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WO2002025090A1 - A combined gas ring and its piston ring-piston assembly - Google Patents

A combined gas ring and its piston ring-piston assembly Download PDF

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Publication number
WO2002025090A1
WO2002025090A1 PCT/CN2001/000542 CN0100542W WO0225090A1 WO 2002025090 A1 WO2002025090 A1 WO 2002025090A1 CN 0100542 W CN0100542 W CN 0100542W WO 0225090 A1 WO0225090 A1 WO 0225090A1
Authority
WO
WIPO (PCT)
Prior art keywords
ring
piston
groove
cover
combined air
Prior art date
Application number
PCT/CN2001/000542
Other languages
French (fr)
Chinese (zh)
Inventor
Weimin Tang
Original Assignee
Weimin Tang
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from CN 00126547 external-priority patent/CN1343837A/en
Application filed by Weimin Tang filed Critical Weimin Tang
Priority to AU2001263730A priority Critical patent/AU2001263730A1/en
Publication of WO2002025090A1 publication Critical patent/WO2002025090A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J9/00Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
    • F16J9/12Details
    • F16J9/14Joint-closures
    • F16J9/16Joint-closures obtained by stacking of rings

Definitions

  • the invention relates to a piston ring, in particular to a combined air ring.
  • the invention also relates to a piston ring-piston assembly using the combined air ring, which is suitable for various reciprocating piston engines, especially for reciprocating piston two- or four-stroke engines. Background technique
  • the traditional air ring is usually a one-piece air ring, and a straight-through air leakage channel exists at the cut of the air ring. Therefore, the existing air ring seals on the cylinder are based on the throttling principle.
  • Two to three air rings are sequentially installed in the ring grooves on the piston in the axial direction, and the cuts of the air rings are staggered in the circumferential direction.
  • This structure has a series of disadvantages caused by inter-ring gas flow and inter-ring gas flow. It cannot eliminate the short-circuit gas leakage phenomenon when the upper and lower piston ring counterparts. The righting effect of the piston ring on the piston is also caused by the rotation of the upper and lower rings. And worse.
  • the existing piston ring-piston assemblies currently used in reciprocating piston engines all adopt an air-sealing structure in which a plurality of air rings are sequentially arranged in the axial direction on the piston. At least two air rings are required for this type of gas sealing. Therefore, the conventional piston ring-piston assembly cannot reduce the reciprocating inertial mass of the piston by reducing the number of air rings. On the other hand, due to the structural position relationship, the load difference of each constituent ring is large, and it is difficult to improve the overall performance of the engine by giving full play to the working performance of each constituent ring.
  • An object of the present invention is to provide a combined air ring, which can prevent straight-through gas leakage to achieve the technical effects of enhancing gas sealing and controlling oil consumption of the engine oil.
  • Another object of the present invention is to provide a piston ring-piston assembly applied to a reciprocating piston engine.
  • the number of air rings can be reduced to reduce the reciprocating inertial mass of the piston.
  • a combination of a reciprocating piston ring-piston assembly is provided.
  • Type gas ring the combined gas ring includes a groove ring, a cover ring, zero to several upper steel sheet rings, and a sealing sheet, wherein, in an assembled state with a piston and a cylinder liner, a cutout on the groove ring and The cut of the cover ring located above it is staggered in the circumferential direction, and the sealing sheet is installed at the cut on the groove ring so that the cut on the groove ring is blocked in the radial direction by the sealing sheet live.
  • a piston ring-piston assembly for a reciprocating piston engine wherein the piston is provided with a combined air ring according to the first aspect of the present invention.
  • the combined gas ring of the present invention does not have a free leaking channel, it has good air tightness, good performance of controlling oil, and many disadvantageous factors such as heating the piston caused by blow-by gas between the rings and damaging the oil film are eliminated together. Therefore, by adopting the combined air ring of the present invention, the overall performance of the engine can be comprehensively improved and improved, and a two-ring piston structure with one air ring and one oil ring can be realized.
  • FIG. 1 is a partial axial cross-sectional view showing a preferred embodiment of the combined air ring of the present invention
  • FIG. 2 is a cross-sectional view taken along line A-A of FIG. 1;
  • FIG. 3 is a partial enlarged view of part B in FIG. 2, showing the relative positional relationship between the cut of the groove ring, the protrusion of the sealing sheet and the groove of the cover ring;
  • FIG. 4 is a schematic diagram showing the crust shape of the sealing sheet
  • FIG. 5 is a plan view showing a structure of a cover ring groove of the present invention.
  • FIG. 6 is a plan view showing another structure of the cover ring groove of the present invention.
  • FIG. 7 is a half cross-sectional view of the first embodiment of the piston ring-piston assembly of the present invention.
  • FIG. 8 is a half cross-sectional view of a second embodiment of the piston ring-piston assembly of the present invention.
  • FIG. 9 is a half cross-sectional view of a third embodiment of the piston ring-piston assembly of the present invention.
  • Fig. 10 is a half cross-sectional view of a fourth embodiment of the piston ring-piston assembly of the present invention. Detailed description of the preferred embodiment
  • the combined air ring 20 of the present invention includes a grooved ring 1 having elasticity and all openings 11, a cover ring 2 with all openings 15, zero to several upper steel sheet rings 3, and One sealing sheet 7.
  • An axially curved notch 10 extending in the circumferential direction is formed on each of the two ends of the slot ring 1 on both sides of the cutout 11, and the sealing piece 7 is inserted into the arced groove formed by the two arced notches 10.
  • the sealing sheet 7 includes a main body portion 60 and a protrusion 6 located at one end of the main body portion. Face of cover ring 2 A groove 5 is provided on one side of the groove ring 1. As shown in FIG.
  • the groove 5 is provided at a position of the cover ring 2 substantially opposite to the cover ring cutout 15 and is used for receiving the protrusion 6 of the sealing sheet.
  • the groove 5 is sized to accommodate the entire protrusion 6.
  • the sealing piece 7 is inserted into the arc-shaped groove of the groove ring, and the axial height HI of the main part of the sealing piece is equal to or slightly lower than the axial thickness of the groove ring 1 so that The notch 11 of the groove ring is blocked from the radial direction over the entire axial height of 1.
  • the groove 5 is axially aligned with the protrusion 6 of the sealing sheet 7 so that the protrusion 6 of the sealing sheet 7 protruding above the upper surface of the groove ring can be inserted therein, so that the protrusion 6 and the groove 5 form a positioning device. It is used to restrict the rotation of the cover ring with respect to the groove ring to prevent the cutout 15 of the cover ring and the cutout 11 of the groove ring from axially aligning to cause leakage.
  • the axial height H2 of the protrusion 6 is greater than the maximum axial gap that may occur between the cover ring 2 and the groove ring 1 to ensure the limit effect of the protrusion 6 on the cover ring.
  • Figures 5 and 6 show two structural forms of the cover ring groove 5, respectively.
  • the groove 5 shown in Figure 5 is open to the inner diameter of the cover ring 2, while the groove 5 shown in Figure 6 is not open to the inner diameter.
  • the size of the cover ring groove 5 and the sealing sheet protrusion 6 relative to the groove ring cut 11 The circumferential position is set so that the cover ring groove 5 cannot communicate with the cutout 11 on the groove ring due to the limiting effect of the sealing piece protrusion 6 to avoid high-pressure gas passing through the groove 5 and the cutout portion located radially outward of the sealing piece leakage.
  • the combined air ring can have various combinations.
  • the cutout 11 of the groove ring and the cutout 15 of the cover ring located above it are staggered in the circumferential direction.
  • the sealing sheet 7 is inserted into the arc-shaped groove located at the cut of the groove ring and blocks the cut 11 of the groove ring from the radial direction.
  • the protrusion 6 of the sealing sheet 7 is inserted into the groove 5 matched with it Limiting the rotation of the cover ring relative to the groove ring is a basic feature of the combined air ring.
  • the sealing sheet 7 blocks the notch 11 of the groove ring 1 in the radial direction; the notch 11 of the groove ring and the notch 15 of the cover ring are located at different positions in the circumferential direction and are inserted through
  • the sealing piece protrusion 6 installed in the cover ring groove 5 locks the groove ring and the cover ring in this orientation.
  • the high-pressure gas 4 in the cylinder can neither leak downwards directly through the cutouts of any constituent ring, nor can it bypass the ringbacks of each constituent ring and pass through the notch 11 of the groove ring, the piston ring bank 13 and the cylinder wall 14 Leakage occurred in channel 12. It can be seen that the sealing principle of the combined air ring of the present invention to the cylinder has changed. It is no longer the traditional throttling working principle, but is based on the full sealing working principle.
  • the cover ring 2 may not be formed with a groove, and the sealing sheet does not have a protrusion 6 accordingly.
  • the top end of the sealing sheet 7 is approximately the same as the upper surface of the groove ring 1.
  • Qi Flat it is preferable to additionally provide a positioning member that prevents the groove ring and the cover ring from relatively rotating in the circumferential direction.
  • the shape of the notches formed at both ends of the notch of the groove ring is not limited to the above-mentioned arc shape, and other shapes of notches such as linear notches can also be used.
  • FIG. 7 is a half cross-sectional view of the first embodiment of the piston ring-piston assembly of the present invention.
  • the piston 8 is provided with only one combined air ring 20 of the present invention, which is mainly used for a two-stroke engine.
  • the piston 8 is provided with two piston rings, and the first ring groove arranged above is the combined air ring 20 of the present invention.
  • the second ring groove below is an oil ring 30, which is a typical two-ring piston structure.
  • FIG. 9 shows an embodiment of a piston ring-piston assembly having three piston rings according to the invention. The piston used in the piston ring-piston assembly of the present invention shown in FIG.
  • the piston ring-piston assembly of the example is the first ring located at the top is the combined air ring 20 of the present invention; the second ring located at the middle is the oil ring 30; and the third ring located at the bottom is the third ring
  • the piston ring is a conical ring 40 having a tapered outer peripheral surface.
  • oil return holes 50 and pressure relief holes 60 are respectively drilled at the bottom and the bottom of the ring groove where the cone surface ring is located toward the pressure bearing surface of the piston.
  • FIG. 10 shows another three-piston ring piston ring-piston assembly of the present invention, which is mainly used in a diesel engine. In the piston ring-piston assembly shown in FIG.
  • the first piston ring located at the top is a trapezoidal ring, a cymbal ring or an air ring 70 having another shape in section;
  • the second piston ring located in the middle is the original ring Invented combined air ring 20;
  • the third piston ring located at the bottom is the oil ring 30.
  • the air ring 70 located above the combined air ring of the present invention plays a shielding role, and adopts a trapezoidal or cymbal ring, which can solve the problem of the ring groove cementing snap ring.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)

Abstract

The invention discloses a combined gas ring for reciprocating piston ring-piston assembly. The combined gas ring includes elastic groove-ring (1), cap-ring (2), zero to several upper steel disc-ring (3) and enclosure piece (7). Under the assembled state of the gas ring with piston and cylinder, the cut-out (11) of groove-ring (1) and the cut-out (15) of cap-ring (2) stagger around their periphery. The enclosure piece (7) is located at the cut-out (11) of groove-ring (1), so that the cut-out (11) is enclosed by the enclosure piece. The invention also discloses a piston and piston ring assembly with the combined gas ring. Because there isn't leakage passage in the gas ring, gas-tight and oil control ability is good, the shortage of heating piston and destroying oil film is eliminated. Using the invention of combined gas ring can improve the engine performance and attain the piston structure with one gas ring and one oil ring.

Description

一种組合式气环及其活塞环-活塞总成  Combined air ring and piston ring-piston assembly
所属技术领域 Technical field
本发明涉及一种活塞环, 特别是一种组合式气环。本发明还涉及一种使 用该組合式气环的活塞环 -活塞总成, 它适用于各种往复活塞式发动机, 特 别是用于往复活塞式二、 四沖程发动机。 背景技术  The invention relates to a piston ring, in particular to a combined air ring. The invention also relates to a piston ring-piston assembly using the combined air ring, which is suitable for various reciprocating piston engines, especially for reciprocating piston two- or four-stroke engines. Background technique
传统的气环通常为单件气环, 气环切口处存在有直通式漏气通道。所以 现有气环对气缸的密封都是依据节流式工作原理, 2 - 3道气环沿轴向依次 装设在活塞上的各环槽中,且各气环的切口沿周向相互错开以构成"逑宫式" 封气结构。 这种结构存在环间窜气和由环间窜气造成的一系列弊病, 无法根 除上下活塞环对口时出现的短路漏气现象, 活塞环对活塞的扶正作用也因上 下环转动, 切口相互靠近而变差。  The traditional air ring is usually a one-piece air ring, and a straight-through air leakage channel exists at the cut of the air ring. Therefore, the existing air ring seals on the cylinder are based on the throttling principle. Two to three air rings are sequentially installed in the ring grooves on the piston in the axial direction, and the cuts of the air rings are staggered in the circumferential direction. In order to form the "逑 宫 式" gas-sealing structure. This structure has a series of disadvantages caused by inter-ring gas flow and inter-ring gas flow. It cannot eliminate the short-circuit gas leakage phenomenon when the upper and lower piston ring counterparts. The righting effect of the piston ring on the piston is also caused by the rotation of the upper and lower rings. And worse.
此外, 目前用于往复活塞式发动机中的现有活塞环-活塞总成, 都是采 用活塞上沿轴向依次装设数道气环的封气结构。 这种封气结抅至少需要两道 气环, 因此, 这种传统的活塞环-活塞总成不能通过減少气环数量来減少活 塞的往复惯性质量。 另一方面, 由于结构位置关系, 各个組成环的负荷差异 较大, 很难通过充分发挥各个組成环的工作性能来提高发动机的整机性能。 技术解决方案  In addition, the existing piston ring-piston assemblies currently used in reciprocating piston engines all adopt an air-sealing structure in which a plurality of air rings are sequentially arranged in the axial direction on the piston. At least two air rings are required for this type of gas sealing. Therefore, the conventional piston ring-piston assembly cannot reduce the reciprocating inertial mass of the piston by reducing the number of air rings. On the other hand, due to the structural position relationship, the load difference of each constituent ring is large, and it is difficult to improve the overall performance of the engine by giving full play to the working performance of each constituent ring. Technical solutions
本发明的一个目的是提供一种組合式气环, 能够防止直通式漏气 以达 到增强封气和控制机油油耗的技术效果。  An object of the present invention is to provide a combined air ring, which can prevent straight-through gas leakage to achieve the technical effects of enhancing gas sealing and controlling oil consumption of the engine oil.
本发明另一目的是提供一种应用于往复活塞式发动机的活塞环-活塞 总成, 它在实现良好密封效果的基础上, 可以通过減少气环数量来达到減轻 活塞的往复惯性质量。  Another object of the present invention is to provide a piston ring-piston assembly applied to a reciprocating piston engine. On the basis of achieving a good sealing effect, the number of air rings can be reduced to reduce the reciprocating inertial mass of the piston.
根据本发明第一方面, 提供了一种用于往复式活塞环-活塞总成的組合 式气环, 所述組合式气环包括槽环、 盖环、 零至数个上钢片环以及封口片, 其中, 在与活塞、 缸套的裝配状态下, 所述槽环上的切口与位于其上方的所 述盖环的切口沿周向错开, 所述封口片装设在所述槽环上的切口处使得所述 槽环上的切口借助于所述封口片在径向上被封堵住。 According to a first aspect of the present invention, a combination of a reciprocating piston ring-piston assembly is provided. Type gas ring, the combined gas ring includes a groove ring, a cover ring, zero to several upper steel sheet rings, and a sealing sheet, wherein, in an assembled state with a piston and a cylinder liner, a cutout on the groove ring and The cut of the cover ring located above it is staggered in the circumferential direction, and the sealing sheet is installed at the cut on the groove ring so that the cut on the groove ring is blocked in the radial direction by the sealing sheet live.
根据本发明第二方面, 提供了一种用于往复活塞式发动机的活塞环-活 塞总成, 其中, 所述活塞上装设有根据本发明第一方面的组合式气环。  According to a second aspect of the present invention, a piston ring-piston assembly for a reciprocating piston engine is provided, wherein the piston is provided with a combined air ring according to the first aspect of the present invention.
由于本发明的组合式气环不存在自由泄漏通道, 因此气密性好, 控制机 油的性能佳, 由环间窜气造成的加热活塞、 破坏油膜等诸多不利因素一并排 除。 所以, 采用本发明的组合式气环, 能够全面改善和提高发动机的整机性 能, 能够实现一道气环加一道油环的二环活塞结构。 附图的简要说明  Since the combined gas ring of the present invention does not have a free leaking channel, it has good air tightness, good performance of controlling oil, and many disadvantageous factors such as heating the piston caused by blow-by gas between the rings and damaging the oil film are eliminated together. Therefore, by adopting the combined air ring of the present invention, the overall performance of the engine can be comprehensively improved and improved, and a two-ring piston structure with one air ring and one oil ring can be realized. Brief description of the drawings
下面结合附图和实施例对本发明作进一步详细的说明, 其中  The present invention is further described in detail below with reference to the accompanying drawings and embodiments.
图 1是一局部轴向剖面视图, 表明本发明組合式气环的一优选实施例; 图 2是沿图 1的 A - A线所取的剖面视图;  FIG. 1 is a partial axial cross-sectional view showing a preferred embodiment of the combined air ring of the present invention; FIG. 2 is a cross-sectional view taken along line A-A of FIG. 1;
图 3是图 2中部分 B的局部放大视图, 表明槽环的切口、封口片凸起与 盖环凹槽之间的相对位置关系;  FIG. 3 is a partial enlarged view of part B in FIG. 2, showing the relative positional relationship between the cut of the groove ring, the protrusion of the sealing sheet and the groove of the cover ring;
图 4是表明封口片结抅形状的示意图;  FIG. 4 is a schematic diagram showing the crust shape of the sealing sheet;
图 5是一平面視图, 表明本发明盖环凹槽的一种结构;  5 is a plan view showing a structure of a cover ring groove of the present invention;
图 6是一平面视图, 表明本发明盖环凹槽的另一种结构;  6 is a plan view showing another structure of the cover ring groove of the present invention;
图 7是本发明活塞环-活塞总成的第一实施例的半剖视图;  7 is a half cross-sectional view of the first embodiment of the piston ring-piston assembly of the present invention;
图 8是本发明活塞环-活塞总成的第二实施例的半剖视图;  8 is a half cross-sectional view of a second embodiment of the piston ring-piston assembly of the present invention;
图 9是本发明活塞环-活塞总成的第三实施例的半剖视图;  9 is a half cross-sectional view of a third embodiment of the piston ring-piston assembly of the present invention;
图 10是本发明活塞环-活塞总成的第四实施例的半剖视图。 优选实施例的详细说明  Fig. 10 is a half cross-sectional view of a fourth embodiment of the piston ring-piston assembly of the present invention. Detailed description of the preferred embodiment
如图 1 、 2和 3所示, 本发明的组合式气环 20 包括具有弹性和一切口 11的槽环 1 , 带有一切口 15的盖环 2, 零至数个上钢片环 3 以及一个封口 片 7 。槽环 1的位于切口 11 两侧的两端各形成有一沿周向延伸的轴向弧形槽 口 10,封口片 7插装于上述两个弧形槽口 10形成的弧形槽中。如图 4所示, 封口片 7包括一主体部分 60以及位于主体部分一端的凸起 6 。盖环 2的面向 槽环 1的一侧有一凹槽 5, 如图 2所示, 凹槽 5设置在盖环 2的大致与盖环 切口 15径向相对的位置处, 并用于容放封口片的凸起 6, 凹槽 5的大小能包 容整个凸起 6 。在图 1所示的组装状态下,封口片 7插装于槽环的弧形槽中, 封口片主体部分的轴向高度 HI等于或略低于槽环 1 的轴向厚度, 以便在槽 环 1的整个轴向高度上从径向封堵住槽环的切口 11 。凹槽 5沿轴向对中于封 口片 7的凸起 6, 使得封口片 7的突出于槽环上表面上方的凸起 6可以插入 其中, 从而凸起 6和凹槽 5形成一定位装置, 用以限制盖环相对于槽环的转 动以避免盖环的切口 15与槽环的切口 11轴向对准而发生泄漏。 优选地, 凸 起 6的轴向高度 H2大于盖环 2与槽环 1之间可能出现的最大轴向间隙, 以 确保凸起 6对于盖环的限位作用。 As shown in FIGS. 1, 2 and 3, the combined air ring 20 of the present invention includes a grooved ring 1 having elasticity and all openings 11, a cover ring 2 with all openings 15, zero to several upper steel sheet rings 3, and One sealing sheet 7. An axially curved notch 10 extending in the circumferential direction is formed on each of the two ends of the slot ring 1 on both sides of the cutout 11, and the sealing piece 7 is inserted into the arced groove formed by the two arced notches 10. As shown in FIG. 4, the sealing sheet 7 includes a main body portion 60 and a protrusion 6 located at one end of the main body portion. Face of cover ring 2 A groove 5 is provided on one side of the groove ring 1. As shown in FIG. 2, the groove 5 is provided at a position of the cover ring 2 substantially opposite to the cover ring cutout 15 and is used for receiving the protrusion 6 of the sealing sheet. The groove 5 is sized to accommodate the entire protrusion 6. In the assembled state shown in FIG. 1, the sealing piece 7 is inserted into the arc-shaped groove of the groove ring, and the axial height HI of the main part of the sealing piece is equal to or slightly lower than the axial thickness of the groove ring 1 so that The notch 11 of the groove ring is blocked from the radial direction over the entire axial height of 1. The groove 5 is axially aligned with the protrusion 6 of the sealing sheet 7 so that the protrusion 6 of the sealing sheet 7 protruding above the upper surface of the groove ring can be inserted therein, so that the protrusion 6 and the groove 5 form a positioning device. It is used to restrict the rotation of the cover ring with respect to the groove ring to prevent the cutout 15 of the cover ring and the cutout 11 of the groove ring from axially aligning to cause leakage. Preferably, the axial height H2 of the protrusion 6 is greater than the maximum axial gap that may occur between the cover ring 2 and the groove ring 1 to ensure the limit effect of the protrusion 6 on the cover ring.
图 5和 6分别示出了盖环凹槽 5的两种结构形式, 图 5所示的凹槽 5与 盖环 2的内径开通, 而图 6所示的凹槽 5不与内径开通。 但不论凹槽 5与盖 环 2内径开通与否, 在本发明組合式气环与活塞的装配状态下, 所述盖环凹 槽 5的尺寸和封口片凸起 6相对于槽环切口 11的周向位置如此设定使得盖环 凹槽 5由于封口片凸起 6的限位作用不能与槽环上的切口 11连通,以避免高 压燃气经由凹槽 5 、 位于封口片径向外侧的切口部分泄漏。  Figures 5 and 6 show two structural forms of the cover ring groove 5, respectively. The groove 5 shown in Figure 5 is open to the inner diameter of the cover ring 2, while the groove 5 shown in Figure 6 is not open to the inner diameter. Regardless of whether the inner diameter of the groove 5 and the cover ring 2 is open or not, in the assembled state of the combined air ring and piston of the present invention, the size of the cover ring groove 5 and the sealing sheet protrusion 6 relative to the groove ring cut 11 The circumferential position is set so that the cover ring groove 5 cannot communicate with the cutout 11 on the groove ring due to the limiting effect of the sealing piece protrusion 6 to avoid high-pressure gas passing through the groove 5 and the cutout portion located radially outward of the sealing piece leakage.
由于本发明的组合式气环各组成环的数量可以不同, 且各组成环可以具 有不同的断面形状, 因此组合式气环可以有多种組合形式。 但是, 不论其组 合形式如何, 组合式气环在活塞环 -活塞总成装设于气缸套 9中的装配状态 下, 槽环的切口 11与位于其上方的盖环的切口 15沿周向错开, 封口片 7插 装在位于槽环切口处的弧形槽内从径向封堵住槽环的切口 11,封口片 7的凸 起 6插入盖环 2上与之配对的凹槽 5中以限制盖环相对于槽环的转动, 这是 组合式气环的基本特征。 在組装状态下, 如图 2所示, 封口片 7在径向上封 堵住槽环 1的切口 11 ;槽环的切口 11和盖环的切口 15沿周向位于不同的方 位, 并通过插装于盖环凹槽 5中的封口片凸起 6将槽环和盖环锁定于这一方 位。 因此气缸内的高压气体 4既不能通过任一组成环的切口直接向下泄漏, 也不能绕过各組成环的环背而经由槽环的切口 11 、活塞环岸 13与气缸壁 14 之间形成的通道 12发生泄漏。由此可见,本发明的組合式气环对气缸的密封 原理发生了变化, 已不是传统的节流工作原理, 而是依据全密封工作原理。  Since the number of each constituent ring of the combined air ring of the present invention can be different, and each of the constituent rings can have different cross-sectional shapes, the combined air ring can have various combinations. However, regardless of the combination form, in the assembled state of the combined air ring in the piston ring-piston assembly installed in the cylinder liner 9, the cutout 11 of the groove ring and the cutout 15 of the cover ring located above it are staggered in the circumferential direction. The sealing sheet 7 is inserted into the arc-shaped groove located at the cut of the groove ring and blocks the cut 11 of the groove ring from the radial direction. The protrusion 6 of the sealing sheet 7 is inserted into the groove 5 matched with it Limiting the rotation of the cover ring relative to the groove ring is a basic feature of the combined air ring. In the assembled state, as shown in FIG. 2, the sealing sheet 7 blocks the notch 11 of the groove ring 1 in the radial direction; the notch 11 of the groove ring and the notch 15 of the cover ring are located at different positions in the circumferential direction and are inserted through The sealing piece protrusion 6 installed in the cover ring groove 5 locks the groove ring and the cover ring in this orientation. Therefore, the high-pressure gas 4 in the cylinder can neither leak downwards directly through the cutouts of any constituent ring, nor can it bypass the ringbacks of each constituent ring and pass through the notch 11 of the groove ring, the piston ring bank 13 and the cylinder wall 14 Leakage occurred in channel 12. It can be seen that the sealing principle of the combined air ring of the present invention to the cylinder has changed. It is no longer the traditional throttling working principle, but is based on the full sealing working principle.
作为上述实施例的一种改型, 盖环 2上可以不形成凹槽, 相应地封口片 也不带有凸起 6, 在组装状态下, 封口片 7的顶端与槽环 1的上表面大致齐 平。 采用这种结构, 优选地, 另外设置一防止槽环和盖环沿周向相对转动的 定位件。 另外, 于槽环切口两端形成的的槽口形状也不局限于上述的弧形, 其他形状的槽口例如直线形槽口也可采用。 As a modification of the above embodiment, the cover ring 2 may not be formed with a groove, and the sealing sheet does not have a protrusion 6 accordingly. In the assembled state, the top end of the sealing sheet 7 is approximately the same as the upper surface of the groove ring 1. Qi Flat. With this structure, it is preferable to additionally provide a positioning member that prevents the groove ring and the cover ring from relatively rotating in the circumferential direction. In addition, the shape of the notches formed at both ends of the notch of the groove ring is not limited to the above-mentioned arc shape, and other shapes of notches such as linear notches can also be used.
下面结合图 7 - 10说明本发明的活塞'环-活塞总成的各优选实施例。 图 7是本发明活塞环-活塞总成的第一实施例的半剖视图。 如图 7所示, 活 塞 8上只配置一个本发明的組合式气环 20, 主要用于二沖程发动机。在图 8 所示的活塞环 -活塞总成的实施例中, 活塞 8上装有两个活塞环, 配装在上 方第一道环槽中的是本发明的組合式气环 20,配装在下方第二道环槽中的是 一油环 30, 是典型的二环活塞结构。在传统的具有三个活塞环的活塞环 -活 塞总成中, 位于上方的两个活塞环是气环, 而位于最下方的活塞环是油环。 图 9示出本发明的具有三个活塞环的活塞环 -活塞总成的实施例。 图 9所示 本发明活塞环 -活塞总成所使用的活塞与传统的三活塞环活塞环 -活塞总成 所用的活塞相类似, 只是各活塞环的配置有所不同: 在本发明第三实施例的 活塞环-活塞总成中, 位于最上方的第一遒活塞环是本发明的組合式气环 20 ; 位于中间的第二道活塞环为油环 30 ; 而位于最下方的第三遒活塞环为 外周面为锥面的锥靣环 40 。为便于回油,在这道锥面环所在的环槽的底部和 下方朝向活塞承压面方向分别钻有回油孔 50和泄压孔 60 。 采用这种结构, 由于提高了油环 30的工作温度, 加之第三道活塞环 40有粗括机油的作用, 所以可以在保持原有压縮高度基本不变的情况下, 提高刮油效果, 減少机油 油耗。 对于本发明第三实施例的活塞环-活塞总成, 由于其中的活塞在结构 上与现有活塞类似, 因此本发明第三实施例的活塞环 -活塞总成结构可直接 应用于现有发动机, 而无需对现有活塞结构作大的改进。图 10示出本发明另 一种三活塞环活塞环 -活塞总成,主要用于柴油发动机。在图 10所示的活塞 环-活塞总成中, 位于最上方的第一道活塞环是梯形环、 禊形环或剖面呈其 他形状的气环 70 ; 位于中间的第二道活塞环是本发明的組合式气环 20 ; 位 于最下面的第三道活塞环是油环 30 。在这种结构中,位于本发明組合式气环 上方的气环 70起屏蔽作用,且采用梯形或禊形环, 可一并解决环槽结胶卡环 问题。由于第一遒气环 70分扭了部分燃气压力,处于其下面的本发明組合式 气环承受的燃气压力相对減小, 所以这种结构适用于压力较高的柴油机, 特 别是增压柴油机。 由本发明上述四个实施例的活塞环-活塞总成可以看出, 其基本特征是其上都设置有本发明的组合式气环。 图 7和 8所示的单活塞环 和双活塞环活塞结构, 其封气控油性能远比采用传统的单件气环的活塞结构 好。 图 9和 10所示的本发明三环活塞结构, 可以直接应用于现有活塞。 The following describes preferred embodiments of the piston'ring-piston assembly of the present invention with reference to FIGS. 7-10. FIG. 7 is a half cross-sectional view of the first embodiment of the piston ring-piston assembly of the present invention. As shown in FIG. 7, the piston 8 is provided with only one combined air ring 20 of the present invention, which is mainly used for a two-stroke engine. In the embodiment of the piston ring-piston assembly shown in FIG. 8, the piston 8 is provided with two piston rings, and the first ring groove arranged above is the combined air ring 20 of the present invention. In the second ring groove below is an oil ring 30, which is a typical two-ring piston structure. In a conventional piston ring-piston assembly with three piston rings, the upper two piston rings are air rings and the lowermost piston ring is an oil ring. FIG. 9 shows an embodiment of a piston ring-piston assembly having three piston rings according to the invention. The piston used in the piston ring-piston assembly of the present invention shown in FIG. 9 is similar to the piston used in the conventional three-piston ring piston ring-piston assembly, except that the configuration of each piston ring is different: In the third embodiment of the present invention In the piston ring-piston assembly of the example, the first ring located at the top is the combined air ring 20 of the present invention; the second ring located at the middle is the oil ring 30; and the third ring located at the bottom is the third ring The piston ring is a conical ring 40 having a tapered outer peripheral surface. In order to facilitate oil return, oil return holes 50 and pressure relief holes 60 are respectively drilled at the bottom and the bottom of the ring groove where the cone surface ring is located toward the pressure bearing surface of the piston. With this structure, because the operating temperature of the oil ring 30 is increased, and the third piston ring 40 has the function of roughing the oil, the oil scraping effect can be improved while the original compression height is basically unchanged. Reduce oil consumption. For the piston ring-piston assembly of the third embodiment of the present invention, since the piston therein is similar in structure to the existing piston, the piston ring-piston assembly structure of the third embodiment of the present invention can be directly applied to the existing engine Without having to make major improvements to the existing piston structure. FIG. 10 shows another three-piston ring piston ring-piston assembly of the present invention, which is mainly used in a diesel engine. In the piston ring-piston assembly shown in FIG. 10, the first piston ring located at the top is a trapezoidal ring, a cymbal ring or an air ring 70 having another shape in section; the second piston ring located in the middle is the original ring Invented combined air ring 20; the third piston ring located at the bottom is the oil ring 30. In this structure, the air ring 70 located above the combined air ring of the present invention plays a shielding role, and adopts a trapezoidal or cymbal ring, which can solve the problem of the ring groove cementing snap ring. Since the first radon gas ring twists a part of the gas pressure by 70 minutes, the gas pressure of the combined gas ring of the present invention below it is relatively reduced, so this structure is suitable for a diesel engine with a higher pressure, especially a supercharged diesel engine. As can be seen from the piston ring-piston assembly of the above-mentioned four embodiments of the present invention, its basic feature is that it is provided with the combined air ring of the present invention. Single piston ring shown in Figures 7 and 8 And double piston ring piston structure, its gas sealing and oil control performance is much better than the traditional one-piece air ring piston structure. The three-ring piston structure of the present invention shown in FIGS. 9 and 10 can be directly applied to an existing piston.
上面对本发明优选实施例进行了说明。 然而, 业内人士应当理解, 上述 实施例是例示性的而非限制性的, 在不背离所附杈利要求限定的本发明精神 和范围的情况下可以对本发明作出各种改进。  The preferred embodiments of the present invention have been described above. However, those skilled in the art should understand that the foregoing embodiments are illustrative and not restrictive, and various improvements can be made to the present invention without departing from the spirit and scope of the present invention as defined by the appended claims.

Claims

杈利要求书 Request for Profit
1. 一种用于往复式活塞环 -活塞总成的组合式气环,所述组合式气环包 括具有弹性的槽环 (1)、 盖环 (2)、 零至数个上钢片环 (3)以及封口片(7), 其中, 所述組合式气环在与活塞 (8)、缸套 (9)的装配状态下,所述槽环 (1)上的切口(11) 与位于其上方的所述盖环 (2)的切口(15)沿周向错开, 所述封口片(7)装设在所 述槽环 (1)上的切口(11)处,使得所述槽环 (1)上的切口(11)借助于所述封口片(7) 在径向上被封堵住。 1. A combined air ring for a reciprocating piston ring-piston assembly, the combined air ring comprising an elastic groove ring (1), a cover ring (2), and zero to several upper steel plate rings (3) and a sealing sheet (7), wherein, in the assembled state of the combined air ring with the piston (8) and the cylinder liner (9), the cutout (11) on the groove ring (1) and the The cutouts (15) of the cover ring (2) above it are staggered in the circumferential direction, and the sealing piece (7) is installed at the cutouts (11) on the grooved ring (1) so that the grooved ring The cut (11) in (1) is blocked in the radial direction by means of the sealing sheet (7).
2. 根据杈利要求 1所述的組合式气环, 其中, 还设置有一限制槽环和盖 环沿周向相对转动的定位装置, 以确保盖环切口(15)和槽环切口(11)不会对 2. The combined air ring according to claim 1, further comprising a positioning device for restricting the relative rotation of the groove ring and the cover ring in the circumferential direction to ensure the cover ring cutout (15) and the groove ring cutout (11) Not right
V。 V.
3. 根据杈利要求 1所述的組合式气环,其中,所述槽环 (1)的位于切口 O ) 两侧的两端各有一沿周向延伸的轴向弧形槽口(10), 所述封口片(7)插装在两 弧形槽口(10)形成的弧形槽内, 所述封口片的轴向高度 (HI)等于或略低于槽 环 (1)的轴向高度。  3. The combined air ring according to claim 1, wherein two ends of the groove ring (1) located on both sides of the cutout O) each have an axial arc-shaped groove (10) extending in a circumferential direction. The sealing piece (7) is inserted into an arc groove formed by two curved notches (10), and the axial height (HI) of the sealing piece is equal to or slightly lower than the axial direction of the groove ring (1). height.
4. 根据杈利要求 3 所述的组合式气环, 其中, 所述封口片(7)在其一周 向端部有一朝向所述盖环伸出的并高于槽环的轴向高度的凸起 (6), 而所述盖 环 (2)在面向所述槽环 (1)的一侧上形成有一与所述封口片凸起 (6)配对的能包 容整个凸起的凹槽 (5), 在组装状态下, 所述盖环凹槽 (5)与配装在所述槽环弧 形槽中的封口片凸起 (6)轴向对中,所述封口片(7)的凸起 (6)插入所述盖环凹槽 (5), 用以限制盖环 (2)相对于槽环 (1)的转动。  4. The combined air ring according to claim 3, wherein the sealing piece (7) has a protrusion protruding toward the cover ring at one end of the sealing piece and higher than the axial height of the groove ring. (6), and the cover ring (2) is formed on a side facing the groove ring (1) with a groove (5) capable of accommodating the entire protrusion paired with the sealing piece protrusion (6) ), In the assembled state, the cover ring groove (5) is axially centered with the sealing piece protrusion (6) fitted in the grooved ring arc groove, and the convexity of the sealing piece (7) The lifting ring (6) is inserted into the cover ring groove (5) to limit the rotation of the cover ring (2) relative to the groove ring (1).
5. 根据杈利要求 4 所述的組合式气环, 其中, 所述盖环凹槽 (5)与所述 盖环上的切口(15)处在基本上径向相对的位置处。  5. The combined air ring according to claim 4, wherein the cover ring groove (5) and the cutout (15) on the cover ring are located at substantially opposite radial positions.
6. 根据杈利要求 4 所述的組合式气环, 其中, 所述盖环上的凹槽 (5)既 可以与所述盖环的内径开通, 也可以不与所述盖环的内径开通。  6. The combined air ring according to claim 4, wherein the groove (5) on the cover ring can be opened to the inside diameter of the cover ring or not to be opened to the inside diameter of the cover ring. .
7. 根据杈利要求 4所述的組合式气环, 其中,所述封口片凸起的轴向高 度 (H2)大于盖环与槽环之间可能出现的最大轴向间隙。  7. The combined air ring according to claim 4, wherein the axial height (H2) of the sealing piece protrusion is greater than the maximum axial gap that may occur between the cover ring and the groove ring.
8. 根据杈利要求 4 所述的组合式气环, 其中, 所述盖环凹槽 (5)的尺寸 和封口片凸起 (6)相对于槽环切口(11)的周向位置如此设定使得盖环凹槽 (5)由 于封口片凸起的限位作用不能与槽环上的切口(11)连通。  8. The combined air ring according to claim 4, wherein the size of the cover ring groove (5) and the circumferential position of the sealing sheet protrusion (6) relative to the groove ring cut (11) are set as such It is determined that the cover ring groove (5) cannot communicate with the cutout (11) on the groove ring due to the limiting effect of the sealing sheet protrusion.
9. 一种用于往复活塞式发动机的活塞环 -活塞总成, 其中, 所述活塞上 装设有杈利要求 1 - 8中任一项所述的組合式气环 (20)。 9. A piston ring-piston assembly for a reciprocating piston engine, wherein the piston is The combination air ring (20) according to any one of claims 1 to 8 is installed.
10. 根据杈利要求 9所述的活塞环 -活塞总成, 其中, 所述活塞环-活 塞总成上只有一个组合式气环 (20)。  10. The piston ring-piston assembly according to claim 9, wherein there is only one combined air ring (20) on the piston ring-piston assembly.
11. 根据杈利要求 9所述的活塞环 -活塞总成, 其中, 所述活塞环-活 塞总成为具有两个活塞环的活塞环 -活塞总成, 活塞上的第一道环槽配置所 述组合式气环 (20) , 第二道环槽配置一油环 (30)。  11. The piston ring-piston assembly according to claim 9, wherein the piston ring-piston is a piston ring-piston assembly having two piston rings, and a first ring groove is arranged on the piston. The combined air ring (20) is described, and the second ring groove is provided with an oil ring (30).
12. 根据杈利要求 9所述的活塞环 -活塞总成, 其中, 所述活塞环-活 塞总成为具有三个活塞环的活塞环 -活塞总成, 活塞上的第一道环槽配置所 述组合式气环 (20), 第二道环槽配置一油环 (30), 而第三道环槽配置外周面是 锥面的锥面环 (40)。  12. The piston ring-piston assembly according to claim 9, wherein the piston ring-piston is a piston ring-piston assembly having three piston rings, and a first ring groove is arranged on the piston. The combined air ring (20) is described. The second ring groove is provided with an oil ring (30), and the third ring groove is provided with a tapered surface ring (40) whose outer peripheral surface is a tapered surface.
13. 根据杈利要求 12所述的所述活塞环-活塞总成, 其中,在所述第三 道环槽的底部和该环槽下方朝向活塞承压面方向分别钻有回油孔 (50)和泻压 礼 (60)。  13. The piston ring-piston assembly according to claim 12, wherein, at the bottom of the third ring groove and below the ring groove, oil return holes (50 ) And Diarrhea (60).
14. 根据杈利要求 9所述的活塞环 -活塞总成, 其中, 所述活塞环-活 塞总成为具有三个活塞环的活塞环 -活塞总成, 活塞上第一道环槽配置一梯 形、 禊形或其他截面形状的气环 (70), 第二道环槽配置所述組合式气环 (20), 而第三道环槽配置一油环 (30)。  14. The piston ring-piston assembly according to claim 9, wherein the piston ring-piston assembly has a piston ring-piston assembly with three piston rings, and a trapezoid is arranged on the first ring groove of the piston. The air ring (70) of the U-shape or the other shape is configured with the combined air ring (20) in the second ring groove and an oil ring (30) in the third ring groove.
PCT/CN2001/000542 2000-09-20 2001-04-03 A combined gas ring and its piston ring-piston assembly WO2002025090A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2001263730A AU2001263730A1 (en) 2000-09-20 2001-04-03 A combined gas ring and its piston ring-piston assembly

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
CN00126547.4 2000-09-20
CN 00126547 CN1343837A (en) 2000-09-20 2000-09-20 Combined O-shaped pressure ring
CN00263881.9 2000-11-28
CN00263881 2000-11-28

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102017118773A1 (en) * 2017-08-17 2019-02-21 Federal-Mogul Burscheid Gmbh Piston ring set, piston and internal combustion engine

Citations (8)

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Publication number Priority date Publication date Assignee Title
CN2131993Y (en) * 1991-06-23 1993-05-05 唐为民 Combined z-type airtight ring
CN2160763Y (en) * 1993-06-23 1994-04-06 谭军 Combined piston ring
CN2171684Y (en) * 1993-05-31 1994-07-13 郑昭 Piston with compound ring
DE4327621A1 (en) * 1993-08-17 1995-02-23 Mahle Gmbh Piston ring arrangement for pistons of internal combustion engines
WO1997011295A1 (en) * 1995-09-22 1997-03-27 Man B & W Diesel A/S A piston ring for a piston in an internal combustion engine
CN2267330Y (en) * 1996-05-31 1997-11-12 常柴股份有限公司 Piece insertion type piston ring
WO1998041749A1 (en) * 1997-03-14 1998-09-24 Man B & W Diesel A/S A piston for a two-stroke crosshead engine of the diesel type
CN2381795Y (en) * 1999-04-20 2000-06-07 唐为民 Crossed assembling piston ring

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2131993Y (en) * 1991-06-23 1993-05-05 唐为民 Combined z-type airtight ring
CN2171684Y (en) * 1993-05-31 1994-07-13 郑昭 Piston with compound ring
CN2160763Y (en) * 1993-06-23 1994-04-06 谭军 Combined piston ring
DE4327621A1 (en) * 1993-08-17 1995-02-23 Mahle Gmbh Piston ring arrangement for pistons of internal combustion engines
WO1997011295A1 (en) * 1995-09-22 1997-03-27 Man B & W Diesel A/S A piston ring for a piston in an internal combustion engine
CN2267330Y (en) * 1996-05-31 1997-11-12 常柴股份有限公司 Piece insertion type piston ring
WO1998041749A1 (en) * 1997-03-14 1998-09-24 Man B & W Diesel A/S A piston for a two-stroke crosshead engine of the diesel type
CN2381795Y (en) * 1999-04-20 2000-06-07 唐为民 Crossed assembling piston ring

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102017118773A1 (en) * 2017-08-17 2019-02-21 Federal-Mogul Burscheid Gmbh Piston ring set, piston and internal combustion engine

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