JP4975131B2 - Cylinder liner manufacturing method - Google Patents

Description

  The present invention relates to a method for manufacturing a cast liner cylinder liner applied to a cylinder block.

  An engine cylinder block having a cylinder liner has been put into practical use. In general, a cylinder liner is applied to a cylinder block made of an aluminum alloy. In addition, as such a cylinder liner for cast-in, the thing of patent document 1 is known, for example.

Japanese Utility Model Publication No. 62-52255

  By the way, in the engine, the cylinder bore is thermally expanded due to the temperature rise of the cylinder. On the other hand, since the temperature of the cylinder changes in accordance with the position in the axial direction, the amount of deformation of the cylinder bore is also different in the axial direction. Such a difference in the deformation amount of the cylinder bore leads to an increase in piston friction, and is one of the factors that deteriorate the fuel consumption rate.

  The present invention has been made in view of such circumstances, and an object of the present invention is to provide a cylinder liner manufacturing method capable of improving the fuel consumption rate by reducing the temperature difference in the axial direction of the cylinder. is there.

In the following, means for achieving the above object and its effects are described.
(1) According to the first aspect of the present invention, in the method for manufacturing a cast-in cylinder liner applied to a cylinder block, the continuous aspect extends from the outer peripheral surface of the upper portion in the axial direction to the outer peripheral surface of the lower portion in the axial direction. A thermal spray layer is formed by a thermal spraying device, and when the thermal spray layer is formed on the upper outer peripheral surface, the thermal spraying device is separated from the outer peripheral surface by a first distance, and the thermal spray layer is formed on the lower outer peripheral surface. The gist of the invention is to separate the thermal spraying device from the outer peripheral surface by a second distance larger than the first distance.

  When the deposition efficiency of the thermal spray material is low at the time of thermal spraying, in the thermal spray material sprayed from the thermal spraying device, the ratio of the thermal spray material that does not adhere to the outer peripheral surface of the cylinder liner and oxidizes around the periphery increases. A part of the sprayed material after oxidation is mixed in the coating on the outer peripheral surface, so that a sprayed layer containing a large amount of oxide is formed on the outer peripheral surface of the cylinder liner. Become.

  In the above invention, the distance between the outer peripheral surface and the thermal spraying device is set to the first distance when forming the thermal spray layer on the upper portion of the cylinder liner, and the outer peripheral surface and the thermal spraying device when forming the thermal spray layer on the lower portion of the cylinder liner. This distance is set to a second distance at which the deposition efficiency of the sprayed material is lower than that at the first distance. Therefore, there is a difference in thermal conductivity between the thermal spray layer on the upper part of the cylinder liner and the thermal spray layer on the lower part of the cylinder liner, and the thermal conductivity of the thermal spray layer on the upper part of the cylinder liner is higher than the thermal conductivity of the thermal spray layer on the lower part of the cylinder liner. Also grows. As a result, the thermal conductivity between the cylinder block and the cylinder liner upper portion is improved, while the thermal conductivity between the cylinder block and the cylinder liner lower portion is lowered, so that the temperature difference in the axial direction of the cylinder is reduced. Will be able to.

  (2) The invention according to claim 2 is the method of manufacturing a cylinder liner according to claim 1, wherein the thermal spray layer formed on the outer peripheral surface of the lower part is formed on the outer peripheral surface of the upper part. The gist is that it is smaller than the thickness of the layer.

  According to the above invention, the thermal conductivity of the thermal spray layer at the upper part of the cylinder liner is larger than the thermal conductivity of the thermal spray layer at the lower part of the cylinder liner, so that the thermal conductivity between the cylinder block and the upper part of the cylinder liner is improved. Thus, the thermal conductivity between the cylinder block and the lower part of the cylinder liner is lowered. As a result, the difference in deformation amount of the cylinder bore as well as the temperature difference in the axial direction of the cylinder is reduced, so that the fuel consumption rate can be improved through the reduction of friction.

  (3) The invention according to claim 3 is the cylinder liner manufacturing method according to claim 1 or 2, wherein the sprayed layer is formed including a portion where the thickness gradually decreases from the upper part toward the lower part. The gist is to be done.

  According to the invention, since the thickness of the sprayed layer is set to be smaller from the upper part toward the lower part, a rapid temperature change in the axial direction of the cylinder is suppressed, so that the fuel consumption is reduced through stabilization of the deformation of the cylinder bore. The rate can be improved.

The block diagram which shows the whole structure of the engine provided with the cylinder liner about 1st Embodiment which actualized the cylinder liner concerning this invention. The perspective view which shows the perspective structure about the cylinder liner of the embodiment. The figure which shows an example of the composition ratio of the cast iron used as the raw material about the cylinder liner of the embodiment. Sectional drawing which shows the structure of the cross section along an axial direction about the cylinder liner of the embodiment. Sectional drawing which shows the structure of the cross section along an axial direction about the cylinder liner of the embodiment. [A] Sectional drawing which shows the cross-section along an axial direction about the cylinder liner of the embodiment. [B] The graph which shows an example of the relationship between the position of an axial direction, and cylinder wall temperature about the cylinder liner of the embodiment. Sectional drawing which shows the structure of the cross section along an axial direction about 2nd Embodiment which actualized the cylinder liner concerning this invention. Process drawing which shows an example of the manufacturing process of the membrane | film | coat about the cylinder liner of the embodiment. The perspective view which shows the perspective structure about 3rd Embodiment which actualized the cylinder liner concerning this invention. The model figure which shows typically the processus | protrusion of the constricted shape about the cylinder liner of the embodiment. The model figure which shows typically the processus | protrusion of the constricted shape about the cylinder liner of the embodiment. Sectional drawing which shows the cross-section of the ZA part of FIG. 9 about the cylinder liner of the embodiment. Sectional drawing which shows the cross-section of the ZB part of FIG. 9 about the cylinder liner of the embodiment. The process figure which shows the list of a manufacturing process about manufacture of the cylinder liner by metal mold | die centrifugal casting. The figure which shows the formation aspect of the constricted-shaped concave hole in a coating layer about manufacture of the cylinder liner by metal mold | die centrifugal casting. The figure which shows an example of the measurement procedure of each parameter by the three-dimensional laser measuring method about the cylinder liner of the embodiment. The figure which shows an example of the contour map obtained by the three-dimensional laser measuring method about the cylinder liner of the embodiment. The figure which shows the relationship between measurement height and a contour line about the cylinder liner of the embodiment. The figure which shows an example of the contour map obtained by the three-dimensional laser measuring method about the cylinder liner of the embodiment. The figure which shows an example of the contour map obtained by the three-dimensional laser measuring method about the cylinder liner of the embodiment.

(First embodiment)
A first embodiment of the present invention will be described with reference to FIGS.
In the present embodiment, it is assumed that the present invention is embodied as a cylinder liner of an aluminum alloy engine.

<Engine configuration>
FIG. 1 shows an overall configuration of an engine provided with a cylinder liner according to the present invention.
The engine 1 includes a cylinder block 11, a cylinder head 12, and the like.

The cylinder block 11 includes a plurality of cylinders 13.
The cylinder 13 includes the cylinder liner 2.
In the cylinder block 11, a wall surface (cylinder inner wall 14) on the inner peripheral side of the cylinder 13 is formed by the inner peripheral surface (liner inner peripheral surface 21) of the cylinder liner 2. A cylinder bore 15 is formed surrounded by the liner inner circumferential surface 21.

The cylinder liner 2 is joined to the cylinder block 11 on the outer peripheral surface (liner outer peripheral surface 22) side through a cast ball made of a casting material.
As an aluminum alloy used as a material of the cylinder block 11, for example, “JIS ADC10 (related standard: US ASTM A380.0)” or “JIS ADC12 (related standard: US ASTM A383.0)” can be used. In the present embodiment, the above ADC 12 is adopted as the aluminum alloy to constitute the cylinder block.

<Configuration of cylinder liner>
FIG. 2 shows a perspective structure of a cylinder liner to which the present invention is applied.
The cylinder liner 2 is formed from cast iron.

  The composition of cast iron can be set as shown in FIG. 3, for example. Basically, the components shown in “Basic composition” can be selected as the composition of cast iron. Moreover, the component shown in "auxiliary composition" can also be added as needed.

In this embodiment, each part of the cylinder liner 2 is shown as follows.
The upper end of the cylinder liner 2 is the liner upper end 23.
The lower end of the cylinder liner 2 is the liner lower end 24.
A range from the upper end 23 of the liner to a predetermined position in the axial direction is defined as an upper portion 25 of the liner.
A range from the liner lower end 24 to a predetermined position in the axial direction is a liner lower portion 26.
A range between the liner upper portion 25 and the liner lower portion 26 is a liner middle portion 27.

  The liner upper end 23 indicates the end of the cylinder liner 2 located on the combustion chamber side in the engine 1. The liner lower end 24 indicates an end portion of the cylinder liner 2 located on the opposite side of the engine 1 from the combustion chamber.

FIG. 4 shows a cross-sectional structure of the cylinder liner 2 along the axial direction.
In the cylinder liner 2, a high thermal conductive film 3 and a low thermal conductive film 4 are formed on the liner outer peripheral surface 22.

  The high thermal conductive film 3 is formed of a material capable of improving the thermal conductivity between the cylinder block 11 and the cylinder liner 2 as compared with a state where the same film is not formed. In addition, the detail about the raw material and manufacturing method of the high heat conductive film 3 is mentioned later.

  The low thermal conductive film 4 is formed of a material capable of reducing the thermal conductivity between the cylinder block 11 and the cylinder liner 2 as compared with a state where the same film is not formed. In addition, the detail about the raw material and manufacturing method of the low heat conductive film 4 is mentioned later.

The high thermal conductive film 3 and the low thermal conductive film 4 are configured as follows.
The high thermal conductive film 3 is formed on the liner outer peripheral surface 22 of the liner upper portion 25 and the liner middle portion 27. That is, it is formed in the range from the liner upper end 23 to the liner lower portion 26.

The high thermal conductive film 3 includes a film base portion 31 located at the liner upper portion 25 and a film inclined portion 32 located at the liner middle portion 27.
The film base 31 and the film inclined part 32 are formed as one continuous film.

  The film base portion 31 is formed so as to have a substantially constant thickness. On the other hand, the coating inclined portion 32 is formed so that the thickness gradually decreases from the liner upper end 23 side to the liner lower end 24 side.

The low thermal conductive film 4 is formed on the liner outer peripheral surface 22 of the liner lower portion 26 and the liner middle portion 27. That is, it is formed in the range from the liner lower end 24 to the liner upper portion 25.
The low thermal conductive film 4 is composed of a film base part 41 located at the liner lower part 26 and a film inclined part 42 located at the liner middle part 27.

The film base 41 and the film inclined part 42 are formed as one continuous film.
The film base 41 is formed so as to have a substantially constant thickness. On the other hand, the coating inclined portion 42 is formed so that the thickness gradually decreases from the liner lower end 24 side to the liner upper end 23 side.

  In the cylinder liner 2, a film laminated portion 30 in which the high thermal conductive film 3 and the low thermal conductive film 4 are stacked is formed on the liner outer peripheral surface 22 of the liner middle portion 27. In the film laminated portion 30, the high thermal conductive film 3 is formed on the liner outer peripheral surface 22, and the low thermal conductive film 4 is formed on the high thermal conductive film 3.

  In the cylinder liner 2 of the present embodiment, the coating layered portion 30 is configured as described above, but the relationship between the high thermal conductive film 3 and the low thermal conductive coating 4 in the coating layered portion 30 is changed as shown in FIG. You can also. That is, the low-heat conductive film 4 can be formed on the liner outer peripheral surface 22, and the high-heat conductive film 3 can be formed on the low-heat conductive film 4.

<Formation of film>
The form (formation position and thickness of the film) of the high thermal conductive film 3 and the low thermal conductive film 4 in the cylinder liner 2 will be described.

[1] “Film formation position”
With reference to FIG. 6, the setting aspect of the formation position of the high heat conductive film 3 and the low heat conductive film 4 is demonstrated. FIG. 6A shows a cross-sectional structure of the cylinder liner 2 along the axial direction. FIG. 6B shows an example of a change tendency in the axial direction of the cylinder temperature (cylinder wall temperature TW) in the steady operation state of the engine. Hereinafter, the cylinder liner in a state in which the high thermal conductive film 3 and the low thermal conductive film 4 are removed from the cylinder liner 2 will be referred to as a reference cylinder liner. An engine having a reference cylinder liner is used as a reference engine.

In this embodiment, the formation positions of the high thermal conductive film 3 and the low thermal conductive film 4 in the cylinder liner 2 are set based on the cylinder wall temperature TW of the reference engine.
Here, the changing tendency of the cylinder wall temperature TW in the reference engine will be described. In FIG. 6B, the solid line indicates the cylinder wall temperature TW of the reference engine, and the broken line indicates the cylinder wall temperature TW of the engine 1 of the present embodiment. Hereinafter, the maximum temperature in the cylinder wall temperature TW is referred to as the maximum cylinder wall temperature TWH, and the minimum temperature in the cylinder wall temperature TW is referred to as the minimum cylinder wall temperature TWL.

In the reference engine, the cylinder wall temperature TW changes as follows.
(A) In the range from the liner lower end 24 to the liner middle portion 27, the influence of the combustion gas is small, so that the cylinder wall temperature TW gradually increases from the liner lower end 24 to the liner middle portion 27. In the vicinity of the liner lower end 24, the cylinder wall temperature TW becomes the minimum cylinder wall temperature TWL1.
(B) In the range from the liner middle part 27 to the liner upper end 23, the influence of the combustion gas is large, so that the cylinder wall temperature TW rapidly increases. Further, in the vicinity of the liner upper end 23, the cylinder wall temperature TW becomes the maximum cylinder wall temperature TWH1.

  In a normal engine such as the above-described reference engine, the cylinder bore is thermally expanded due to an increase in the cylinder wall temperature TW. On the other hand, as described above, the cylinder wall temperature TW changes according to the position in the axial direction, and accordingly, the deformation amount of the cylinder bore also varies in the axial direction. Such a difference in the deformation amount of the cylinder bore leads to an increase in piston friction, and is one of the factors that deteriorate the fuel consumption rate.

  Therefore, in the cylinder liner 2 of the present embodiment, the high thermal conductive film 3 is formed on the liner outer peripheral surface 22 of the liner upper portion 25, while the low thermal conductive film 4 is formed on the liner outer peripheral surface 22 of the liner lower portion 26. The difference (cylinder wall temperature difference ΔTW) between the cylinder wall temperature TWH and the minimum cylinder wall temperature TWL is reduced.

  In the engine 1 of the present embodiment, the thermal conductivity between the cylinder block 11 and the liner upper portion 25 is enhanced by the high thermal conductive film 3. As a result, the cylinder wall temperature TW of the liner upper portion 25 decreases, so that the maximum cylinder wall temperature TWH becomes the maximum cylinder wall temperature TWH2 that is smaller than the maximum cylinder wall temperature TWH1.

  Further, in the engine 1, the thermal conductivity between the cylinder block 11 and the liner lower part 26 is lowered by the low thermal conductive film 4. As a result, the cylinder wall temperature TW of the liner lower portion 26 increases, so that the minimum cylinder wall temperature TWL becomes a minimum cylinder wall temperature TWL2 that is higher than the minimum cylinder wall temperature TWL1.

  Thus, in the engine 1, the difference between the maximum cylinder wall temperature TWH and the minimum cylinder wall temperature TWL (cylinder wall temperature difference ΔTW) is reduced. Thereby, the width of the deformation amount of the cylinder bore 15 in the axial direction of the cylinder 13 is reduced (the deformation amount is made uniform), so that the fuel consumption rate can be improved through the reduction of friction. In addition, since the coating laminated portion 30 is formed, a rapid change in the cylinder wall temperature TW at the liner middle portion 27 is suppressed, so that the deformation amount of the cylinder bore 15 can be more evenly uniformed. .

  The boundary (wall temperature boundary 28) between the liner upper portion 25 and the liner middle portion 27 can be grasped based on the cylinder wall temperature TW of the reference engine. On the other hand, the length of the liner upper portion 25 (the length from the cylinder upper end 23 to the wall temperature boundary 28) is often the length of the cylinder liner 2 (the length from the liner upper end 23 to the liner lower end 24 (liner overall length). )) Of about 1/3 to 1/4. Therefore, when setting the formation position of the high thermal conductive film 3, the range from the liner upper end 23 to 1/3 to 1/4 of the entire length of the liner can be handled as the liner upper portion 25 without strictly grasping the wall temperature boundary 28. it can.

[2] “Thickness of coating”
The setting aspect of the thickness of the high heat conductive film 3 and the low heat conductive film 4 is demonstrated.
In the cylinder liner 2, the thickness of the coating base portion 31 of the high thermal conductive coating 3 and the thickness of the coating base portion 41 of the low thermal conductive coating 4 are set to substantially the same size. In addition, the thickness of the film lamination portion 30 is set to be approximately the same as the thickness of the film base portion 31 of the high heat conductive film 3 and the thickness of the film base portion 41 of the low heat conductive film 4. That is, the thicknesses of the high thermal conductive film 3 and the low thermal conductive film 4 are set so that a film having a substantially uniform thickness is formed from the liner upper end 23 to the liner lower end 24.

<Formation of high thermal conductive film>
As a raw material of the high thermal conductive film 3, a material satisfying at least one of the following (A) and (B) can be used.
(A) A material having a melting point equal to or lower than the molten metal temperature of the casting material (reference molten metal temperature TC), or a material containing such a material. The reference molten metal temperature TC can be more accurately described as follows. That is, for the molten metal of the casting material of the cylinder block 11, the temperature of the molten metal when supplied into the mold when casting the cylinder liner 2 corresponds to the reference molten metal temperature TC.
(B) A material that is metallurgically bonded to the casting material of the cylinder block 11 or a material containing such a material.

As a manufacturing method of the high thermal conductive film 3, the following manufacturing method can be mainly employed.
[1] Thermal spray [2] Shot coating [3] Plating The following is a main example of the specific configuration of the high thermal conductive film 3.

[1] “Configuration 1 of high thermal conductive film”
In the cylinder liner 2, a sprayed layer formed through spraying can be employed as the high thermal conductive film 3. As the material for the thermal spray layer, aluminum, aluminum alloy, copper or copper alloy can be mainly used.

When the high thermal conductive film 3 is constituted by a sprayed layer of an aluminum alloy (Al—Si alloy), the cylinder block 11 and the cylinder liner 2 are joined in the following state.
About the joining state of the liner upper part 25 and the high heat conductive film 3, since the high heat conductive film 3 is formed by thermal spraying, the liner upper part 25 and the high heat conductive film 3 are mechanically bonded with sufficient adhesion and bonding strength. Is done. The adhesion between the liner upper portion 25 and the high thermal conductive film 3 is higher than the adhesion between the cylinder block and the reference cylinder liner in the reference engine.

  As for the joining state between the cylinder block 11 and the high thermal conductive film 3, the high thermal conductive film 3 is formed through an Al-Si alloy having a melting point equal to or lower than the reference molten metal temperature TC and high wettability with the casting material of the cylinder block 11. Thus, the cylinder block 11 and the high thermal conductive film 3 are mechanically joined with sufficient adhesion and joining strength. In addition, the adhesiveness between the cylinder block 11 and the high thermal conductive film 3 is higher than the adhesiveness between the cylinder block and the reference cylinder liner in the reference engine.

In the engine 1, when the cylinder block 11 and the liner upper part 25 are joined in such a state, the following effects can be obtained.
[A] Since the adhesiveness between the cylinder block 11 and the liner upper portion 25 is ensured through the high thermal conductive film 3, the thermal conductivity between the cylinder block 11 and the liner upper portion 25 is improved.
[B] Since the bonding strength between the cylinder block 11 and the liner upper portion 25 is ensured through the high thermal conductive film 3, peeling between the cylinder block 11 and the liner upper portion 25 is suppressed. Thereby, since the adhesiveness between the cylinder block 11 and the liner upper portion 25 is ensured even when the cylinder bore 15 is expanded, a decrease in thermal conductivity is suppressed.

Moreover, when the said structure is employ | adopted as a structure of the high heat conductive film 3, the following effects can also be acquired.
[C] Since the high thermal conductive film 3 is formed through the sprayed layer of Al—Si alloy, the difference between the degree of expansion of the cylinder block 11 and the degree of expansion of the high thermal conductive film 3 is reduced. In this case, the adhesion between the cylinder block 11 and the cylinder liner 2 is ensured.
[D] Since an Al—Si alloy having high wettability with the casting material of the cylinder block 11 is employed, the adhesion and bonding strength between the cylinder block 11 and the high thermal conductive film 3 are further improved.

  In the engine 1, since the amount of gaps between these members increases as the adhesion between the cylinder block 11 and the liner upper portion 25 and the high thermal conductive film 3 decreases, the space between the cylinder block 11 and the liner upper portion 25 is increased. The thermal conductivity of the liquid becomes lower. Further, as the bonding strength between the cylinder block 11 and the liner upper portion 25 and the high thermal conductive film 3 decreases, these members are easily separated from each other. Therefore, when the cylinder bore 15 expands, the adhesion between the cylinder block 11 and the liner upper portion 25 decreases. To come to.

  By the way, when the melting point of the high thermal conductive film 3 is equal to or lower than the reference molten metal temperature TC, it is considered that the high thermal conductive film 3 is melted and metallurgically joined to the casting material when the cylinder block 11 is manufactured. However, according to the test results conducted by the inventors, it has been confirmed that the cylinder block 11 and the high thermal conductive film 3 are mechanically joined as described above. In some cases, the presence of metallurgically joined portions has also been confirmed, but basically they are mechanically joined.

  Moreover, according to the test conducted by the present inventors, the following has been further confirmed. That is, even if the casting material and the high thermal conductive film 3 are not metallurgically bonded (or only partially metallurgically bonded), the high thermal conductive film 3 has a melting point equal to or lower than the reference molten metal temperature TC. In this case, the adhesion between the cylinder block 11 and the liner upper portion 25 and the bonding strength can be improved. Although the mechanism has not been accurately grasped at present, the solidification rate of the casting material is reduced due to the fact that the heat of the casting material is not easily taken away by the high thermal conductive film 3. It is thought that there is.

[2] “Configuration 2 of high thermal conductive film”
In the cylinder liner 2, a shot coating layer formed through shot coating can be employed as the high thermal conductive film 3. As a material for the shot coating layer, aluminum, aluminum alloy and zinc can be mainly used.

When the high thermal conductive film 3 is composed of an aluminum shot coating layer, the cylinder block 11 and the cylinder liner 2 are joined in the following state.
About the joining state of the liner upper part 25 and the high thermal conductive film 3, since the high thermal conductive film 3 is formed through shot coating, the liner upper part 25 and the high thermal conductive film 3 are mechanically and sufficiently bonded to each other with sufficient adhesion and bonding strength. Joined metallurgically. That is, the liner upper portion 25 and the high thermal conductive film 3 are joined in a state where a mechanically joined portion and a metallurgically joined portion are mixed. The adhesion between the liner upper portion 25 and the high thermal conductive film 3 is higher than the adhesion between the cylinder block and the reference cylinder liner in the reference engine.

  About the joining state of the cylinder block 11 and the high thermal conductive film 3, the high thermal conductive film 3 is formed through aluminum having a melting point equal to or lower than the reference molten metal temperature TC and high wettability with the casting material of the cylinder block 11. The cylinder block 11 and the high thermal conductive film 3 are mechanically bonded with sufficient adhesion and bonding strength. In addition, the adhesiveness between the cylinder block 11 and the high thermal conductive film 3 is higher than the adhesiveness between the cylinder block and the reference cylinder liner in the reference engine.

  In the engine 1, the cylinder block 11 and the liner upper portion 25 are joined in such a state, so that [A] and [B] described in “[1]“ Configuration 1 of the high thermal conductive film ”” are performed. An effect comes to be acquired. In addition, regarding the mechanical joining between the cylinder block 11 and the high thermal conductive film 3, the same description as that described in “[1]“ High thermal conductive film by thermal spraying ”” can be applied.

Moreover, when the said structure is employ | adopted as a structure of the high heat conductive film 3, the following effects can also be acquired.
[C] In shot coating, since the high thermal conductive film 3 can be formed without melting the coating material, it is difficult for the high thermal conductive film 3 to contain an oxide. Therefore, a decrease in the thermal conductivity of the high thermal conductive film 3 due to oxidation is suppressed.

[3] “Configuration 3 of high thermal conductive film”
In the cylinder liner 2, a plating layer formed through plating can be employed as the high thermal conductive film 3. As the material for the plating layer, aluminum, aluminum alloy, copper and copper alloy can be mainly used.

  When the high thermal conductive film 3 is composed of a copper alloy plating layer, the cylinder block 11 and the cylinder liner 2 are joined in the following state. In addition, the film lamination | stacking part 30 is comprised as shown in FIG.

  About the joining state of the liner upper part 25 and the high thermal conductive film 3, since the high thermal conductive film 3 is formed through plating, the liner upper part 25 and the high thermal conductive film 3 are mechanically joined with sufficient adhesion and joint strength. Has been. The adhesion between the liner upper portion 25 and the high thermal conductive film 3 is higher than the adhesion between the cylinder block and the reference cylinder liner in the reference engine.

  Although the high thermal conductive film 3 is formed of a copper alloy having a melting point higher than the reference molten metal temperature TC, the cylinder block 11 and the high thermal conductive film 3 are sufficient for the joining state between the cylinder block 11 and the high thermal conductive film 3. Metallurgically bonded with adhesion and bonding strength. In addition, the adhesiveness between the cylinder block 11 and the high thermal conductive film 3 is higher than the adhesiveness between the cylinder block and the reference cylinder liner in the reference engine.

  In the engine 1, the cylinder block 11 and the liner upper portion 25 are joined in such a state, so that [A] and [B] described in “[1]“ Configuration 3 of the high thermal conductive film ”” are performed. An effect comes to be acquired.

Moreover, when the said structure is employ | adopted as a structure of the high heat conductive film 3, the following effects can also be acquired.
[C] Since the cylinder block 11 and the high thermal conductive film 3 are metallurgically bonded, the adhesion and bonding strength between the cylinder block 11 and the liner upper portion 25 are further improved.
[D] Since the high thermal conductive film 3 is formed through a copper alloy having a thermal conductivity higher than that of the cylinder block 11, the thermal conductivity between the cylinder block 11 and the liner upper portion 25 is further improved.

  In order to join the cylinder block 11 and the high thermal conductive film 3 metallurgically, it is considered that the high thermal conductive film 3 is basically required to be formed of a metal material having a melting point equal to or lower than the reference molten metal temperature TC. . However, according to the test results conducted by the present inventor, even if the high thermal conductive film 3 is formed of a metal material having a melting point higher than the reference molten metal temperature TC, as described above, the cylinder block 11 and the high thermal conductivity are formed. It has been confirmed that the coating 3 may be metallurgically bonded.

<Formation of low thermal conductive film>
As a raw material of the low thermal conductive film 4, a material satisfying at least one of the following (A) and (B) can be used.
(A) A material that reduces the adhesion of the cylinder block 11 to the casting material or a material containing such a material.
(B) A material having a thermal conductivity smaller than at least one of the cylinder block 11 and the cylinder liner 2 or a material containing such a material.

As a manufacturing method of the low thermal conductive film 4, the following manufacturing method can be mainly employed.
[1] Thermal spray [2] Paint [3] Resin coating [4] Chemical conversion treatment The following is a main example of the specific configuration of the low thermal conductive film 4.

[1] “Configuration 1 of low thermal conductive film”
In the cylinder liner 2, a sprayed layer formed through spraying can be employed as the low thermal conductive film 4. As a material for the thermal spray layer, ceramic materials such as alumina and zirconia can be mainly used. In addition to this, the low thermal conductive film 4 can also be constituted by a sprayed layer of an iron-based material containing many oxides and pores.

When the low thermal conductive film 4 is composed of an alumina sprayed layer, the cylinder block 11 and the cylinder liner 2 are joined in the following state.
Regarding the joining state between the cylinder block 11 and the low thermal conductive film 4, the low thermal conductive film 4 is formed through alumina having a lower thermal conductivity than the cylinder block 11, so that the cylinder block 11 and the low thermal conductive film 4 are thermally conductive. Mechanically joined in a low state.

  In the engine 1, when the cylinder block 11 and the liner lower portion 26 are joined in such a state, the following effects can be obtained. That is, since the thermal conductivity between the cylinder block 11 and the liner lower portion 26 is lowered through the low thermal conductive film 4, the cylinder wall temperature TW of the liner lower portion 26 can be increased.

[2] “Configuration 2 of low thermal conductive film”
In the cylinder liner 2, a layer of a release agent for die casting formed through painting can be employed as the low thermal conductive film 4. As the release agent, for example, the following can be employed.
-A mold release agent prepared by mixing vermiculite, mitazole, and water glass.
-A mold release agent prepared by mixing a liquid material mainly composed of silicon and water glass.

When the low thermal conductive film 4 is composed of a release agent layer, the cylinder block 11 and the cylinder liner 2 are joined in the following state.
About the joining state of the cylinder block 11 and the low thermal conductive film 4, the low thermal conductive film 4 is formed through a release agent having low adhesion to the cylinder block 11. It is joined via.

  In the engine 1, when the cylinder block 11 and the liner lower portion 26 are joined in such a state, the following effects can be obtained. That is, since the thermal conductivity between the cylinder block 11 and the liner lower part 26 is lowered through the gap, the cylinder wall temperature TW of the liner lower part 26 can be increased. Moreover, since it becomes possible to divert the die-casting release agent or its raw material used at the time of manufacture of the cylinder block 11, reduction of a man-hour and cost comes to be achieved.

[3] “Configuration 3 of low thermal conductive film”
In the cylinder liner 2, a coating agent layer for mold centrifugal casting formed through painting can be used as the low thermal conductive film 4. As the coating agent, for example, the following can be employed.
・ Coating agent formulated with diatomaceous earth as the main component.
・ A coating agent formulated with graphite as the main component.

When the low thermal conductive film 4 is formed of a coating agent layer, the cylinder block 11 and the cylinder liner 2 are joined in the following state.
About the joining state of the cylinder block 11 and the low thermal conductive film 4, the low thermal conductive film 4 is formed through a coating agent having low adhesion to the cylinder block 11. It is joined via.

  In the engine 1, when the cylinder block 11 and the liner lower portion 26 are joined in such a state, the following effects can be obtained. That is, since the thermal conductivity between the cylinder block 11 and the liner lower part 26 is lowered through the gap, the cylinder wall temperature TW of the liner lower part 26 can be increased. Moreover, since it becomes possible to divert the coating agent for centrifugal mold casting used for the manufacture of the cylinder liner 2 or its raw material, man-hours and costs can be reduced.

[4] “Configuration 4 of low thermal conductive film”
In the cylinder liner 2, a metallic paint layer formed through painting can be used as the low thermal conductive film 4.

When the low thermal conductive film 4 is composed of a metallic paint layer, the cylinder block 11 and the cylinder liner 2 are joined in the following state.
About the joining state of the cylinder block 11 and the low heat conductive film 4, since the low heat conductive film 4 is formed through a metallic paint having low adhesion to the cylinder block 11, there is no gap between the cylinder block 11 and the low heat conductive film 4. Are joined through.

  In the engine 1, when the cylinder block 11 and the liner lower portion 26 are joined in such a state, the following effects can be obtained. That is, since the thermal conductivity between the cylinder block 11 and the liner lower part 26 is lowered through the gap, the cylinder wall temperature TW of the liner lower part 26 can be increased.

[5] “Structure 5 of low thermal conductive film”
In the cylinder liner 2, a low adhesion agent layer formed through painting can be employed as the low thermal conductive film 4. As the low adhesion agent, for example, the following can be employed.
・ Low adhesion agent prepared by mixing graphite, water glass and water.
・ Low adhesion agent prepared by mixing boron nitride and water glass.

When the low thermal conductive film 4 is formed of a low adhesion agent layer, the cylinder block 11 and the cylinder liner 2 are joined in the following state.
About the joining state of the cylinder block 11 and the low thermal conductive film 4, the low thermal conductive film 4 is formed through a low adhesion agent having low adhesion to the cylinder block 11. It is joined via.

  In the engine 1, when the cylinder block 11 and the liner lower portion 26 are joined in such a state, the following effects can be obtained. That is, since the thermal conductivity between the cylinder block 11 and the liner lower part 26 is lowered through the gap, the cylinder wall temperature TW of the liner lower part 26 can be increased.

[6] “Configuration 6 of low thermal conductive film”
In the cylinder liner 2, a heat-resistant resin layer formed through resin coating can be employed as the low thermal conductive film 4.

When the low thermal conductive film 4 is composed of a heat resistant resin layer, the cylinder block 11 and the cylinder liner 2 are joined in the following state.
About the joining state of the cylinder block 11 and the low heat conductive film 4, since the low heat conductive film 4 is formed through a heat resistant resin having low adhesion to the cylinder block 11, there is no gap between the cylinder block 11 and the low heat conductive film 4. Are joined through.

  In the engine 1, when the cylinder block 11 and the liner lower portion 26 are joined in such a state, the following effects can be obtained. That is, since the thermal conductivity between the cylinder block 11 and the liner lower part 26 is lowered through the gap, the cylinder wall temperature TW of the liner lower part 26 can be increased.

[7] “Configuration 7 of low thermal conductive film”
In the cylinder liner 2, a chemical conversion treatment layer formed through chemical conversion treatment can be employed as the low thermal conductive film 4. As the chemical conversion treatment layer, for example, the following layers can be formed.
・ Phosphate chemical conversion treatment layer.
・ Chemical conversion layer of iron trioxide.

  When the low thermal conductive film 4 is formed of a chemical conversion treatment layer, the cylinder block 11 and the cylinder liner 2 are joined in the following state. In addition, the film lamination | stacking part 30 is comprised as shown in FIG.

  As for the bonding state between the cylinder block 11 and the low thermal conductive film 4, the low thermal conductive film 4 is formed through the chemical conversion treatment layer so that the cylinder block 11 and the low thermal conductive film 4 have a gap. Are joined through.

  In the engine 1, when the cylinder block 11 and the liner lower portion 26 are joined in such a state, the following effects can be obtained. That is, since the thermal conductivity between the cylinder block 11 and the liner lower part 26 is lowered through the gap, the cylinder wall temperature TW of the liner lower part 26 can be increased. Moreover, since the low thermal conductive film 4 having a sufficient thickness is formed also in the constricted portion 63 of the protrusion 6, a void is easily formed around the constricted portion 63, so that the effect of lowering the thermal conductivity is enhanced. It becomes like this.

<Structure of the film stack>
About the high heat conductive film 3 and the low heat conductive film 4, depending on a manufacturing method (mainly plating or chemical conversion treatment), it is difficult to arbitrarily set the shape of these films. Accordingly, in order to form the cylinder liner 2 by appropriately combining the high thermal conductive film 3 and the low thermal conductive film 4 exemplified above, it is necessary to adopt the configuration of the film lamination portion 30 according to each manufacturing method. That is, by appropriately setting the formation order of the respective films according to the manufacturing method, it is possible to eliminate the disadvantage that a combination that cannot be selected occurs.

Here, the configuration of the film stacking unit 30 is classified into the following “first stacked configuration” and “second stacked configuration”.
-A 1st lamination structure shows the structure in which the low heat conductive film 4 is located on the high heat conductive film 3 while the high heat conductive film 3 is located on the liner outer peripheral surface 22 in the film lamination part 30. That is, it corresponds to the configuration of the film lamination portion 30 shown in FIG.
The second laminated structure shows a structure in which the low thermal conductive film 4 is located on the liner outer peripheral surface 22 while the high thermal conductive film 3 is located on the low thermal conductive film 4 in the film laminated portion 30. That is, it corresponds to the configuration of the film lamination portion 30 shown in FIG.

Hereinafter, the structure (sequence of film formation) of the film lamination portion 30 suitable for the method for producing each of the high heat conductive film 3 and the low heat conductive film 4 will be described.
(A) When employing thermal spraying or shot coating as the method for producing the high thermal conductive film 3, both the first laminated structure and the second laminated structure can be selected as the structure of the film laminated portion 30. That is, the order of forming the coating can be arbitrarily set.

(B) When plating is employed as the method for producing the high thermal conductive film 3, only the second laminated structure can be selected as the structure of the film laminated portion 30. That is, by setting the film formation order as follows, the film stacking portion 30 having an appropriate configuration can be obtained.
[1] The low thermal conductive film 4 is formed by any one of spraying, painting, and resin coating.
[2] After the low thermal conductive film 4 is formed, the high thermal conductive film 3 is formed through plating.

  (C) When employing thermal spraying as a method for producing the low thermal conductive film 4, both the first laminated structure and the second laminated structure can be selected as the structure of the film laminated portion 30. That is, the order of forming the coating can be arbitrarily set.

(D) When coating or resin coating is employed as the method for producing the low thermal conductive film 4, both the first laminated structure and the second laminated structure can be selected as the structure of the film laminated portion 30. However, since the moldability of the film may be greatly lowered depending on the material, it is desirable to select the first laminated structure as the structure of the film laminated part 30. That is, the moldability of the film stacking portion 30 can be improved by setting the film formation order as follows.
[1] The high thermal conductive film 3 is formed by either a thermal spraying method or a shot coating manufacturing method.
[2] After the formation of the high thermal conductive film 3, the low thermal conductive film 4 is formed through painting or resin coating.

(E) When a chemical conversion treatment is adopted as a method for producing the low thermal conductive film 4, only the first laminated structure can be selected as the structure of the film laminated portion 30. That is, by setting the film formation order as follows, the film stacking portion 30 having an appropriate configuration can be obtained.
[1] The high thermal conductive film 3 is formed by either a thermal spraying method or a shot coating manufacturing method.
[2] After the formation of the high thermal conductive film 3, the low thermal conductive film 4 is formed through chemical conversion treatment.

<Effect of embodiment>
As described above in detail, according to the cylinder liner and the manufacturing method thereof of the present embodiment, the following effects can be obtained.

  (1) In the cylinder liner 2 of the present embodiment, the high thermal conductive film 3 is formed on the liner outer peripheral surface 22 of the liner upper portion 25, while the low thermal conductive film 4 is formed on the liner outer peripheral surface 22 of the liner lower portion 26. Yes. As a result, the difference between the maximum cylinder wall temperature TWH and the minimum cylinder wall temperature TWL in the engine 1 is reduced, so that the amount of deformation of the cylinder bore 15 in the axial direction of the cylinder 13 is reduced. Since the friction is reduced by making the deformation amount of the cylinder bore 15 uniform, the fuel consumption rate can be improved.

  (2) In the cylinder liner 2 of the present embodiment, the coating laminated portion 30 is formed on the liner outer peripheral surface 22 of the liner middle portion 27. Thereby, since a rapid change in the cylinder wall temperature TW in the axial direction of the cylinder 13 is suppressed, the fuel consumption rate can be improved through stabilization of the deformation of the cylinder bore 15.

  (3) In the cylinder liner 2 of the present embodiment, the thickness of the coating inclined portion 32 of the high thermal conductive coating 3 is set gradually smaller from the liner upper end 23 side to the liner lower end 24 side. As a result, since the effect of improving the thermal conductivity by the high thermal conductive film 3 decreases from the liner upper portion 25 toward the liner lower portion 26, a sudden change in the cylinder wall temperature TW can be more suitably suppressed. .

  (4) In the cylinder liner 2 of the present embodiment, the thickness of the coating inclined portion 42 of the low thermal conductive coating 4 is set to be gradually reduced from the liner lower end 24 side to the liner upper end 23 side. As a result, the effect of lowering the thermal conductivity due to the low thermal conductive film 4 decreases from the liner lower portion 26 toward the liner upper portion 25, so that a rapid change in the cylinder wall temperature TW can be more suitably suppressed. .

  (5) In the reference engine, the consumption of engine oil is promoted due to the cylinder wall temperature TW of the liner upper portion 25 becoming excessively high, so the tension of the piston ring should be set to a larger value. Is required. That is, the fuel consumption rate is inevitably deteriorated as the piston ring tension increases.

  According to the cylinder liner 2 of the present embodiment, a state in which the cylinder block 11 and the liner upper portion 25 are in close contact, that is, a state in which there is less air gap around the liner upper portion 25 is obtained. The thermal conductivity between the two becomes higher. As a result, the cylinder wall temperature TW of the liner upper portion 25 is reduced, so that consumption of engine oil can be suppressed. And, by suppressing the consumption of the engine oil, it becomes possible to employ a piston ring having a lower tension than that of the reference engine, so that the fuel consumption rate can be improved.

  (6) In the reference engine, the cylinder wall temperature TW of the liner lower portion 26 becomes a relatively small temperature, so that the engine oil viscosity on the liner inner peripheral surface 21 of the liner lower portion 26 becomes excessively high. That is, since the friction of the piston in the liner lower portion 26 of the cylinder 13 is large, the deterioration of the fuel consumption rate due to the increase of the friction is inevitable. Note that the deterioration of the fuel consumption rate due to the cylinder wall temperature TW becomes more prominent in engines having a relatively large thermal conductivity of the cylinder block, such as an aluminum alloy engine.

  According to the cylinder liner 2 of this embodiment, since the thermal conductivity between the cylinder block 11 and the liner lower portion 26 is low, the cylinder wall temperature TW of the liner lower portion 26 can be increased. As a result, the viscosity of the engine oil is reduced on the liner inner peripheral surface 21 of the liner lower portion 26, so that the fuel consumption rate can be improved through the reduction of friction.

<Other configuration of the embodiment>
In addition, the said 1st Embodiment can also be implemented as the following forms which changed this suitably, for example.

In the first embodiment, the film lamination portion 30 is formed in the liner middle portion 27. However, the formation position of the film lamination portion 30 is an appropriate position according to the relationship with the required cylinder wall temperature TW. Can be changed. About the formation position of the film lamination | stacking part 30, as the setting aspect other than the said embodiment, the setting aspect of following [A]-[D] is mentioned.
[A] The laminated film portion 30 is formed on the liner upper portion 25.
[B] The film stack 30 is formed across the liner upper portion 25 and the liner middle portion 27.
[C] The film stacking portion 30 is formed across the liner middle portion 27 and the liner lower portion 26.
[D] The film stack 30 is formed across the liner upper portion 25 and the liner lower portion 26.
[E] The laminated film portion 30 is formed in the liner lower portion 26.

-The manufacturing method of the high heat conductive film 3 is not restricted to the manufacturing method (spraying, shot coating, and plating) illustrated in the said 1st Embodiment, A suitable manufacturing method is employable.
-The manufacturing method of the low heat conductive film 4 is not restricted to the manufacturing method (spraying, coating, resin coating, and chemical conversion treatment) illustrated in the said 1st Embodiment, A suitable manufacturing method is employable.

  In the first embodiment, the film thickness TP of the high thermal conductive film 3 can be gradually increased from the liner upper end 23 to the liner middle part 27. In this case, since the thermal conductivity between the cylinder block 11 and the liner upper portion 25 decreases from the liner upper end 23 toward the liner middle portion 27, the difference in the cylinder wall temperature TW in the axial direction of the liner upper portion 25 is made smaller. Will be able to.

  In the first embodiment, the film thickness TP of the low thermal conductive film 4 can be gradually decreased from the liner lower end 24 to the liner middle part 27. In this case, since the thermal conductivity between the cylinder block 11 and the liner lower portion 26 is improved from the liner lower end 24 toward the liner middle portion 27, the difference in the cylinder wall temperature TW in the axial direction of the liner lower portion 26 is further reduced. Will be able to.

-In the said 1st Embodiment, the formation aspect of the high heat conductive film 3 can also be changed as follows. That is, the high thermal conductive film 3 can be formed using an appropriate material within a range where at least one of the following conditions (A) and (B) is satisfied.
(A) The thermal conductivity of the high thermal conductive film 3 is larger than the thermal conductivity of the cylinder liner 2.
(B) The thermal conductivity of the high thermal conductive film 3 is larger than the thermal conductivity of the cylinder block 11.

-In each said embodiment, the formation aspect of the low heat conductive film 4 can also be changed as follows. That is, the low thermal conductive film 4 can be formed using an appropriate material within a range where at least one of the following conditions (A) and (B) is satisfied.
(A) The thermal conductivity of the low thermal conductive film 4 is smaller than the thermal conductivity of the cylinder liner 2.
(B) The thermal conductivity of the low thermal conductive film 4 is smaller than the thermal conductivity of the cylinder block 11.

  In the first embodiment, the low thermal conductive film 4 is formed over the entire circumferential direction of the cylinder liner 2, but the formation position of the low thermal conductive film 4 can be changed as follows. That is, it is possible to prevent the coating 4 from being formed on the liner outer circumferential surface 22 between the cylinder bores 15 in the arrangement direction of the cylinders 13. In other words, in the arrangement direction of the cylinders 13, the low thermal conductive film 4 can be formed within a range excluding the liner outer peripheral surface 22 facing the liner outer peripheral surface 22 of the adjacent cylinder liner 2. When such a configuration is adopted, the following effects (a) and (b) can be obtained.

  (A) Since the heat from the adjacent cylinders 13 tends to be trapped between the cylinder bores 15, the cylinder wall temperature TW tends to be higher than the portion other than between the cylinder bores 15 in the circumferential direction of the cylinder 13. Therefore, by adopting the formation mode of the low thermal conductive film 4, it is possible to suppress the cylinder wall temperature TW at a location located between the cylinder bores 15 in the circumferential direction of the cylinder 13 from becoming excessively high.

  (B) In the cylinder 13, as described above, the cylinder wall temperature TW varies depending on the position in the circumferential direction, and accordingly, the deformation amount of the cylinder bore 15 also varies in the circumferential direction. Such a difference in the deformation amount of the cylinder bore 15 causes an increase in piston friction, which is one of the factors that deteriorate the fuel consumption rate.

  When the above-described film formation mode is employed, the thermal conductivity of portions other than between the cylinder bores 15 in the circumferential direction of the cylinder 13 is reduced, while the thermal conductivity between the cylinder bores 15 is the same as that of a normal engine. The difference between the cylinder wall temperature TW at a location other than the interval and the cylinder wall temperature TW between the cylinder bores 15 is reduced. As a result, the difference in the deformation amount of the cylinder bore 15 in the circumferential direction is reduced (the deformation amount is made uniform), so that the fuel consumption rate can be improved through the reduction of piston friction.

(Second Embodiment)
A second embodiment of the present invention will be described with reference to FIGS.
In this embodiment, the film formation mode in the cylinder liner of the first embodiment is changed as described below. The cylinder liner of this embodiment is the same as that of the first embodiment except for the configuration described below.

<Formation of film>
With reference to FIG. 7, the formation aspect of a membrane | film | coat is demonstrated. FIG. 7A shows a cross-sectional structure of the cylinder liner 2 along the axial direction. FIG. 7B shows the relationship between the axial position and the film thickness.

In the cylinder liner 2, a coating 51 is formed on the liner outer peripheral surface 22 from the liner upper end 23 to the liner lower end 24.
The coating 51 is composed of an Al—Si alloy sprayed layer. Further, it is composed of a high heat conduction portion 51A located in the liner upper portion 25, a low heat conduction portion 51B located in the liner lower portion 26, and a film inclined portion 51C located in the liner middle portion 27. The high heat conduction part 51A, the low heat conduction part 51B, and the film inclined part 51C are formed as one continuous film.

In the film 51, the thickness of each part is set as follows.
-The thickness of the high heat conducting portion 51A is set to a substantially constant size.
-The thickness of the low heat conduction part 51B is set to a substantially constant size.
-The thickness of the low heat conduction part 51B is set smaller than the thickness of the high heat conduction part 51A.
The thickness of the coating inclined portion 51C is set so as to gradually decrease from the liner upper end 23 side to the liner lower end 24 side.

<Method for producing film>
With reference to FIG. 8, the manufacturing method of the film | membrane 51 is demonstrated.
In the present embodiment, when the coating 51 is formed by thermal spraying, the coating 51 having the above shape is formed by adjusting the distance (spraying distance L) between the spray port of the thermal spraying device 52 and the liner outer peripheral surface 22. That is, a coating is formed on the liner outer peripheral surface 22 of the liner upper portion 25 through thermal spraying at the reference spraying distance LA, while a coating is formed on the liner outer peripheral surface 22 of the liner lower portion 26 through thermal spraying at a low rate spraying distance LB. ing.

The reference spray distance LA and the low rate spray distance LB are set as follows.
(A) The reference spray distance LA is set as the spray distance L when the deposition efficiency of the spray material 53 is the highest.
(B) The low rate spraying distance LB is set as the spraying distance L when the deposition efficiency of the spraying material 53 is lower than when the spraying distance L is set to the reference spraying distance LA. That is, the spraying distance L is set to be larger than the reference spraying distance LA.

  When the deposition efficiency of the thermal spray material 53 is low at the time of thermal spraying, in the thermal spray material 53 sprayed from the thermal spraying device 52, the ratio of the thermal spray material 53 that does not adhere to the liner outer peripheral surface 22 but oxidizes around it increases. Since a part of the sprayed material 53 after oxidation is mixed into the sprayed layer being formed on the liner outer peripheral surface 22, a large amount of oxide is contained inside the sprayed layer after the formation. It becomes like this.

  Therefore, when the spraying distance L is set to the low rate spraying distance LB at the time of spraying, a sprayed layer containing a large amount of oxide inside, that is, a sprayed layer having a low thermal conductivity, is formed on the liner outer peripheral surface 22. become. On the other hand, when the spraying distance L is set to the reference spraying distance LA at the time of spraying, a thermal spray layer having a higher thermal conductivity is formed on the liner outer peripheral surface 22 than when the spraying distance L is set to the low rate spraying distance LB. Become so.

  In the present embodiment, as described above, the thermal spray distance L when forming the thermal spray layer on the liner upper portion 25 is set to the reference thermal spray distance LA, while the thermal spray distance L when forming the thermal spray layer on the liner lower portion 26 is reduced. The rate spraying distance LB is set. Accordingly, there is a difference in thermal conductivity between the high thermal conductivity portion 51A of the liner upper portion 25 and the low thermal conductivity portion 51B of the liner lower portion 26, and the thermal conductivity of the high thermal conductivity portion 51A is greater than the thermal conductivity of the low thermal conductivity portion 51B. Also grows. As a result, the thermal conductivity between the cylinder block 11 and the liner upper portion 25 is improved, while the thermal conductivity between the cylinder block 11 and the liner lower portion 26 is lowered, so that the maximum cylinder wall temperature TWH in the engine 1 is increased. And the minimum cylinder wall temperature TWL are reduced.

Hereinafter, a specific method for forming the film 51 will be described.
Specifically, the film 51 can be formed by the following procedure.
[1] In a state where the spraying distance L is set to the reference spraying distance LA, the spraying device 52 is moved from the liner upper end 23 to the boundary between the liner upper part 25 and the liner middle part 27, so that the liner outer peripheral surface 22 of the liner upper part 25 is moved. A highly heat conductive portion 51A of the film 51 is formed (FIG. 8A). [2] After the spraying device 52 moves to the boundary between the liner upper portion 25 and the liner middle portion 27, the spraying device 52 is changed from the reference spraying distance LA to the low-rate spraying distance LB while changing the spraying device 52 to the liner middle portion 27 and the liner lower portion. 26 is formed on the liner outer peripheral surface 22 of the liner middle portion 27 (FIG. 8B).
[3] After the thermal spraying device 52 has moved to the boundary between the liner middle portion 27 and the liner lower portion 26, the thermal spraying device 52 is moved to the liner lower end 24 in a state where the thermal spraying distance L is set to the low rate thermal spraying distance LB. A low thermal conductive portion 51B of the film 51 is formed on the liner outer peripheral surface 22 of the liner lower portion 26 (FIG. 8C).

<Effect of embodiment>
As described above in detail, according to the cylinder liner and the manufacturing method thereof according to the second embodiment, in addition to the following effects, the above-described (5) and (6) according to the first embodiment. An effect comes to be acquired.

  (7) In the cylinder liner 2 of the present embodiment, the high thermal conductive portion 51A of the coating 51 is formed on the liner outer peripheral surface 22 of the liner upper portion 25, while the low thermal conductive portion 51B of the coating 51 is formed on the liner outer peripheral surface 22 of the liner lower portion 26. To form. As a result, the difference between the maximum cylinder wall temperature TWH and the minimum cylinder wall temperature TWL in the engine 1 is reduced, so that the amount of deformation of the cylinder bore 15 in the axial direction of the cylinder 13 is reduced. Since the friction is reduced by making the deformation amount of the cylinder bore 15 uniform, the fuel consumption rate can be improved.

  (8) In the cylinder liner 2 of the present embodiment, the coating inclined portion 51 </ b> C of the coating 51 is formed on the liner outer peripheral surface 22 of the liner middle portion 27. Thereby, since a rapid change in the cylinder wall temperature TW in the axial direction of the cylinder 13 is suppressed, the fuel consumption rate can be improved through stabilization of the deformation of the cylinder bore 15.

  (9) In the manufacturing method of the cylinder liner 2 of the present embodiment, the high thermal conductivity portion 51A and the low thermal conductivity portion 51B of the coating 51 are obtained by changing the thermal spray distance L between the reference thermal spray distance LA and the low rate thermal spray distance LB. To form. As a result, the coating 51 for reducing the cylinder wall temperature difference ΔTW can be formed by the single thermal spray material 53, so that it is possible to reduce the cost and the labor of the thermal spray material 53. become.

<Other configuration of the embodiment>
In addition, the said 2nd Embodiment can also be implemented as the following forms which changed this suitably, for example.

-As a raw material of the film | membrane 51, the material which satisfy | fills at least one of the following (A) and (B) can be used.
(A) A material having a melting point equal to or lower than the reference molten metal temperature TC, or a material containing such a material.
(B) A material that is metallurgically bonded to the casting material of the cylinder block 11 or a material containing such a material.

-In the said 2nd Embodiment, the manufacturing method of the membrane | film | coat 51 can also be changed as follows.
[1] In a state where the spraying distance L is set to the low rate spraying distance LB, the liner outer peripheral surface 22 of the liner lower part 26 is moved by moving the spraying device 52 from the liner lower end 24 to the boundary between the liner lower part 26 and the liner middle part 27. The low thermal conduction part 51B of the film 51 is formed on the substrate.
[2] After the spraying device 52 moves to the boundary between the liner lower portion 26 and the liner middle portion 27, the spraying device 52 is changed from the low rate spraying distance LB to the reference spraying distance LA while the spraying device 52 is changed from the liner middle portion 27 to the liner upper portion. 25, the coating inclined portion 51 </ b> C of the coating 51 is formed on the liner outer peripheral surface 22 of the liner middle portion 27.
[3] After the thermal spraying device 52 has moved to the boundary between the liner middle portion 27 and the liner upper portion 25, the thermal spraying device 52 is moved to the liner upper end 23 in a state where the thermal spraying distance L is set to the reference thermal spraying distance LA. A highly heat conductive portion 51 </ b> A of the coating 51 is formed on the liner outer peripheral surface 22 of the upper portion 25.

  In the second embodiment, the spraying distance L when the deposition efficiency of the sprayed material 53 is highest is set as the reference spraying distance LA, but the setting mode of the reference spraying distance LA is not limited to such a setting mode. . In short, if the spraying distance L enables the formation of the high thermal conductivity portion 51A capable of improving the thermal conductivity, an appropriate spraying distance L can be set as the reference spraying distance LA.

(Third embodiment)
A third embodiment of the present invention will be described with reference to FIGS.
In the present embodiment, the configuration of the cylinder liner of the first embodiment is changed as described below. The cylinder liner of this embodiment is the same as that of the first embodiment except for the configuration described below.

<Configuration of cylinder liner>
FIG. 9 shows a perspective structure of the cylinder liner.
A plurality of constricted projections (projections 6) are formed on the outer peripheral surface of the cylinder liner 2 (liner outer peripheral surface 22).

The protrusion 6 is formed on the entire liner outer peripheral surface 22 from the upper end of the cylinder liner 2 (liner upper end 23) to the lower end of the cylinder liner 2 (liner lower end 24).
In the cylinder liner 2, the high thermal conductive film 3 and the low thermal conductive film 4 are formed on the liner outer peripheral surface 22 including the surface of the protrusion 6.

<Structure of protrusion>
FIG. 10 shows a model diagram of the protrusion 6. Hereinafter, the radial direction (arrow A direction) of the cylinder liner 2 is defined as the axial direction of the protrusion 6. The axial direction of the cylinder liner 2 (arrow B direction) is the radial direction of the protrusion 6. FIG. 10 shows the shape of the protrusion 6 as viewed from the radial direction of the protrusion 6.

The protrusion 6 is formed integrally with the cylinder liner 2. Further, the base end portion 61 is connected to the liner outer peripheral surface 22.
A top surface 62 </ b> A corresponding to the tip surface of the protrusion 6 is formed at the tip portion 62 of the protrusion 6. The top surface 62A is formed to be substantially smooth.

A constricted portion 63 is formed between the proximal end portion 61 and the distal end portion 62 in the axial direction of the protrusion 6.
The constricted portion 63 is formed such that the area of the cross section along the radial direction (radial cross sectional area SR) is smaller than the radial cross sectional area SR of the base end portion 61 and the distal end portion 62.

The protrusion 6 is formed so that the radial sectional area SR gradually increases from the constricted portion 63 to the proximal end portion 61 and the distal end portion 62.
FIG. 11 shows a model diagram of the protrusion 6 that marks the constricted space 64 of the cylinder liner 2.

In the cylinder liner 2, a constricted space 64 (shaded area) is formed through the constricted portion 63 of the protrusion 6.
The constricted space 64 is defined by a curved surface (the straight line DD corresponds to the curved surface in FIG. 11) passing through the maximum tip portion 62B along the axial direction of the protrusion 6 and the surface of the constricted portion 63 (constricted surface 63A). Corresponds to the enclosed area. The maximum tip portion 62B indicates a portion where the length in the radial direction of the protrusion 6 is the largest at the tip portion 62.

  In the engine 1 including the cylinder liner 2, the cylinder block 11 and the cylinder liner 2 are joined in a state where a part of the cylinder block 11 enters the constricted space 64 (a state where the cylinder block 11 and the protrusion 6 are engaged with each other). Therefore, the bonding strength (liner bonding strength) between the cylinder block 11 and the cylinder liner 2 is sufficiently ensured. Further, since the deformation of the cylinder bore 15 is suppressed by improving the liner bonding strength, the fuel consumption rate can be improved through the reduction of friction.

<Formation of film>
In the present embodiment, the high thermal conductive film 3 and the low thermal conductive film 4 are basically formed in a mode according to the mode of formation in the first embodiment. Further, as the protrusions 6 are provided on the liner outer peripheral surface 22, the thicknesses of the high thermal conductive film 3 and the low thermal conductive film 4 are set as follows. In addition, the thickness of the high heat conductive film 3 and the low heat conductive film 4 can be measured through a microscope or the like.

[1] “Thickness of high thermal conductive film”
In the cylinder liner 2, the thickness of the high thermal conductive film 3 (film thickness TP) is set to 0.5 mm or less. When the film thickness TP is larger than 0.5 mm, the anchor effect by the protrusion 6 is reduced, so that the bonding strength between the cylinder block 11 and the liner upper portion 25 is significantly reduced.

  In the present embodiment, the high thermal conductive film 3 is formed so that the average value of the film thickness TP at a plurality of locations on the liner upper portion 25 is 0.5 mm or less. The high thermal conductive film 3 can also be formed so as to be 0.5 mm or less.

[2] “Low thermal conductive film thickness”
In the cylinder liner 2, the thickness of the low thermal conductive film 4 (film thickness TP) is set to 0.5 mm or less. When the film thickness TP is larger than 0.5 mm, the anchor effect by the protrusion 6 is reduced, so that the bonding strength between the cylinder block 11 and the liner lower portion 26 is significantly reduced.

  In the present embodiment, the low thermal conductive film 4 is formed so that the average value of the film thickness TP at a plurality of locations of the liner lower part 26 is 0.5 mm or less. The low thermal conductive film 4 can also be formed so as to be 0.5 mm or less.

<State around the protrusion>
FIG. 12 shows a cross-sectional structure of the ZA portion in FIG.
In the cylinder liner 2, the high thermal conductive film 3 is formed along the liner outer peripheral surface 22 and the surface of the protrusion 6. Further, the high thermal conductive film 3 is formed so that the constricted space 64 is not filled. That is, the high thermal conductive film 3 is formed so that the casting material flows into the constricted space 64 when the cylinder liner 2 is cast. When the constricted space 64 is filled with the high thermal conductive film 3, the constricted space 64 is not filled with the casting material, so that the anchor effect by the protrusion 6 cannot be obtained in the liner upper portion 25.

FIG. 13 shows a cross-sectional structure of the ZB portion of FIG.
In the cylinder liner 2, the low thermal conductive film 4 is formed along the liner outer peripheral surface 22 and the surface of the protrusion 6. Further, the low thermal conductive film 4 is formed so that the constricted space 64 is not filled. That is, the low thermal conductive film 4 is formed so that the casting material flows into the constricted space 64 when the cylinder liner 2 is cast. When the constricted space 64 is filled with the low thermal conductive film 4, since the cast material is not filled in the constricted space 64, the anchor effect by the protrusion 6 cannot be obtained in the liner lower portion 26.

<Formation of protrusions>
With reference to Table 1, the formation state of the protrusion 6 in the cylinder liner 2 will be described.
In the present embodiment, as parameters (formation state parameters) indicating the formation state of the protrusions 6, “first area ratio SA”, “second area ratio SB”, “standard cross-sectional area SD”, “standard protrusion number NP”, and “Standard protrusion length HP” is defined.

Here, the “measurement height H”, “first reference plane PA”, and “second reference plane PB”, which are the basis of the formation state parameters, will be described.
(A) “Measurement height H” indicates the axial distance (the height of the protrusion 6) of the protrusion 6 with respect to the liner outer peripheral surface 22. The measurement height H at the liner outer peripheral surface 22 is 0 mm. Further, the measurement height H is the largest on the top surface 62A of the protrusion 6.
(B) “First reference plane PA” indicates a plane along the radial direction of the protrusion 6 at a position where the measurement height is 0.4 mm.
(C) The “second reference plane PB” indicates a plane along the radial direction of the protrusion 6 at a position where the measurement height is 0.2 mm.

The contents of the formation state parameter will be described.
[A] “First Area Ratio SA”: The first area ratio SA indicates the ratio of the area of the protrusion 6 (radial cross-sectional area SR) to the unit area of the first reference plane PA on the liner outer peripheral surface 22.
[B] “Second Area Ratio SB”: The second area ratio SB indicates the ratio of the area of the protrusion 6 (radial cross-sectional area SR) to the unit area of the second reference plane PB on the liner outer peripheral surface 22.
[C] “Standard Cross-sectional Area SD”: The standard cross-sectional area SD indicates the area (radial cross-sectional area SR) of one protrusion 6 on the first reference plane PA on the liner outer peripheral surface 22.
[D] “Standard number of protrusions NP”: The standard number of protrusions NP indicates the number of protrusions 6 formed per unit area (1 cm ² ) on the liner outer peripheral surface 22.
[E] “Standard protrusion length HP”: The standard protrusion length HP indicates an average value of the measurement heights H at a plurality of positions on the protrusion 6.

本実施形態では、上記〔Ａ〕〜〔Ｅ〕の形成状態パラメータを表１の選択範囲内の値に設定することで、突起６によるライナ接合強度の向上の効果をさらに高めるとともに、突起６間における鋳造材料の充填性の向上を図るようにしている。ちなみに、鋳造材料の充填性が高められることにより、シリンダブロック１１とシリンダライナ２との間に空隙が形成されにくくなるため、シリンダブロック１１とシリンダライナ２とがより密着した状態で接合されるようになる。

In the present embodiment, by setting the formation state parameters [A] to [E] to values within the selection range of Table 1, the effect of improving the liner bonding strength by the protrusions 6 is further enhanced, and the distance between the protrusions 6 is increased. The filling property of the casting material is improved. By the way, since the filling property of the casting material is improved, it becomes difficult to form a gap between the cylinder block 11 and the cylinder liner 2, so that the cylinder block 11 and the cylinder liner 2 are joined in a more closely contacted state. become.

  In the present embodiment, in addition to the setting of the parameters [A] to [E], the cylinder liner 2 is formed so that each protrusion 6 exists independently on the first reference plane PA. I also try to get adhesion.

<Cylinder liner manufacturing method>
A method for manufacturing the cylinder liner 2 will be described with reference to FIGS. 14 and 15 and Table 2. FIG.
In the present embodiment, the cylinder liner 2 is manufactured by mold centrifugal casting. Further, in order to keep the value of the formation state parameter within the selection range of Table 1, the values of parameters (hereinafter referred to as [A] to [F]) related to the mold centrifugal casting are set within the selection range of Table 2. I am doing so.
[A] Mixing ratio of the refractory base material 71A in the suspension 71.
[B] Mixing ratio of the binder 71B in the suspension 71.
[C] Mixing ratio of water 71C in the suspension 71.
[D] Average particle diameter of the refractory base material 71A.
[E] Ratio of addition of surfactant 72 to suspension 71
[F] Thickness of layer of coating agent 73 (coating layer 74).

シリンダライナ２の製造は、図１４に示す手順をもって行われる。

The cylinder liner 2 is manufactured according to the procedure shown in FIG.

  [Step A] A suspension 71 is prepared by blending refractory base material 71A, binder 71B, and water 71C in a predetermined ratio. In this step, the blending ratio of the refractory base material 71A, the binder 71B and the water 71C, and the average particle diameter of the refractory base material 71A are set to values within the selection range of Table 2.

  [Step B] A predetermined amount of a surfactant 72 is added to the suspension 71 to form a coating agent 73. In this step, the addition ratio of the surfactant 72 to the suspension 71 is set to a value within the selection range shown in Table 2.

  [Step C] After the rotating mold 75 is heated to a specified temperature, the coating agent 73 is sprayed onto the inner peripheral surface (mold inner peripheral surface 75A). At this time, the coating agent 73 is applied so that the layer of the coating agent 73 (the coating layer 74) is formed with a substantially uniform thickness over the entire circumference of the inner peripheral surface 75A of the mold. In this step, the thickness of the coating layer 74 is set to a value within the selection range in Table 2.

In the coating layer 74 of the mold 75, a concave hole having a constricted shape is formed after the above [Step C] is performed.
With reference to FIG. 15, the formation aspect of the constricted concave hole is demonstrated.
[1] On the mold inner peripheral surface 75A of the mold 75, the coating layer 74 is formed in a state including a plurality of bubbles 74A.
[2] When the surfactant 72 acts on the bubbles 74 </ b> A, a concave hole 74 </ b> B is formed on the inner peripheral side of the coating layer 74.
[3] By enlarging the tip of the concave hole 74B until it abuts against the inner peripheral surface 75A of the mold, a concave hole 74C having a shape confined in the coating layer 74 is formed.

  [Step D] After the coating layer 74 is dried, a cast iron melt 76 is cast into the rotating mold 75. At this time, since the molten metal 76 flows into the concavity-shaped concave hole 74 </ b> C of the coating layer 74, a constriction (protrusion 6) constricted by the cylinder liner 2 after casting is formed.

[Step E] After the molten metal 76 is solidified to form the cylinder liner 2, the cylinder liner 2 is removed from the mold 75 together with the coating layer 74.
[Step F] The coating layer 74 (coating agent 73) is removed from the outer periphery of the cylinder liner 2 by the blast processing device 77.

<Measuring method of formation state parameter>
With reference to FIG. 16, a method for measuring formation state parameters by a three-dimensional laser measurement method will be described. The standard protrusion length HP is measured by a separate method.

Each formation state parameter can be measured by the following procedure.
[1] A test piece 81 for measuring protrusions is created from the cylinder liner 2.
[2] In the non-contact type three-dimensional laser measuring instrument 82, the protrusion measuring test piece 81 is set on the test table 84 so that the irradiation direction of the laser beam 83 and the axial direction of the protrusion 6 are substantially parallel (see FIG. 16 [A]).
[3] A laser beam 83 is irradiated from the three-dimensional laser measuring instrument 82 toward the test piece 81 for measuring protrusions. (FIG. 16 [B]).
[4] The measurement result of the three-dimensional laser measuring instrument 82 is taken into the image processing device 85.
[5] The contour map 86 (FIG. 17) of the protrusion 6 is displayed through image processing by the image processing device 85, and each formation state parameter is calculated based on the contour map 86.

<Contour map of protrusion>
With reference to FIGS. 17 and 18, a contour diagram 86 of the protrusion 6 will be described. FIG. 17 shows an example of a contour map 86. FIG. 18 shows the relationship between the measured height H and the contour line HL. FIG. 17 shows a contour diagram 86 for a protrusion 6 different from the protrusion 6 of FIG.

In the contour map 86, a contour line HL is displayed for every fixed measurement height H.
For example, when the contour line HL is displayed every 0.2 mm in the range from the measurement height of 0 mm to the measurement height of 1.0 mm, in the contour diagram 86, the contour line HL0 of the measurement height of 0 mm, the measurement height of 0. A 2 mm contour line HL2, a measurement height 0.4 mm contour line HL4, a measurement height 0.6 mm contour line HL6, a measurement height 0.8 mm contour line HL8, and a measurement height 1.0 mm contour line HL10 are displayed.

  In FIG. 18, the contour line HL4 corresponds to the first reference plane PA. Further, the contour line HL2 corresponds to the second reference plane PB. Although the case where the contour lines HL are displayed at intervals of 0.2 mm is illustrated here, the contour lines HL can be displayed at appropriate intervals in the actual contour map 86.

  The first region RA and the second region RB in the contour map 86 will be described with reference to FIGS. FIG. 19 shows a contour map 86 (first contour map 86A) in which the contour lines HL other than the contour line HL4 having a measurement height of 0.4 mm are not displayed. FIG. 20 shows a contour map 86 (second contour map 86B) in which the contour lines HL other than the contour line HL2 having a measurement height of 0.2 mm are not displayed. In FIGS. 19 and 20, the solid line indicates the contour line HL in the display state, and the broken line indicates the contour line HL in the non-display state.

  In the present embodiment, the region surrounded by the contour line HL4 in the contour map 86 is the first region RA. That is, the shaded area in the first contour map 86A corresponds to the first area RA. In the contour map 86, a region surrounded by the contour line HL2 is a second region RB. That is, the shaded area in the second contour map 86B corresponds to the second area RB.

<Calculation method of formation state parameter>
With respect to the cylinder liner 2 of the present embodiment, the formation state parameters can be calculated as follows based on the contour map 86, respectively.

[A] "About the first area ratio SA"
The first area ratio SA can be calculated as a ratio of the area of the first region RA to the area of the contour map 86. That is, the first area ratio SA can be calculated by the following formula.

SA = SRA / ST x 100 [%]

In the above formula, “ST” indicates the entire area of the contour map 86. “SRA” represents the total area of the first regions RA in the contour map 86. For example, when the first contour map 86A in FIG. 19 is used as a model, the area of the square region is “ST”. Further, the area of the hatched area is “SRA”. In calculating the first area ratio SA, it is assumed that the contour map 86 does not include a portion other than the liner outer circumferential surface 22.

[B] “About the second area ratio SB”
The second area ratio SB can be calculated as a ratio of the area of the second region RB to the area of the contour map 86. That is, the second area ratio SB can be calculated by the following formula.

SB = SRB / ST x 100 [%]

In the above formula, “ST” indicates the entire area of the contour map 86. “SRB” represents the total area of the second regions RB in the contour map 86. For example, when the second contour map 86B of FIG. 20 is used as a model, the area of the square region is “ST”. The area of the hatched area is “SRB”. In calculating the second area ratio SB, it is assumed that the contour map 86 does not include a portion other than the liner outer peripheral surface 22.

[C] “Standard cross-sectional area SD”
The standard cross-sectional area SD can be calculated as the area of each first region RA in the contour map 86. For example, when the first contour diagram 86A in FIG. 19 is used as a model, the area of the hatched area is the standard cross-sectional area SD.

[D] “Standard number of protrusions NP”
The standard protrusion number NP can be calculated as the number of protrusions 6 per unit area (here, 1 cm ² ) in the contour map 86. For example, when the first contour diagram 86A in FIG. 19 or the second contour diagram 86B in FIG. 20 is used as a model, the number of projections (one) in the figure is the standard projection number NP. In the cylinder liner 2 of the present embodiment, since 5 to 60 protrusions 6 are formed per unit area (1 cm ² ), the actual standard protrusion number NP and the first contour diagrams 86A and 2nd It becomes a value different from the standard projection number NP in the contour diagram 86B.

[E] “Standard protrusion length HP”
The standard protrusion length HP can be calculated as an average value of the height of one place or a plurality of places measured for each protrusion 6. In addition, the height of the protrusion 6 can be measured by a measuring device such as a dial depth gauge.

  Whether or not each projection 6 exists independently on the first reference plane PA can be confirmed based on the first region RA in the contour map 86. That is, it can be confirmed that the protrusions 6 are independent on the first reference plane PA because the first regions RA do not interfere with each other.

<Effect of embodiment>
As described above in detail, according to the cylinder liner and the engine of this embodiment, in addition to the effects (1) to (6) of the first embodiment, the following effects can be obtained. become.

  (10) In the cylinder liner 2 of the present embodiment, a plurality of protrusions 6 are formed on the liner outer peripheral surface 22. Thereby, since the cylinder block 11 and the cylinder liner 2 are joined in a state where the cylinder block 11 and the protrusion 6 are engaged with each other, the joining strength between the cylinder block 11 and the cylinder liner 2 can be sufficiently ensured. Become. And, since the peeling between the cylinder block 11 and the high thermal conductive film 3 and the low thermal conductive film 4 is suppressed through the improvement of the bonding strength, the effect of improving and decreasing the thermal conductivity by these films can be suitably maintained. It becomes like this. Further, the deformation of the cylinder bore 15 can be suppressed through the improvement of the bonding strength.

  (11) In the cylinder liner 2 of the present embodiment, the high thermal conductive film 3 is formed so that the film thickness TP is 0.5 mm or less. As a result, it is possible to suppress a decrease in the bonding strength between the cylinder block 11 and the liner upper portion 25.

  (12) In the cylinder liner 2 of the present embodiment, the low thermal conductive film 4 is formed so that the film thickness TP is 0.5 mm or less. Thereby, the fall of the joint strength of the cylinder block 11 and the liner lower part 26 can be suppressed now.

  (13) In the cylinder liner 2 of the present embodiment, the protrusions 6 are formed so that the standard protrusion number NP is included in the range of “5 to 60”. As a result, the liner bonding strength can be improved. Moreover, the filling property of the casting material between the protrusions 6 can be improved.

  When the standard projection number NP is out of the selection range, the following problems occur. When the number of standard protrusions NP is less than 5, the number of protrusions 6 is insufficient, leading to a decrease in liner bonding strength. When the number of standard protrusions NP is more than 60, the space between the protrusions 6 is narrow, so that the filling property of the casting material between the protrusions 6 is lowered.

  (14) In the cylinder liner 2 of the present embodiment, the protrusions 6 are formed so that the standard protrusion length HP is included in the range of “0.5 mm to 1.0 mm”. As a result, the liner bonding strength and the outer diameter accuracy of the cylinder liner 2 can be improved.

  When the standard protrusion length HP is out of the selection range, the following problems occur. When the standard protrusion length HP is smaller than 0.5 mm, the height of the protrusion 6 is insufficient, leading to a decrease in liner bonding strength. When the standard protrusion length HP is larger than 1.0 mm, the protrusion 6 is likely to be broken, leading to a decrease in liner bonding strength. Moreover, since the height of the protrusion 6 is not uniform, the outer diameter accuracy is lowered.

  (15) In the cylinder liner 2 of the present embodiment, the protrusions 6 are formed so that the first area ratio SA is included in the range of “10% to 50%”. As a result, a sufficiently large liner bonding strength can be ensured. Moreover, the filling property of the casting material between the protrusions 6 can be improved.

  When the first area ratio SA is out of the selection range, the following problem occurs. When the first area ratio SA is smaller than 10%, the liner bonding strength is significantly reduced as compared with the case where the first area ratio SA is 10% or more. When the first area ratio SA is larger than 50%, the second area ratio SB exceeds the upper limit value (55%), so that the filling property of the casting material between the protrusions 6 is significantly lowered.

  (16) In the cylinder liner 2 of the present embodiment, the protrusions 6 are formed so that the second area ratio SB is included in the range of “20% to 55%”. Thereby, the filling property of the casting material between the protrusions 6 can be improved. In addition, a sufficiently large liner bonding strength can be ensured.

  When the second area ratio SB is out of the selection range, the following problem occurs. When the second area ratio SB is smaller than 20%, the first area ratio SA is less than the lower limit (10%), which leads to a significant decrease in liner bonding strength. When the second area ratio SB is larger than 55%, the filling property of the casting material between the protrusions 6 is significantly reduced as compared with the case where the second area ratio SB is 55% or less.

(17) In the cylinder liner 2 of the present embodiment, the protrusion 6 is formed so that the standard cross-sectional area SD is included in the range of “0.2 mm ^{2 to} 3.0 mm ² ”. Thereby, breakage of the protrusion 6 in the manufacturing process of the cylinder liner 2 can be suppressed. Moreover, the filling property of the casting material between the protrusions 6 can be improved.

In addition, when the standard cross-sectional area SD is out of the selection range, the following problem occurs. When the standard cross-sectional area SD is smaller than 0.2 mm ² , the strength of the projection 6 is insufficient, and thus the projection 6 is damaged in the manufacturing process of the cylinder liner 2. When the standard cross-sectional area SD is larger than 3.0 mm ^2, the space between the protrusions 6 is narrow, so that the filling property of the casting material between the protrusions 6 is lowered.

  (18) In the cylinder liner 2 of the present embodiment, the protrusions 6 are formed such that each protrusion 6 (first region RA) exists independently on the first reference plane PA. Thereby, the filling property of the casting material between the protrusions 6 can be improved. In addition, when each processus | protrusion 6 (1st area | region RA) is not independent on 1st reference plane PA, since the space | interval of processus | protrusions 6 is narrow, the filling property of the casting material between processus | protrusions 6 falls. Become.

<Other configuration of the embodiment>
In addition, the said 3rd Embodiment can also be implemented as the following forms which changed this suitably, for example.

-About the said 3rd Embodiment, the structure can also be applied to the cylinder liner 2 of the said 2nd Embodiment.
In the third embodiment, the selection range of the first area ratio SA and the second area ratio SB is set to the selection range of Table 1, but can be changed as follows.

First area ratio SA: 10% to 30%
Second area ratio SB: 20% to 45%

By adopting such a setting, the liner joint strength and the filling property of the casting material between the protrusions 6 can be further improved.

  In the third embodiment, the high thermal conductive film 3 and the low thermal conductive film 4 are formed on the cylinder liner 2 in which the formation state parameter of the protrusion 6 is set within the selection range of Table 1. The high thermal conductive film 3 and the low thermal conductive film 4 can be formed also on the cylinder liner having the above.

(Other embodiments)
In addition, elements that can be changed in common with each of the above embodiments are listed below.
In each of the above embodiments, the cylinder liner of the present invention is applied to an aluminum alloy engine. However, for example, the cylinder liner of the present invention can also be applied to a magnesium alloy engine. In short, the cylinder liner of the present invention can be applied to any engine provided with a cylinder liner. Even in such a case, by embodying the present invention in a manner according to each of the above-described embodiments, the effect according to the effect of each of the above-described embodiments can be achieved.

DESCRIPTION OF SYMBOLS 1 ... Engine, 11 ... Cylinder block, 12 ... Cylinder head, 13 ... Cylinder, 14 ... Cylinder inner wall, 15 ... Cylinder bore.
2 ... cylinder liner, 21 ... liner inner circumferential surface, 22 ... liner outer circumferential surface, 23 ... liner upper end, 24 ... liner lower end, 25 ... liner upper portion, 26 ... liner lower portion, 27 ... liner inner portion, 28 ... wall temperature boundary.

3 ... High thermal conductive film, 31 ... Film base part, 32 ... Film inclined part, 30 ... Film laminated part.
4 ... Low thermal conductive film, 41 ... Film base part, 42 ... Film inclined part.
DESCRIPTION OF SYMBOLS 51 ... Film | membrane, 51A ... High heat conduction part, 51B ... Low heat conduction part, 51C ... Film | membrane inclination part, 52 ... Thermal spray apparatus, 53 ... Thermal spray material.

6 ... Projection, 61 ... Base end portion, 62 ... Tip portion, 62A ... Top surface, 62B ... Maximum tip portion, 63 ... Constricted portion, 63A ... Constricted surface, 64 ... Constricted space.
71 ... Suspension, 71A ... Refractory base material, 71B ... Binder, 71C ... Water, 72 ... Surfactant, 73 ... Coating material, 74 ... Coating layer, 74A ... Bubble, 74B ... Recessed hole, 74C ... Concave hole with concave shape, 75 ... mold, 75A ... inner peripheral surface of mold, 76 ... molten metal, 77 ... blast treatment device, 81 ... test piece for measuring protrusion, 82 ... three-dimensional laser measuring instrument, 83 ... laser beam , 84 ... Test stand, 85 ... Image processing device, 86 ... Contour map, 86 A ... First contour map, 86 B ... Second contour map.

  TC: Reference molten metal temperature, TW: Cylinder wall temperature, TWH: Maximum cylinder wall temperature, TWL: Minimum cylinder wall temperature, ΔTW: Cylinder wall temperature difference, L: Thermal spray distance, LA: Standard spray distance, LB: Low rate spray distance , SR ... radial cross-sectional area, H ... measurement height, PA ... first reference plane, PB ... second reference plane, SA ... first area ratio, SB ... second area ratio, SD ... standard cross-section area, NP ... Standard number of protrusions, HP ... standard protrusion length, HL ... contour, RA ... first region, RB ... second region.

Claims (3)

In the manufacturing method of the cylinder liner for cast-in-hole applied to the cylinder block,
A thermal spraying layer is formed by a thermal spraying device in a form that extends from the outer peripheral surface of the upper part in the axial direction to the outer peripheral surface of the lower part in the axial direction. Separating the thermal spraying device from the outer peripheral surface by a first distance, and separating the thermal spraying device from the outer peripheral surface by a second distance larger than the first distance when forming a sprayed layer on the lower outer peripheral surface. A method of manufacturing a cylinder liner characterized by the above. In the manufacturing method of the cylinder liner according to claim 1,
The method of manufacturing a cylinder liner, wherein a thickness of the thermal spray layer formed on the outer peripheral surface of the lower portion is smaller than a thickness of the thermal spray layer formed on the outer peripheral surface of the upper portion. In the manufacturing method of the cylinder liner according to claim 1 or 2,
The method of manufacturing a cylinder liner, wherein the sprayed layer is formed including a portion where the thickness gradually decreases from the upper part toward the lower part.

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