JPH0673477A - Cylinder for forming machine and its production - Google Patents

Abstract

PURPOSE:To provide a cylinder for a forming machine excellent in wear resistance and corrosion resistance. CONSTITUTION:This cylinder for a forming machine is the one in which the inside face of a cylinder base metal with a hollow cylindrical shape constituted of alloy steel has a lining layer of an Ni base allay consisting of, by weight, 5 to 20% Cr, 1.5 to 4% B, <=0.7% C, 1 to 4% Si, <=2% Mn, 5 to 20% Fe, 5 to 20% Cu, 3 to 15% W and 3 to 20% Co, and the balance substantial Ni with inevitable impurities. The cylinder base metal is constituted of Cr-Mo steel or Ni-Cr-Mo steel, and the metallic structure of the cylinder base metal subjected to heat treatment consists of >=20% bainite, and the balance sorbite.

Description

Detailed Description of the Invention

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a cylindrical cylinder used for a plastic molding machine and the like and a method for manufacturing the same, and more particularly to a cylinder for a molding machine having excellent wear resistance, corrosion resistance and crack resistance and a method for manufacturing the same.

[0002]

2. Description of the Related Art A cylinder for a molding machine made of plastic or the like has a hollow cylindrical cylinder base material made of steel to prevent corrosion or wear caused by a resin or an additive added to the resin during heat molding. A structure is used in which an alloy material having wear resistance and corrosion resistance is lined by a centrifugal casting method. In recent years, in a cylinder for a molding machine having such a structure, in order to improve productivity, it is desired to shorten the injection molding cycle and increase the injection pressure resistance. Since the lining material made of such an alloy material having low ductility is repeatedly subjected to expansion and contraction stresses and cracks easily occur due to fatigue, the cylinder base material needs to have high strength so as not to expand as much as possible.

However, since the base material of the above-mentioned molding machine cylinder is mainly composed of pearlite and a small amount of ferrite, it does not have sufficient strength for a high-speed and high-pressure injection molding cycle. The lining material expands,
There is a problem that the shrinkage causes fatigue fracture and cracks occur. Therefore, as a method of improving these performances, as shown in FIG. 10, a method of joining the reinforcing member 4 to the molding machine cylinder 1 including the lining material 3 and the cylinder base material 2 by a shrink fitting method can be considered. . However, this method has a problem that the manufacturing cost is increased, and it also takes a lot of time and labor to prolong the manufacturing process.

[0004]

SUMMARY OF THE INVENTION Therefore, the object of the present invention is to prevent the cost increase, the increase in the number of manufacturing steps, and the like.
A cylinder for a molding machine having excellent fatigue strength, crack resistance, and wear resistance. Another object of the present invention is to provide a method for manufacturing such a cylinder for a molding machine.

[0005]

As a result of intensive studies in view of the above problems, the present inventor has lined a hollow cylindrical cylinder base material made of alloy steel with an alloy having wear resistance and corrosion resistance by centrifugal casting. When forming a cylinder for a molding machine, the cylinder base material is made to have a desired structure, and by applying an appropriate heat treatment for this purpose, fatigue strength, especially crack resistance can be achieved without adverse effects such as cost increase and extension of manufacturing steps. It was discovered that a cylinder for a molding machine having excellent properties was obtained, and the present invention was conceived. That is, the cylinder for a molding machine of the present invention has a hollow cylindrical cylinder base material made of alloy steel, and a lining material having excellent wear resistance and corrosion resistance existing on the inner surface of the cylinder base material, and the cylinder base material. The structure of the material is characterized by comprising bainite at 20% or more and the balance sorbite.

The structure of the cylinder base material includes a cylinder base material having a hollow cylindrical shape made of the alloy steel of the present invention and a lining material existing on the inner surface of the cylinder base material and having excellent wear resistance and corrosion resistance. However, in the method for manufacturing a cylinder for a molding machine, which comprises bainite of 20% or more and the balance of sorbite, the lining material is put into the cylinder base material and centrifugally cast, and then bainite transformation occurs at a cooling rate of 20 to 200 ° C./min. After cooling to a temperature range and holding there for 10 minutes or more, at a heating rate of 1 to 10 ° C./min, 550 to 650
It is characterized by heating to an annealing temperature of ° C and cooling to room temperature after annealing.

[0007]

Embodiments and Functions First, a base material of a molding machine cylinder according to an embodiment of the present invention will be described. In this embodiment, alloy steel is used as a cylinder base material for coating a lining material having wear resistance and corrosion resistance. When Cr-Mo steel is used as the alloy steel, the content rate of chemical components is C
0.3 to 0.5% by weight, Si 0.15 to 0.35% by weight, Mn 0.3
~ 1.5 wt% or less, P 0.03 wt% or less, S 0.03 wt% or less, Cr 0.7 to 1.5 wt%, Mo 0.1 to 0.5 wt%
Is preferable in terms of strength, Japanese Industrial Standards (JIS G 4105)
Cr-Mo steels equivalent to SCM440 and SCM445 specified in the above are suitable.

When Ni-Cr-Mo steel is used as the alloy steel, the content ratio of chemical components is C 0.3 to 0.5% by weight, and Si is
0.15 to 0.35% by weight, Mn 0.3 to 1.5% by weight or less, P
0.03% by weight or less, S 0.03% by weight or less, Ni 3.0% by weight or less, Cr 0.7 to 1.5% by weight, Mo 0.1 to 0.5% by weight
Is preferable in terms of strength, Japanese Industrial Standards (JIS G 4103)
A Ni-Cr-Mo steel equivalent to SNCM439 specified in 1 is suitable.

Further, in this embodiment, in order to improve the strength of the cylinder base material, 20% or more of the structure is made of bainite and the rest is made of sorbite. If the bainite of the structure is less than 20%, sufficient strength cannot be obtained, which is not preferable. In order to obtain the above-described structure configuration, in this embodiment, the lining material described above is put into the cylinder base material described above, and after centrifugal casting, heat treatment is performed. This heat treatment method is performed by the heat treatment pattern shown in FIG. explain.

Here, the horizontal axis of FIG. 1 represents time, the vertical axis represents temperature, and A on the heat treatment pattern is a centrifugal casting step, B is a cooling step, C is a holding step, D is a heating step, and E is an E step. Indicates an annealing step, and F indicates a cooling step to room temperature.
In the present embodiment, the molding machine cylinder is formed by the centrifugal casting step shown in A, and then in the cooling step shown in B, it is cooled to a temperature range in which bainite transformation occurs, but the cooling rate at this time is 20 to 200. ° C / min. If the cooling rate is less than 20 ° C./min, troostite is generated, and if it exceeds 200 ° C./min, cracks are likely to occur on the inner surface of the lining material. Next, in the holding step shown in C, the region in which bainite transformation occurs is 300 to 600 ° C.
Is. If the region in which bainite transformation occurs is less than 300 ° C, cracking easily occurs on the inner surface of the lining material due to transformation expansion of the base material at low temperature, and if it exceeds 600 ° C, pearlite occurs. The holding time in the holding process is 1
It requires 0 minutes or more. If the holding time is less than 10 minutes, the amount of bainite in the cylinder base material is less than 20%, and sufficient strength cannot be obtained. Next, heating is performed up to the annealing temperature shown in D, and at this time, the heating rate is 1 to 10 ° C./minute. If the heating rate is less than 1 ° C./minute, the amount of bainite in the cylinder base material becomes excessive and cracks are likely to occur on the inner surface of the lining material. On the other hand, if it exceeds 10 ° C./minute, the amount of bainite is insufficient and strength cannot be obtained. Next, the annealing shown in E is performed, but the annealing temperature is 550 to 6
It is 50 ° C. If it is less than 550 ° C, the purpose of annealing for removing residual stress is not fulfilled, and if it exceeds 650 ° C, it affects the metal structure. Also, the annealing time is 1 to
5 hours. If the annealing time is less than 1 hour, the residual stress cannot be sufficiently removed, and if it exceeds 5 hours, the effect is not significantly changed. Finally, cool to room temperature as shown at F. The molding machine cylinder of the present embodiment formed by the above, because the strength of the cylinder base material is significantly improved,
It has excellent fatigue strength, especially crack resistance.

Next, the alloy components constituting the lining material having wear resistance and corrosion resistance used in this embodiment will be described. The Cr content is 5.0 to 20.0% by weight. Cr
Has the effect of combining with C and B to form carbides and borides and improving wear resistance, and also has the function of forming a solid solution in Ni matrix to improve strength and corrosion resistance. %, The melting point of the alloy is remarkably increased and the castability is impaired, which is not preferable. If it is less than 5.0% by weight, the effect is not exhibited. Particularly preferable Cr content is 10.0 to 15.0.
% By weight. The content of B is 1.5 to 4.0% by weight.
B has a function of combining with Cr and W to precipitate a boride of high hardness in the structure and improve the hardness of the alloy, but if it is less than 1.5% by weight, its effect is not sufficient, and if it exceeds 4.0% by weight. It is not preferable because the hypereutectic structure becomes coarse and brittleness increases. Regarding the relationship between the Cr amount and the B amount, when the Cr amount is increased, the B amount is decreased, and when the Cr amount is decreased, the B amount is increased, so that the alloy has a fine structure and a eutectic composition having high strength. That is, when Cr is 10% by weight, about 2.5% by weight of B is the eutectic composition of the alloy in this embodiment.
It is preferable to keep the balance of. Further, when Cr is 10% by weight, it is preferable to keep the balance of W 5 to 7% by weight.

The C content is 0.7% by weight or less. C
Has the effect of improving the hardness and strength of the base, but 0.7
If it exceeds 5% by weight, the degree of eutecticity increases to make it brittle and the strength decreases, which is not preferable. The Si content is 1.0 to 4.0% by weight. Si has the effect of lowering the melting point of the alloy and improving the castability, but if it is less than 1.0% by weight, the effect becomes insufficient, which is not preferable. Also, Si is Ni, C
Since it forms a metal compound with u and precipitates in the matrix, it has the effect of improving wear resistance, but if it exceeds 4.0% by weight, the toughness of the alloy is impaired, which is not preferable. Mn acts as a deoxidizer, but due to its effect the content is 2.0% by weight.
Below. The Fe content is 5.0 to 20.0% by weight. Even if Fe is not initially contained in the alloy, it intrudes from the cylinder base material by a welding reaction with the cylinder base material made of steel. It is necessary for a predetermined amount of Fe to transfer from the cylinder base material to the alloy in order to achieve complete welding of the lining material and the cylinder base material, but if Fe is less than 5.0% by weight, the effect is not exhibited. Further, if Fe is increased, the hardness is lowered, and if it exceeds 20.0% by weight, its influence cannot be ignored, which is not preferable.

The Cu content is 5.0 to 20.0% by weight. Cu has a function of improving the castability, which is a solid solution in the Ni base to lower the melting point of the alloy, and particularly improves the corrosion resistance to hydrofluoric acid, but if it is less than 5.0% by weight, the function is insufficient. Further, if it exceeds 20.0% by weight, the hardness is remarkably lowered, which is not preferable. Particularly preferably, it is 8.0 to 15.0% by weight. W content is 3.0
~ 15.0% by weight. Like W, W also forms carbides and borides, has the effect of improving wear resistance, and Cu
It works synergistically with and improves corrosion resistance. Further, since it also has the function of refining the structure, it contributes to the increase in strength. 3.
If the amount is less than 0% by weight, the above effect is insufficient.
If it exceeds, the castability is deteriorated, which is not preferable. Particularly preferably, it is 5.0 to 10.0% by weight.

The Co content is 3.0-20.0% by weight. Co combines with Cr and B to form a boride, which improves wear resistance and corrosion resistance, but increases the manufacturing cost due to the increase in Co content, which impairs the economic effect. Therefore, its upper limit is 20.0% by weight. And If it is less than 5.0% by weight, the effect cannot be obtained. Ni provides the wear resistance and the corrosion resistance, so that the remaining amount is% as a base alloy component.

Further, in this embodiment, the wear resistance can be further improved by dispersing NbC in the above-mentioned lining material. In this case, the size of NbC is preferably 50 μm or less in the form of fine particles. The preferable NbC content is 3.0 to 20.0 parts by weight per 100 parts by weight of the lining material. When NbC is less than 3.0 parts by weight with respect to 100 parts by weight of the lining material, the effect cannot be obtained, and when it exceeds 20.0 parts by weight, the viscosity of the lining material is increased and a uniform lining layer is formed by the centrifugal casting method. It becomes impossible to do so, and the strength is greatly reduced.

The present invention will be described in detail with reference to the following specific examples. The heat treatment cycle will be described with reference to FIG. (Example 1) SC specified in Japanese Industrial Standards (JIS G 4105)
The cylinder base material was formed using Cr-Mo steel equivalent to M440. Then, to form an alloy for the lining material,
The alloys having the compositions shown in Table 1 were blended, but since Fe migrates from the cylinder base material during casting, the blending was made in consideration of the amount of Fe that migrates.

[0017]

[Table 1]

The alloy of the present invention for a lining material thus blended is melted by heating and then heated at 1150 ° C. in a heating furnace.
Casting temperature 1450 ℃ in the hollow part of the cylinder base material
By centrifugal casting (A shown in FIG. 1). Then, the cooling temperature 4
After cooling at 0 ° C./min to a temperature at which bainite transformation of 480 ° C. occurs (B shown in FIG. 1), the temperature is maintained for 20 minutes (FIG. 1).
C), then reheat at a heating rate of 5 ° C./min to an annealing temperature of 630 ° C. (D shown in FIG. 1) and hold for 5 hours to perform annealing (E shown in FIG. 1), and then to room temperature. It was cooled all the way (F in FIG. 1). The structure of the cylinder base material of the molding machine cylinder formed as described above was formed to be about 50% sorbite, as shown in the metal structure of FIG. The metal structure of the lining material is shown in FIG.

(Example 2) Using Ni-Cr-Mo steel equivalent to SCM439 defined in Japanese Industrial Standard (JIS G 4103),
A cylinder base material was formed, and then a lining material having the same structure as in Example 1 was formed by the same method. The lining material was centrifugally cast on the cylinder base material at a casting temperature of 1450 ° C. (A shown in FIG. 1) to produce a cylinder for a molding machine, which was then heat treated. The heat treatment conditions at that time were:
Cooling temperature 20 ° C./min (B shown in FIG. 1) Bainite transformation temperature 450 ° C., holding time 20 minutes (C shown in FIG. 1), heating rate 5 ° C./min (D shown in FIG. 1), annealing temperature 600 C., annealing time was 5 hours (E shown in FIG. 1), and other conditions were the same as in Example 1.

(Example 3) Cr-Mo similar to Example 1
Steel is used to form the cylinder preform and then Example 1
A lining material having the same chemical composition as described above, and 10 parts by weight of NbC per 100 parts by weight of the lining material.
The alloy for a lining material was blended so as to contain, and a lining material was formed in the same manner as in Example 1. The lining material was centrifugally cast on the cylinder base material at a casting temperature of 1450 ° C. to prepare a cylinder for a molding machine, which was then heat treated. The heat treatment conditions at that time were the same as in Example 1.
The metal structure of the obtained lining material is shown in FIG. The blended NbC is evenly dispersed.

(Example 4) Ni-Cr similar to Example 2
Similar to Example 1 by forming a cylinder base material using —Mo steel and blending 10 parts by weight of NbC fine particles with 100 parts by weight of an alloy having the same chemical content as in Example 1. The lining material was formed by the method of. The lining material was centrifugally cast on the cylinder base material at a temperature of 1450 ° C. to prepare a cylinder for a molding machine, which was then heat treated. The heat treatment conditions at that time were the same as in Example 1.

(Comparative Example) A Cr-Mo steel similar to that of Example 1 was used to form a cylinder base material, and then an alloy having the composition shown in Table 1 was used to perform a lining material in the same manner as in Example 1. Was formed. The lining material was centrifugally cast on the cylinder base material at a temperature of 1100 ° C. (A shown in FIG. 1) to prepare a cylinder for a molding machine, and then heat treatment was performed. The heat treatment condition at that time was cooling rate 60. C / min (B shown in FIG. 1), cooling to 620 ° C. immediately before bainite transformation, holding time 20 minutes (C shown in FIG. 1), heating rate 5 ° C.
/ Min (D shown in FIG. 1), annealing temperature 630 ° C., annealing time 5 hours (E shown in FIG. 1), and other conditions were the same as in Example 1. The cylinder base material structure of the molding machine cylinder formed as described above had about 90% pearlite, and the balance was composed of ferrite, as shown in the metal structure of FIG.

With respect to the molding machine cylinders of Examples 1 to 4 and Comparative Example described above, the tensile strength of the lining material (value calculated from bending strength and Weibull value) and the yield stress of the cylinder base material were measured. Since almost the same results were obtained for Examples 1 to 4, the results of Example 1 and the comparative example are shown in FIG.

Further, the compressive strength of the molding machine cylinders of Examples 1 to 4 and Comparative Example described above was measured. Since almost the same results were obtained for Examples 1 to 4, the results of Example 1 and the comparative example are shown in FIG.

Samples having a size of 10 mm × 15 mm × 10 mm were prepared from the molding machine cylinders of Examples 1 to 4 and Comparative Example described above, and were pressed against # 400 abrasive paper with a load of 2.0 kg to obtain 480 m of pressure. After sliding for a distance, the amount of wear of the lining material was examined. This result was expressed by a relative value when the result of the comparative example was set to 10, and the abrasion resistance was evaluated. Since the same results as in Example 1 and Example 3 were obtained in Example 2 and Example 4, the results of Examples 1 and 3 and Comparative Example are shown in FIG. Further, from the molding machine cylinders of Examples 1 to 4 and Comparative Example described above, 1.5 mm
Prepare a sample of size 4 mm x 10 mm, 10% of 50 ℃
After immersing in a HCl aqueous solution for 24 hours, the corrosion weight loss rate of the lining material was examined. This result is the result of Comparative Example 1
The corrosion resistance was evaluated by the relative value. Since similar results were obtained for Examples 1 to 4, the results for Example 1 and the comparative example are shown in FIG.

As is clear from FIG. 2, the tensile strength of the lining material forming the molding machine cylinder of Example 1 was remarkably improved by a factor of about 2 or more as compared with the molding machine cylinder of the comparative example. The yield point stress of the cylinder base material of Example 1 was improved by 80% or more as compared with the comparative example. Further, as is clear from FIG. 3, the compressive strength of the molding machine cylinder of Example 1 was improved by about 80% as compared with the molding machine cylinder of the comparative example. As described above, in the molding machine cylinder of the present embodiment, the lining material has sufficient strength, and the strength of the cylinder base material is dramatically improved, so that the crack resistance is significantly improved. Regarding the wear resistance of the lining material of Example 1, the wear resistance was evaluated as shown in FIG.
When the comparative example is set to 10, the relative value is 7, the amount of wear is reduced, and improvement in wear resistance is recognized. The relative value of Comparative Example 1 with respect to the acid of the lining material of Example 1 was 1.0, the corrosion weight loss rate was the same, and sufficient corrosion resistance was obtained.

Regarding the molding machine cylinder of Example 3,
Results similar to those in Example 1 were obtained. However, as for the wear resistance of the lining material, as shown in FIG. 4, the relative value obtained as Comparative Example 10 is 4 or less, the wear amount is reduced by 60% or more, and the wear resistance is dramatically improved. We were able to. As described above, the examples 1 and 3 are compared with the comparative example, but the same results are obtained for the example 2 and the example 4 which obtain the same result as the example 1 and the example 3. It is of course effective. As a summary of the above results, the characteristics of the lining material of the present invention shown in Table 1 are shown in Table 2 together with the comparative example.

[0028]

[Table 2]

[0029]

As described in detail above, in the cylinder for a molding machine of the present invention, a lining material made of a wear-resistant alloy is provided on a hollow cylindrical cylinder base material made of alloy steel. By applying heat treatment according to the method of
20% or more of the structure of the cylinder base material is formed of bainite, and the rest is formed of sorbite. As a result, in response to high-speed and high-pressure injection cycles, even when the lining material is subjected to expansion and contraction stresses, the cylinder base material has excellent strength, so distortion that occurs in the lining material is suppressed, and excellent fatigue strength, A cylinder for a molding machine having a crack resistance can be obtained without any adverse effects such as an increase in cost and an increase in the number of manufacturing steps.

[Brief description of drawings]

FIG. 1 is a pattern diagram showing a heat treatment process of a molding machine cylinder according to an embodiment of the present invention.

FIG. 2 is a diagram showing the tensile strength of the lining materials of Example 1 and a comparative example and the yield point stress of the cylinder base material.

FIG. 3 is a diagram showing pressure resistance strengths of Example 1 and a comparative example.

FIG. 4 is a diagram showing relative values of wear amounts of Example 1, Example 3, and Comparative Example.

FIG. 5 is a diagram showing relative values of corrosion weight loss rates of Example 1 and a comparative example.

6 is a micrograph showing the metal structure of the cylinder base material of Example 1. FIG.

FIG. 7 is a micrograph showing the metal structure of the cylinder lining material of Example 1.

8 is a micrograph showing a metal structure of a lining material of a cylinder of Example 3. FIG.

FIG. 9 is a micrograph showing a metal structure of a cylinder base material of a comparative example.

FIG. 10 is a schematic cross-sectional view showing an example of a molding machine cylinder.

[Explanation of symbols]

 1 Cylinder for molding machine 2 Cylinder base material 3 Lining material 4 Reinforcement member

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[Procedure amendment]

[Submission date] October 25, 1993

[Procedure Amendment 1]

[Document name to be amended] Statement

[Correction target item name] 0017

[Correction method] Change

[Correction content]

[0017]

[Table 1]

[Procedure Amendment 2]

[Document name to be amended] Statement

[Correction target item name] 0018

[Correction method] Change

[Correction content]

The alloy of the present invention for a lining material thus blended is melted by heating and then heated at 1150 ° C. in a heating furnace.
Casting temperature 1450 ℃ in the hollow part of the cylinder base material
By centrifugal casting (A shown in FIG. 1). Then, the cooling temperature 4
After cooling at 0 ° C./min to a temperature at which bainite transformation of 480 ° C. occurs (B shown in FIG. 1), the temperature is maintained for 20 minutes (FIG. 1).
C), then reheat at a heating rate of 5 ° C./min to an annealing temperature of 630 ° C. (D shown in FIG. 1) and hold for 5 hours to perform annealing (E shown in FIG. 1), and then to room temperature. It was cooled all the way (F in FIG. 1). The structure of the cylinder base material of the molding machine cylinder formed as described above was formed to be about 50% sorbite as shown in the metal structure of FIG. 7. The metal structure of the lining material is shown in FIG.

[Procedure 3]

[Document name to be amended] Statement

[Name of item to be corrected] Figure 6

[Correction method] Change

[Correction content]

FIG. 6 is a micrograph showing the metal structure of the cylinder lining material of Example 1.

[Procedure amendment 4]

[Document name to be amended] Statement

[Name of item to be corrected] Figure 7

[Correction method] Change

[Correction content]

7 is a micrograph showing the metal structure of the cylinder base material of Example 1. FIG.

 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Masaaki Amada 1-9-1 Kitahama, Wakamatsu-ku, Kitakyushu City Hitachi Metals Co., Ltd. Wakamatsu Factory

Claims (9)

[Claims] 1. A cylinder for a molding machine, comprising: a hollow cylinder-shaped cylinder base material made of alloy steel; and a lining material existing on the inner surface of the cylinder base material and having excellent wear resistance and corrosion resistance. Cr 5.0 to 20.0% by weight, B 1.5 to 4.0% by weight, C 0.7% by weight or less, Si
1.0-4.0 wt%, Mn 2.0 wt% or less, Fe 5.0-2
A cylinder for a molding machine, comprising 0.0% by weight, Cu 5.0 to 20.0% by weight, W 3.0 to 15.0% by weight, Co 3.0 to 20.0% by weight, and the balance being Ni and an inevitable impurity Ni-based alloy. 2. The cylinder for a molding machine according to claim 1, wherein the structure of the cylinder base material is composed of 20% or more of bainite and the balance sorbite. 3. The molding machine cylinder according to claim 1, wherein the lining material is Cr 5.0 to 2
0.0 wt%, B 1.5 to 4.0 wt%, C 0.7 wt% or less, Si 1.0 to 4.0 wt%, Mn 2.0 wt% or less, F
e 5.0 to 20.0 wt%, Cu 5.0 to 20.0 wt%, W 3.0
% To 15.0 wt%, Co 3.0 to 20.0 wt%, and balance 3.0 to 20.0 parts by weight of NbC per 100 parts by weight of Ni-based alloy consisting essentially of Ni and inevitable impurities. Cylinder. 4. The molding machine cylinder according to claim 1, wherein the lining material has a Cu content of 8.0.
A cylinder for a molding machine, characterized in that the content is up to 15.0% by weight. 5. The molding machine cylinder according to claim 1, wherein the molding machine cylinder contains W 5.0 to 10.0% by weight. 6. The molding machine cylinder according to claim 1, wherein the alloy steel forming the cylinder base material is C 0.3 to 0.5 wt%, Si 0.15 to 0.35 wt%, and Mn 0.3 to 1.5% by weight, P 0.03% by weight or less, S
0.03% by weight or less, Cr 0.7 to 1.5% by weight, Mo 0.1 to
A cylinder for a molding machine, characterized in that it is a Cr-Mo steel consisting of 0.5% by weight, the balance being substantially Fe and inevitable impurities. 7. The cylinder for a molding machine according to claim 1, wherein the alloy steel forming the cylinder base material is C 0.3 to 0.5% by weight, Si 0.15 to 0.35% by weight, and Mn 0.3 to 1.5% by weight, P 0.03% by weight or less, S
0.03% by weight or less, Ni 3.0% by weight or less, Cr 0.7-1.
A cylinder for a molding machine, which is a Ni-Cr-Mo steel containing 5% by weight, 0.1 to 0.5% by weight of Mo, and the balance being substantially Fe and inevitable impurities. 8. The method for manufacturing a cylinder for a molding machine according to claim 2, wherein the lining material is put into the cylinder base material and centrifugally cast, and then bainite is cooled at a cooling rate of 20 to 200 ° C./min. Cool to a temperature range that causes transformation, hold it there for 10 minutes or more, then heat at 1 to 10 ° C / min.
A method characterized by heating to an annealing temperature of 650 ° C. and then cooling to room temperature after annealing. 9. The method for manufacturing a cylinder for a molding machine according to claim 8, wherein the region in which the bainite transformation occurs is 30.
A method characterized in that the temperature is 0 to 600 ° C.