CN204344302U - A kind of engine piston assembly - Google Patents
A kind of engine piston assembly Download PDFInfo
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- CN204344302U CN204344302U CN201420780284.6U CN201420780284U CN204344302U CN 204344302 U CN204344302 U CN 204344302U CN 201420780284 U CN201420780284 U CN 201420780284U CN 204344302 U CN204344302 U CN 204344302U
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- annular groove
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- 230000006835 compression Effects 0.000 claims description 201
- 238000007906 compression Methods 0.000 claims description 201
- 239000007789 gas Substances 0.000 abstract description 33
- 238000000034 method Methods 0.000 abstract description 15
- 229930195733 hydrocarbon Natural products 0.000 abstract description 14
- 150000002430 hydrocarbons Chemical class 0.000 abstract description 14
- 239000004215 Carbon black (E152) Substances 0.000 abstract description 13
- 230000015572 biosynthetic process Effects 0.000 abstract description 7
- 239000000567 combustion gas Substances 0.000 abstract description 7
- 230000000694 effects Effects 0.000 abstract description 6
- 230000021715 photosynthesis, light harvesting Effects 0.000 abstract description 6
- 239000003921 oil Substances 0.000 description 35
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 4
- 229910052799 carbon Inorganic materials 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- 239000010721 machine oil Substances 0.000 description 4
- 239000000446 fuel Substances 0.000 description 3
- 230000008602 contraction Effects 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 239000002737 fuel gas Substances 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
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- Pistons, Piston Rings, And Cylinders (AREA)
Abstract
The utility model discloses a kind of engine piston assembly, be provided with piston structure and the Piston volume tube matched with it and formation one had at least one or more than one ring-type sudden expansion expansion chamber together with the inwall of cylinder body and the clearance passage with described multistage throttle expansion function, this clearance passage compresses at engine mixed gas, enough large flow resistance and energy dissipation effect can be produced in ignition and expansion work process, the combustion gas of high pressure mixing gas and High Temperature High Pressure can be effectively stoped to be leaked from engine chamber and cylinder to the gas blowby of crankcase, in exhaust process, then can guarantee to only have a small amount of hydrocarbon emission thing can overflow from clearance, this engine piston structure assembly significantly can reduce the hydrocarbon emission in the carbon-deposits the cylinder of motor and exhaust emissions effectively, significantly can promote the efficiency gas of motor and the overall performance of motor again, be applicable to applying.
Description
Technical field
The utility model relates to the field of engine fittings, particularly relates to a kind of engine piston assembly.
Background technique
The emission control of motor requires more and more tighter, piston assembly comprises piston only and respective pistons ring group, as one of the crucial sub-component of motor, the matched design between its general structure design and component has decisive influence to the size of hydrocarbon emission in exhaust emissions.First, in engine exhaust process, the hydrocarbon that part to be ensconced between piston and rings and cylinder wall in gap (mainly the above clearance of the first compression ring and part first compression ring and clearance between the second compression ring) can be overflowed outside exhaust valve together with gas of combustion, they are two years old, expand in descending process in engine mixed gas compression stroke and ignition, partial high pressure mixed gas and high-temperature high-pressure fuel gas enter in engine crankcase by gap between piston and rings and cylinder block under huge differential pressure action, the gas blowby forming mixed gas and combustion gas leaks, described gas blowby leaks and the machine oil oil temperature oil pressure in crankcase usually also can be caused to raise and forming machine oil vapor, rebreather of engine is entered together with combustion gas and fuel mixture gas blowby, thus part machine oil steam can enter firing chamber and participate in burning and form unburned carbon hydrogen effulent with outside gas of combustion discharge exhaust valve, moreover the sustained combustion of machine oil can form carbon distribution at piston head and combustor surface, and the formation of carbon distribution can become the hotbed of unburned hydrocarbons, and the hydrocarbon of ensconcing in carbon distribution can be overflowed outside exhaust valve with gas of combustion in exhaust process.Obviously, the size of gas fuel mixing gas blowby leakage rate has very important direct impact to hydrocarbon emission size.
Available engine piston assembly such as to adopt mostly at the piston structure of ring bank diameter and equivalent gullet depth structure, correspondingly the first compression ring and the second compression ring such as are also usually at the radial thickness structure, the clearance passage that itself and respective pistons ring group and cylinder wall are formed cannot produce enough large resistance and energy dissipation effect owing to not having obvious multistage sudden contraction sudden expansion characteristic, thus be difficult to stop a large amount of gas blowbies of high pressure fuel mixed gas and high-temperature high-pressure fuel gas to leak, even if people adopt the way majority also limited use reducing clearance.
Model utility content
The technical problem that the utility model mainly solves is to provide a kind of engine piston assembly, be provided with piston structure and the Piston volume tube matched with it and formation one had at least one or more than one ring-type sudden expansion expansion chamber together with the inwall of cylinder body and the clearance passage with described multistage throttle expansion function, this clearance passage compresses at engine mixed gas, enough large flow resistance and energy dissipation effect can be produced in ignition and expansion work process, the combustion gas of high pressure mixing gas and High Temperature High Pressure can be effectively stoped to be leaked from engine chamber and cylinder to the gas blowby of crankcase, in exhaust process, then can guarantee to only have a small amount of hydrocarbon emission thing can overflow from clearance, this engine piston structure assembly significantly can reduce the hydrocarbon emission in the carbon-deposits the cylinder of motor and exhaust emissions effectively, significantly can promote the efficiency gas of motor and the overall performance of motor again, be applicable to applying.
For solving the problems of the technologies described above, the technological scheme that the utility model adopts is: provide a kind of engine piston assembly, comprise cylinder body, piston only, first compression ring, second compression ring and oil ring assembly, the first described compression ring, second compression ring and oil ring assembly contact with the inwall of cylinder body respectively, the excircle of described piston only is provided with top land from top to bottom successively, first compression annular groove, second ring bank, second compression annular groove, 3rd ring bank and oil ring groove, it is equivalent gullet depth or non-equivalent gullet depth structure that described first compression annular groove and second compresses annular groove, the ratio that first groove depth and second compressing annular groove compresses the groove depth of annular groove is less than or equal to 1.0, described first compression ring and the second compression ring for etc. radial thickness or the radial thickness structure such as non-, first compression piston ring radial thickness is less than or equal to 1.0 with the ratio of the second compression piston ring radial thickness, the ring-type sudden expansion expansion chamber of one or more than one is provided with between the inwall of described second ring bank and cylinder body, described one or more than one ring-type sudden expansion expansion chamber by the ring-type sudden expansion expansion slot of one or more than one on the excircle being located at described second ring bank and cylinder body inwall between region form.
In the utility model preferred embodiment, between the inwall of described 3rd ring bank and cylinder body, be also provided with the ring-type sudden expansion expansion chamber of one or more than one, described one or more than one ring-type sudden expansion expansion chamber by the ring-type sudden expansion expansion slot of one or more than one on the excircle being located at described 3rd ring bank and cylinder body inwall between region form.
For solving the problems of the technologies described above, another technological scheme that the utility model adopts is: provide a kind of engine piston assembly, comprise cylinder body, piston only, first compression ring, second compression ring and oil ring assembly, the first described compression ring, second compression ring and oil ring assembly contact with the inwall of cylinder body respectively, the excircle of described piston only is provided with top land from top to bottom successively, first compression annular groove, second ring bank, second compression annular groove, 3rd ring bank and oil ring groove, it is equivalent gullet depth or non-equivalent gullet depth structure that described first compression annular groove and second compresses annular groove, the ratio that first groove depth and second compressing annular groove compresses the groove depth of annular groove is less than or equal to 1.0, described first compression ring and the second compression ring for etc. radial thickness or the radial thickness structure such as non-, first compression piston ring radial thickness is less than or equal to 1.0 with the ratio of the second compression piston ring radial thickness, the ring-type sudden expansion expansion chamber of one or more than one is provided with between the inwall of described 3rd ring bank and cylinder body, described one or more than one ring-type sudden expansion expansion chamber by the ring-type sudden expansion expansion slot of one or more than one on the excircle being located at described 3rd ring bank and cylinder body inwall between region form.
In the utility model preferred embodiment, the second compression ring and the second back clearance region compressed between annular groove is provided with the ring-type sudden expansion expansion chamber described in.
In the utility model preferred embodiment, described second compression ring groove deep is greater than the second compression piston ring radial thickness, and described second compression piston ring radial thickness is less than 1.0 with the ratio of the second compression ring groove deep, is preferably 0.66-0.69.
In the utility model preferred embodiment, described first compression ring and the second compression ring for etc. radial thickness or the radial thickness structure such as non-, first compression piston ring radial thickness is less than or equal to 1.0 with the ratio of the second compression piston ring radial thickness, is preferably 0.8-0.9.
In the utility model preferred embodiment, described first compression ring and the second compression ring for etc. axial thickness or the axial thickness structure such as non-, first compression ring axial thickness is less than or equal to 1.0 with the ratio of the second compression ring axial thickness, is preferably 0.6-1.0.
In the utility model preferred embodiment, the closed gap length of described first compression ring and the closed gap length of the second compression ring have difference, the closed gap size of the first compression ring is less than 1.0 with the ratio of the closed gap size of the second compression ring, is preferably 0.28-0.55.
For solving the problems of the technologies described above, another technological scheme that the utility model adopts is: provide a kind of engine piston assembly, comprise cylinder body, piston only, first compression ring, second compression ring and oil ring assembly, the excircle of described piston only is provided with top land from top to bottom successively, first compression annular groove, second ring bank, second compression annular groove, 3rd ring bank and oil ring groove, it is equivalent gullet depth or non-equivalent gullet depth structure that described first compression annular groove and second compresses annular groove, the ratio that first groove depth and second compressing annular groove compresses the groove depth of annular groove is less than or equal to 1.0, described first compression ring and the second compression ring for etc. radial thickness or the radial thickness structure such as non-, first compression piston ring radial thickness is less than or equal to 1.0 with the ratio of the second compression piston ring radial thickness, it is characterized in that, the excircle of described second ring bank is provided with the first ring-type sudden expansion expansion slot, between described first ring-type sudden expansion expansion slot and cylinder wall, region then forms the first sudden expansion expansion chamber, described second compression ring groove deep is greater than the second compression piston ring radial thickness, the second sudden expansion expansion chamber is formed in the back clearance region of the second compression annular groove and the second compression piston interannular, the excircle of described 3rd ring bank is also equipped with the second ring-type sudden expansion expansion slot, between the inwall of described second ring-type sudden expansion expansion slot and cylinder body, region then forms the 3rd sudden expansion expansion chamber, described 3rd sudden expansion expansion chamber is positioned in the middle of the 3rd ring bank.
For solving the problems of the technologies described above, another technological scheme that the utility model adopts is: provide a kind of engine piston assembly, comprise cylinder body, piston only, first compression ring, second compression ring and oil ring assembly, the excircle of described piston only is provided with top land from top to bottom successively, first compression annular groove, second ring bank, second compression annular groove, 3rd ring bank and oil ring groove, it is equivalent gullet depth or non-equivalent gullet depth structure that described first compression annular groove and second compresses annular groove, the ratio that first groove depth and second compressing annular groove compresses the groove depth of annular groove is less than or equal to 1.0, described first compression ring and the second compression ring for etc. radial thickness or the radial thickness structure such as non-, first compression piston ring radial thickness is less than or equal to 1.0 with the ratio of the second compression piston ring radial thickness, the excircle of described second ring bank is provided with the first ring-type sudden expansion expansion slot, between described first ring-type sudden expansion expansion slot and cylinder wall, region then forms the first sudden expansion expansion chamber, described second compression ring groove deep is greater than the second compression piston ring radial thickness, the second sudden expansion expansion chamber is formed in the back clearance region of the second compression annular groove and the second compression piston interannular, the excircle of described 3rd ring bank is also equipped with the second ring-type sudden expansion expansion slot, between the inwall of described second ring-type sudden expansion expansion slot and cylinder body, region then forms the 3rd sudden expansion expansion chamber, described 3rd sudden expansion expansion chamber is positioned in the middle of the 3rd ring bank, it is characterized in that, the 4th sudden expansion expansion chamber is also equipped with in the back clearance region of oil ring groove and oil ring inter-module, described oil ring groove groove depth is greater than oil ring assembly radial thickness, oil ring assembly radial thickness is less than 1.0 with the ratio of oil ring groove groove depth, be preferably 0.66-0.69.
The beneficial effects of the utility model are: engine piston assembly of the present utility model, be provided with piston structure and the Piston volume tube matched with it and formation one had at least one or more than one ring-type sudden expansion expansion chamber together with the inwall of cylinder body and the clearance passage with described multistage throttle expansion function, this clearance passage compresses at engine mixed gas, enough large flow resistance and energy dissipation effect can be produced in ignition and expansion work process, the combustion gas of high pressure mixing gas and High Temperature High Pressure can be effectively stoped to be leaked from engine chamber and cylinder to the gas blowby of crankcase, in exhaust process, then can guarantee to only have a small amount of hydrocarbon emission thing can overflow from clearance, this engine piston structure assembly significantly can reduce the hydrocarbon emission in the carbon-deposits the cylinder of motor and exhaust emissions effectively, significantly can promote the efficiency gas of motor and the overall performance of motor again, be applicable to applying.
Accompanying drawing explanation
In order to be illustrated more clearly in the technological scheme in the utility model embodiment, below the accompanying drawing used required in describing embodiment is briefly described, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings, wherein:
Fig. 1 is the structural representation of a preferred embodiment of engine piston assembly of the present utility model;
Fig. 2 is the structural representation of piston only in Fig. 1;
Fig. 3 is the partial enlargement structural representation in the closed gap of the first compression ring in Fig. 1;
Fig. 4 is the partial enlargement structural representation in the closed gap of the second compression ring in Fig. 1;
Fig. 5 is the structural representation of a preferred embodiment of another engine piston assembly of the utility model;
Being labeled as in annex: 1--cylinder body, 2--piston only, 3--first compression ring, 4--second compression ring, 5--oil ring assembly, 201--top land, 202--first compresses annular groove, 203--second ring bank, 204-the second compression annular groove, 205--the 3rd ring bank, 206--oil ring groove, 207--piston skirt, 208--first ring-type sudden expansion expansion slot, 209--second ring-type sudden expansion expansion slot, 301--first compression ring closes gap, 401--second compression ring closes gap.
Embodiment
Be clearly and completely described to the technological scheme in the utility model embodiment below, obviously, described embodiment is only a part of embodiment of the present utility model, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making other embodiments all obtained under creative work prerequisite, all belong to the scope of the utility model protection.
As depicted in figs. 1 and 2, the utility model embodiment comprises:
A kind of engine piston assembly, comprise cylinder body 1, piston only 2, first compression ring 3, second compression ring 4 and oil ring assembly 5, the first described compression ring 3, second compression ring 4 and oil ring assembly 5 contact with the inwall of cylinder body 1 respectively, the excircle of described piston only 2 is provided with top land 201 from top to bottom successively, first compression annular groove 202, second ring bank 203, second compression annular groove 204, 3rd ring bank 205, oil ring groove 206 and piston skirt 207, it is non-equivalent gullet depth structure that described first compression annular groove 202 and second compresses annular groove 204, the ratio that first groove depth and second compressing annular groove 202 compresses the groove depth of annular groove 204 is less than 1.0, the excircle of described second ring bank 203 is provided with the first ring-type sudden expansion expansion slot 208, the first sudden expansion expansion chamber is formed between the inwall of described first ring-type sudden expansion expansion slot 208 and cylinder body 1, described first compression ring 3 and the second compression ring 4 are the radial thickness structure such as non-, first compression ring 3 radial thickness is less than 1.0 with the ratio of the second compression ring 4 radial thickness, described second compression annular groove 204 groove depth is greater than the second compression ring 4 radial thickness, back clearance region between the second compression annular groove 204 and the second compression ring 4 forms the second sudden expansion expansion chamber.
In above-mentioned, described second ring bank 203 surface is compressed annular groove 202 and second respectively and is compressed the crossing angle formed of annular groove 204 and have little chamfering fillet with first.
Wherein, described first sudden expansion expansion chamber is arranged between the second ring bank 203 and the inwall of cylinder body 1, and the first ring-type sudden expansion expansion slot 208 is positioned in the middle of the second ring bank 203.Described first ring-type sudden expansion expansion slot 208 surface all keeps sharp keen, without chamfering without fillet with the top corner angle of the crossing formation of the second ring bank 203 outer circumferential face and bottom corner angle.
Further, described second compression ring 4 radial thickness is less than 1.0 with the second ratio compressing annular groove 204 groove depth, is preferably 0.66-0.69.
Further, described first compression ring 3 and the second compression ring 4 are the radial thickness structure such as non-, and the first compression ring 3 radial thickness and the ratio of the second compression ring 4 radial thickness are less than 1.0, are preferably 0.8-0.9; Described first compression ring 3 and the second compression ring 4 are for waiting axial thickness or the axial thickness structure such as non-, and the first compression ring 3 axial thickness and the ratio of the second compression ring 4 axial thickness are less than or equal to 1.0, preferably 0.6-1.0.
As shown in Figure 3 and Figure 4, closed gap 301 size of described first compression ring 3 and closed gap 401 size of the second compression ring 4 have difference, closed gap 301 size of the first compression ring 3 is less than 1.0 with the ratio of closed gap 401 size of the second compression ring 4, is preferably 0.28-0.55.
As shown in Figure 5, under the higher situation of cylinder pressure of engines, the utility model additionally provides another kind of engine piston assembly, comprise cylinder body 1, piston only 2, first compression ring 3, second compression ring 4 and oil ring assembly 5, the first described compression ring 3, second compression ring 4 and oil ring assembly 5 contact with the inwall of cylinder body 1 respectively, the excircle of described piston only 2 is provided with top land 201 from top to bottom successively, first compression annular groove 202, second ring bank 203, second compression annular groove 204, 3rd ring bank 205, oil ring groove 206 and piston skirt 207, it is non-equivalent gullet depth structure that described first compression annular groove 202 and second compresses annular groove 204, the ratio that first groove depth and second compressing annular groove 202 compresses the groove depth of annular groove 204 is less than 1.0, the excircle of described second ring bank 203 is provided with the first ring-type sudden expansion expansion slot 208, the first sudden expansion expansion chamber is formed between the inwall of described first ring-type sudden expansion expansion slot 208 and cylinder body 1, described first compression ring 3 and the second compression ring 4 are the radial thickness structure such as non-, first compression ring 3 radial thickness is less than 1.0 with the ratio of the second compression ring 4 radial thickness, described second compression annular groove 204 groove depth is greater than the second compression ring 4 radial thickness, back clearance region between the second compression annular groove 204 and the second compression ring 4 forms the second sudden expansion expansion chamber, the excircle of described 3rd ring bank 205 is also equipped with the second ring-type sudden expansion expansion slot 209, described second ring-type sudden expansion expansion slot 209 then forms the 3rd sudden expansion expansion chamber with the inwall of cylinder body 1, described 3rd sudden expansion expansion chamber is positioned in the middle of the 3rd ring bank 205.
Under the higher situation of cylinder pressure of engines, the utility model additionally provides another kind of engine piston assembly, comprise cylinder body 1, piston only 2, first compression ring 3, second compression ring 4 and oil ring assembly 5, the first described compression ring 3, second compression ring 4 and oil ring assembly 5 contact with the inwall of cylinder body 1 respectively, the excircle of described piston only 2 is provided with top land 201 from top to bottom successively, first compression annular groove 202, second ring bank 203, second compression annular groove 204, 3rd ring bank 205, oil ring groove 206 and piston skirt 207, it is non-equivalent gullet depth structure that described first compression annular groove 202 and second compresses annular groove 204, the ratio that first groove depth and second compressing annular groove 202 compresses the groove depth of annular groove 204 is less than 1.0, the excircle of described second ring bank 203 is provided with the first ring-type sudden expansion expansion slot 208, the first sudden expansion expansion chamber is formed between the inwall of described first ring-type sudden expansion expansion slot 208 and cylinder body 1, described first compression ring 3 and the second compression ring 4 are the radial thickness structure such as non-, first compression ring 3 radial thickness is less than 1.0 with the ratio of the second compression ring 4 radial thickness, described second compression annular groove 204 groove depth is greater than the second compression ring 4 radial thickness, back clearance region between the second compression annular groove 204 and the second compression ring 4 forms the second sudden expansion expansion chamber, the excircle of described 3rd ring bank 205 is also equipped with the second ring-type sudden expansion expansion slot 209, described second ring-type sudden expansion expansion slot 209 then forms the 3rd sudden expansion expansion chamber with the inwall of cylinder body 1, described 3rd sudden expansion expansion chamber is positioned in the middle of the 3rd ring bank 205, back clearance region between oil ring groove 206 and oil ring assembly 5 is also equipped with the 4th sudden expansion expansion chamber (scheming not look), described oil ring groove 206 groove depth is greater than oil ring assembly 5 radial thickness, oil ring assembly 5 radial thickness is less than 1.0 with the ratio of oil ring groove 206 groove depth, be preferably 0.66-0.69.
Engine piston assembly of the present utility model from firing chamber to crankcase between be provided with more than at least two-stage can be used for catch sudden contraction throttle structure that gas blowby leaks and sudden expansion expansion structure, formation one had especially the clearance passage of multistage throttle expansion function together with the inwall of cylinder body 1, this clearance passage compresses at engine mixed gas, enough large flow resistance and energy dissipation effect can be produced in ignition and expansion work process, the combustion gas of high pressure mixing gas and High Temperature High Pressure can be effectively stoped to be leaked from engine chamber and cylinder to the gas blowby of crankcase, in exhaust process, then can guarantee to only have a small amount of hydrocarbon emission thing can overflow from clearance.
In sum, the engine piston assembly that the utility model provides, be provided with piston structure and the Piston volume tube matched with it and formation one had at least one or more than one ring-type sudden expansion expansion chamber together with the inwall of cylinder body and the clearance passage with described multistage throttle expansion function, this clearance passage compresses at engine mixed gas, enough large flow resistance and energy dissipation effect can be produced in ignition and expansion work process, the combustion gas of high pressure mixing gas and High Temperature High Pressure can be effectively stoped to be leaked from engine chamber and cylinder to the gas blowby of crankcase, in exhaust process, then can guarantee to only have a small amount of hydrocarbon emission thing can overflow from clearance, this general purpose engine piston structure assembly significantly can reduce the hydrocarbon emission in the carbon-deposits the cylinder of motor and exhaust emissions effectively, significantly can promote the efficiency gas of motor and the overall performance of motor again, be applicable to applying.
The foregoing is only embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every utilize the utility model description to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical field, be all in like manner included in scope of patent protection of the present utility model.
Claims (10)
1. an engine piston assembly, it is characterized in that, comprise cylinder body, piston only, first compression ring, second compression ring and oil ring assembly, the first described compression ring, second compression ring and oil ring assembly contact with the inwall of cylinder body respectively, the excircle of described piston only is provided with top land from top to bottom successively, first compression annular groove, second ring bank, second compression annular groove, 3rd ring bank and oil ring groove, it is equivalent gullet depth or non-equivalent gullet depth structure that described first compression annular groove and second compresses annular groove, the ratio that first groove depth and second compressing annular groove compresses the groove depth of annular groove is less than or equal to 1.0, described first compression ring and the second compression ring for etc. radial thickness or the radial thickness structure such as non-, first compression piston ring radial thickness is less than or equal to 1.0 with the ratio of the second compression piston ring radial thickness, the ring-type sudden expansion expansion chamber of one or more than one is provided with between the inwall of described second ring bank and cylinder body, described one or more than one ring-type sudden expansion expansion chamber by the ring-type sudden expansion expansion slot of one or more than one on the excircle being located at described second ring bank and cylinder body inwall between region form.
2. according to engine piston assembly described in claim 1, it is characterized in that, between the inwall of described 3rd ring bank and cylinder body, be also provided with the ring-type sudden expansion expansion chamber of one or more than one, described one or more than one ring-type sudden expansion expansion chamber by the ring-type sudden expansion expansion slot of one or more than one on the excircle being located at described 3rd ring bank and cylinder body inwall between region form.
3. an engine piston assembly, it is characterized in that, comprise cylinder body, piston only, first compression ring, second compression ring and oil ring assembly, the first described compression ring, second compression ring and oil ring assembly contact with the inwall of cylinder body respectively, the excircle of described piston only is provided with top land from top to bottom successively, first compression annular groove, second ring bank, second compression annular groove, 3rd ring bank and oil ring groove, it is equivalent gullet depth or non-equivalent gullet depth structure that described first compression annular groove and second compresses annular groove, the ratio that first groove depth and second compressing annular groove compresses the groove depth of annular groove is less than or equal to 1.0, described first compression ring and the second compression ring for etc. radial thickness or the radial thickness structure such as non-, first compression piston ring radial thickness is less than or equal to 1.0 with the ratio of the second compression piston ring radial thickness, the ring-type sudden expansion expansion chamber of one or more than one is provided with between the inwall of described 3rd ring bank and cylinder body, described one or more than one ring-type sudden expansion expansion chamber by the ring-type sudden expansion expansion slot of one or more than one on the excircle being located at described 3rd ring bank and cylinder body inwall between region form.
4. according to the described engine piston assembly of one of claim 1-3, it is characterized in that, the second compression ring and the second back clearance region compressed between annular groove is provided with the ring-type sudden expansion expansion chamber described in.
5. according to the described engine piston assembly of one of claim 1-3, it is characterized in that, described second compression ring groove deep is greater than the second compression piston ring radial thickness, and described second compression piston ring radial thickness is less than 1.0 with the ratio of the second compression ring groove deep.
6. according to the described engine piston assembly of one of claim 1-3, it is characterized in that, described first compression ring and the second compression ring for etc. radial thickness or the radial thickness structure such as non-, the first compression piston ring radial thickness is less than or equal to 1.0 with the ratio of the second compression piston ring radial thickness.
7. according to the described engine piston assembly of one of claim 1-3, it is characterized in that, described first compression ring and the second compression ring for etc. axial thickness or the axial thickness structure such as non-, the first compression ring axial thickness is less than or equal to 1.0 with the ratio of the second compression ring axial thickness.
8. according to the described engine piston assembly of one of claim 1-3, it is characterized in that, the closed gap length of described first compression ring and the closed gap length of the second compression ring have difference, and the closed gap size of the first compression ring is less than 1.0 with the ratio of the closed gap size of the second compression ring.
9. an engine piston assembly, comprise cylinder body, piston only, first compression ring, second compression ring and oil ring assembly, the excircle of described piston only is provided with top land from top to bottom successively, first compression annular groove, second ring bank, second compression annular groove, 3rd ring bank and oil ring groove, it is equivalent gullet depth or non-equivalent gullet depth structure that described first compression annular groove and second compresses annular groove, the ratio that first groove depth and second compressing annular groove compresses the groove depth of annular groove is less than or equal to 1.0, described first compression ring and the second compression ring for etc. radial thickness or the radial thickness structure such as non-, first compression piston ring radial thickness is less than or equal to 1.0 with the ratio of the second compression piston ring radial thickness, it is characterized in that, the excircle of described second ring bank is provided with the first ring-type sudden expansion expansion slot, between described first ring-type sudden expansion expansion slot and cylinder wall, region then forms the first sudden expansion expansion chamber, described second compression ring groove deep is greater than the second compression piston ring radial thickness, the second sudden expansion expansion chamber is formed in the back clearance region of the second compression annular groove and the second compression piston interannular, the excircle of described 3rd ring bank is also equipped with the second ring-type sudden expansion expansion slot, between the inwall of described second ring-type sudden expansion expansion slot and cylinder body, region then forms the 3rd sudden expansion expansion chamber, described 3rd sudden expansion expansion chamber is positioned in the middle of the 3rd ring bank.
10. an engine piston assembly, comprise cylinder body, piston only, first compression ring, second compression ring and oil ring assembly, the excircle of described piston only is provided with top land from top to bottom successively, first compression annular groove, second ring bank, second compression annular groove, 3rd ring bank and oil ring groove, it is equivalent gullet depth or non-equivalent gullet depth structure that described first compression annular groove and second compresses annular groove, the ratio that first groove depth and second compressing annular groove compresses the groove depth of annular groove is less than or equal to 1.0, described first compression ring and the second compression ring for etc. radial thickness or the radial thickness structure such as non-, first compression piston ring radial thickness is less than or equal to 1.0 with the ratio of the second compression piston ring radial thickness, the excircle of described second ring bank is provided with the first ring-type sudden expansion expansion slot, between described first ring-type sudden expansion expansion slot and cylinder wall, region then forms the first sudden expansion expansion chamber, described second compression ring groove deep is greater than the second compression piston ring radial thickness, the second sudden expansion expansion chamber is formed in the back clearance region of the second compression annular groove and the second compression piston interannular, the excircle of described 3rd ring bank is also equipped with the second ring-type sudden expansion expansion slot, between the inwall of described second ring-type sudden expansion expansion slot and cylinder body, region then forms the 3rd sudden expansion expansion chamber, described 3rd sudden expansion expansion chamber is positioned in the middle of the 3rd ring bank, it is characterized in that, the 4th sudden expansion expansion chamber is also equipped with in the back clearance region of oil ring groove and oil ring inter-module, described oil ring groove groove depth is greater than oil ring assembly radial thickness, oil ring assembly radial thickness is less than 1.0 with the ratio of oil ring groove groove depth.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420780284.6U CN204344302U (en) | 2014-12-12 | 2014-12-12 | A kind of engine piston assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420780284.6U CN204344302U (en) | 2014-12-12 | 2014-12-12 | A kind of engine piston assembly |
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| Publication Number | Publication Date |
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| CN204344302U true CN204344302U (en) | 2015-05-20 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420780284.6U Expired - Fee Related CN204344302U (en) | 2014-12-12 | 2014-12-12 | A kind of engine piston assembly |
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|---|---|
| CN (1) | CN204344302U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104454226A (en) * | 2014-12-12 | 2015-03-25 | 陶凝 | Engine piston assembly |
| WO2016090895A1 (en) * | 2014-12-12 | 2016-06-16 | 陶凝 | Energy-saving and emission-reducing multistage throttling expansion method for engine |
| US10359112B2 (en) | 2016-03-28 | 2019-07-23 | Progress Rail Locomotive Inc. | Piston ring set for internal combustion engine and system and method thereof |
-
2014
- 2014-12-12 CN CN201420780284.6U patent/CN204344302U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104454226A (en) * | 2014-12-12 | 2015-03-25 | 陶凝 | Engine piston assembly |
| WO2016091177A1 (en) * | 2014-12-12 | 2016-06-16 | 陶凝 | Engine piston assembly |
| WO2016090895A1 (en) * | 2014-12-12 | 2016-06-16 | 陶凝 | Energy-saving and emission-reducing multistage throttling expansion method for engine |
| US10359112B2 (en) | 2016-03-28 | 2019-07-23 | Progress Rail Locomotive Inc. | Piston ring set for internal combustion engine and system and method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150520 |