CN1333859A - Reciprocating piston engine - Google Patents
Reciprocating piston engine Download PDFInfo
- Publication number
- CN1333859A CN1333859A CN99815460A CN99815460A CN1333859A CN 1333859 A CN1333859 A CN 1333859A CN 99815460 A CN99815460 A CN 99815460A CN 99815460 A CN99815460 A CN 99815460A CN 1333859 A CN1333859 A CN 1333859A
- Authority
- CN
- China
- Prior art keywords
- groove
- described reciprocating
- reciprocating machine
- filler
- aforesaid right
- Prior art date
- Legal status (The legal status 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 status listed.)
- Granted
Links
- 239000000463 material Substances 0.000 claims abstract description 42
- 239000000945 filler Substances 0.000 claims description 33
- 229910052782 aluminium Inorganic materials 0.000 claims description 26
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 20
- 239000004519 grease Substances 0.000 claims description 20
- 229910000906 Bronze Inorganic materials 0.000 claims description 15
- 239000010974 bronze Substances 0.000 claims description 15
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 claims description 15
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 12
- 229910002804 graphite Inorganic materials 0.000 claims description 12
- 239000010439 graphite Substances 0.000 claims description 12
- 239000010949 copper Substances 0.000 claims description 7
- 229910052742 iron Inorganic materials 0.000 claims description 7
- 239000000203 mixture Substances 0.000 claims description 7
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 7
- 229910045601 alloy Inorganic materials 0.000 claims description 5
- 239000000956 alloy Substances 0.000 claims description 5
- 239000004411 aluminium Substances 0.000 claims description 5
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- 230000015572 biosynthetic process Effects 0.000 claims description 4
- 239000011248 coating agent Substances 0.000 claims description 4
- 238000000576 coating method Methods 0.000 claims description 4
- 230000001050 lubricating effect Effects 0.000 claims description 4
- 229910052748 manganese Inorganic materials 0.000 claims description 3
- 229910052710 silicon Inorganic materials 0.000 claims description 3
- 229910052790 beryllium Inorganic materials 0.000 claims description 2
- 229910052793 cadmium Inorganic materials 0.000 claims description 2
- 229910052799 carbon Inorganic materials 0.000 claims description 2
- 229910052804 chromium Inorganic materials 0.000 claims description 2
- 229910052718 tin Inorganic materials 0.000 claims description 2
- 229910052725 zinc Inorganic materials 0.000 claims description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims 1
- 229910052802 copper Inorganic materials 0.000 claims 1
- 239000010703 silicon Substances 0.000 claims 1
- 230000001681 protective effect Effects 0.000 abstract 1
- 230000003628 erosive effect Effects 0.000 description 5
- 230000002349 favourable effect Effects 0.000 description 5
- 239000008187 granular material Substances 0.000 description 5
- 239000000314 lubricant Substances 0.000 description 5
- 238000012856 packing Methods 0.000 description 4
- 230000001186 cumulative effect Effects 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 210000002268 wool Anatomy 0.000 description 2
- 229910001208 Crucible steel Inorganic materials 0.000 description 1
- 206010037660 Pyrexia Diseases 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000027950 fever generation Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000007750 plasma spraying Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000013022 venting Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
- F02F1/18—Other cylinders
- F02F1/20—Other cylinders characterised by constructional features providing for lubrication
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J10/00—Engine or like cylinders; Features of hollow, e.g. cylindrical, bodies in general
- F16J10/02—Cylinders designed to receive moving pistons or plungers
- F16J10/04—Running faces; Liners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F7/00—Casings, e.g. crankcases or frames
- F02F2007/0097—Casings, e.g. crankcases or frames for large diesel engines
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Coating By Spraying Or Casting (AREA)
Abstract
The invention relates to a reciprocating piston engine comprising at least one cylinder whose cylinder liner (2) is provided with at least one groove (9) which forms an oil pocket (8) and which is situated in the area of the running surface (4) of said liner, whereby the running surface (4) faces the piston (6) assigned to the cylinder. The aim of the invention is to create a particularly protective operating mode and thus attain a particularly long service life of the cylinder liner (2). To this end, the groove (9) has a depth which corresponds to the maximum depth of the wear of the cylinder liner (2). A filling (10) is allocated to said groove. The material used for the filling (10) in the groove (9) has a lower capacity of resistance to wear than the basic material of the cylinder liner (2).
Description
The present invention relates to a kind of reciprocating machine, particularly large two-stroke diesel engine, it has at least one cylinder, and its cylinder liner is provided with the groove that at least one is used to form the grease chamber at it in the zone of the slip surface of the piston of attaching troops to a unit.
By GB 1473058 known a kind of like this internal-combustion piston engines.The cross section of grease chamber or heavy wool chamber is equivalent to cross section that each is attached troops to a unit, the groove that cuts out on cylinder liner in this known device.The degree of depth of groove reduces along with the wearing and tearing of cumulative cylinder liner.In this known device, also reduce the degree of depth of the grease chamber that forms by groove itself with same degree.Therefore its working condition of prolongation along with service time constantly worsens.And another very special shortcoming of known equipment is, because the material granule that possible heat erosion etc. are peeled off from cylinder liner can not reside at the groove of known device.Therefore exist such danger, this material granule fall between cylinder liner and the piston and pulverized or rubbed with the hands therein broken, thereby this may cause damaging with strong local pyrexia and quicken heat erosion and/or kill.Therefore prove that the operation of this known device is reliable inadequately.
Therefore set out thus, the objective of the invention is, avoiding improving same kind equipment in simple and cost-effective mode under the condition of described shortcoming, make it reach long-term height operational reliability.
This purpose reaches like this according to the present invention, arrangements of grooves one filler, the degree of depth of groove is equivalent to the greatest wear thickness of cylinder liner at least, and the material that forms the filler of groove has less wear resistance than the body material of cylinder liner.
Under news, groove can be filled up fully by the filler of configuration.Therefore obtain the outer surface of a smooth non-moulding, it is easy to processing.Yet in running-in period since the wearing and tearing of packing material than the fast grease chamber that has formed requirement of body material, its degree of depth is undoubtedly less than the degree of depth of groove and along with the cumulative wearing and tearing of cylinder liner develop into the degree that depends on these wearing and tearing.Though therefore groove depth reduces gradually, but through forming the uniform state about the quite big degree of the cross section of grease chamber after over a long time, thereby this is through guaranteeing after over a long time at the lubricated reliably of the domain of dependence of cylinder liner and being avoided heat erosion reliably and kill.The grease chamber that forms or the degree of depth of heavy wool chamber are relevant with the intensity of wearing and tearing.Big more each grease chamber of wearing and tearing is dark more and thereby it is strong more to lubricate, and vice versa.Therefore in fact form a kind of self-adjusting pattern.Therefore also might reduce SFC.But another the very special advantage according to measure of the present invention is, because of cylinder liner inevitably the material granule that peeled off of wearing and tearing can be pressed in the softer packing material and fix on the spot.Therefore stoped the unrestricted motion of this material granule by the groove that is provided with filler.Therefore the groove that is provided with filler according to the present invention also plays a part highly effectively to stop groove.Therefore can also prevent the damage that material granule caused and the fault of peeling off effectively by measure of the present invention by cylinder liner, for example material welding or material bonding, it causes quickening heat erosion and kills.Therefore guaranteed long working life in an advantageous manner by measure of the present invention.
The favourable structure and the further formation that meets purpose of above-mentioned measure have been described in the dependent claims.Like this, form the material of the filler of groove and can be suitably have stronger thermal expansion than the body material of cylinder liner.Can make whereby that filler expands quickly than body material under overheated situation, therefore can make piston stable and prevent so-called killing thus.When also having dry lubricating performance in an advantageous manner, more given prominence to packing material this advantage.
In favourable the further developing of above-mentioned measure, the filler of groove can be at least in part be made of aluminium and/or aluminum bronze and/or graphite, wherein preferably can adopt contain 9～11%Al, 0.5～2%Fe, all the other are the aluminum bronze of Cu.This material has the superior performance of above-mentioned requirement.Yet also might adopt the graphite alloy of the aluminum bronze that for example preferably contains 15～25% graphite and 75～85%.This material also has the performance of the high level of requirement.
Can be advantageously provided at least one spiral groove.Thereby obtain oily especially good distribution interior and good especially conveying thus and also obtain extra high reliability along the big zone of cylinder liner.
According to another favourable development of above-mentioned measure, filler can constitute weld layer or sprayfused coating according to the applicability of the material that is adopted.This has guaranteed the reliable bonding of imporous filler on body material with plain mode.
The favourable development of other of above-mentioned measure and the further formation that meets purpose are seen remaining dependent claims and can be learnt in more detail the description of example by means of accompanying drawing by following.
In accompanying drawing described below:
Fig. 1 illustrates the part section of a cylinder of large two-stroke diesel engine;
Fig. 2 illustrates the enlarged view according to the zone of groove of the present invention of being provided with of cylinder liner slip surface;
Fig. 3 illustrates a scheme about trench cross-section, and
Fig. 4 illustrates the another program about trench cross-section.
The present invention is applied to preferably in the reciprocating machine, particularly internal-combustion piston engine with the large two-stroke diesel engine of operation slowly.The structure of this equipment and mode of operation are known in itself, therefore no longer need in this article to illustrate in greater detail.
The cylinder of large two-stroke diesel engine shown in Fig. 1 comprises that one is provided with the cylinder liner 2 of a plurality of suction ports 1, and installation one comprises the cylinder head 3 of a venting gas appliance that wherein is not shown specifically on it.The inner face of cylinder liner 2 constitutes slip surface 4, and itself and a periphery are provided with reciprocating piston 6 concurrent operations of piston ring 5.Slip surface 4 is supplied with lubricant oil via lubricant oil supplying tube 7.
In order to make the zone by experience lubricant oil undersupply, for example the upper area of slip surface 4 obtains good lubricant oil distribution and particularly good lubricant oil is supplied with, and this zone is provided with each grease chamber 8 suitable, that only hint out in Fig. 1.
For this reason,, the groove 9 of at least one incision is set in the zone of slip surface 4, wherein constitutes the grease chamber 8 of a configuration as being clear that by Fig. 2.Groove 9 comprises a filler 10, and it is made of the wear resistance materials with smaller of wear resistance than the body material of cylinder liner.Cylinder liner is made of cast steel usually.Can advantageously adopt aluminum bronze to form filler 10.As experiment prove that this aluminum bronze should comprise at least 2～20%, preferred 9～11%Al, 0.5～8%, preferred 0.5～2%Fe and all the other are Cu.The condition that specific composition exists at each situation.Wherein Fe content is high more, and the hardness of material is high more.In the cylinder liner of large two-stroke diesel engine, adopt the aluminum bronze that comprises following composition to obtain good result:
2～20%, preferred 9～11%Al,
0.5～8%, preferred 0.5～2%Fe,
0.1～8％Mn，0.1～2％Si，0.1～1％Ni，
0.1～2%C has at least a composition among Sb, Co, Be, Cr, Sn, Cd, Zn and the Pb of the highest 5～20% content respectively, all the other are Cu.
But also may adopt graphite alloy such as nickel graphite or 3 SiC 2/graphite or aluminium graphite or aluminum bronze graphite, it comprises 5～60% respectively, preferred 15～25% graphite and comprise 40～95% of other compositions respectively, preferred 75～85% content.Adopt the aluminum bronze graphite alloy can obtain the good especially anticorrosive and performance of killing.Wherein the composition of aluminum bronze can be according to above-mentioned composition.
The filler of this groove 9 is suitably reached the level of slip surface 4.Slip surface 4 can be through processing all sidedly, for example honing then.Because it is more less than the wear resistance of the body material of cylinder liner 2 to form the material of filler 10, the wearing and tearing of filler 10 are bigger in the running-in period wearing and tearing than cylinder liner 2.The lubricated oil of material under the mill washes away.Therefore form the grease chamber 8 that requires, it remained between the whole spreadable life of cylinder liner.
Therefore the degree of depth with the groove shown in the d 9 among Fig. 2 is equivalent to the wearing and tearing thickness of cylinder liner 2 and preferably big slightly at least.Yet because dark like this groove 9 is provided with filler 10, its wearing and tearing along with cylinder liner are are also worn and torn, just its wearing and tearing are fast slightly, and in being formed between whole spreadable life of cylinder liner 2 quite big degree uniformly, be different from the cross-sectional profile of the grease chamber 8 of groove 9 cross sections own.
Can advantageously adopt such material in order to form filler 10, it has the performance of expansion stronger than the body material of cylinder liner when being heated.More than Jian Yi material has such performance.Therefore filler 10 expansion stronger than the body material of cylinder liner 2 under the situation of local superheating can make piston 6 stable, the expansion line 11 that dots as shown in Figure 2 thus.More than the material of Jian Yi filler 10 also has good dry lubricating performance, and this particularly obtains favourable supporting under overheated situation.But also may be in packing material in conjunction with or insert the material that has good dry lubricating performance in addition.
One or more grooves 9 can be set.They are met the place that the destination is arranged on the dangerous of lack of lubrication and thereby danger such as heat erosion are arranged according to experience so far.This is particularly in the situation of the upper area of slip surface 4.In Fig. 1, in the zone of the slip surface 4 that limits in the top dead center position of piston 6 by first and second piston rings 5, a groove with annular of corresponding grease chamber 8 is set.Another groove that disposes grease chamber 8 is arranged in the zone of below of nethermost piston ring 5.Also show the grease chamber 8 of other darker configuration in the example shown.
Can constitute the radial groove of annular as the groove 9 on the basis of grease chamber 8.But, one or more grooves 9 that dispose the spiral extension of grease chamber 8 also can be set in addition or instead.They can extend along zone of slip surface 4 or along its total length.
Fig. 2 is the groove 9 based on a spiral extension.The helical pitch that this groove 9 usefulness P represent can be 1.5%～20% of the diameter D of slip surface 4.Helical pitch P can be a constant along the groove total length.But also might be that the helical pitch that changes is so that obtain bigger grease chamber's density at predispose to damage especially zone ratio in little predispose to damage zone.The depth d of above-mentioned groove 9 suitably is in 0.1%～0.4% the scope of diameter D.Exit width W suitably is 1%～2% of diameter D
Above-mentioned sized data also is applicable to other the scheme according to Fig. 3 and 4.Fig. 3 illustrates a vee-cut 9, and it has the filler that comprises grease chamber 8 10 of configuration.Groove 9 among Fig. 4 has a circular arc cross section.Thereby the inside width that reduces gradually of the grease chamber 8 that also forms inside narrowed cross-section gradually and formation filler 10 here and wherein form.
Claims (18)
1. reciprocating machine, particularly large two-stroke diesel engine, it has at least one cylinder.Its cylinder liner (2) is provided with at least one groove that is used to form grease chamber (8) (9) at it in the zone of the slip surface (4) of the piston (6) of configuration, it is characterized in that, groove (9) has disposed a filler (10), the degree of depth of groove is equivalent to the greatest wear thickness of cylinder liner (2) at least, and the material that forms the filler (10) of groove (9) has less wear resistance than the body material of cylinder liner (2).
2. according to the described reciprocating machine of claim 1, it is characterized in that the material of the filler (10) of formation groove (9) has stronger thermal expansion than the body material of cylinder liner (2).
3. according to one of an aforesaid right requirement described reciprocating machine, the material that it is characterized in that forming the filler (10) of groove (9) has dry lubricating performance.
4. one of require a described reciprocating machine according to aforesaid right, the material that it is characterized in that forming the filler (10) of groove (9) is made of aluminium and/or aluminum bronze and/or graphite at least in part.
5. according to the described reciprocating machine of claim 4, it is characterized in that comprising aluminium, iron and copper at least for the aluminum bronze that the filler (10) that forms groove (9) is adopted.
6. according to one of an aforesaid right requirement described reciprocating machine, it is characterized in that the aluminum bronze that is adopted for the filler (10) that forms groove (9) comprises following alloy part at least:
2～20%, preferred 9～11%Al,
0.5～8%, preferred 0.5～2%Fe,
All the other are Cu.
7. according to claim 5 or 6 described reciprocating machines, it is characterized in that the aluminum bronze that is adopted for the filler (10) that forms groove (9) comprises following alloy part:
2～20%, preferred 9～11%Al,
0.5～8%, preferred 0.5～2%Fe,
0.1～8%Mn, 0.1～2%Si, 0.1～1%Ni, 0.1～2%C has at least a composition among Sb, Co, Be, Cr, Sn, Cd, Zn and the Pb of the highest 5～20% content respectively, and all the other are Cu.
8. according to one of claim 4～7 described reciprocating machine, it is characterized in that, the material that forms the filler (10) of groove (9) comprises 5～60%, preferred 15～25% graphite and 40～95%, preferred 75～85% aluminium and/or aluminum bronze and/or nickel and/or silicon.
9. according to one of an aforesaid right requirement described reciprocating machine, it is characterized in that being provided with at least one spiral groove (9).
10. according to one of an aforesaid right requirement described reciprocating machine, it is characterized in that, at least one groove (9) is set in the upper area of cylinder liner (2) at least.
11. according to one of an aforesaid right requirement described reciprocating machine, it is characterized in that, in the zone of the slip surface (4) that limits in the top dead center position of piston (6) by first and second piston rings (5) at least one groove (9) be set at least.
12. according to one of an aforesaid right requirement described reciprocating machine, it is characterized in that, in the zone of the top dead center position of piston (6) at least one groove (9) be set in the below of nethermost piston ring (5) at least.
13., it is characterized in that at least one groove (9) extends continuously along the guiding length of slip surface (4) according to one of an aforesaid right requirement described reciprocating machine.
14. according to aforesaid right one of require a described reciprocating machine, the helical pitch that it is characterized in that spiral groove (9) be slip surface (4) diameter 1.5%～20%.
15. according to aforesaid right one of require a described reciprocating machine, the degree of depth that it is characterized in that groove (9) be slip surface (4) diameter 0.1%～0.4%.
16. according to aforesaid right one of require a described reciprocating machine, the exit width that it is characterized in that groove (9) be slip surface (4) diameter 1%～2%.
17., it is characterized in that groove (9) inwardly has narrowed cross-section gradually according to one of an aforesaid right requirement described reciprocating machine.
18., it is characterized in that the filler (10) of groove (9) constitutes weld layer or sprayfused coating according to one of an aforesaid right requirement described reciprocating machine.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19900386A DE19900386C1 (en) | 1999-01-08 | 1999-01-08 | Reciprocating machine |
| DE19900386.6 | 1999-01-08 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1333859A true CN1333859A (en) | 2002-01-30 |
| CN1116510C CN1116510C (en) | 2003-07-30 |
Family
ID=7893737
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN99815460A Expired - Lifetime CN1116510C (en) | 1999-01-08 | 1999-12-22 | Reciprocating piston engine |
Country Status (9)
| Country | Link |
|---|---|
| JP (1) | JP3636664B2 (en) |
| KR (1) | KR100411867B1 (en) |
| CN (1) | CN1116510C (en) |
| AU (1) | AU2100800A (en) |
| DE (1) | DE19900386C1 (en) |
| GB (1) | GB2361982B (en) |
| NO (1) | NO20013177L (en) |
| PL (1) | PL349134A1 (en) |
| WO (1) | WO2000040850A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103421979A (en) * | 2013-08-27 | 2013-12-04 | 苏州长盛机电有限公司 | Chromium copper alloy |
| CN103511112A (en) * | 2012-06-20 | 2014-01-15 | 通用电气公司 | Variable thickness coating for cylinder liner |
| CN107542593A (en) * | 2016-06-23 | 2018-01-05 | 曼卡车和巴士股份公司 | Internal combustion engine, especially stroke piston combustion engine |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2410313B (en) * | 2004-01-22 | 2007-08-08 | Ford Global Tech Llc | An engine and a method of making same |
| JP4190570B2 (en) * | 2005-07-28 | 2008-12-03 | サンエツ金属株式会社 | Lead-free free-cutting copper alloy extruded material |
| MX2009004280A (en) * | 2007-01-09 | 2009-05-05 | Federal Mogul Burscheid Gmbh | Piston ring with a multilayer assembly, and a method for the production thereof. |
| EP2182094A1 (en) * | 2008-10-31 | 2010-05-05 | Wärtsilä Schweiz AG | Cylinder for a large diesel motor |
| JP5514593B2 (en) * | 2009-03-31 | 2014-06-04 | 日本ピストンリング株式会社 | Cylinder |
| CN103201487B (en) * | 2010-11-03 | 2016-06-29 | 斗山英维高株式会社 | Irregular cylinder is formed at internal face |
| DE102011106564A1 (en) | 2011-07-05 | 2013-01-10 | Mahle International Gmbh | Method for producing a cylinder surface and cylinder liner |
| CN102537065B (en) * | 2012-02-23 | 2013-11-27 | 杭州钱王机械有限公司 | Bearing for copper-based heavy-load self-lubricating ship and preparation method thereof |
| CN102606332A (en) * | 2012-03-30 | 2012-07-25 | 常熟市赵市水磨粉厂 | High-temperature wear-resistant cylinder structure |
| DE102015006498A1 (en) * | 2015-05-22 | 2016-11-24 | Mahle International Gmbh | Cylinder bore for a cylinder housing of an internal combustion engine and arrangement of such a cylinder bore and a piston |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH493738A (en) * | 1968-07-01 | 1970-07-15 | Sulzer Ag | Cylinder of a piston internal combustion engine |
| CH582307A5 (en) * | 1974-09-26 | 1976-11-30 | Sulzer Ag | |
| JPS56127845U (en) * | 1980-02-29 | 1981-09-29 | ||
| US4987865A (en) * | 1989-10-11 | 1991-01-29 | Wickes Manufacturing Company | Reduced friction piston |
| DE4238525C1 (en) * | 1992-11-14 | 1993-11-18 | Man B & W Diesel Ag | Cylinder liner with a wear resistant layer |
| US5363821A (en) * | 1993-07-06 | 1994-11-15 | Ford Motor Company | Thermoset polymer/solid lubricant coating system |
-
1999
- 1999-01-08 DE DE19900386A patent/DE19900386C1/en not_active Expired - Fee Related
- 1999-12-22 KR KR10-2001-7008539A patent/KR100411867B1/en active IP Right Grant
- 1999-12-22 WO PCT/EP1999/010267 patent/WO2000040850A1/en not_active Application Discontinuation
- 1999-12-22 AU AU21008/00A patent/AU2100800A/en not_active Abandoned
- 1999-12-22 GB GB0115516A patent/GB2361982B/en not_active Expired - Fee Related
- 1999-12-22 PL PL99349134A patent/PL349134A1/en unknown
- 1999-12-22 JP JP2000592533A patent/JP3636664B2/en not_active Expired - Lifetime
- 1999-12-22 CN CN99815460A patent/CN1116510C/en not_active Expired - Lifetime
-
2001
- 2001-06-22 NO NO20013177A patent/NO20013177L/en not_active Application Discontinuation
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103511112A (en) * | 2012-06-20 | 2014-01-15 | 通用电气公司 | Variable thickness coating for cylinder liner |
| US9534559B2 (en) | 2012-06-20 | 2017-01-03 | General Electric Company | Variable thickness coatings for cylinder liners |
| CN103511112B (en) * | 2012-06-20 | 2018-06-12 | 通用电气公司 | For the coating of the variable thickness of cylinder liner |
| CN103421979A (en) * | 2013-08-27 | 2013-12-04 | 苏州长盛机电有限公司 | Chromium copper alloy |
| CN107542593A (en) * | 2016-06-23 | 2018-01-05 | 曼卡车和巴士股份公司 | Internal combustion engine, especially stroke piston combustion engine |
| CN107542593B (en) * | 2016-06-23 | 2021-12-03 | 曼卡车和巴士股份公司 | Internal combustion engine, in particular reciprocating piston internal combustion engine |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2361982B (en) | 2002-07-10 |
| KR20010089772A (en) | 2001-10-08 |
| NO20013177D0 (en) | 2001-06-22 |
| PL349134A1 (en) | 2002-07-01 |
| GB2361982A (en) | 2001-11-07 |
| KR100411867B1 (en) | 2003-12-18 |
| WO2000040850A1 (en) | 2000-07-13 |
| AU2100800A (en) | 2000-07-24 |
| NO20013177L (en) | 2001-08-10 |
| JP3636664B2 (en) | 2005-04-06 |
| GB0115516D0 (en) | 2001-08-15 |
| CN1116510C (en) | 2003-07-30 |
| DE19900386C1 (en) | 2000-11-16 |
| JP2002534635A (en) | 2002-10-15 |
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Owner name: MAN DIESEL ENGINES AND TURBINE GERMAN SUBSIDIARY, Free format text: FORMER OWNER: MAN DIESEL AS Effective date: 20101214 Owner name: MAN DIESEL AS Free format text: FORMER OWNER: MAN B + W DIESEL AS. Effective date: 20101214 Owner name: MAN DIESEL AS Free format text: FORMER OWNER: MAN DIESEL AS Effective date: 20101214 |
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Effective date of registration: 20101214 Address after: Copenhagen, Denmark Patentee after: MAN DIESEL & TURBO FILIAL AF MAN DIESEL & TURBO SE TYSKLAND Address before: Copenhagen, Denmark Patentee before: MAN DIESEL & TURBO FILIAL AF MAN DIESEL & TURBO SE TYSKLAND Effective date of registration: 20101214 Address after: Copenhagen, Denmark Patentee after: MAN DIESEL & TURBO FILIAL AF MAN DIESEL & TURBO SE TYSKLAND Address before: Copenhagen, Denmark Patentee before: MAN DIESEL filial af MAN Diesel SE Tyskland Effective date of registration: 20101214 Address after: Copenhagen, Denmark Patentee after: MAN DIESEL filial af MAN Diesel SE Tyskland Address before: Copenhagen, Denmark Patentee before: MAN B & W DIESEL A/S |
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