WO2013161528A1 - Engine combustion chamber structure - Google Patents
Engine combustion chamber structure Download PDFInfo
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- WO2013161528A1 WO2013161528A1 PCT/JP2013/060194 JP2013060194W WO2013161528A1 WO 2013161528 A1 WO2013161528 A1 WO 2013161528A1 JP 2013060194 W JP2013060194 W JP 2013060194W WO 2013161528 A1 WO2013161528 A1 WO 2013161528A1
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- WIPO (PCT)
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- combustion chamber
- film
- boehmite
- heat
- piston
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- 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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/04—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B77/00—Component parts, details or accessories, not otherwise provided for
- F02B77/02—Surface coverings of combustion-gas-swept parts
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B77/00—Component parts, details or accessories, not otherwise provided for
- F02B77/11—Thermal or acoustic insulation
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- 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
- F02F3/00—Pistons
- F02F3/10—Pistons having surface coverings
- F02F3/12—Pistons having surface coverings on piston heads
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- 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
- F02F3/00—Pistons
- F02F3/10—Pistons having surface coverings
- F02F3/12—Pistons having surface coverings on piston heads
- F02F3/14—Pistons having surface coverings on piston heads within combustion chambers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0603—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston at least part of the interior volume or the wall of the combustion space being made of material different from the surrounding piston part, e.g. combustion space formed within a ceramic part fixed to a metal piston head
- F02B2023/0612—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston at least part of the interior volume or the wall of the combustion space being made of material different from the surrounding piston part, e.g. combustion space formed within a ceramic part fixed to a metal piston head the material having a high temperature and pressure resistance, e.g. ceramic
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2251/00—Material properties
- F05C2251/04—Thermal properties
- F05C2251/048—Heat transfer
Definitions
- the present invention relates to a combustion chamber structure for an engine having a combustion chamber defined by a cylinder bore, a cylinder head lower surface, and a piston top.
- the combustion chamber of a diesel engine is generally defined by a cylinder bore, the lower surface of the cylinder head, and the top of the piston.
- a cavity is recessed at the top of the piston, and fuel is injected into the cavity from a fuel injection valve disposed above the piston.
- Patent Document 1 Such a combustion chamber structure of a diesel engine is disclosed in Patent Document 1, for example.
- a heat insulation paint or a heat insulation paint is applied to the heat insulation object as a method for simply insulating the heat insulation object.
- thermal insulation paint or thermal barrier paint When applying thermal insulation paint or thermal barrier paint to the wall surface of the combustion chamber, it is necessary to firmly bond the thermal insulation paint or thermal insulation paint to the wall surface of the combustion chamber because the flame hits the thermal insulation paint or thermal insulation paint during fuel combustion. There is.
- an object of the present invention is to firmly apply a heat insulating paint or a heat insulating paint (heat insulating film) to the wall of the combustion chamber when forming a heat insulating film by applying a heat insulating paint or a heat insulating paint on the wall of the combustion chamber. It is to be combined.
- a combustion chamber structure of an engine according to the present invention includes a combustion chamber defined by a cylinder bore, a cylinder head lower surface, and a piston top, and at least a part of the wall surface of the combustion chamber is made of aluminum or
- a heat shielding film formed by applying a heat insulating paint or a heat shielding paint.
- the boehmite film may be formed on the wall surface of the combustion chamber by performing a boehmite treatment on the wall surface of the combustion chamber.
- the heat-insulating paint or heat-shielding paint when forming a heat-shielding film by applying a heat-insulating paint or a heat-shielding paint on the wall surface of the combustion chamber, the heat-insulating paint or heat-shielding paint (heat-shielding film) is firmly bonded to the wall surface of the combustion chamber. There is an excellent effect of being able to.
- (A) is the schematic of the combustion chamber structure of the engine which concerns on one Embodiment of this invention
- (b) is the A section enlarged view of (a). It is the schematic of the combustion chamber structure of the engine which concerns on other embodiment of this invention.
- FIG. 1 shows a combustion chamber structure of an engine according to an embodiment of the present invention.
- an engine 10 in this embodiment, a diesel engine 10 includes a cylinder bore 12 formed in a cylinder block 11, and a piston made of aluminum or aluminum alloy that reciprocates up and down in the cylinder bore 12. 13, and a cylinder head 15 made of aluminum or aluminum alloy attached to the upper part of the cylinder block 11 with a gasket 14 interposed therebetween.
- a space surrounded by the cylinder bore 12, the lower surface of the cylinder head 15, and the top of the piston 13 forms a combustion chamber 16.
- the cylinder head 15 has an intake / exhaust port (intake port 17 and exhaust port 18) communicating with the combustion chamber 16, an intake valve 19 that opens and closes the intake port 17, an exhaust valve 20 that opens and closes the exhaust port 18, and fuel.
- a fuel injection valve (injector) 21 for injecting the combustion chamber 16 from above is provided.
- a cavity in the illustrated example, a cavity with a lip
- 13 b is formed in the top surface 13 a of the piston 13.
- the fuel in the combustion chamber 16 is automatically injected by injecting the fuel from the fuel injection valve 21 into the combustion chamber 16. Ignite and burn.
- a plurality of nozzle holes 22 are provided at the tip of the fuel injection valve 21, and each nozzle 22 is configured so that the fuel injected from the nozzle 22 near the compression top dead center of the piston 13 is directed toward the lip 13c of the cavity 13b. It is oriented.
- a heat shield film 23 for suppressing heat transfer from the combustion gas in the combustion chamber 16 to the piston 13 is formed on the top of the piston 13 forming the combustion chamber 16. More specifically, the thermal barrier film 23 is formed over the entire circumference on the top surface 13a of the piston 13 and a part of the cavity 13b (in the figure, in the vicinity of the lip portion 13c of the cavity 13b).
- the boehmite treatment is performed as an anchor treatment (pretreatment before applying the paint) for the thermal barrier film 23. That is, in this embodiment, by performing a boehmite treatment on the surface of the piston 13, a boehmite film 24 is formed on the surface of the piston 13, and by applying a heat insulating paint or a thermal barrier paint on the boehmite film 24, A thermal barrier film 23 is formed on the boehmite film 24 (see FIG. 1B).
- boehmite treatment the surface of the base (aluminum or aluminum alloy) and the like blowing hot steam (distilled water), an alumina 1 represented by a composition of Al 2 O 3 ⁇ H 2 O on the surface of the base It forms hydrates (boehmite).
- the boehmite treatment may be performed by adding a small amount of an additive such as aqueous ammonia to high-temperature distilled water.
- This boehmite treatment is mainly performed as an antirust treatment for aluminum.
- alumina monohydrate (boehmite) formed by boehmite treatment has a needle-like crystal structure.
- the thickness (film thickness) Ta (see FIG. 1B) of the heat shield film 23 is, for example, about 100 ⁇ m. Further, the thickness (film thickness) Tb (see FIG. 1B) of the boehmite film 24 is, for example, about 0.1 ⁇ m to 10 ⁇ m.
- the boehmite film 24 is formed on the surface of the piston 13 by performing a boehmite treatment on the surface of the piston 13, and the boehmite film is applied to the boehmite film 24 by applying a heat insulating paint or a thermal barrier paint.
- a heat shield film 23 is formed on the film 24.
- the heat-insulating paint or the heat-shielding paint applied on the boehmite film 24 can penetrate into the boehmite film 24 firmly and deeply.
- the bonding force between the heat insulating paint or the heat insulating paint (heat insulating film 23) and the surface of the piston 13 becomes very strong. Therefore, when forming the heat shield film 23 by applying a heat insulating paint or a heat insulating paint on the surface of the piston 13, the heat insulating paint or the heat insulating paint (heat insulating film 23) may be firmly bonded to the surface of the piston 13. It becomes possible.
- the boehmite film 24 is chemically bonded to the surface of the piston 13 which is a base material (aluminum or aluminum alloy), the boehmite film 24 itself is firmly bonded to the surface of the piston 13. Therefore, by performing the boehmite treatment as the anchor treatment for the heat shield film 23, the heat insulating paint or the heat shield paint (heat shield film 23) is bonded to the surface of the piston 13 more firmly than when the anchor treatment is not performed. be able to.
- the heat shielding film 23 is formed on the top of the piston 13, but this is not a limitation, and as shown in FIG. 2, the lower surface of the cylinder head 15 that forms the combustion chamber 16 is formed. It is also possible to form the heat shield film 23.
- the thermal barrier film 23 may be formed only on the portion of the lower surface of the cylinder head 15 that faces the combustion chamber 16.
- the heat shield film 23 may be formed on the entire lower surface of the cylinder head 15. In either case, the boehmite treatment is performed as an anchor treatment for the thermal barrier film 23, and the boehmite film 24 is formed on the surface of the cylinder head 15.
- the heat shield film 23 is formed on a part of the top surface 13 a and the cavity 13 b of the piston 13.
- the present invention is not limited to this, and the heat shield film 23 is formed on the top of the piston 13.
- a heat shielding film 23 may be formed on the entire top surface 13 a and the cavity 13 b of the piston 13.
- the boehmite process is performed as an anchor process for the heat shield film 23, and the boehmite film 24 is formed on the surface of the piston 13.
- the engine 10 is not limited to a diesel engine, and may be a gasoline engine or the like. Further, the engine 10 is not limited to a direct injection type, and may be a spark ignition type.
- the shape of the cavity 13b recessed at the top of the piston 13, in the case of a diesel engine is not limited to a lip type, and may be a reentrant type or a toroidal type.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Acoustics & Sound (AREA)
- Physics & Mathematics (AREA)
- Inorganic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
In the present invention, when forming a heat shield film by means of applying a heat insulating coating material or a heat shielding coating material to the wall surface of a combustion chamber, the heat insulating coating material or heat shielding coating material (heat shield film) is strongly bonded to the wall surface of the combustion chamber. This engine (10) combustion chamber structure is provided with a combustion chamber (16) demarcated by a cylinder bore (12), a cylinder head (15) bottom surface, and a piston (13) apex, and at least a portion of the wall surface of the combustion chamber (16) is configured from aluminum or an aluminum alloy. The engine (10) combustion chamber structure is provided with: a boehmite coating film (24) formed at the wall surface of the combustion chamber (16) configured from aluminum or an aluminum alloy; and a heat shield film (23) that is provided to the surface of the boehmite coating film (24) and is formed by means of applying a heat insulating coating material or a heat shielding coating material to the surface of the boehmite coating film (24).
Description
本発明は、シリンダボアとシリンダヘッド下面とピストン頂部とで区画される燃焼室を有するエンジンの燃焼室構造に関する。
The present invention relates to a combustion chamber structure for an engine having a combustion chamber defined by a cylinder bore, a cylinder head lower surface, and a piston top.
ディーゼルエンジンの燃焼室は、一般的に、シリンダボアとシリンダヘッドの下面とピストンの頂部とで区画される。ピストンの頂部にキャビティが凹設されており、ピストンの上方に配置された燃料噴射弁からキャビティ内に燃料が噴射されるようになっている。
The combustion chamber of a diesel engine is generally defined by a cylinder bore, the lower surface of the cylinder head, and the top of the piston. A cavity is recessed at the top of the piston, and fuel is injected into the cavity from a fuel injection valve disposed above the piston.
このようなディーゼルエンジンの燃焼室構造は、例えば特許文献1に開示されている。
Such a combustion chamber structure of a diesel engine is disclosed in Patent Document 1, for example.
ところで、冷却損失(燃焼室内の燃焼ガスからの熱伝達)を低減するため、燃焼室の壁面(特に、キャビティの淵に沿って全周)を遮熱することが望ましい。
By the way, in order to reduce the cooling loss (heat transfer from the combustion gas in the combustion chamber), it is desirable to shield the wall of the combustion chamber (especially the entire circumference along the edge of the cavity).
遮熱対象物を簡易的に遮熱する方法として、断熱塗料又は遮熱塗料と称されるものを遮熱対象物に塗布することが知られている。断熱塗料又は遮熱塗料を燃焼室の壁面に塗布する場合、燃料の燃焼時に火炎が断熱塗料又は遮熱塗料に当たること等から、断熱塗料又は遮熱塗料を燃焼室の壁面に強固に結合させる必要がある。
It is known that a heat insulation paint or a heat insulation paint is applied to the heat insulation object as a method for simply insulating the heat insulation object. When applying thermal insulation paint or thermal barrier paint to the wall surface of the combustion chamber, it is necessary to firmly bond the thermal insulation paint or thermal insulation paint to the wall surface of the combustion chamber because the flame hits the thermal insulation paint or thermal insulation paint during fuel combustion. There is.
そこで、本発明の目的は、燃焼室の壁面に断熱塗料又は遮熱塗料の塗布による遮熱膜を形成する際に、断熱塗料又は遮熱塗料(遮熱膜)を燃焼室の壁面に強固に結合させることにある。
Therefore, an object of the present invention is to firmly apply a heat insulating paint or a heat insulating paint (heat insulating film) to the wall of the combustion chamber when forming a heat insulating film by applying a heat insulating paint or a heat insulating paint on the wall of the combustion chamber. It is to be combined.
上述の目的を達成するために、本発明に係るエンジンの燃焼室構造は、シリンダボアとシリンダヘッド下面とピストン頂部とで区画される燃焼室を備え、前記燃焼室の壁面の少なくとも一部がアルミニウム又はアルミニウム合金から構成されるエンジンの燃焼室構造であって、アルミニウム又はアルミニウム合金から構成される前記燃焼室の壁面に形成されたベーマイト皮膜と、前記ベーマイト皮膜の表面に設けられ、前記ベーマイト皮膜の表面に断熱塗料又は遮熱塗料を塗布することにより形成される遮熱膜とを備えるものである。
In order to achieve the above object, a combustion chamber structure of an engine according to the present invention includes a combustion chamber defined by a cylinder bore, a cylinder head lower surface, and a piston top, and at least a part of the wall surface of the combustion chamber is made of aluminum or A combustion chamber structure of an engine composed of an aluminum alloy, the boehmite film formed on the wall surface of the combustion chamber composed of aluminum or an aluminum alloy, and the surface of the boehmite film provided on the surface of the boehmite film And a heat shielding film formed by applying a heat insulating paint or a heat shielding paint.
前記ベーマイト皮膜は、前記燃焼室の壁面にベーマイト処理を施すことにより前記燃焼室の壁面に形成されるものであっても良い。
The boehmite film may be formed on the wall surface of the combustion chamber by performing a boehmite treatment on the wall surface of the combustion chamber.
本発明によれば、燃焼室の壁面に断熱塗料又は遮熱塗料の塗布による遮熱膜を形成する際に、断熱塗料又は遮熱塗料(遮熱膜)を燃焼室の壁面に強固に結合させることができるという優れた効果を奏する。
According to the present invention, when forming a heat-shielding film by applying a heat-insulating paint or a heat-shielding paint on the wall surface of the combustion chamber, the heat-insulating paint or heat-shielding paint (heat-shielding film) is firmly bonded to the wall surface of the combustion chamber. There is an excellent effect of being able to.
以下、本発明の好適な実施形態を添付図面に基づいて詳述する。
Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings.
図1に本発明の一実施形態に係るエンジンの燃焼室構造を示す。
FIG. 1 shows a combustion chamber structure of an engine according to an embodiment of the present invention.
図1(a)に示すように、エンジン(本実施形態では、ディーゼルエンジン)10は、シリンダブロック11に形成されたシリンダボア12と、シリンダボア12内を上下に往復運動するアルミニウム又はアルミニウム合金製のピストン13と、シリンダブロック11の上部にガスケット14を挟んで取り付けられたアルミニウム又はアルミニウム合金製のシリンダヘッド15とを備えている。シリンダボア12と、シリンダヘッド15の下面と、ピストン13の頂部とで囲まれた空間が、燃焼室16を形成する。シリンダヘッド15には、燃焼室16に連通する吸排気ポート(吸気ポート17及び排気ポート18)と、吸気ポート17を開閉する吸気弁19と、排気ポート18を開閉する排気弁20と、燃料を上方から燃焼室16内に噴射する燃料噴射弁(インジェクタ)21とが設けられている。また、ピストン13の頂面13aには、キャビティ(図例では、リップ付タイプのキャビティ)13bが凹設されている。
As shown in FIG. 1 (a), an engine (in this embodiment, a diesel engine) 10 includes a cylinder bore 12 formed in a cylinder block 11, and a piston made of aluminum or aluminum alloy that reciprocates up and down in the cylinder bore 12. 13, and a cylinder head 15 made of aluminum or aluminum alloy attached to the upper part of the cylinder block 11 with a gasket 14 interposed therebetween. A space surrounded by the cylinder bore 12, the lower surface of the cylinder head 15, and the top of the piston 13 forms a combustion chamber 16. The cylinder head 15 has an intake / exhaust port (intake port 17 and exhaust port 18) communicating with the combustion chamber 16, an intake valve 19 that opens and closes the intake port 17, an exhaust valve 20 that opens and closes the exhaust port 18, and fuel. A fuel injection valve (injector) 21 for injecting the combustion chamber 16 from above is provided. In addition, a cavity (in the illustrated example, a cavity with a lip) 13 b is formed in the top surface 13 a of the piston 13.
図1(a)に示すエンジン10では、例えばピストン13が圧縮上死点付近に位置するときに燃料を燃料噴射弁21から燃焼室16内に噴射することで、燃焼室16内の燃料が自着火して燃焼する。燃料噴射弁21の先端部には噴口22が複数設けられており、各噴口22は、ピストン13の圧縮上死点付近において噴口22から噴射された燃料がキャビティ13bのリップ部13cに向かうように指向されている。
In the engine 10 shown in FIG. 1A, for example, when the piston 13 is located near the compression top dead center, the fuel in the combustion chamber 16 is automatically injected by injecting the fuel from the fuel injection valve 21 into the combustion chamber 16. Ignite and burn. A plurality of nozzle holes 22 are provided at the tip of the fuel injection valve 21, and each nozzle 22 is configured so that the fuel injected from the nozzle 22 near the compression top dead center of the piston 13 is directed toward the lip 13c of the cavity 13b. It is oriented.
本実施形態では、燃焼室16を形成するピストン13の頂部に、燃焼室16内の燃焼ガスからピストン13への伝熱を抑制するための遮熱膜23が形成されている。より詳細には、遮熱膜23は、ピストン13の頂面13a及びキャビティ13bの一部(図例では、キャビティ13bのリップ部13c近傍)に全周に亘って形成されている。
In this embodiment, a heat shield film 23 for suppressing heat transfer from the combustion gas in the combustion chamber 16 to the piston 13 is formed on the top of the piston 13 forming the combustion chamber 16. More specifically, the thermal barrier film 23 is formed over the entire circumference on the top surface 13a of the piston 13 and a part of the cavity 13b (in the figure, in the vicinity of the lip portion 13c of the cavity 13b).
本実施形態では、ベーマイト処理を遮熱膜23のためのアンカー処理(塗料を塗布する前の前処理)として行う。即ち、本実施形態では、ピストン13の表面にベーマイト処理を施すことにより、ピストン13の表面にベーマイト皮膜24を形成し、そのベーマイト皮膜24の上に断熱塗料又は遮熱塗料を塗布することにより、ベーマイト皮膜24の上に遮熱膜23を形成する(図1(b)参照)。
In this embodiment, the boehmite treatment is performed as an anchor treatment (pretreatment before applying the paint) for the thermal barrier film 23. That is, in this embodiment, by performing a boehmite treatment on the surface of the piston 13, a boehmite film 24 is formed on the surface of the piston 13, and by applying a heat insulating paint or a thermal barrier paint on the boehmite film 24, A thermal barrier film 23 is formed on the boehmite film 24 (see FIG. 1B).
ベーマイト処理とは、母材(アルミニウム又はアルミニウム合金)の表面に高温の水蒸気(蒸留水)を吹き付ける等して、母材の表面にAl2O3・H2Oの組成で表されるアルミナ1水和物(ベーマイト)を形成するものである。また、ベーマイト処理においては、高温の蒸留水に少量のアンモニア水等の添加剤を添加して行う場合もある。このベーマイト処理は、主にアルミニウムの防錆処理として行われるものである。また、ベーマイト処理により形成されるアルミナ1水和物(ベーマイト)は、針状結晶構造である。
The boehmite treatment, the surface of the base (aluminum or aluminum alloy) and the like blowing hot steam (distilled water), an alumina 1 represented by a composition of Al 2 O 3 · H 2 O on the surface of the base It forms hydrates (boehmite). In addition, the boehmite treatment may be performed by adding a small amount of an additive such as aqueous ammonia to high-temperature distilled water. This boehmite treatment is mainly performed as an antirust treatment for aluminum. In addition, alumina monohydrate (boehmite) formed by boehmite treatment has a needle-like crystal structure.
遮熱膜23の厚さ(膜厚さ)Ta(図1(b)参照)は、例えば100μm程度とする。また、ベーマイト皮膜24の厚さ(皮膜厚さ)Tb(図1(b)参照)は、例えば0.1μm~10μm程度とする。
The thickness (film thickness) Ta (see FIG. 1B) of the heat shield film 23 is, for example, about 100 μm. Further, the thickness (film thickness) Tb (see FIG. 1B) of the boehmite film 24 is, for example, about 0.1 μm to 10 μm.
本実施形態の作用効果を説明する。
The function and effect of this embodiment will be described.
本実施形態では、ピストン13の表面にベーマイト処理を施すことにより、ピストン13の表面にベーマイト皮膜24を形成し、そのベーマイト皮膜24の上に断熱塗料又は遮熱塗料を塗布することにより、ベーマイト皮膜24の上に遮熱膜23を形成するようにしている。
In the present embodiment, the boehmite film 24 is formed on the surface of the piston 13 by performing a boehmite treatment on the surface of the piston 13, and the boehmite film is applied to the boehmite film 24 by applying a heat insulating paint or a thermal barrier paint. A heat shield film 23 is formed on the film 24.
ベーマイト皮膜24を構成するアルミナ1水和物(ベーマイト)が針状結晶構造であるため、ベーマイト皮膜24の上に塗布した断熱塗料又は遮熱塗料がベーマイト皮膜24にしっかりと深く食い込むことができ、断熱塗料又は遮熱塗料(遮熱膜23)とピストン13の表面との結合力は非常に強固となる。そのため、ピストン13の表面に断熱塗料又は遮熱塗料の塗布による遮熱膜23を形成する際に、断熱塗料又は遮熱塗料(遮熱膜23)をピストン13の表面に強固に結合させることが可能となる。
Since the alumina monohydrate (boehmite) constituting the boehmite film 24 has a needle-like crystal structure, the heat-insulating paint or the heat-shielding paint applied on the boehmite film 24 can penetrate into the boehmite film 24 firmly and deeply. The bonding force between the heat insulating paint or the heat insulating paint (heat insulating film 23) and the surface of the piston 13 becomes very strong. Therefore, when forming the heat shield film 23 by applying a heat insulating paint or a heat insulating paint on the surface of the piston 13, the heat insulating paint or the heat insulating paint (heat insulating film 23) may be firmly bonded to the surface of the piston 13. It becomes possible.
また、ベーマイト皮膜24は、母材(アルミニウム又はアルミニウム合金)であるピストン13の表面と化学結合しているため、ベーマイト皮膜24自体がピストン13の表面に強固に結合する。よって、ベーマイト処理を遮熱膜23のためのアンカー処理として行うことにより、アンカー処理を行わない場合よりも強固に、断熱塗料又は遮熱塗料(遮熱膜23)をピストン13の表面に結合させることができる。
Further, since the boehmite film 24 is chemically bonded to the surface of the piston 13 which is a base material (aluminum or aluminum alloy), the boehmite film 24 itself is firmly bonded to the surface of the piston 13. Therefore, by performing the boehmite treatment as the anchor treatment for the heat shield film 23, the heat insulating paint or the heat shield paint (heat shield film 23) is bonded to the surface of the piston 13 more firmly than when the anchor treatment is not performed. be able to.
以上、本発明の好適な実施形態について説明したが、本発明は上述の実施形態には限定されず他の様々な実施形態を採ることが可能である。
The preferred embodiments of the present invention have been described above, but the present invention is not limited to the above-described embodiments, and various other embodiments can be adopted.
例えば、上述の実施形態では、ピストン13の頂部に遮熱膜23を形成するとしたが、これには限定はされず、図2に示すように、燃焼室16を形成するシリンダヘッド15の下面に遮熱膜23を形成することも可能である。シリンダヘッド15の下面に遮熱膜23を形成する場合には、図2に示すように、シリンダヘッド15の下面における燃焼室16内に臨む部分のみに遮熱膜23を形成しても良く、図示はしないが、シリンダヘッド15の下面全体に遮熱膜23を形成しても良い。いずれの場合も、ベーマイト処理を遮熱膜23のためのアンカー処理として行い、シリンダヘッド15の表面にベーマイト皮膜24を形成する。
For example, in the above-described embodiment, the heat shielding film 23 is formed on the top of the piston 13, but this is not a limitation, and as shown in FIG. 2, the lower surface of the cylinder head 15 that forms the combustion chamber 16 is formed. It is also possible to form the heat shield film 23. When the thermal barrier film 23 is formed on the lower surface of the cylinder head 15, as shown in FIG. 2, the thermal barrier film 23 may be formed only on the portion of the lower surface of the cylinder head 15 that faces the combustion chamber 16. Although not shown, the heat shield film 23 may be formed on the entire lower surface of the cylinder head 15. In either case, the boehmite treatment is performed as an anchor treatment for the thermal barrier film 23, and the boehmite film 24 is formed on the surface of the cylinder head 15.
また、上述の実施形態では、ピストン13の頂面13a及びキャビティ13bの一部に遮熱膜23を形成したが、これには限定はされず、ピストン13の頂部に遮熱膜23を形成する際には、図2に示すように、ピストン13の頂面13a及びキャビティ13bの全体に遮熱膜23を形成しても良い。この場合も、ベーマイト処理を遮熱膜23のためのアンカー処理として行い、ピストン13の表面にベーマイト皮膜24を形成する。
In the above-described embodiment, the heat shield film 23 is formed on a part of the top surface 13 a and the cavity 13 b of the piston 13. However, the present invention is not limited to this, and the heat shield film 23 is formed on the top of the piston 13. In this case, as shown in FIG. 2, a heat shielding film 23 may be formed on the entire top surface 13 a and the cavity 13 b of the piston 13. Also in this case, the boehmite process is performed as an anchor process for the heat shield film 23, and the boehmite film 24 is formed on the surface of the piston 13.
また、エンジン10は、ディーゼルエンジンには限定はされず、ガソリンエンジン等であっても良い。さらに、エンジン10は、直噴式のものには限定はされず、火花点火式のものであっても良い。
Further, the engine 10 is not limited to a diesel engine, and may be a gasoline engine or the like. Further, the engine 10 is not limited to a direct injection type, and may be a spark ignition type.
さらに、ピストン13の頂部に凹設されるキャビティ13bの形状に関しては、ディーゼルエンジンの場合、リップ付タイプに限定はされず、リエントラントタイプやトロイダルタイプ等であっても良い。
Furthermore, regarding the shape of the cavity 13b recessed at the top of the piston 13, in the case of a diesel engine, it is not limited to a lip type, and may be a reentrant type or a toroidal type.
10 エンジン
12 シリンダボア
13 ピストン
15 シリンダヘッド
16 燃焼室
23 遮熱膜
24 ベーマイト皮膜 10Engine 12 Cylinder bore 13 Piston 15 Cylinder head 16 Combustion chamber 23 Thermal barrier film 24 Boehmite film
12 シリンダボア
13 ピストン
15 シリンダヘッド
16 燃焼室
23 遮熱膜
24 ベーマイト皮膜 10
Claims (2)
- シリンダボアとシリンダヘッド下面とピストン頂部とで区画される燃焼室を備え、前記燃焼室の壁面の少なくとも一部がアルミニウム又はアルミニウム合金から構成されるエンジンの燃焼室構造であって、アルミニウム又はアルミニウム合金から構成される前記燃焼室の壁面に形成されたベーマイト皮膜と、前記ベーマイト皮膜の表面に設けられ、前記ベーマイト皮膜の表面に断熱塗料又は遮熱塗料を塗布することにより形成される遮熱膜とを備えることを特徴とするエンジンの燃焼室構造。 A combustion chamber structure of an engine comprising a combustion chamber defined by a cylinder bore, a cylinder head lower surface, and a piston top, wherein at least a part of a wall surface of the combustion chamber is made of aluminum or an aluminum alloy. A boehmite film formed on a wall surface of the combustion chamber, and a heat insulating film provided on the surface of the boehmite film and formed by applying a heat insulating paint or a heat insulating paint on the surface of the boehmite film. An engine combustion chamber structure characterized by comprising:
- 前記ベーマイト皮膜は、前記燃焼室の壁面にベーマイト処理を施すことにより前記燃焼室の壁面に形成される請求項1に記載のエンジンの燃焼室構造。 The engine combustion chamber structure according to claim 1, wherein the boehmite film is formed on a wall surface of the combustion chamber by performing a boehmite treatment on the wall surface of the combustion chamber.
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5984240U (en) * | 1982-11-29 | 1984-06-07 | イズミ工業株式会社 | Piston for internal combustion engine |
JPH03224144A (en) * | 1989-12-18 | 1991-10-03 | Fujitsu Ltd | Optical disk substrate |
JP2001329273A (en) * | 2000-05-25 | 2001-11-27 | Mitsubishi Heavy Ind Ltd | Apparatus for selective oxidation of carbon monoxide and method of removing carbon monoxide |
JP2012072745A (en) * | 2010-09-30 | 2012-04-12 | Mazda Motor Corp | Heat insulating structure of aluminum alloy product |
Family Cites Families (3)
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JPS5161445A (en) * | 1974-11-27 | 1976-05-28 | Nippon Paint Co Ltd | ARUMINIUMUKISHITSUNO SHORIHOHO |
JPS5423044A (en) * | 1977-07-23 | 1979-02-21 | Riken Keikinzoku Kogyo Kk | Transparent coating method of aluminum materials |
US5477820A (en) * | 1994-09-29 | 1995-12-26 | Ford Motor Company | Thermal management system for heat engine components |
-
2012
- 2012-04-25 JP JP2012100195A patent/JP2013227910A/en active Pending
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2013
- 2013-04-03 WO PCT/JP2013/060194 patent/WO2013161528A1/en active Application Filing
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5984240U (en) * | 1982-11-29 | 1984-06-07 | イズミ工業株式会社 | Piston for internal combustion engine |
JPH03224144A (en) * | 1989-12-18 | 1991-10-03 | Fujitsu Ltd | Optical disk substrate |
JP2001329273A (en) * | 2000-05-25 | 2001-11-27 | Mitsubishi Heavy Ind Ltd | Apparatus for selective oxidation of carbon monoxide and method of removing carbon monoxide |
JP2012072745A (en) * | 2010-09-30 | 2012-04-12 | Mazda Motor Corp | Heat insulating structure of aluminum alloy product |
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