WO2011111615A1 - シリンダブロックの加工方法、シリンダブロック及び溶射用シリンダブロック - Google Patents
シリンダブロックの加工方法、シリンダブロック及び溶射用シリンダブロック Download PDFInfo
- Publication number
- WO2011111615A1 WO2011111615A1 PCT/JP2011/055029 JP2011055029W WO2011111615A1 WO 2011111615 A1 WO2011111615 A1 WO 2011111615A1 JP 2011055029 W JP2011055029 W JP 2011055029W WO 2011111615 A1 WO2011111615 A1 WO 2011111615A1
- Authority
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- WIPO (PCT)
- Prior art keywords
- cylinder bore
- cylinder
- protrusion
- cylinder block
- crankcase
- Prior art date
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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
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/18—After-treatment
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
- C23C4/14—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying for coating elongate material
-
- 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
-
- 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
- F02F1/004—Cylinder 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
- F02F7/0021—Construction
-
- 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
- F02F7/0095—Constructing engine casings
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49231—I.C. [internal combustion] engine making
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/4927—Cylinder, cylinder head or engine valve sleeve making
Definitions
- the present invention relates to a cylinder block processing method for forming a spray coating on the inner surface of a cylinder bore, a cylinder block having a spray coating, and a cylinder block for spraying.
- a spraying gun for spraying the spraying material is rotated while moving in the axial direction into the cylinder bore to form a sprayed coating. Thereafter, for example, the surface of the coating is ground by a honing process and finished.
- Patent Document 1 in order to suppress peeling of the spray coating, particularly the crankcase end, the crankcase end on the inner surface of the cylinder bore is removed. That is, after the sprayed coating is formed, the inner surface of the cylinder bore is removed including the end of the sprayed coating on the crankcase side so that the inner diameter of the cylinder bore at the end of the sprayed coating on the crankcase side is increased.
- An object of the present invention is to ensure a sufficient removal allowance while achieving downsizing of the cylinder block when removing the sprayed coating including the sprayed coating on the crankcase side end of the cylinder bore. It is in.
- a protrusion projecting toward the crankcase side is provided at an end portion of the cylinder bore on the crankcase side, and the protrusions continuous with the inner surface of the cylinder bore and the inner surface of the cylinder bore are provided.
- a cylinder block according to a second aspect of the present invention is provided with a cylinder, an end of the cylinder bore on the crankcase side of the cylinder, a protrusion protruding toward the crankcase, an inner surface of the cylinder bore, and an inner surface of the cylinder bore And a thermal spray coating formed on the inner surface of the projection that is continuous with the projection. And at least one part of the said protrusion is removed with the sprayed coating formed in the inner surface of the said protrusion.
- the cylinder block for thermal spraying is a cylinder block that forms a thermal spray coating on the inner surface of the cylinder bore.
- the cylinder block for thermal spraying includes a cylinder and a protrusion provided on an end of the cylinder bore on the crankcase side of the cylinder and protruding toward the crankcase side. And as for the said protrusion, the thickness of the front-end
- FIG. 1 is a cross-sectional view of a cylinder block showing an embodiment of the present invention.
- FIG. 2 is a manufacturing process diagram of the cylinder block of FIG.
- FIG. 3 is an operation explanatory view at the time of rough surface processing (b) in the manufacturing process of FIG.
- FIG. 4 is an enlarged cross-sectional view of a portion IV in FIG.
- an engine cylinder block 1 has a structure in which a cylinder 2 and a crankcase 9 are integrated. Further, the cylinder block 1 has a sprayed coating 5 formed on the inner surface of the cylinder bore 3.
- the cylinder block 1 can be formed from cast iron, an aluminum alloy, or the like, and the thermal spray coating 5 can be formed from an iron-based metal material.
- a rough surface 7 having an uneven shape is formed in advance on the base portion of the cylinder block 1 on which the thermal spray coating 5 is formed. The rough surface 7 enhances the adhesion of the thermal spray coating 5 to the inner surface of the cylinder bore 3.
- the protrusion 11 which protrudes toward the crankcase 9 side along the axial direction of the cylinder bore 3 is formed in the edge part by the side of the crankcase 9 of the cylinder bore 3. As shown in FIG.
- the protrusion 11 is formed in an annular shape over the entire circumference of the cylinder bore 3.
- the thermal spray coating 5 is also continuously formed on the inner surface of the protrusion 11.
- the protrusion 11 is obtained by forming the thermal spray coating 5 and then removing the tip portion 11a having a substantially triangular cross section by machining as a machining allowance. Further, the sprayed coating 5 a is also formed on the tip 11 a of the protrusion 11 continuously from the sprayed coating 5 on the inner surface of the cylinder bore 3. In the drawing, the tip end portion 11a is indicated by a two-dot chain line.
- the thermal spray coating 5 has a low degree of adhesion, particularly in the axial end of the cylinder bore 3 compared to other parts. Therefore, by removing the tip portion 11a of the protrusion 11 together with the thermal spray coating 5a, it is possible to reduce the number of portions with low adhesion and to increase the adhesion as a whole.
- FIG. 2 shows only the left side portion of the cylinder 2 in FIG.
- FIG. 2A shows a state after the cylinder block 1 is cast.
- a projection 11 is formed at the end of the cylinder bore 3 on the crankcase 9 side before the tip 11a is removed.
- the inner surface 11b is continuous in the axial direction with respect to the inner surface 3a of the cylinder bore 3, and constitutes the axial end portion of the cylinder bore 3. Therefore, the protrusion 11 and the inner surface 11b are formed in an annular shape.
- an inclined surface 11c is formed on the opposite side of the protrusion 11 from the inner surface 11b.
- the inclined surface 11c is inclined so that the tip end side of the protrusion 11 is directed toward the radial center of the cylinder bore 3.
- the inclined surface 11 c is also formed in an annular shape over the entire circumference of the cylinder bore 3.
- the protrusion 11 has the thickest thickness L at the base end portion that contacts the cylinder 2 or the crankcase 9, and the tip portion (the lower end side in FIG. 2A) is thinner.
- the minimum value of the wall thickness L is 4 mm
- the minimum value of the protrusion height H is 1.3 mm + [film thickness of sprayed coating after finishing / tan (chamfering angle)]. .
- the chamfer angle corresponds to the angle ⁇ in FIG.
- the rough surface 7 is formed by subjecting the inner surface 3a of the cylinder bore 3 of FIG.
- the degree of adhesion of the thermal spray coating 5 formed thereafter to the inner surface 3 a of the cylinder bore 3 is increased.
- the base rough surface processing can be performed using a boring apparatus.
- a tool (blade) 15 is mounted on the outer periphery of the tip of the boring bar 13 can be used.
- the boring bar 13 is rotated and moved downward in the axial direction, whereby the inner surface 3a of the cylinder bore 3 and the inner surface 11b of the projection 11 are formed into a screw shape.
- the rough surface 7 which consists of unevenness
- the sprayed coating 5 is formed on the inner surface 3a of the cylinder bore 3 and the inner surface 11b of the protrusion 11.
- the thermal spray coating 5 is formed on the inner surface 3a of the cylinder bore 3 and the inner surface 11b of the protrusion 11 so as to have a substantially uniform thickness.
- the thermal spraying method the method described in Patent Document 1 and the like can be used, but is not limited to this method.
- the tip end portion 11a which is a removal processed portion of the protrusion 11, is removed as shown in FIG. 2D.
- the processing method is not particularly limited, and processing from the crankcase 9 side is also possible.
- a finishing process such as a honing process is performed on the surface of the thermal spray coating 5.
- the cylinder bore inner surface side 11e is opposed to the cylinder bore inner surface 3a and the radially opposite side 11f. 3 is inclined so as to be opposite to the crankcase 9 in the axial direction. That is, the end surface 11d in FIG. 4 is inclined so that the right end portion 11e is above the left end portion 11f in the axial direction of the cylinder bore 3.
- Such a shape of the end surface 11 d extends over the entire circumference of the cylinder bore 3.
- the angle ⁇ formed between the inner surface of the cylinder bore 3 (more precisely, the surface of the thermal spray coating 5) and the end surface 11d becomes an obtuse angle.
- the end surface 11d may be a horizontal surface (a surface perpendicular to the axis of the cylinder bore 3) without being inclined.
- the end portion on the crankcase 9 side particularly the end portion in the axial direction of the cylinder bore 3, has a lower degree of adhesion than other portions. It has become a thing.
- the end of the cylinder bore 3 on the crankcase 9 side is provided with a protrusion 11.
- the thermal spray coating 5 having a low degree of adhesion is removed together with the ground. Therefore, the adhesion degree of the thermal spray coating 5 to the cylinder bore 3 can be increased as a whole, and a high-quality cylinder block 1 can be obtained.
- the removal processing part is set to a protrusion 11 protruding from the cylinder bore 3 toward the crankcase 9. That is, the protrusion 11 is merely projected into the space in the crankcase 9. For this reason, even if it provides the protrusion 11 which is a removal process site
- the protrusion 11 has a smaller volume while increasing the rigidity of the protrusion 11 by making the thickness of the distal end portion thinner than the base end portion.
- the rigidity of the protrusions 11 it is possible to suppress the deformation of the protrusions 11 during the rough surface processing shown in FIG. 3.
- the removal machining allowance becomes smaller, the time spent for the removal processing can be shortened, and as a result, the manufacturing cost can be reduced.
- the end surface 11d of the protrusion 11 after the removal of the leading end portion 11a is such that the cylinder bore inner surface side 11e is crankshaft in the axial direction of the cylinder bore 3 with respect to the side 11f opposite to the cylinder bore inner surface 3a. It is inclined to be opposite to 9. As shown in FIG. 4, the inclined end surface 11 d of the projection 11 is formed from the base of the cylinder bore 3 to the surface of the thermal spray coating 5. Therefore, the angle ⁇ formed between the inner surface of the cylinder bore 3 (more precisely, the surface of the thermal spray coating 5) and the end surface 11d becomes an obtuse angle as shown in FIG.
- the base portion on the cylinder block main body side of the sprayed coating 5 protrudes toward the crankcase 9 in the axial direction of the cylinder bore 3. For this reason, the sprayed coating 5 will adhere more stably to the underlying portion, and damage (peeling or chipping) of the sprayed coating 5 can be suppressed.
- an inclined surface 11c serving as an inner wall facing surface facing the inner wall 9a of the crankcase 9 is provided on the side opposite to the cylinder bore inner surface 3a in the protrusion 11 after removing the leading end portion 11a which is the machining allowance. Yes.
- the oil that is swept along the inner wall 9a due to the rotation of the crankshaft (not shown) enters the cylinder bore 3 more than necessary by the inclined surface 11c. Suppress.
- the amount of oil consumed in the bore 3 can be reduced. Therefore, the maintenance cost of the user can be reduced, and the amount of oil contained in the exhaust gas can be reduced to clean the exhaust properties of the engine.
- the inner wall facing surface of the projection 11 facing the inner wall 9a is an inclined surface 11c that is inclined so as to be closer to the radial center of the cylinder bore 3 toward the tip end side. As a result, it is possible to more reliably suppress the raked oil from flowing down more smoothly and entering the cylinder bore 3.
- the protrusion 11 is made thinner at the tip than at the base end, the entire thickness may be equal.
- the inclined surface 11 c in FIG. 2A is an inner wall facing surface parallel to the axial direction of the cylinder bore 3. Even if the inner wall facing surface is a parallel surface, it is possible to prevent the oil scooped along the inner wall 9a from entering the cylinder bore 3 more than necessary.
- the removal processing part at the crankcase side end of the cylinder bore for suppressing the peeling of the sprayed coating is a protrusion protruding from the inner surface of the cylinder bore toward the crankcase side. Therefore, when removing the end of the cylinder bore on the crankcase side including the thermal spray coating, a sufficient removal allowance can be secured while achieving downsizing of the cylinder block.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
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- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Coating By Spraying Or Casting (AREA)
Abstract
Description
3 シリンダボア
3a シリンダボアの内面
5 溶射皮膜
5a 突起の先端部における溶射皮膜
9 クランクケース
9a クランクケースの内壁
11 突起
11a 突起の先端部(突起の一部)
11b 突起の内面
11c 突起の内面と反対側の傾斜面(内壁対向面)
11d 先端部を除去した後の突起の端面
Claims (13)
- シリンダボアのクランクケース側の端部に、前記クランクケース側に突出する突起を設け、前記シリンダボアの内面及び前記シリンダボア内面に連続する前記突起の内面に溶射皮膜を形成する工程と、
前記溶射皮膜の形成後に、前記突起の少なくとも一部を前記突起の内面に形成した溶射皮膜と共に除去する工程と、
を有することを特徴とするシリンダブロックの加工方法。 - 前記突起は、基端部よりも先端部の肉厚が薄くなっていることを特徴とする請求項1に記載のシリンダブロックの加工方法。
- 前記少なくとも一部を除去した後の突起の端面は、シリンダボア内面側が、シリンダボア内面と反対側に対し、前記シリンダボアの軸方向で前記クランクケースと反対側となるように傾斜していることを特徴とする請求項1又は2に記載のシリンダブロックの加工方法。
- 前記傾斜している突起の端面は、前記シリンダボアの下地から前記溶射皮膜にわたり形成されていることを特徴とする請求項3に記載のシリンダブロックの加工方法。
- 前記少なくとも一部を除去した後の突起のシリンダボア内面と反対側に、前記クランクケースの内壁に対向する内壁対向面を備えていることを特徴とする請求項1乃至4のいずれか1項に記載のシリンダブロックの加工方法。
- 前記突起の内壁対向面は、先端側ほどシリンダボアの径方向中心側となるように傾斜していることを特徴とする請求項5に記載のシリンダブロックの加工方法。
- シリンダと、
前記シリンダにおけるシリンダボアのクランクケース側の端部に設けられ、前記クランクケース側に突出する突起と、
前記シリンダボアの内面及び前記シリンダボアの内面に連続する前記突起の内面に形成された溶射皮膜と、
を備え、
前記突起の少なくとも一部が前記突起の内面に形成した溶射皮膜と共に除去されていることを特徴とするシリンダブロック。 - 前記突起は、基端部よりも先端部の肉厚が薄くなっていることを特徴とする請求項7に記載のシリンダブロック。
- 前記少なくとも一部を除去した後の突起の端面は、シリンダボア内面側が、シリンダボア内面と反対側に対し、シリンダボアの軸方向で前記クランクケースと反対側となるように傾斜していることを特徴とする請求項7又は8に記載のシリンダブロック。
- 前記傾斜している突起の端面は、前記シリンダボアの下地から前記溶射皮膜にわたり形成されていることを特徴とする請求項9に記載のシリンダブロック。
- 前記少なくとも一部を除去した後の突起のシリンダボア内面と反対側に、前記クランクケースの内壁に対向する内壁対向面を備えていることを特徴とする請求項7乃至10のいずれか1項に記載のシリンダブロック。
- 前記突起の内壁対向面は、先端側ほどシリンダボアの径方向中心側となるように傾斜していることを特徴とする請求項11に記載のシリンダブロック。
- シリンダボアの内面に溶射皮膜を形成する溶射用シリンダブロックであって、
シリンダと、
前記シリンダにおけるシリンダボアのクランクケース側の端部に設けられ、前記クランクケース側に突出する突起と、
を備え、
前記突起は、基端部よりも先端部の肉厚が薄くなっていることを特徴とする溶射用シリンダブロック。
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/576,086 US8794207B2 (en) | 2010-03-11 | 2011-03-04 | Method for processing cylinder block, cylinder block and thermal-sprayed cylinder block |
CN201180007805.3A CN102741534B (zh) | 2010-03-11 | 2011-03-04 | 缸体的加工方法、缸体及喷镀用缸体 |
EP11753274.7A EP2546503B1 (en) | 2010-03-11 | 2011-03-04 | Method for machining cylinder block, cylinder block, and cylinder block for thermal spraying |
RU2012143405/02A RU2516211C1 (ru) | 2010-03-11 | 2011-03-04 | Способ обработки блока цилиндров, блок цилиндров и блок цилиндров с термическим напылением |
MX2012009161A MX345396B (es) | 2010-03-11 | 2011-03-04 | Método para el maquinado de bloque de cilindros, bloque de cilindros y bloque de cilindros para pulverización térmica. |
BR112012022689A BR112012022689B8 (pt) | 2010-03-11 | 2011-03-04 | Bloco de cilindro e método para o processamento de um bloco de cilindro |
KR1020127026484A KR101420955B1 (ko) | 2010-03-11 | 2011-03-04 | 실린더 블럭의 가공 방법, 실린더 블럭 및 용사용 실린더 블럭 |
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JP2010054403A JP5499790B2 (ja) | 2010-03-11 | 2010-03-11 | シリンダブロックの加工方法、シリンダブロック及び溶射用シリンダブロック |
JP2010-054403 | 2010-03-11 |
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WO2011111615A1 true WO2011111615A1 (ja) | 2011-09-15 |
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Country Status (9)
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US (1) | US8794207B2 (ja) |
EP (1) | EP2546503B1 (ja) |
JP (1) | JP5499790B2 (ja) |
KR (1) | KR101420955B1 (ja) |
CN (1) | CN102741534B (ja) |
BR (1) | BR112012022689B8 (ja) |
MX (1) | MX345396B (ja) |
RU (1) | RU2516211C1 (ja) |
WO (1) | WO2011111615A1 (ja) |
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JP5962078B2 (ja) * | 2012-03-06 | 2016-08-03 | 日産自動車株式会社 | シリンダブロック及び溶射前処理方法 |
DE102016116815A1 (de) * | 2016-09-08 | 2018-03-08 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Verfahren zur Beschichtung eines Zylinders einer Verbrennungskraftmaschine und Zylinder für eine Verbrennungskraftmaschine |
WO2018215054A1 (de) * | 2017-05-23 | 2018-11-29 | Gühring KG | Verfahren und werkzeug zum entfernen einer beschichtung von einem substrat |
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CN100529153C (zh) | 2006-03-07 | 2009-08-19 | 日产自动车株式会社 | 基础构件、筒状内表面处理方法及其处理设备 |
JP4710802B2 (ja) | 2006-03-07 | 2011-06-29 | 日産自動車株式会社 | 円形の穴内面を備えた部材,円形の穴内面の加工方法および加工装置 |
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- 2011-03-04 CN CN201180007805.3A patent/CN102741534B/zh active Active
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Publication number | Priority date | Publication date | Assignee | Title |
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JP2007056793A (ja) * | 2005-08-25 | 2007-03-08 | Toyota Motor Corp | シリンダブロック及びシリンダブロックの製造方法 |
JP2007211307A (ja) | 2006-02-10 | 2007-08-23 | Nissan Motor Co Ltd | 円筒内面の加工方法および円筒部材 |
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RU2516211C1 (ru) | 2014-05-20 |
EP2546503A4 (en) | 2015-04-22 |
MX2012009161A (es) | 2012-08-23 |
BR112012022689B1 (pt) | 2020-12-29 |
US20120304955A1 (en) | 2012-12-06 |
KR20120130249A (ko) | 2012-11-29 |
CN102741534B (zh) | 2014-07-02 |
EP2546503A1 (en) | 2013-01-16 |
MX345396B (es) | 2017-01-30 |
BR112012022689A2 (pt) | 2018-05-22 |
KR101420955B1 (ko) | 2014-07-17 |
JP2011185246A (ja) | 2011-09-22 |
EP2546503B1 (en) | 2016-10-19 |
BR112012022689B8 (pt) | 2023-02-14 |
US8794207B2 (en) | 2014-08-05 |
CN102741534A (zh) | 2012-10-17 |
JP5499790B2 (ja) | 2014-05-21 |
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