss closest to the axis of the piston body and the outer wall is 4% to 5% of the outer diameter of the piston body;
所述第二环槽的外侧壁通过第一圆角与所述第三环槽连接,通过第二 圆角与所述底壁连接;在所述活塞本体的轴线方向上所述平面部与所述第二圆角的圆心之间的距离为所述活塞本体的外径的1.1%~1.3%;The outer side wall of the second ring groove is connected to the third ring groove through a first fillet, and the outer wall of the second ring groove is connected to the third ring groove through a first fillet. The fillet is connected to the bottom wall; the distance between the flat part and the center of the second fillet in the axial direction of the piston body is 1.1% to 1.3% of the outer diameter of the piston body;
所述第二环槽外侧壁处的口径为所述活塞本体的外径的55%~65%;The caliber at the outer wall of the second annular groove is 55% to 65% of the outer diameter of the piston body;
所述第二环槽的底壁包括锥面,所述锥面与所述活塞本体的顶面之间的夹角的为8°~25°。The bottom wall of the second annular groove includes a tapered surface, and an included angle between the tapered surface and the top surface of the piston body is 8° to 25°.
可选地,所述第一环槽的最低部位与所述活塞本体的顶面之间的距离为所述活塞本体的外径的13%~20%。Optionally, the distance between the lowest part of the first annular groove and the top surface of the piston body is 13% to 20% of the outer diameter of the piston body.
可选地,所述第一环槽包括圆滑连接的第一圆弧段和第二圆弧段,所述第一圆弧段位于所述第一环槽的底部,所述第二圆弧段连接所述第一圆弧段与所述第二环槽;Optionally, the first annular groove includes a first arc segment and a second arc segment that are smoothly connected, the first arc segment is located at the bottom of the first annular groove, and the second arc segment Connect the first arc segment and the second annular groove;
以所述第一圆弧段所在的圆为第一圆,所述第二圆弧段所在的圆为第二圆,所述第二圆位于所述第一圆中,并与所述第一圆相切,且所述第一圆的圆心较所述第二圆的圆心靠近所述活塞本体的轴线;在所述第一圆最靠近所述活塞本体的轴线的部位与所述第二圆最远离所述活塞本体的轴线的部位之间的距离为W1,W1/H1的值为1.65~1.9。The circle where the first arc segment is located is the first circle, the circle where the second arc segment is located is the second circle, and the second circle is located in the first circle and is connected with the first circle. The circles are tangent, and the center of the first circle is closer to the axis of the piston body than the center of the second circle; the part of the first circle closest to the axis of the piston body is in contact with the second circle. The distance between the parts farthest from the axis of the piston body is W1, and the value of W1/H1 is 1.65-1.9.
可选地,所述凸起部包括设置于所述燃烧室底部并位于所述燃烧室中的圆台部以及设置于所述圆台部朝向所述活塞本体顶面的一侧的球面部,其中,所述圆台部的锥角为92°~96°,所述球面部的半径为15~20毫米。Optionally, the raised portion includes a truncated cone portion disposed at the bottom of the combustion chamber and located in the combustion chamber, and a spherical portion disposed on a side of the truncated cone portion facing the top surface of the piston body, wherein, The cone angle of the truncated cone portion is 92° to 96°, and the radius of the spherical portion is 15 to 20 mm.
本申请还提供一种发动机,包括上述技术方案中提供的任意一种活塞。This application also provides an engine, including any piston provided in the above technical solutions.
本申请提供的发动机能够减少热损失、有效降低活塞的传热损失、提高热效率,降低发动机油耗。同时,活塞充分利用了整个燃烧室的空间形成均匀混合气,如此一来,在燃烧过程中减少了燃油过浓区域,减少了燃烧室内部高温燃烧区域,因而,可明显降低氮氧化合物的形成,同时燃油与空间混合充分可以明显降低颗粒物的形成。The engine provided by this application can reduce heat loss, effectively reduce the heat transfer loss of the piston, improve thermal efficiency, and reduce engine fuel consumption. At the same time, the piston makes full use of the entire combustion chamber space to form a uniform mixture. This reduces the excessively rich fuel area during the combustion process and reduces the high-temperature combustion area inside the combustion chamber. Therefore, the formation of nitrogen oxide compounds can be significantly reduced. , and at the same time, sufficient mixing of fuel and space can significantly reduce the formation of particulate matter.
附图说明Description of the drawings
图1为本申请实施例提供的一种活塞的结构示意图;Figure 1 is a schematic structural diagram of a piston provided by an embodiment of the present application;
图2为对图1所示的活塞中的部分结构进行标注时的结构示意图;Figure 2 is a schematic structural diagram of the partial structure of the piston shown in Figure 1 when marked;
图3为图1的E处放大图; Figure 3 is an enlarged view of E in Figure 1;
图4为对图1所示的活塞中的另一部分结构进行标注时的结构示意图;Figure 4 is a schematic structural diagram of another part of the structure of the piston shown in Figure 1;
图5为本申请实施例提供的一种活塞中燃油的路径示意图(图中由活塞本体轴线引出的箭头表示喷油器喷出的燃油,其他箭头表示喷射到燃烧室侧壁上后,经燃烧室侧壁引导后的燃油的路径);Figure 5 is a schematic diagram of the path of fuel in a piston provided by an embodiment of the present application (the arrow drawn from the axis of the piston body in the figure represents the fuel sprayed by the injector, and other arrows represent the fuel injected into the side wall of the combustion chamber and then burned through the The path of the fuel after being guided by the side wall of the chamber);
图6为发动机采用本申请提供的活塞时,燃烧室中混合气分布仿真云图;Figure 6 is a simulation cloud diagram of the mixture distribution in the combustion chamber when the engine uses the piston provided by this application;
图7为发动机采用本实施例之外的活塞时,燃烧室中混合气分布仿真云图。Figure 7 is a simulation cloud diagram of the mixture distribution in the combustion chamber when the engine uses a piston other than that of this embodiment.
图标:1-活塞本体;2-燃烧室;3-凸起部;21-第一环槽;22-第二环槽;221-外侧壁;222-底壁;23-第三环槽;231-弧形凹面部;232-平面部;233-弧形凸面部;24-凸台;4-第一圆;5-第二圆。Icon: 1-piston body; 2-combustion chamber; 3-convex portion; 21-first ring groove; 22-second ring groove; 221-outside wall; 222-bottom wall; 23-third ring groove; 231 -Arc-shaped concave portion; 232-Planar portion; 233-Arc-shaped convex portion; 24-Boss; 4-First circle; 5-Second circle.
具体实施方式Detailed ways
现有的燃烧室能够有效地组织其内部的油气混合,但是对于燃烧室外缘区域空气的利用率非常低。如果通过增大现有燃烧室在活塞顶面处的直径的方式来使燃烧室外缘尽可能靠近活塞外缘,必然会造成大量油气混合气贴近缸套内壁燃烧,从而造成烧机油、增大活塞环与缸套的磨损、发动机的soot(碳烟)排放增大,加大后处理的捕集压力,增大发动机的排气背压,提高了后处理的成本。同时,发动机排气背压的增大又反过来降低了发动机的燃油经济性。现有的燃烧室由于无法充分利用燃烧室外缘附近的空气,造成柴油机工作时(曲轴转角约8°~30°附近时)放热率比较低,导致发动机的热效率相对较低。The existing combustion chamber can effectively organize the mixing of oil and gas inside it, but the utilization rate of the air in the peripheral area of the combustion chamber is very low. If the diameter of the existing combustion chamber at the top surface of the piston is increased to bring the outer edge of the combustion chamber as close as possible to the outer edge of the piston, a large amount of oil-gas mixture will inevitably burn close to the inner wall of the cylinder liner, resulting in oil burning and piston enlargement. The wear of the ring and cylinder liner, the increase in soot (soot) emissions from the engine, increase the collection pressure of the after-treatment, increase the exhaust back pressure of the engine, and increase the cost of the after-treatment. At the same time, the increase in engine exhaust back pressure in turn reduces the engine's fuel economy. Since the existing combustion chamber cannot fully utilize the air near the edge of the combustion chamber, the heat release rate is relatively low when the diesel engine is working (when the crankshaft angle is about 8° to 30°), resulting in a relatively low thermal efficiency of the engine.
如图1所示,本实施例提供的一种活塞包括活塞本体1,活塞本体1的顶部设有燃烧室2,燃烧室2的底部设有凸起部3;燃烧室2包括在活塞本体1的底部指向活塞本体1的顶部的方向上依次设置的第一环槽21、第二环槽22和第三环槽23,第一环槽21、第二环槽22和第三环槽23的口径依次增大,第一环槽21、第二环槽22和第三环槽23同轴并相互连通,且第一环槽21、第二环槽22和第三环槽23均环绕凸起部3设置;As shown in Figure 1, a piston provided in this embodiment includes a piston body 1, a combustion chamber 2 is provided at the top of the piston body 1, and a boss 3 is provided at the bottom of the combustion chamber 2; the combustion chamber 2 is included in the piston body 1 The bottom of the first annular groove 21, the second annular groove 22 and the third annular groove 23 are arranged sequentially in the direction of the top of the piston body 1. The first annular groove 21, the second annular groove 22 and the third annular groove 23 are The caliber increases sequentially, the first annular groove 21, the second annular groove 22 and the third annular groove 23 are coaxial and connected with each other, and the first annular groove 21, the second annular groove 22 and the third annular groove 23 all surround the bulge Part 3 settings;
其中,如图2所示,第二环槽22包括环状的外侧壁221以及位于外侧 壁221内侧并与外侧壁221连接的底壁222,底壁222与第一环槽21之间形成有向活塞本体1的轴线所在方向延伸的凸台24;As shown in FIG. 2 , the second annular groove 22 includes an annular outer wall 221 and an outer There is a bottom wall 222 inside the wall 221 and connected to the outer wall 221. A boss 24 extending in the direction of the axis of the piston body 1 is formed between the bottom wall 222 and the first annular groove 21;
第三环槽23包括弧形凹面部231,弧形凹面部231的内端与外侧壁221远离底壁222的一端连接,弧形凹面部231的外端与活塞本体1的顶面连接;发动机运行过程中,弧形凹面部231能够与混合气之间形成空气夹层F(如图5和图6所示,其中,图6中没有对空气夹层进行标号)。The third ring groove 23 includes an arc-shaped concave portion 231. The inner end of the arc-shaped concave portion 231 is connected to an end of the outer wall 221 away from the bottom wall 222. The outer end of the arc-shaped concave portion 231 is connected to the top surface of the piston body 1; engine During operation, the arc-shaped concave portion 231 can form an air interlayer F between the mixed gas (as shown in Figures 5 and 6, where the air interlayer is not numbered in Figure 6).
本实施例提供的活塞包括顶部设有燃烧室2的活塞本体1,燃烧室2的底部设有凸起部3,燃烧室2包括在活塞本体1的底部指向活塞本体1的顶部的方向上依次设置且口径依次增大的第一环槽21、第二环槽22和第三环槽23,第一环槽21、第二环槽22和第三环槽23同轴并相互连通,且均环绕凸起部3设置。其中,第二环槽22包括环状的外侧壁221以及位于外侧壁221内侧并与外侧壁221连接的底壁222,底壁222与第一环槽21之间形成有向活塞本体1的轴线所在方向延伸的凸台24。借助燃油本身的动能和第二环槽22可以有效引导喷射到燃烧室2壁面上的燃油,进而引导油束射向第三环槽23的空间中。而第三环槽23包括弧形凹面部231,弧形凹面部231的内端与第二环槽22的外侧壁221远离第二环槽22底壁222的一端连接,弧形凹面部231的外端与活塞本体1的顶面连接。活塞运行过程中,到达预定位置(例如:活塞运行到发动机上止点附近)时,会形成由外缘向燃烧室2中心的强挤流,该强挤流使从第二环槽22导流过来的燃油向燃烧室2中心流动,最终在第二环槽22和第三环槽23上部空间形成相对均匀的混合气,充分利用燃烧室2内的湍流,在第二环槽22和第三环槽23上部空间形成混合气进行燃烧,使得本实施例提供的活塞可以充分利用燃烧室2的空间,在整个燃烧室2内部形成均匀混合气。而充分利用燃烧室2的空间进行混合及燃烧,可以充分提高整个燃烧过程的放热率,特别是曲轴转角8°~30°时的放热率,进而提升发动机热效率,提高发动机燃油经济性。The piston provided in this embodiment includes a piston body 1 with a combustion chamber 2 at the top. The combustion chamber 2 is provided with a protrusion 3 at the bottom. The combustion chamber 2 is included in the direction from the bottom of the piston body 1 to the top of the piston body 1. The first annular groove 21, the second annular groove 22 and the third annular groove 23 are arranged and have their diameters increased sequentially. The first annular groove 21, the second annular groove 22 and the third annular groove 23 are coaxial and connected with each other, and are evenly spaced. Set around the raised portion 3. The second annular groove 22 includes an annular outer wall 221 and a bottom wall 222 located inside the outer wall 221 and connected to the outer wall 221 . An axis directed toward the piston body 1 is formed between the bottom wall 222 and the first annular groove 21 . The boss 24 extends in the same direction. The fuel injected onto the wall of the combustion chamber 2 can be effectively guided by the kinetic energy of the fuel itself and the second annular groove 22 , and then the fuel beam is guided to the space of the third annular groove 23 . The third ring groove 23 includes an arc-shaped concave portion 231. The inner end of the arc-shaped concave portion 231 is connected to an end of the outer wall 221 of the second ring groove 22 away from the bottom wall 222 of the second ring groove 22. The outer end is connected to the top surface of the piston body 1. During the operation of the piston, when it reaches a predetermined position (for example, when the piston moves to near the top dead center of the engine), a strong squeezing flow will be formed from the outer edge to the center of the combustion chamber 2. This strong squeezing flow will guide the flow from the second annular groove 22 The incoming fuel flows toward the center of the combustion chamber 2, and finally forms a relatively uniform mixture in the upper space of the second annular groove 22 and the third annular groove 23, making full use of the turbulence in the combustion chamber 2, and creates a mixture between the second annular groove 22 and the third annular groove 23. The upper space of the annular groove 23 forms a mixture for combustion, so that the piston provided in this embodiment can fully utilize the space of the combustion chamber 2 and form a uniform mixture inside the entire combustion chamber 2 . Making full use of the space of the combustion chamber 2 for mixing and combustion can fully increase the heat release rate of the entire combustion process, especially the heat release rate when the crankshaft angle is 8° to 30°, thus improving the engine thermal efficiency and engine fuel economy.
同时,发动机运行过程中,在活塞边缘的强挤流和油束的相互作用下,第三环槽23的弧形凹面部231与混合气之间会形成空气夹层(如图5和图6所示),空气夹层能够减少热损失、有效降低活塞的传热损失、提高热效率,进一步降低发动机油耗。 At the same time, during engine operation, under the interaction of the strong squeezing flow at the edge of the piston and the oil jet, an air interlayer will be formed between the arc-shaped concave portion 231 of the third annular groove 23 and the mixture (as shown in Figures 5 and 6 (shown), the air interlayer can reduce heat loss, effectively reduce the heat transfer loss of the piston, improve thermal efficiency, and further reduce engine fuel consumption.
此外,本实施例提供的活塞充分利用了整个燃烧室2的空间形成均匀混合气,如此一来,在燃烧过程中减少了燃油过浓区域,减少了燃烧室2内部高温燃烧区域,因而,可明显降低氮氧化合物的形成,同时燃油与空间混合充分可以明显降低颗粒物的形成。In addition, the piston provided in this embodiment fully utilizes the space of the entire combustion chamber 2 to form a uniform mixture. In this way, the fuel-rich area is reduced during the combustion process, and the high-temperature combustion area inside the combustion chamber 2 is reduced. Therefore, it is possible to The formation of nitrogen oxides is significantly reduced, and sufficient mixing of fuel and space can significantly reduce the formation of particulate matter.
如图7所示,经过仿真,如果第三环槽23为锥面,则无论第三环槽23与活塞本体1顶面之间的夹角怎样设置,均无法形成本实施例中的空气夹层,即,无法达到减少热损失、降低活塞传热损失、提高热效率的效果。As shown in Figure 7, after simulation, if the third annular groove 23 is a tapered surface, no matter how the angle between the third annular groove 23 and the top surface of the piston body 1 is set, the air interlayer in this embodiment cannot be formed. , that is, the effects of reducing heat loss, reducing piston heat transfer loss, and improving thermal efficiency cannot be achieved.
沿活塞本体1的轴线方向,凸起部3的顶部与活塞本体1顶面之间的距离H0与喷油器的凸出量有关,可以根据实际需要设置,而且,本领域技术人员知晓,凸起部3的顶部低于活塞本体1的顶面。Along the axis direction of the piston body 1, the distance H0 between the top of the protrusion 3 and the top surface of the piston body 1 is related to the protrusion amount of the injector and can be set according to actual needs. Moreover, those skilled in the art know that the protrusion The top of the rising portion 3 is lower than the top surface of the piston body 1 .
燃烧室2的底部设有凸起部3,一种可选的实现方式中,凸起部3设置于燃烧室2底部的中心,第一环槽21、第二环槽22、第三环槽23以及凸起部3的轴线均可以与活塞本体1的轴线重合。The bottom of the combustion chamber 2 is provided with a protruding portion 3. In an optional implementation, the protruding portion 3 is provided at the center of the bottom of the combustion chamber 2. The first annular groove 21, the second annular groove 22, and the third annular groove 23 and the axis of the protrusion 3 can be coincident with the axis of the piston body 1 .
具体设置上述凸起部3时,一种可选的实现方式中,凸起部3包括设置于燃烧室2底部并位于燃烧室2中的圆台部以及设置于圆台部朝向活塞本体1顶面的一侧的球面部,其中,圆台部的锥角α为92°~96°,球面部的半径R0为15~20毫米。When specifically setting the above-mentioned raised portion 3, in an optional implementation, the raised portion 3 includes a truncated cone portion disposed at the bottom of the combustion chamber 2 and located in the combustion chamber 2, and a truncated cone portion disposed on the truncated cone portion facing the top surface of the piston body 1. As for the spherical portion on one side, the cone angle α of the truncated cone portion is 92° to 96°, and the radius R0 of the spherical portion is 15 to 20 mm.
需要说明的是,本实施例中提到的第一环槽21的口径是指第一环槽21远离活塞本体1的底部的一端的直径,第二环槽22的口径是指第二环槽22远离第一环槽21的一端的直径,第三环槽23的口径是指第三环槽23远离第二环槽22的一端的直径。It should be noted that the diameter of the first annular groove 21 mentioned in this embodiment refers to the diameter of the end of the first annular groove 21 away from the bottom of the piston body 1 , and the diameter of the second annular groove 22 refers to the diameter of the second annular groove 22 . 22 is the diameter of the end of the third annular groove 23 away from the first annular groove 21 , and the diameter of the third annular groove 23 refers to the diameter of the end of the third annular groove 23 away from the second annular groove 22 .
第二环槽22的底壁222与第一环槽21之间形成有向活塞本体1的轴线所在方向延伸的凸台24,为了便于加工,同时能够对喷射到凸台24上的燃油起到更好的引导作用,具体设置上述凸台24时,一种可选的实现方式中,凸台24为弧面凸台。A boss 24 extending in the direction of the axis of the piston body 1 is formed between the bottom wall 222 of the second ring groove 22 and the first ring groove 21. In order to facilitate processing, it can also play a role in controlling the fuel injected onto the boss 24. For better guiding effect, when specifically setting the above-mentioned boss 24, in an optional implementation manner, the boss 24 is a curved boss.
请继续参照图1,一种可选的实现方式中,凸台24最靠近活塞本体1轴线的部位的直径D1为活塞本体1的外径的50%~55%。Please continue to refer to FIG. 1 . In an optional implementation, the diameter D1 of the portion of the boss 24 closest to the axis of the piston body 1 is 50% to 55% of the outer diameter of the piston body 1 .
一种可选的实现方式中,凸台24为弧面凸台,沿活塞本体1的轴线方向,在活塞本体1的纵向截面(即经过活塞本体1轴线的截面)上,弧面凸台的弧面所在圆的圆心与第一环槽21的最低部位之间的距离为H1,H1 为活塞本体1的外径的7%~8%,从而使得第一环槽21能够更有效地利用燃烧室2中的空气。In an optional implementation, the boss 24 is an arcuate boss. Along the axis direction of the piston body 1, on the longitudinal section of the piston body 1 (that is, the section passing through the axis of the piston body 1), the arcuate boss is The distance between the center of the circle where the arc surface is located and the lowest part of the first ring groove 21 is H1, H1 It is 7% to 8% of the outer diameter of the piston body 1 , so that the first annular groove 21 can utilize the air in the combustion chamber 2 more effectively.
示例性地,弧面凸台的半径R1可以为2.5~3.5毫米,例如:3毫米。For example, the radius R1 of the arcuate boss may be 2.5-3.5 mm, for example, 3 mm.
为了对喷射到其上的油气混合气起到更好的引导效果,一种可选的实现方式中,如图2和图3所示,第三环槽23包括平面部232和弧形凸面部233,平面部232的内端与第二环槽22连接,平面部232的外端与弧形凹面部231的内端连接;弧形凸面部233的内端与弧形凹面部231的外端连接,弧形凸面部233的外端与活塞本体1的顶面连接。In order to better guide the oil-air mixture injected onto it, in an optional implementation, as shown in Figures 2 and 3, the third annular groove 23 includes a flat portion 232 and an arc-shaped convex portion. 233, the inner end of the flat part 232 is connected with the second annular groove 22, the outer end of the flat part 232 is connected with the inner end of the arc concave part 231; the inner end of the arc convex part 233 is connected with the outer end of the arc concave part 231 The outer end of the arc-shaped convex portion 233 is connected to the top surface of the piston body 1 .
一种可选的实现方式中,第二环槽22的外侧壁221垂直于活塞本体1的顶面;In an optional implementation, the outer side wall 221 of the second annular groove 22 is perpendicular to the top surface of the piston body 1;
请继续参照图2,在活塞本体1的径向方向上,平面部232的外端与第二环槽22的外侧壁221之间的距离为W3,弧形凸面部233的外端和第二环槽22的外侧壁221之间的距离为W4,W4/W3的值为3~4(即,W4与W3的比值为3至4),从而进一步提高第三环槽23对喷射到其上的油气混合气的引导效果。Please continue to refer to Figure 2. In the radial direction of the piston body 1, the distance between the outer end of the flat portion 232 and the outer wall 221 of the second annular groove 22 is W3, and the outer end of the arc-shaped convex portion 233 and the second The distance between the outer side walls 221 of the annular groove 22 is W4, and the value of W4/W3 is 3 to 4 (that is, the ratio of W4 to W3 is 3 to 4), thereby further improving the efficiency of the third annular groove 23 to be sprayed thereon. The guiding effect of the oil-gas mixture.
第三环槽23包括平面部232和弧形凸面部233,一种可选的实现方式中,弧形凹面部231的半径R4是弧形凸面部233的半径R5的2~3倍,例如:R4是R5的2.5倍。The third annular groove 23 includes a flat portion 232 and an arc-shaped convex portion 233. In an optional implementation, the radius R4 of the arc-shaped concave portion 231 is 2 to 3 times the radius R5 of the arc-shaped convex portion 233, for example: R4 is 2.5 times that of R5.
第三环槽23的深度H4为活塞本体1的厚度的2.5%~4.5%;The depth H4 of the third ring groove 23 is 2.5% to 4.5% of the thickness of the piston body 1;
第三环槽23的口径D3(即弧形凸面部233与活塞本体1顶面的连接处第三环槽23的直径)为活塞本体1的外径的80%~90%。The diameter D3 of the third annular groove 23 (that is, the diameter of the third annular groove 23 at the connection point between the arc-shaped convex portion 233 and the top surface of the piston body 1) is 80% to 90% of the outer diameter of the piston body 1.
在一些实施例中,上述半径R4是弧形凸面部233的半径R5的2~3倍、深度H4为活塞本体1的厚度的2.5%~4.5%、口径D3为活塞本体1的外径的80%~90%三种尺寸关系,可以仅具有其中的一种,也可以具有其中的任意两种,也可以同时具有三种。In some embodiments, the above-mentioned radius R4 is 2 to 3 times the radius R5 of the arc-shaped convex portion 233 , the depth H4 is 2.5% to 4.5% of the thickness of the piston body 1 , and the diameter D3 is 80% of the outer diameter of the piston body 1 There are three size relationships of % to 90%, and you can have only one of them, any two of them, or three of them at the same time.
第三环槽23采用上述设置,更有利于弧形凹面部231与混合气之间形成空气夹层。The above arrangement of the third ring groove 23 is more conducive to the formation of an air interlayer between the arc-shaped concave portion 231 and the mixture.
一种可选的实现方式中,若第二环槽22的底壁222与第一环槽21之间形成的凸台24为弧面凸台,则:In an optional implementation, if the boss 24 formed between the bottom wall 222 of the second ring groove 22 and the first ring groove 21 is an arc boss, then:
弧面凸台内径最小的部位为喉口;在活塞本体1的同一半径上,第一 环槽21距离活塞本体1轴线最远的部位与喉口的相应部位之间的距离为d,当活塞本体1的外径小于等于150毫米时,d为活塞本体1的外径的0.5%~1%;The part with the smallest inner diameter of the arc boss is the throat; on the same radius of the piston body 1, the first The distance between the farthest part of the annular groove 21 from the axis of the piston body 1 and the corresponding part of the throat is d. When the outer diameter of the piston body 1 is less than or equal to 150 mm, d is 0.5%~ of the outer diameter of the piston body 1 1%;
或者,活塞本体1的纵向截面上,弧面凸台的弧面所在的圆的圆心与第一环槽21的最低部位在活塞本体1的轴线方向上的距离f为d的9~10倍。Alternatively, in the longitudinal section of the piston body 1, the distance f between the center of the circle where the arc surface of the arcuate boss is located and the lowest part of the first annular groove 21 in the axial direction of the piston body 1 is 9 to 10 times d.
当然,上述d为活塞本体1的外径的0.5%~1%和距离f为d的9~10倍,也可以在同一实施例中一起采用。Of course, the above d is 0.5% to 1% of the outer diameter of the piston body 1 and the distance f is 9 to 10 times d, which can also be used together in the same embodiment.
第一环槽21采用上述设置使得从喷油器喷出的油束与被第一环槽21反卷回来的混合气不易重叠,能够提升第一环槽21内部油气混合气的均匀性。The above arrangement of the first annular groove 21 makes it difficult for the oil jet ejected from the injector to overlap with the air-fuel mixture rolled back by the first annular groove 21 , thereby improving the uniformity of the oil-air mixture inside the first annular groove 21 .
一种可选的实现方式中,第二环槽22的外侧壁221垂直于活塞本体1的顶面,在活塞本体1的同一半径上,凸台24最靠近活塞本体1轴线的部位与第二环槽22的外侧壁221之间的距离W2(如图4所示)为活塞本体1的外径的4%~5%,以对喷射到凸台24上的燃油起到更好的引导作用。In an optional implementation, the outer wall 221 of the second annular groove 22 is perpendicular to the top surface of the piston body 1. On the same radius of the piston body 1, the part of the boss 24 closest to the axis of the piston body 1 is in contact with the second ring groove 22. The distance W2 (as shown in Figure 4) between the outer side walls 221 of the annular groove 22 is 4% to 5% of the outer diameter of the piston body 1, so as to better guide the fuel injected onto the boss 24. .
一种可选的实现方式中,第二环槽22的外侧壁221通过第一圆角R3与第三环槽23连接,通过第二圆角R2与底壁222连接,第三环槽23包括平面部232,平面部232的内端与第二环槽22连接,平面部232的外端与弧形凹面部231的内端连接;沿活塞本体1的轴线方向上,平面部232与第二圆角R2的圆心之间的距离H3为活塞本体1的外径的1.1%~1.3%;示例性地,R2较R3大,R3尽量小,例如:R2=1.5mm,R3=1mm。In an optional implementation, the outer side wall 221 of the second ring groove 22 is connected to the third ring groove 23 through the first fillet R3, and is connected to the bottom wall 222 through the second fillet R2. The third ring groove 23 includes Planar portion 232, the inner end of the planar portion 232 is connected to the second annular groove 22, and the outer end of the planar portion 232 is connected to the inner end of the arc concave portion 231; along the axis direction of the piston body 1, the planar portion 232 is connected to the second annular groove 22. The distance H3 between the centers of the fillets R2 is 1.1% to 1.3% of the outer diameter of the piston body 1; for example, R2 is larger than R3, and R3 is as small as possible, for example: R2=1.5mm, R3=1mm.
一种可选的实现方式中,第二环槽22外侧壁221处的口径D2为活塞本体1的外径的55%~65%;In an optional implementation, the diameter D2 at the outer side wall 221 of the second annular groove 22 is 55% to 65% of the outer diameter of the piston body 1;
一种可选的实现方式中,第二环槽22的底壁222包括锥面,锥面与活塞本体1的顶面之间的夹角b的为8°~25°。第二环槽22的底壁222为倾斜结构,有利于燃油的导向。In an optional implementation, the bottom wall 222 of the second annular groove 22 includes a tapered surface, and the angle b between the tapered surface and the top surface of the piston body 1 is 8° to 25°. The bottom wall 222 of the second annular groove 22 has an inclined structure, which is beneficial to fuel guidance.
第二环槽22采用上述设置更有利于将喷射到其上的油气混合气向上方引导,有利于提高油气混合气的混合均匀性。The above-mentioned arrangement of the second annular groove 22 is more conducive to guiding the oil-air mixture injected onto it upward, and is conducive to improving the mixing uniformity of the oil-air mixture.
为了提高油气混合气混合的均匀性,一种可选的实现方式中,第一环槽21的最低部位与活塞本体1的顶面之间的距离H2为活塞本体1的外径 的13%~20%。In order to improve the uniformity of the oil-air mixture, in an optional implementation, the distance H2 between the lowest part of the first annular groove 21 and the top surface of the piston body 1 is the outer diameter of the piston body 1 13% to 20%.
进一步地,一种可选的实现方式中,第一环槽21包括圆滑连接的第一圆弧段和第二圆弧段,第一圆弧段位于第一环槽21的底部,第二圆弧段连接第一圆弧段与第二环槽22;Further, in an optional implementation, the first annular groove 21 includes a first circular arc segment and a second circular arc segment that are smoothly connected. The first circular arc segment is located at the bottom of the first annular groove 21 and the second circular arc segment is located at the bottom of the first annular groove 21 . The arc segment connects the first arc segment and the second annular groove 22;
以第一圆弧段所在的圆为第一圆4,第二圆弧段所在的圆为第二圆5,第二圆5位于第一圆4中,并与第一圆4相切,且第一圆4的圆心较第二圆5的圆心靠近活塞本体1的轴线;在第一圆4最靠近活塞本体1的轴线的部位与第二圆5最远离活塞本体1的轴线的部位之间的距离为W1,W1/H1的值为1.65~1.9。The circle where the first arc segment is located is the first circle 4, the circle where the second arc segment is located is the second circle 5, the second circle 5 is located in the first circle 4 and is tangent to the first circle 4, and The center of the first circle 4 is closer to the axis of the piston body 1 than the center of the second circle 5; between the part of the first circle 4 closest to the axis of the piston body 1 and the part of the second circle 5 farthest from the axis of the piston body 1 The distance is W1, and the value of W1/H1 is 1.65~1.9.
W1/H1的值为1.65~1.9,使得发动机在燃烧初期从喷油器喷出的油束与第一环槽21反卷回来的混合气不易重叠,能够提升第一环槽21内部油气的混合均匀性,有效提升燃烧初期的放热率、提高热效率,降低燃油消耗率;同时,在第一环槽21内油气混合均匀,可以有效降低soot排放。The value of W1/H1 is 1.65~1.9, which makes it difficult for the oil jet ejected from the injector in the early stage of combustion of the engine to overlap with the mixed gas recirculated from the first annular groove 21, which can improve the mixing of oil and gas inside the first annular groove 21. Uniformity can effectively improve the heat release rate in the early stage of combustion, improve thermal efficiency, and reduce fuel consumption rate; at the same time, the oil and gas are evenly mixed in the first ring groove 21, which can effectively reduce soot emissions.
本实施例提供的活塞,燃烧室2包括三个环槽,通过将油气混合气强制分成不同的环流路径(如图5所示),改善了燃烧室2内部各区域空气的充分利用问题。同时,多环槽的设计方案,可以通过环槽之间的阶跃形成多次油束射流,有利于油气充分混合。多环槽设计中的最外层环槽(本实施例中即第三环槽23)可以充分利用燃烧室2外缘靠近缸套内壁附近的空气;提高了燃烧室2内部油气混合气的均匀性。本实施例中活塞的三环槽设计可以充分利用活塞压缩时产生的挤流使油气混合气更容易往燃烧室2中心方向流动,避免了混合气靠近缸套内壁燃烧带来的烧机油及磨损加剧等可靠性问题;同时,优化的环槽设计可以利用活塞边缘的挤流和油束的相互作用,在混合气和活塞的第三环槽23之间形成空气夹层,空气夹层可以有效降低活塞的传热损失,进一步降低发动机油耗。In the piston provided in this embodiment, the combustion chamber 2 includes three annular grooves, which improves the full utilization of air in each area inside the combustion chamber 2 by forcibly dividing the oil-air mixture into different circulation paths (as shown in Figure 5). At the same time, the design of multiple ring grooves can form multiple oil jets through steps between ring grooves, which is conducive to the complete mixing of oil and gas. The outermost ring groove (the third ring groove 23 in this embodiment) in the multi-ring groove design can make full use of the air near the outer edge of the combustion chamber 2 close to the inner wall of the cylinder liner; improving the uniformity of the oil-gas mixture inside the combustion chamber 2 sex. In this embodiment, the three-ring groove design of the piston can make full use of the squeezing flow generated when the piston is compressed to make the oil-air mixture flow more easily toward the center of the combustion chamber 2, avoiding oil burning and wear caused by the mixture burning close to the inner wall of the cylinder liner. Reliability problems such as aggravation; at the same time, the optimized annular groove design can take advantage of the squeezing flow at the edge of the piston and the interaction of the oil beam to form an air interlayer between the mixture and the third annular groove 23 of the piston. The air interlayer can effectively reduce the piston heat transfer loss, further reducing engine fuel consumption.
此外,本实施例中燃烧室2环槽的设计使得燃烧室2更容易与气道进行匹配,无论气道布置形式如何,涡流比强度大小都可以很容易与该燃烧室2进行最优化匹配。In addition, the design of the annular groove of the combustion chamber 2 in this embodiment makes it easier for the combustion chamber 2 to match the air passage. Regardless of the arrangement of the air passage, the swirl ratio intensity can be easily optimally matched to the combustion chamber 2.
本实施例提供的一种发动机包括上述活塞。This embodiment provides an engine including the above-mentioned piston.
本实施例提供的发动机包括上述活塞,因而,至少能够达到上述活塞所能够达到的技术效果,该技术效果此处不再赘述。 The engine provided by this embodiment includes the above-mentioned piston. Therefore, it can at least achieve the technical effects that the above-mentioned piston can achieve, and the technical effects will not be described again here.
本实施例提供的发动机在满足国六排放的前提下,能够进一步提升柴油机热效率、降低发动机油耗。The engine provided in this embodiment can further improve the thermal efficiency of the diesel engine and reduce the engine fuel consumption on the premise of meeting the National VI emissions.
需要说明的是,本实施例中提到的发动机可以为柴油发动机或者汽油发动机。 It should be noted that the engine mentioned in this embodiment may be a diesel engine or a gasoline engine.

Claims (12)

  1. 一种活塞,包括活塞本体(1),所述活塞本体(1)的顶部设有燃烧室(2),所述燃烧室(2)的底部设有凸起部(3);所述燃烧室(2)包括在所述活塞本体(1)的底部指向所述活塞本体(1)的顶部的方向上依次设置的第一环槽(21)、第二环槽(22)和第三环槽(23),所述第一环槽(21)、所述第二环槽(22)和所述第三环槽(23)的口径依次增大,所述第一环槽(21)、所述第二环槽(22)和所述第三环槽(23)同轴并相互连通,且所述第一环槽(21)、所述第二环槽(22)和所述第三环槽(23)均环绕所述凸起部(3)设置;A piston includes a piston body (1), a combustion chamber (2) is provided at the top of the piston body (1), and a protrusion (3) is provided at the bottom of the combustion chamber (2); the combustion chamber (2) It includes a first annular groove (21), a second annular groove (22) and a third annular groove arranged sequentially in the direction from the bottom of the piston body (1) to the top of the piston body (1). (23), the diameters of the first annular groove (21), the second annular groove (22) and the third annular groove (23) increase in sequence, the first annular groove (21), the The second ring groove (22) and the third ring groove (23) are coaxial and connected with each other, and the first ring groove (21), the second ring groove (22) and the third ring groove The grooves (23) are all arranged around the raised portion (3);
    其中,所述第二环槽(22)包括环状的外侧壁(221)以及位于所述外侧壁(221)内侧并与所述外侧壁(221)连接的底壁(222),所述底壁(222)与所述第一环槽(21)之间形成有向所述活塞本体(1)的轴线所在方向延伸的凸台(24);Wherein, the second annular groove (22) includes an annular outer wall (221) and a bottom wall (222) located inside the outer wall (221) and connected to the outer wall (221). A boss (24) extending in the direction of the axis of the piston body (1) is formed between the wall (222) and the first annular groove (21);
    所述第三环槽(23)包括弧形凹面部(231),所述弧形凹面部(231)的内端与所述外侧壁(221)远离所述底壁(222)的一端连接,所述弧形凹面部(231)的外端与所述活塞本体(1)的顶面连接;发动机运行过程中,所述弧形凹面部(231)能够与混合气之间形成空气夹层。The third annular groove (23) includes an arc-shaped concave portion (231), and the inner end of the arc-shaped concave portion (231) is connected to an end of the outer wall (221) away from the bottom wall (222). The outer end of the arc-shaped concave portion (231) is connected to the top surface of the piston body (1); during engine operation, the arc-shaped concave portion (231) can form an air interlayer with the mixture.
  2. 根据权利要求1所述的活塞,其中:所述凸台(24)最靠近所述活塞本体(1)轴线的部位的直径为所述活塞本体(1)的外径的50%~55%。The piston according to claim 1, wherein the diameter of the portion of the boss (24) closest to the axis of the piston body (1) is 50% to 55% of the outer diameter of the piston body (1).
  3. 根据权利要求1所述的活塞,其中,所述凸台(24)为弧面凸台,沿所述活塞本体(1)的轴线方向,在所述活塞本体(1)的纵向截面上,所述弧面凸台的弧面所在圆的圆心与所述第一环槽(21)的最低部位之间的距离为H1,H1为所述活塞本体(1)的外径的7%~8%。The piston according to claim 1, wherein the boss (24) is a curved boss, along the axis direction of the piston body (1), on the longitudinal section of the piston body (1), the The distance between the center of the circle where the arc surface of the arc surface boss is located and the lowest part of the first annular groove (21) is H1, and H1 is 7% to 8% of the outer diameter of the piston body (1). .
  4. 根据权利要求1所述的活塞,其中,所述第三环槽(23)包括平面部(232)和弧形凸面部(233),所述平面部(232)的内端与所述第二环槽(22)连接,所述平面部(232)的外端与所述弧形凹面部(231)的内端连接;所述弧形凸面部(233)的内端与所述弧形凹面部(231)的外端连接,所述弧形凸面部(233)的外端与所述活塞本体(1)的顶面连接。The piston according to claim 1, wherein the third annular groove (23) includes a flat portion (232) and an arc-shaped convex portion (233), and the inner end of the flat portion (232) is in contact with the second The annular groove (22) is connected, the outer end of the flat part (232) is connected with the inner end of the arc-shaped concave part (231); the inner end of the arc-shaped convex part (233) is connected with the arc-shaped concave part The outer end of the arc-shaped convex portion (233) is connected to the top surface of the piston body (1).
  5. 根据权利要求4所述的活塞,其中,所述第二环槽(22)的外侧壁(221)垂直于所述活塞本体(1)的顶面; The piston according to claim 4, wherein the outer wall (221) of the second annular groove (22) is perpendicular to the top surface of the piston body (1);
    在所述活塞本体(1)的径向方向上,所述平面部(232)的外端与所述第二环槽(22)的外侧壁(221)之间的距离为W3,所述弧形凸面部(233)的外端和所述第二环槽(22)的外侧壁(221)之间的距离为W4,W4/W3的值为3~4。In the radial direction of the piston body (1), the distance between the outer end of the flat portion (232) and the outer wall (221) of the second annular groove (22) is W3, and the arc The distance between the outer end of the convex portion (233) and the outer wall (221) of the second annular groove (22) is W4, and the value of W4/W3 is 3-4.
  6. 根据权利要求4所述的活塞,还包括以下方案中的至少一种:The piston according to claim 4, further comprising at least one of the following solutions:
    所述弧形凹面部(231)的半径是所述弧形凸面部(233)的半径的2~3倍;The radius of the arc-shaped concave portion (231) is 2 to 3 times the radius of the arc-shaped convex portion (233);
    所述第三环槽(23)的深度为所述活塞本体(1)的厚度的2.5%~4.5%;The depth of the third annular groove (23) is 2.5% to 4.5% of the thickness of the piston body (1);
    所述第三环槽(23)的口径为所述活塞本体(1)的外径的80%~90%。The diameter of the third annular groove (23) is 80% to 90% of the outer diameter of the piston body (1).
  7. 根据权利要求3所述的活塞,其中,还包括以下方案中的至少一种:The piston according to claim 3, further comprising at least one of the following solutions:
    所述弧面凸台内径最小的部位为喉口,在所述活塞本体(1)的同一半径上,所述第一环槽(21)距离所述活塞本体(1)轴线最远的部位与所述喉口的相应部位之间的距离为d,当所述活塞本体(1)的外径小于等于150毫米时,d为所述活塞本体(1)的外径的0.5%~1%;The part with the smallest inner diameter of the arc boss is the throat. On the same radius of the piston body (1), the part of the first annular groove (21) farthest from the axis of the piston body (1) is the same as that of the piston body (1). The distance between the corresponding parts of the throat is d. When the outer diameter of the piston body (1) is less than or equal to 150 mm, d is 0.5% to 1% of the outer diameter of the piston body (1);
    所述活塞本体(1)的纵向截面上,所述弧面凸台的弧面所在的圆的圆心与所述第一环槽(21)的最低部位在所述活塞本体(1)的轴线方向上的距离为d的9~10倍。In the longitudinal section of the piston body (1), the center of the circle where the arc surface of the arcuate boss is located and the lowest part of the first annular groove (21) are in the axial direction of the piston body (1). The distance above is 9 to 10 times of d.
  8. 根据权利要求5所述的活塞,还包括以下方案中的至少一种:The piston according to claim 5, further comprising at least one of the following solutions:
    在所述活塞本体(1)的同一半径上,所述凸台(24)最靠近所述活塞本体(1)轴线的部位与所述外侧壁(221)之间的距离为所述活塞本体(1)的外径的4%~5%;On the same radius of the piston body (1), the distance between the part of the boss (24) closest to the axis of the piston body (1) and the outer wall (221) is the distance of the piston body (221) 1) 4% to 5% of the outer diameter;
    所述第二环槽(22)的外侧壁(221)通过第一圆角与所述第三环槽(23)连接,通过第二圆角与所述底壁(222)连接;沿所述活塞本体(1)的轴线方向上所述平面部(232)与所述第二圆角的圆心之间的距离为所述活塞本体(1)的外径的1.1%~1.3%;The outer side wall (221) of the second annular groove (22) is connected to the third annular groove (23) through a first fillet and connected to the bottom wall (222) through a second fillet; along the The distance between the flat part (232) and the center of the second fillet in the axial direction of the piston body (1) is 1.1% to 1.3% of the outer diameter of the piston body (1);
    所述第二环槽(22)的外侧壁(221)处的口径为所述活塞本体(1)的外径的55%~65%;The diameter of the outer wall (221) of the second annular groove (22) is 55% to 65% of the outer diameter of the piston body (1);
    所述第二环槽(22)的底壁(222)包括锥面,所述锥面与所述活塞本体(1)的顶面之间的夹角的为8°~25°。The bottom wall (222) of the second annular groove (22) includes a tapered surface, and the angle between the tapered surface and the top surface of the piston body (1) is 8° to 25°.
  9. 根据权利要求1-8任一项所述的活塞,其中,所述第一环槽(21) 的最低部位与所述活塞本体(1)的顶面之间的距离为所述活塞本体(1)的外径的13%~20%。The piston according to any one of claims 1-8, wherein the first annular groove (21) The distance between the lowest part and the top surface of the piston body (1) is 13% to 20% of the outer diameter of the piston body (1).
  10. 根据权利要求3所述的活塞,其中,所述第一环槽(21)包括圆滑连接的第一圆弧段和第二圆弧段,所述第一圆弧段位于所述第一环槽(21)的底部,所述第二圆弧段连接所述第一圆弧段与所述第二环槽(22);The piston according to claim 3, wherein the first annular groove (21) includes a first arc segment and a second arc segment that are smoothly connected, and the first arc segment is located in the first annular groove. (21) at the bottom, the second arc segment connects the first arc segment and the second annular groove (22);
    以所述第一圆弧段所在的圆为第一圆(4),所述第二圆弧段所在的圆为第二圆(5),所述第二圆(5)位于所述第一圆(4)中,并与所述第一圆(4)相切,且所述第一圆(4)的圆心较所述第二圆(5)的圆心靠近所述活塞本体(1)的轴线;在所述第一圆(4)最靠近所述活塞本体(1)的轴线的部位与所述第二圆(5)最远离所述活塞本体(1)的轴线的部位之间的距离为W1,W1/H1的值为1.65~1.9。The circle where the first arc segment is located is the first circle (4), the circle where the second arc segment is located is the second circle (5), and the second circle (5) is located on the first in the circle (4) and tangent to the first circle (4), and the center of the first circle (4) is closer to the center of the piston body (1) than the center of the second circle (5) Axis; the distance between the part of the first circle (4) closest to the axis of the piston body (1) and the part of the second circle (5) farthest from the axis of the piston body (1) is W1, and the value of W1/H1 is 1.65~1.9.
  11. 根据权利要求1-8任一项所述的活塞,其中,所述凸起部(3)包括设置于所述燃烧室底部并位于所述燃烧室中的圆台部以及设置于所述圆台部朝向所述活塞本体(1)顶面的一侧的球面部,其中,所述圆台部的锥角为92°~96°,所述球面部的半径为15~20毫米。The piston according to any one of claims 1 to 8, wherein the raised portion (3) includes a truncated cone portion disposed at the bottom of the combustion chamber and located in the combustion chamber, and a truncated cone portion disposed toward the bottom of the combustion chamber. As for the spherical portion on one side of the top surface of the piston body (1), the cone angle of the truncated cone portion is 92° to 96°, and the radius of the spherical portion is 15 to 20 mm.
  12. 一种发动机,包括权利要求1-11任一项所述的活塞。 An engine including the piston according to any one of claims 1-11.
PCT/CN2023/077047 2022-03-17 2023-02-16 Piston and engine WO2023174003A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN202210260961.0 2022-03-17
CN202210260961.0A CN114352431B (en) 2022-03-17 2022-03-17 Piston and engine

Publications (1)

Publication Number Publication Date
WO2023174003A1 true WO2023174003A1 (en) 2023-09-21

Family

ID=81094586

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2023/077047 WO2023174003A1 (en) 2022-03-17 2023-02-16 Piston and engine

Country Status (2)

Country Link
CN (1) CN114352431B (en)
WO (1) WO2023174003A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114352431B (en) * 2022-03-17 2022-06-07 潍柴动力股份有限公司 Piston and engine
CN114526152A (en) * 2022-04-22 2022-05-24 潍柴动力股份有限公司 Combustion chamber and diesel engine
CN115680928A (en) * 2022-11-18 2023-02-03 中国重汽集团济南动力有限公司 Piston, diesel engine and vehicle
CN116006347A (en) * 2023-03-28 2023-04-25 潍柴动力股份有限公司 Piston, engine and vehicle

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109162804A (en) * 2018-10-22 2019-01-08 东风商用车有限公司 Low heat waste diesel engine combustion chamber structure
CN210799166U (en) * 2019-11-08 2020-06-19 江苏中孚动力产业链有限公司 Piston of diesel internal combustion engine
CN210858963U (en) * 2019-09-29 2020-06-26 潍柴动力股份有限公司 Engine piston, engine and vehicle
US20200340391A1 (en) * 2016-03-10 2020-10-29 Avl List Gmbh Air-compressing internal combustion engine
CN213235251U (en) * 2020-09-10 2021-05-18 潍柴动力股份有限公司 Engine piston and diesel engine
CN113982741A (en) * 2021-09-30 2022-01-28 东风商用车有限公司 Step type combustion chamber peripheral guiding gutter structure
CN114352431A (en) * 2022-03-17 2022-04-15 潍柴动力股份有限公司 Piston and engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102444496B (en) * 2011-12-09 2013-09-04 石家庄金刚内燃机零部件集团有限公司 Pressurizing oil-saving type piston of diesel engine
CN103696870B (en) * 2013-12-09 2016-03-16 潍柴动力股份有限公司 A kind of cylinder of diesel engine piston and apply the diesel engine of this firing chamber
CN105909420A (en) * 2016-06-14 2016-08-31 广西玉柴机器股份有限公司 Combustion chamber capable of reducing soot in diesel engine cylinder
CN109372650A (en) * 2018-11-29 2019-02-22 汽解放汽车有限公司 The piston-top surface structure of soot in a kind of reduction cylinder of diesel engine
CN212079456U (en) * 2020-05-13 2020-12-04 清华大学 Diesel engine combustion chamber
CN213775520U (en) * 2020-12-08 2021-07-23 一汽解放汽车有限公司 Diesel engine combustion chamber, diesel engine and automobile

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20200340391A1 (en) * 2016-03-10 2020-10-29 Avl List Gmbh Air-compressing internal combustion engine
CN109162804A (en) * 2018-10-22 2019-01-08 东风商用车有限公司 Low heat waste diesel engine combustion chamber structure
CN210858963U (en) * 2019-09-29 2020-06-26 潍柴动力股份有限公司 Engine piston, engine and vehicle
CN210799166U (en) * 2019-11-08 2020-06-19 江苏中孚动力产业链有限公司 Piston of diesel internal combustion engine
CN213235251U (en) * 2020-09-10 2021-05-18 潍柴动力股份有限公司 Engine piston and diesel engine
CN113982741A (en) * 2021-09-30 2022-01-28 东风商用车有限公司 Step type combustion chamber peripheral guiding gutter structure
CN114352431A (en) * 2022-03-17 2022-04-15 潍柴动力股份有限公司 Piston and engine

Also Published As

Publication number Publication date
CN114352431A (en) 2022-04-15
CN114352431B (en) 2022-06-07

Similar Documents

Publication Publication Date Title
WO2023174003A1 (en) Piston and engine
JP5908890B2 (en) Piston with combustion bowl shaped to balance combustion efficiency and exhaust gas performance
WO2006040936A1 (en) Shape of combustion chamber of direct injection diesel engine
CN110953067A (en) Engine and double-jet combustion method thereof
JP2012189041A (en) Diesel engine
JP2007247420A (en) Auxiliary-chamber type internal combustion engine
CN116398313A (en) Diesel engine combustion chamber, piston and diesel engine
CN116398315A (en) Diesel engine combustion chamber, piston and diesel engine
CN109404156B (en) Combustion chamber of direct injection diesel engine
CN107355297B (en) Engine combustion chamber suitable for gasoline fuel combustion instead of diesel engine
CN207018102U (en) A kind of gasoline compression ignition piston combustion bowl
CN100465416C (en) Method for operating a direct-injection diesel engine
CN202611915U (en) Piston combustion chamber with large throat area and small depth
CN203067111U (en) Piston, crankshaft and connecting rod mechanism and diesel engine
CN110966113A (en) Gasoline engine and piston top structure thereof
CN114635814A (en) Scaling spray pipe acceleration mixer for enhancing oil-gas mixing of high-intensity diesel engine
CN201330656Y (en) Piston of natural gas engine
CN210264972U (en) Combustion system of direct-injection supercharged gasoline engine in middle-placed cylinder
CN208122957U (en) engine assembly
CN220979658U (en) Combustion chamber, combustion system and engine
CN2900826Y (en) Low discharge single cylinder diesel engine piston combustion chamber
CN214007345U (en) Natural gas engine piston
CN201739005U (en) Low-emission combustion chamber of vehicle direct-injection diesel
CN1811143A (en) Swirl chamber burning system for direct injection diesel engine
CN213235253U (en) Piston and engine

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 23769511

Country of ref document: EP

Kind code of ref document: A1