CN1320150C - Gray cast iron alloy and cast internal combustion engine component - Google Patents
Gray cast iron alloy and cast internal combustion engine component Download PDFInfo
- Publication number
- CN1320150C CN1320150C CNB03811027XA CN03811027A CN1320150C CN 1320150 C CN1320150 C CN 1320150C CN B03811027X A CNB03811027X A CN B03811027XA CN 03811027 A CN03811027 A CN 03811027A CN 1320150 C CN1320150 C CN 1320150C
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- alloy
- cast iron
- grey cast
- vanadium
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- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 38
- 239000000956 alloy Substances 0.000 title claims abstract description 38
- 229910001060 Gray iron Inorganic materials 0.000 title claims abstract description 27
- 238000002485 combustion reaction Methods 0.000 title description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 13
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 12
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 11
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 11
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims abstract description 11
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims abstract description 10
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 10
- 239000011733 molybdenum Substances 0.000 claims abstract description 10
- 239000011651 chromium Substances 0.000 claims abstract description 9
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 8
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims abstract description 8
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims abstract description 8
- 239000005864 Sulphur Substances 0.000 claims abstract description 8
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 8
- 239000010955 niobium Substances 0.000 claims abstract description 8
- 229910052698 phosphorus Inorganic materials 0.000 claims abstract description 8
- 239000011574 phosphorus Substances 0.000 claims abstract description 8
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 8
- 239000010703 silicon Substances 0.000 claims abstract description 8
- 239000010949 copper Substances 0.000 claims abstract description 7
- 239000012535 impurity Substances 0.000 claims abstract description 7
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 7
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims abstract description 7
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 6
- 229910052802 copper Inorganic materials 0.000 claims abstract description 6
- 229910052742 iron Inorganic materials 0.000 claims abstract description 6
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 14
- 239000011572 manganese Substances 0.000 claims description 8
- 239000010936 titanium Substances 0.000 claims description 8
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 7
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 7
- 238000005266 casting Methods 0.000 claims description 7
- 229910052748 manganese Inorganic materials 0.000 claims description 7
- 229910052757 nitrogen Inorganic materials 0.000 claims description 7
- 229910052719 titanium Inorganic materials 0.000 claims description 7
- 239000004411 aluminium Substances 0.000 claims description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 5
- 239000003921 oil Substances 0.000 claims description 5
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 2
- 229910052759 nickel Inorganic materials 0.000 claims description 2
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 abstract 1
- 239000000463 material Substances 0.000 description 9
- 239000000203 mixture Substances 0.000 description 6
- 239000010451 perlite Substances 0.000 description 6
- 235000019362 perlite Nutrition 0.000 description 6
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 4
- 230000007547 defect Effects 0.000 description 4
- 238000002360 preparation method Methods 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 239000010439 graphite Substances 0.000 description 2
- 229910002804 graphite Inorganic materials 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical group [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009661 fatigue test Methods 0.000 description 1
- 239000002054 inoculum Substances 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/08—Making cast-iron alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C37/00—Cast-iron alloys
- C22C37/06—Cast-iron alloys containing chromium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C37/00—Cast-iron alloys
- C22C37/10—Cast-iron alloys containing aluminium or silicon
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
Abstract
A substantially perlitic, grey cast iron alloy comprising, by weight, 3.2 - 3.49% carbon, 1.8 - 2.2% silicon, < 0.15% sulphur, < 0.15% phosphorus, 0.3 - 0.8% manganese, 0.2 - 0.4% chromium, 0.1 - 0.4% molybdenum, 0.03 - 0.3% vanadium, 0.3 - 1.0% copper, < 0.15% niobium, the balance iron and impurities.
Description
Technical field
The present invention relates to a kind of grey cast iron alloy.More particularly, the present invention relates to a kind of grey cast iron of pearly-lustre basically, it also comprises the alloy element that improves fatigue strength.
The invention still further relates to the internal combustion engine component that derives from grey cast iron alloy of the present invention.
Background technology
Grey cast iron is low relatively owing to cost, and functional even excellent, so it is the most attracting material that for example is used for the internal combustion (IC) engine airframe of transportation means.The compositing range of known in the past grey cast iron is quite wide, and these form normally the performance at material therefor, for example tensile strength, polishing machine etc. and processability, for example compromise between cost, the machinability etc.
Therefore, with regard to the casting internal combustion (IC) engine airframe, basic material 0120 has 1 the composition of being listed in the table below, and the composition of common standard alloy is also listed in table 1, and therefore the Scania standard alloy provides grey cast iron and zero defect (atresia) material with perlitic structure because of having high relatively carbon content.
Yet although can accept fully at present, replenishing of the existing performance of conduct needs the fatigue strength of raising at present, and expands the possible purposes of this existing grey cast iron.
An object of the present invention is to provide a kind of grey cast iron, it has flawless relatively structure and good workability is provided, and compares with standard alloy in addition to have the fatigue strength that improves greatly.
Another object of the present invention provides a kind of grey cast iron internal combustion engine component, engine body for example, and it is compared with standard alloy has the fatigue strength that improves greatly.
Summary of the invention
The objective of the invention is that grey cast iron alloy by following a kind of pearly-lustre basically realizes, described grey cast iron comprises by weight:
The carbon of 3.2-3.49%,
The silicon of 1.8-2.2%,
<0.15% sulphur,
<0.15% phosphorus,
The manganese of 0.3-0.8%,
The chromium of 0.2-0.4%,
The molybdenum of 0.1-0.4%,
The vanadium of 0.03-0.3%,
The copper of 0.3-1.0%,
<0.15% niobium,
The titanium of 0.007-0.015%,
The nitrogen of 0.005-0.017%,
The iron of surplus and impurity.
In addition, purpose of the present invention also realizes by a kind of oil engine casting engine parts.Described oil engine casting engine parts are made by the grey cast iron alloy of pearly-lustre basically, and described alloy comprises:
The carbon of 3.2-3.49%,
The silicon of 1.8-2.2%,
<0.15% sulphur,
<0.15% phosphorus,
The manganese of 0.3-0.8%,
The chromium of 0.2-0.4%,
The molybdenum of 0.1-0.4%,
The vanadium of 0.03-0.3%,
The copper of 0.3-1.0%,
The titanium of 0.007-0.013%,
<0.15% niobium,
The nitrogen of 0.005-0.015%,
<0.01% aluminium,
The iron of surplus and impurity.
Description of drawings
Fig. 1 has shown the W hler fatigue curve of basic alloy, standard alloy and alloy of the present invention.
Embodiment
In the following description, all per-cents of element all provide with weight percent in the concrete alloy.
Alloy of the present invention is to have the grey cast iron of perlitic structure basically, and its carbon content is 3.2-3.49%.Higher carbon content has promoted a kind of zero defect structure.Add the chromium of 0.2-0.4%, it has perlite/carbide stability, and the purified perlitic structure is provided.
Add molybdenum, the 0.03-0.3% of 0.1-0.4% vanadium, 0.007-0.015% titanium and<0.15% niobium, except its carbide forms performance, also work the nuclear core that makes cast iron (as the sedimentary carbide of primary and secondary) have refined pearl-like structure and flake graphite structure.Molybdenum can also at high temperature be stablized perlite.
Preferred vanadium exists to be lower than 0.1% amount, and aluminium exists to be lower than 0.01% amount, and nickel exists to be lower than 0.1% amount, and tin exists to be lower than 0.1% amount.
Silicon exists with the amount of 1.8-2.2%, promotes grey iron to form.
The manganese of 0.3-0.8% exists as the perlite stablizer.
Copper, the amount with 0.3-1.0% exists here, promotes perlite to form and stablize this perlite, also promotes the formation of refining structure.
The content of sulphur and phosphorus should remain on below 0.15%.
Nitrogen content is 0.005-0.017%, and it compresses flake graphite and promotes perlite to form, and aluminium content be<0.01%, plays graphite formation agent.
The grey cast iron alloy also comprises the iron and the normal impurity of surplus.Titanium, nitrogen and aluminium still can be through preferred in the normal impurities scope.
A kind of preferred grey cast iron alloy of the present invention comprises: the carbon of 3.3-3.4%, the silicon of 1.8-2.2%,<0.1% sulphur,<0.05% phosphorus, the manganese of 0.4-0.6%, the chromium of 0.2-0.4%, the molybdenum of 0.2-0.3% and the vanadium of 0.05-0.1%.
Oil engine casting engine parts of the present invention are engine body parts or cylinder head sub-assembly preferably.
Embodiment
The preparation 1500kg batch of material, each batch of material is cast into the engine body of 4 300kg, cast in begin under 1420 ℃ and in casting cycle temperature reduce about 10 ℃.
Use basic alloy, ten various combinations of preparation molybdenum, vanadium, titanium and niobium and batch of material.
And the content of nitrogen and aluminium forms agent (Inoculant) with different nuclear cores and changes in 16 different batch of materials.
Water the foundry goods from each and to extract the Fatigue Test sample and to carry out fatigue measurement.
Further, preparation have the optimum that shows said determination composition batch of material and carry out fatigue measurement.
The results are shown in Fig. 1, curve 3 is corresponding to the composition in compositing range of the present invention, and this composition also is presented at table 1.
Grey cast iron of the present invention provides the fatigue strength than grey cast iron basic alloy high about 40%, and the fatigue strength than model engine body grey cast iron high about 30% is provided, and the grey cast iron that obtains high performance at aspects such as workability, zero defects is provided.
As mentioned above, grey cast iron alloy of the present invention is specially adapted to oil engine foundry goods engine parts, engine body parts for example, and described alloy has workability, zero defect and high fatigue strength simultaneously.This alloy also can be used for other parts, for example cylinder head etc.
The composition of table 1. prior art and grey cast iron of the present invention, weight %
Alloy | |||||
Compound | Basic alloy 0120 | Standard alloy | Conventional alloy of the present invention | Preferred implementation | The embodiment alloy 3 of Fig. 1 |
C | 3.2-3.5 | ~3.4 | 3.2-3.49 | 3.3-3.4 | 3.37 |
Si | 1.8-2.3 | ~2.0 | 1.8-2.2 | 1.8-2.2 | 1.8 |
S | 0.06-0.15 | <0.14 | <0.15 | <0.1 | 0.1 |
P | <0.20 | <0.10 | <0.15 | <0.05 | 0.05 |
Mn | 0.6-0.8 | 0.6-0.8 | 0.3-0.8 | 0.4-0.6 | 0.68 |
Cr | 0.2-0.35 | 0.2-0.4 | 0.2-0.4 | 0.34 | |
Mo | 0.1-0.4 | 0.2-0.3 | 0.26 | ||
V | 0.03-0.3 | 0.05-0.1 | 0.1 | ||
Cu | 0.4-0.8 | 0.3-1.0 | 0.5-1.0 | 0.6 | |
Ni | <0.1 | <0.1 | |||
Ti | 0.007-0.015 | 0.007-0.013 | 0.013 | ||
Nb | <0.15 | <0.10 | 0.04 | ||
N | 0.005-0.017 | 0.005-0.015 | 0.010 | ||
Sn | <0.1 | <0.1 | |||
Al | <0.01 | <0.01 |
Claims (8)
1, a kind of grey cast iron alloy of pearly-lustre basically comprises by weight:
The carbon of 3.2-3.49%,
The silicon of 1.8-2.2%,
<0.15% sulphur,
<0.15% phosphorus,
The manganese of 0.3-0.8%,
The chromium of 0.2-0.4%,
The molybdenum of 0.1-0.4%,
The vanadium of 0.03-0.3%,
The copper of 0.3-1.0%,
<0.15% niobium,
The titanium of 0.007-0.015%,
The nitrogen of 0.005-0.017%,
The iron of surplus and impurity.
2, alloy as claimed in claim 1 comprises
The carbon of 3.3-3.4%,
The silicon of 1.8-2.2%,
<0.1% sulphur,
<0.05% phosphorus,
The manganese of 0.4-0.6%,
The chromium of 0.2-0.4%,
The molybdenum of 0.2-0.3% and
The vanadium of 0.05-0.1%.
3, alloy as claimed in claim 1 or 2 is characterised in that vanadium exists to be lower than 0.1% amount.
4, alloy as claimed in claim 1 or 2 is characterised in that aluminium exists to be lower than 0.01% amount.
5, alloy as claimed in claim 1 or 2 is characterised in that nickel exists to be lower than 0.1% amount.
6, alloy as claimed in claim 1 or 2 is characterised in that tin exists to be lower than 0.1% amount.
7, a kind of oil engine casting engine parts, it is made by the grey cast iron alloy of pearly-lustre basically, and described alloy comprises:
The carbon of 3.2-3.49%,
The silicon of 1.8-2.2%,
<0.15% sulphur,
<0.15% phosphorus,
The manganese of 0.3-0.8%,
The chromium of 0.2-0.4%,
The molybdenum of 0.1-0.4%,
The vanadium of 0.03-0.3%,
The copper of 0.3-1.0%,
The titanium of 0.007-0.013%,
<0.15% niobium,
The nitrogen of 0.005-0.015%,
<0.01% aluminium,
The iron of surplus and impurity.
8, parts as claimed in claim 7 are characterised in that it is engine body parts or cylinder head sub-assembly.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0201431A SE526903C2 (en) | 2002-05-13 | 2002-05-13 | Gray iron alloy and cast internal combustion engine component |
SE02014314 | 2002-05-13 |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1653202A CN1653202A (en) | 2005-08-10 |
CN1320150C true CN1320150C (en) | 2007-06-06 |
Family
ID=20287840
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNB03811027XA Expired - Fee Related CN1320150C (en) | 2002-05-13 | 2003-05-12 | Gray cast iron alloy and cast internal combustion engine component |
Country Status (13)
Country | Link |
---|---|
EP (1) | EP1506323B1 (en) |
JP (1) | JP4137054B2 (en) |
KR (1) | KR100616649B1 (en) |
CN (1) | CN1320150C (en) |
AT (1) | ATE477347T1 (en) |
AU (1) | AU2003243063A1 (en) |
BR (1) | BR0309975B1 (en) |
DE (1) | DE60333748D1 (en) |
DK (1) | DK1506323T3 (en) |
ES (1) | ES2350478T3 (en) |
SE (1) | SE526903C2 (en) |
SI (1) | SI1506323T1 (en) |
WO (1) | WO2003095692A1 (en) |
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SE0300752L (en) | 2003-03-19 | 2004-09-20 | Volvo Lastvagnar Ab | Gray iron for engine cylinder blocks and top caps |
DE102004010917C5 (en) | 2004-03-05 | 2018-05-17 | Federal-Mogul Burscheid Gmbh | Cast iron material with high strength |
KR100656470B1 (en) | 2006-02-07 | 2006-12-11 | 주식회사 하이닉스반도체 | Driver control device and method for semiconductor memory |
US8333923B2 (en) * | 2007-02-28 | 2012-12-18 | Caterpillar Inc. | High strength gray cast iron |
FR2948744B1 (en) * | 2009-07-29 | 2015-04-24 | Peugeot Citroen Automobiles Sa | CYLINDER SHOE FOR THE CUTTING OF THE CYLINDRICAL WALL OF A CYLINDER OF AN INTERNAL COMBUSTION ENGINE |
CN102465230A (en) * | 2010-11-17 | 2012-05-23 | 常州朗锐活塞有限公司 | Alloy cast iron piston material |
SE535043C2 (en) * | 2010-12-02 | 2012-03-27 | Scania Cv Ab | Gray iron alloy and brake disc including gray iron alloy |
CN102409246B (en) * | 2011-12-09 | 2013-01-02 | 河南省中原内配股份有限公司 | Bainite cylinder jacket lining and preparation method thereof |
EP2816127B1 (en) * | 2012-02-17 | 2017-03-15 | Honda Motor Co., Ltd. | Cast iron and brake part |
CN102864369A (en) * | 2012-09-05 | 2013-01-09 | 陈敏 | Anti-fatigue cast iron alloy |
CN102876963A (en) * | 2012-09-05 | 2013-01-16 | 忻峰 | Anti-fatigue cast iron alloy |
CN102851567A (en) * | 2012-09-14 | 2013-01-02 | 虞海香 | Cast iron alloy |
CN102864370A (en) * | 2012-09-14 | 2013-01-09 | 黄宣斐 | Grey cast iron alloy material |
CN102864367A (en) * | 2012-09-14 | 2013-01-09 | 虞海盈 | Gray cast iron alloy |
CN103572150A (en) * | 2013-10-12 | 2014-02-12 | 广西玉柴机器股份有限公司 | Engine air cylinder cover gray cast iron |
CN104561750B (en) * | 2013-10-25 | 2016-08-17 | 河南星鹏铸件有限责任公司 | Ferrum liquid and the casting method of pressure disc foundry goods for casting pressure dish foundry goods |
CN103834852A (en) * | 2014-03-19 | 2014-06-04 | 四川大学 | A kind of tin-niobium composite alloy gray cast iron and its production process |
CN104313456A (en) * | 2014-10-20 | 2015-01-28 | 熊荣鑫 | Anti-fatigue iron alloy |
CN104962839A (en) * | 2015-05-22 | 2015-10-07 | 南京飞燕活塞环股份有限公司 | Piston ring material high in wear resistance, fracture resistance, and hardness |
CN104962820A (en) * | 2015-06-11 | 2015-10-07 | 龙口市和义机械配件有限公司 | Alloy steel for racing car brake disc and preparation method of alloy steel |
KR101794876B1 (en) | 2016-09-05 | 2017-11-07 | 티피알 가부시키가이샤 | Cylindrical member made of flake graphite cast iron |
CN108070778A (en) * | 2016-11-18 | 2018-05-25 | 山东恒圆精工部件股份有限公司 | Piston ring cast-iron alloy and its manufacturing method |
CN107119221B (en) * | 2017-04-26 | 2018-08-07 | 含山县朝霞铸造有限公司 | A kind of micro alloyed high strength grey cast iron part and its method of smelting |
CN108913985A (en) * | 2018-06-06 | 2018-11-30 | 东风商用车有限公司 | High-carbon-equivalent high-strength gray cast iron and preparation method thereof |
CN109182890B (en) * | 2018-10-19 | 2020-05-26 | 中车大连机车车辆有限公司 | Gray cast iron and smelting method thereof |
CN110079726B (en) * | 2019-06-01 | 2021-04-06 | 亚新科国际铸造(山西)有限公司 | Process for improving normal-temperature tension-compression fatigue strength of gray cast iron engine cylinder cover |
CN111334705A (en) * | 2020-04-07 | 2020-06-26 | 中原内配集团股份有限公司 | High-strength pearlite antifriction cast iron and preparation method and application thereof |
US11879168B2 (en) * | 2021-08-31 | 2024-01-23 | GM Global Technology Operations LLC | High-modulus, high-strength, low alloy gray cast iron for cylinder liners and automotive applications |
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2002
- 2002-05-13 SE SE0201431A patent/SE526903C2/en unknown
-
2003
- 2003-05-12 JP JP2004503680A patent/JP4137054B2/en not_active Expired - Fee Related
- 2003-05-12 CN CNB03811027XA patent/CN1320150C/en not_active Expired - Fee Related
- 2003-05-12 BR BRPI0309975-0A patent/BR0309975B1/en not_active IP Right Cessation
- 2003-05-12 AU AU2003243063A patent/AU2003243063A1/en not_active Abandoned
- 2003-05-12 DE DE60333748T patent/DE60333748D1/en not_active Expired - Lifetime
- 2003-05-12 SI SI200331893T patent/SI1506323T1/en unknown
- 2003-05-12 AT AT03750007T patent/ATE477347T1/en active
- 2003-05-12 WO PCT/SE2003/000770 patent/WO2003095692A1/en active Application Filing
- 2003-05-12 EP EP03750007A patent/EP1506323B1/en not_active Expired - Lifetime
- 2003-05-12 KR KR1020047018233A patent/KR100616649B1/en not_active IP Right Cessation
- 2003-05-12 ES ES03750007T patent/ES2350478T3/en not_active Expired - Lifetime
- 2003-05-12 DK DK03750007.1T patent/DK1506323T3/en active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1051396A (en) * | 1990-12-07 | 1991-05-15 | 济南钢铁总厂 | A kind of thermal fatigue resistance graphitic cast iron that goes bad |
US5242510A (en) * | 1992-09-25 | 1993-09-07 | Detroit Diesel Corporation | Alloyed grey iron having high thermal fatigue resistance and good machinability |
CN1100150A (en) * | 1993-09-09 | 1995-03-15 | 株洲市机械工业研究所 | Impact fatigue-resistant wear-proof alloy cast iron |
US5972128A (en) * | 1996-02-28 | 1999-10-26 | Kabushiki Kaisha Riken | Cast iron and piston ring |
Also Published As
Publication number | Publication date |
---|---|
SE0201431D0 (en) | 2002-05-13 |
CN1653202A (en) | 2005-08-10 |
KR100616649B1 (en) | 2006-08-28 |
BR0309975B1 (en) | 2010-12-14 |
SE526903C2 (en) | 2005-11-15 |
JP4137054B2 (en) | 2008-08-20 |
ATE477347T1 (en) | 2010-08-15 |
SI1506323T1 (en) | 2011-01-31 |
EP1506323B1 (en) | 2010-08-11 |
AU2003243063A1 (en) | 2003-11-11 |
SE0201431L (en) | 2003-11-14 |
ES2350478T3 (en) | 2011-01-24 |
JP2005525468A (en) | 2005-08-25 |
KR20050010796A (en) | 2005-01-28 |
DE60333748D1 (en) | 2010-09-23 |
DK1506323T3 (en) | 2010-11-22 |
BR0309975A (en) | 2005-02-22 |
WO2003095692A1 (en) | 2003-11-20 |
EP1506323A1 (en) | 2005-02-16 |
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