JP5060083B2 - Piston ring manufacturing method - Google Patents

Description

  The present invention relates to a piston ring used in an internal combustion engine such as an automobile engine, and more particularly to a piston ring excellent in heat resistance and a method for manufacturing the same.

Piston rings used in reciprocating internal combustion engines are distinguished by their functions into pressure rings and oil rings. As shown in FIG. 1, the pressure ring is divided into a first pressure ring (hereinafter referred to as “top ring”) 1 located on the combustion chamber side and a second pressure ring (hereinafter referred to as “second ring”) 2 located below the pressure ring. These piston rings 1 and 2 are fitted in the ring grooves 3 and 4 of the piston, respectively, and are sliding members for airtightness and lubrication between the cylinder and the piston by tension. It is placed below. In particular, the top ring 1 is closest to the combustion chamber and has a high temperature and is exposed to a harsh operating environment in which it is difficult to sufficiently supply the lubricating oil, and the oil ring 5 scrapes the oil from the cylinder wall 6 to receive the oil. The ring that works to return is under severe operating conditions in which the oil is scraped while being always subjected to a forced spring force by the spring 7 attached for the purpose of efficiently scraping the oil. as mentioned above,
Both piston rings are in a frictional state that they are always in contact with the inner wall of the cylinder.

  Conventionally, the material for piston rings of internal combustion engines has been mainly made of cast iron. However, in recent years, internal combustion engines have been increasingly demanded for higher speed, higher output, and lower fuel consumption. Since the ring cannot fully meet the requirements, the transition to a steel piston ring with better mechanical properties than cast iron is being made, and Si-Cr steel or martensitic stainless steel is used. It became so. However, since these piston ring materials are not sufficient in abrasion resistance and seizure resistance, the outer peripheral surface is subjected to surface treatment. Usually, the hard chromium plating 8 as shown in FIG. 2 is applied to the Si—Cr steel, and the nitriding treatment 9 as shown in FIG. 3 is applied to the martensitic stainless steel. As shown in FIG. 4, the required internal combustion engine uses martensitic stainless steel in which a hard ceramic coating 10 (chromium nitride, titanium nitride, etc.) is applied to the outer peripheral surface of nitriding treatment 9 by ion plating. Yes. 2 to 4, reference numerals 11, 12, and 13 denote piston rings, and reference numeral 14 denotes a piston ring groove.

  For example, Patent Document 1 states that “C is 0.70 to 1.00 wt%, Si is 2.00 wt% or less, Mn is 1.00 wt% or less, and Cr is 7.00 to 11.00 wt%. , Steel for piston rings containing 0.50 to 1.50% by weight of Mo and 0.10 to 0.50% by weight of V.

Patent Document 2 states that “a film having chromium, tungsten, and nitrogen as main constituent elements and having a wear-resistant film made of CrN-type chromium nitride crystal in which 3 to 20 atomic% of tungsten is dissolved. Piston ring "is disclosed.
JP 2002-348639 A JP 2003-64469 A

  The piston rings of Patent Documents 1 and 2 use a large amount of expensive Cr and W, which has a drawback of greatly increasing the manufacturing cost.

  By the way, in recent years, the demand for low fuel consumption for internal combustion engines has become very strong. However, it seems that fuel efficiency can be improved by reducing energy loss caused by friction, and lowering the friction coefficient can improve fuel efficiency. It is thought that it has a positive influence on it.

  Although it is preferable to apply a hard ceramic coating by ion plating to improve the sliding characteristics, since ion plating is performed at a high temperature for a long time (about 5 to 10 hours at about 440 to 550 ° C.), the ion plating is performed. During the heat treatment that accompanies, hardness decreases or thermal deformation occurs. For example, when ion plating treatment is performed on Si—Cr steel, the hardness of the base material of about 500 HV is reduced to about 380 HV. With this degree of hardness, the wear resistance is insufficient and it cannot be used as a piston ring. In this respect, since martensitic stainless steel has high strength at high temperatures, the hardness does not decrease and thermal deformation does not occur during heat treatment accompanying ion plating. However, martensitic stainless steel is a very expensive material containing a large amount of Cr.

  The present invention has been made in view of such problems of the prior art, and the purpose thereof is low cost without using a large amount of expensive alloy elements, and excellent heat resistance. A piston ring and a manufacturing method thereof are provided.

  In order to achieve the above object, the piston ring of the present invention has a C of 0.45 to 0.80% by weight, Si of 0.80 to 2.50% by weight, Mn of 0.10 to 1.00% by weight, Heat treatment is applied to a wire material in which Cr is 0.30 to 1.20% by weight, Ni is 0.20 to 1.50% by weight, V is 0.05 to 0.50% by weight, and the balance is mainly Fe. Piston obtained by drawing into a rectangular cross section by drawing and processing into a piston ring shape after quenching and tempering, and applying ion plating after strain relief annealing on the piston ring The ring is characterized in that the hardness of the material after strain relief annealing is 480 to 550 in terms of Vickers hardness (HV0.5).

  In other words, since the Cr amount is kept low so as to form an appropriate amount of carbide, the material after strain relief annealing can be performed by the carbide that is appropriately precipitated in the heat treatment in the piston ring manufacturing process without reducing the cold workability. When the hardness is 480 to 550 in terms of Vickers hardness (HV0.5), thermal deformation can be suppressed even when subjected to long-time heat treatment associated with ion plating treatment.

Further, the manufacturing method of the piston ring of the present invention is such that C is 0.45 to 0.80 wt%, Si is 0.80 to 2.50 wt%, Mn is 0.10 to 1.00 wt%, and Cr is 0.30 to 1.20% by weight, Ni is 0.20 to 1.50% by weight, V is 0.05 to 0.50% by weight , Cu is 0.15% by mass or less , and the balance is Fe. The resulting wire is subjected to heat treatment and wire drawing to plastic processing into a rectangular cross-section, quenched and tempered, then processed into a piston ring shape, subjected to strain relief annealing, and then subjected to ion plating. In the method of manufacturing a piston ring by applying, the tempering temperature is 450 to 515 ° C, and the strain relief annealing temperature is 520 to 550 ° C.

  That is, since the Cr amount was kept low so as to form an appropriate amount of carbide, by performing strain relief annealing at a temperature of 520 to 550 ° C. after processing into a piston ring shape without reducing the cold workability, Even when subjected to a long-time heat treatment associated with the plating process, a decrease in hardness and thermal deformation can be suppressed.

Since this invention is comprised as mentioned above, there exist the following effects.
(1) Since the content of expensive noble metals such as Cr and V is small, the carbides that are appropriately precipitated at a low cost reduce the hardness reduction and thermal deformation associated with the ion plating process.
(2) Since the Cr and V contents are kept low, the cold workability is excellent.

The reason for limiting the components of the piston ring of the present invention will be described below.
(1) C is preferably contained in an amount of 0.45 to 0.80% by weight.

C is an interstitial solid solution element, a part of which is dissolved in the matrix and contributes to improvement in hardness and fatigue strength. The other part is an important element for generating carbides and improving wear resistance. In order to enjoy these effects, C is preferably contained at least 0.45% by weight. However, since the cold workability is lowered when a large amount is added, the upper limit value of C is preferably 0.80% by weight.
(2) It is preferable to contain Si 0.80-2.50weight%.

Si is an element necessary for increasing the high-temperature strength, and is preferably contained in an amount of 0.80% by weight or more. However, if added in a large amount, not only the cold workability is lowered, but also the toughness is remarkably lowered and it is harmful to the hot workability. Therefore, the upper limit of Si is preferably 2.50% by weight.
(3) It is preferable to contain 0.10 to 1.00% by weight of Mn.

Mn is an element added for deoxidation during the melting of steel and fixation of S in the steel, and is preferably contained in an amount of 0.10% by weight or more. However, since the cold workability is lowered when a large amount is added, the upper limit of Mn is preferably 1.00% by weight.
(4) It is preferable to contain Cr 0.30 to 1.20% by weight.

Cr combines with C to form carbides and has the effect of increasing the hardness of the nitrided layer during nitriding, and is therefore an indispensable element for improving wear resistance. In order to enjoy these effects, Cr is preferably contained at 0.30% by weight. However, since the cold workability is lowered when a large amount is added, the upper limit value of Cr is preferably 1.20% by weight.
(5) Ni is preferably contained in an amount of 0.20 to 1.50% by weight.

Ni is an element necessary for improving toughness, and is preferably contained in an amount of 0.20% by weight or more. However, when a large amount of Ni is added, a large amount of retained austenite is generated, and the required hardness may not be obtained, or the structure may be changed and the dimensions may be distorted. Therefore, the upper limit of Ni is preferably 1.50% by weight.
(6) V is preferably contained in an amount of 0.05 to 0.50% by weight.

V has the effect of improving the temper softening resistance and is effective in improving thermal deformation during the ion plating process. Also, carbide is formed in the same manner as Cr, and the hardness of the nitrogen layer is increased during the nitriding treatment to improve the wear resistance. In order to enjoy these effects, V is preferably contained at least 0.05% by weight. However, if it exceeds 0.50% by weight, not only the effect is saturated, but also hot workability and cold workability are impaired, so the upper limit value of V is preferably 0.50% by weight.
(7) Other elements Cu is an element that contributes to the improvement of toughness during cold working. However, when added in a large amount, the hot workability deteriorates, so the upper and lower values of Cu are 0.15% by weight. Is preferred.

  As a solid solution strengthening element, W may be contained by 1.0% by weight or less, and Co may be contained by 1.0% by weight or less.

  Further, Ti or Nb may be contained in an amount of 0.50% by weight or less for improving the high temperature strength or refining crystal grains by combining with C.

  Further, in order to improve the high temperature strength or the grain boundary strength, B may be contained in an amount of 0.01% by weight or less and Zr may be contained in an amount of 0.10% by weight or less.

  Furthermore, in order to improve hot workability, 0.01 wt% or less of Mg and Ca can be contained.

Since the piston ring of the present invention has the above component composition, the heat resistance is improved by the mechanism described below. That is, the present inventor has found a point for improving the heat resistance based on the examination result of the manufacturing process of the conventional piston ring.
(1) Conventional Piston Ring Manufacturing Process First, a material having a predetermined composition is melted, and after hot ingoting, a wire having a predetermined wire diameter is obtained by hot rolling. Next, the wire is subjected to cold wire drawing (primary wire drawing), followed by intermediate heat treatment (annealing), and further, a wire having a predetermined wire diameter is obtained by cold wire drawing (secondary wire drawing). Next, after the wire is rolled into a rectangular cross section (deformed processing), it is quenched and tempered under predetermined conditions to ensure straightness and hardness of the wire. The wire having a rectangular cross section is coiled so as to match the outer diameter of the piston ring. However, since distortion occurs along with the coiling, heat treatment for removing distortion is performed. Finally, nitriding treatment and ion plating are generally performed.

  That is, “melting” → “hot rolling” → “primary wire drawing” → “intermediate heat treatment” → “secondary wire drawing” → “deformation” → “quenching / tempering” → “coiling” → “ The piston ring can be obtained through “strain relief heat treatment” → “nitriding treatment and ion plating”.

In general, the steps described above are performed from the start of melting until the final piston ring is obtained. It is particularly important to withstand the long-term heat treatment associated with ion plating, and to suppress the hardness reduction and thermal deformation of the piston ring, the quenching / tempering process after deforming and the distortion removing heat treatment process after coiling. Seem.
(2) Points for improving heat resistance When lattice defects are increased by deforming, these defects become precipitation sites, and carbide is precipitated in crystal grains by quenching and tempering after deforming to improve strength. Can be made. Therefore, by appropriately selecting the tempering temperature, it is possible to control the precipitation amount of carbides, and to suppress a decrease in hardness and thermal deformation even when subjected to a high-temperature and long-time heat treatment during the ion plating process, which is a subsequent process.

  Similarly, when lattice defects are increased by plastic working accompanying coiling, the defects can become precipitation sites. Therefore, it is possible to control the precipitation amount of carbide by appropriately selecting the heat treatment temperature for strain relief, and to suppress the decrease in hardness and thermal deformation even if it is subjected to heat treatment for a long time at a high temperature during the subsequent ion plating treatment. .

  Therefore, the strain relief annealing temperature is preferably 520 to 550 ° C. If it is less than 520 degreeC, the hardness after strain relief annealing will become high too much and Vickers hardness (HV0.5) may exceed 550. As described above, when the ion plating process is performed on the piston ring having a Vickers hardness (HV 0.5) exceeding 550, the ring diameter may be largely changed before and after the process. This is because if the initial hardness is too high, the ring diameter tends to increase due to a decrease in hardness and a large amount of thermal deformation due to ion plating for a long time at a high temperature. However, the piston ring diameter needs to be within a certain range because of its function. Therefore, for the piston ring having a ring diameter exceeding a certain range, additional processing steps such as polishing are further increased, which disadvantageously increases the manufacturing cost.

  On the other hand, in strain relief annealing exceeding 550 ° C., the hardness after annealing becomes too low, and the Vickers hardness (HV0.5) may be less than 480. The piston ring having a Vickers hardness (HV0.5) of less than 480 has a disadvantage that the hardness necessary for the piston ring (Vickers hardness (HV0.5) ≧ 465) cannot be obtained after the ion plating process.

Examples of the present invention will be described below. However, the present invention is not limited to the following examples, and can be appropriately changed and modified without departing from the technical scope of the present invention.
(1) Test material A material having a composition (% by weight) as shown in Table 1 below was used as a test material.

(2) Elongation amount and heat resistance during coiling molding The test material 3 in the steel types shown in Table 1 was melted, hot rolled after ingot forming, and rolled to a wire diameter of 5.0 mm. Next, the wire rod was subjected to a patenting treatment and then cold-drawn to a wire diameter of 3.5 mm (cross-sectional reduction rate = 51%). Further, the wire was kept at 700 ° C. for 4 hours and then air-cooled. Next, after rolling the wire to a rectangular section of 2.0 mm thickness × 4.8 mm width, the temperature was raised to 850 ° C. and held for 4 minutes, then oil cooled, tempered to 450 ° C. and held for 8 minutes, Air cooled. Then, after coiling the wire so that the outer diameter becomes 80 mm, it is cut into the shape of the piston ring 15 as shown in FIG. 5, and the temperature is raised to 520 to 550 ° C. and held for 1 hour to remove distortion. Cooled to (in air). Furthermore, as a heat treatment simulating the thermal history of the ion plating process (hereinafter also referred to as AIP), the temperature was raised to 440 to 460 ° C., held for 6 hours, and then cooled to room temperature (in the atmosphere). Then, by measuring the ring outer diameter after coiling, the ring outer diameter after strain relief heat treatment, and the ring outer diameter after AIP simulation heat treatment with calipers, the following equation 1 (ring diameter change rate during strain relief heat treatment) and The dimensional change rate of the piston ring was determined as shown in Formula 2 (Ring diameter change rate during simulated AIP heat treatment). At the time of the coiling molding, a part of the wire was molded with an extension amount of 5%, and another part of the wire was molded with an extension amount of 10%. As shown in FIG. 6, the ring outer diameter was measured at three locations d ₁ , d ₂ , and d ₃ for one piston ring, and measured for 10 piston rings.

  The result of calculating the ring diameter change rate based on the arithmetic average value of the above ring dimension measurement results is shown in FIGS. In FIG. 7, symbols x, y, and z indicate cases where the strain relief heat treatment temperatures are 520 ° C., 535 ° C., and 550 ° C., respectively, and the AIP simulated heat treatment temperature is constant at 450 ° C. In FIG. 8, symbols a, b, and c indicate strain relief heat treatment temperatures of 520 ° C. and AIP simulated heat treatment temperatures of 440 ° C., 450 ° C., and 460 ° C., respectively, and symbols d, e, and f indicate strain relief. The heat treatment temperature is 535 ° C., the AIP simulated heat treatment temperatures are 440 ° C., 450 ° C., and 460 ° C., respectively, the symbols g, h, and i are the strain relief heat treatment temperature is 550 ° C., and the AIP simulated heat treatment temperature is 440 ° C., respectively. 450 ° C. and 460 ° C. are indicated. In FIG. 7 and FIG. 8, the symbols “x”, “●”, and “◯” indicate the 0%, 5%, and 10% elongation amounts during coiling molding, respectively.

As shown in FIG. 7 and FIG. 8, it can be seen that the ring diameter change rate (thermal deformation amount) tends to be reduced by applying a slight extension during coiling.
(3) Comparison of steel types a. Comparison of Specimen 1, Specimen 2, Specimen 3, Specimen 4 Specimen 1, Specimen 2, Specimen 3, and Specimen 4 in the steel types shown in Table 1 were dissolved. Then, a cold wire with a wire diameter of 3.5 mm was obtained by the same process. Further, the wire was kept at 700 ° C. for 4 hours and then air-cooled. Next, the wire was rolled into a rectangular cross section having a thickness of 2.0 mm × 4.8 mm, then heated to the temperatures shown in Tables 2 and 3, held for 4 minutes, and then oil-cooled. Tables 2 and 3 After tempering to the temperature shown in FIG. Then, after coiling the wire to an outer diameter of 80 mm, cutting it into the shape of a piston ring 15 as shown in FIG. 5, raising the temperature to 525 ° C. and holding it for 1 hour to cool it down to room temperature for distortion removal (In the atmosphere). Further, as a heat treatment simulating the thermal history of AIP, the temperature was raised to 450 ° C., held for 6 hours, and then cooled to room temperature (in the atmosphere). Then, the dimensional change rate of the piston ring was obtained by measuring the ring outer diameter after the strain relief heat treatment and the ring outer diameter after the AIP simulation heat treatment with calipers as shown in the above equation 2. At the time of the coiling molding, a 5% stretching treatment was performed. As shown in FIG. 6, the ring outer diameter was measured at three locations d ₁ , d ₂ , and d ₃ for one piston ring, and measured for 10 piston rings.

  The result of calculating the ring diameter change rate (ring diameter change rate during AIP simulated heat treatment) based on the arithmetic average value of the above ring dimension measurement results and the Vickers hardness (HV0 after AIP simulated heat treatment of 10 piston rings) .5) are shown in Tables 2 and 3, respectively.

  As can be seen from Table 2, the sample material 2, the sample material 3, and the sample material 4 have a smaller change rate (thermal deformation amount) of the ring diameter than the sample material 1.

As can be seen from Table 3, the hardness of the specimen 2 is markedly higher than other steel types.
b. Comparison of Specimen 1, Specimen 2, Specimen 3, and Specimen 5 Melt Specimen 1, Specimen 2, Specimen 3, and Specimen 5 in the steel types shown in Table 1. Then, a cold wire with a wire diameter of 3.5 mm was obtained by the same process. Further, the wire was kept at 700 ° C. for 4 hours and then air-cooled. Next, the wire was rolled into a 2.0 mm thick × 4.8 mm wide rectangular cross section, heated to the temperature shown in Table 4, held for 4 minutes, oil cooled, and tempered to the temperature shown in Table 4. For 8 minutes and then air cooled. Then, after coiling the wire to an outer diameter of 80 mm, the wire is cut into the shape of the piston ring 15 as shown in FIG. Cooled to room temperature (in air). Further, as a heat treatment simulating the thermal history of AIP, the temperature was raised to 450 ° C., held for 6 hours, and then cooled to room temperature (in the atmosphere). Then, the dimensional change rate of the piston ring was obtained by measuring the ring outer diameter after the strain relief heat treatment and the ring outer diameter after the AIP simulation heat treatment with calipers as shown in the above equation 2. During the coiling molding, no stretching treatment was performed. As shown in FIG. 6, the ring outer diameter was measured at three locations d ₁ , d ₂ , and d ₃ for one piston ring, and measured for 10 piston rings.

  FIG. 9 shows the result of calculating the ring diameter change rate based on the arithmetic average value of the above ring dimension measurement results and the arithmetic average value of the Vickers hardness (HV0.5) after the AIP simulated heat treatment for 10 piston rings. Show. In FIG. 9, A represents the sample material 2, B represents the sample material 3, C represents the sample material 1, and D represents the sample material 5.

As is apparent from FIG. 9, the hardness of the specimen 2 is the highest, and the ring diameter change rate (thermal deformation amount) of the specimen 2 is about the same as that of the specimen 5 which is a high Cr stainless steel with a large amount of Cr. It is.
(4) Optimal heat treatment conditions for test material 2 As a result of the above test, it was found that the steel material suitable for the piston ring material having the least amount of thermal deformation and the highest hardness was test material 2. Then, the optimum heat treatment conditions were obtained, and experiments as described below were conducted.
a. Tempering temperature The test material 2 in the steel types shown in Table 1 was melted, and a cold-drawn material having a wire diameter of 3.5 mm was obtained by the same process. Further, the wire was kept at 700 ° C. for 4 hours and then air-cooled. Next, the wire was rolled into a rectangular section of 2.0 mm thickness × 4.8 mm width, heated to 850 ° C. and held for 4 minutes, then oil cooled, tempered to 430 to 520 ° C. and held for 8 minutes. After that, it was air-cooled. Then, after coiling the wire so that the outer diameter becomes 80 mm, cut into the shape of the piston ring 15 as shown in FIG. 5, to remove distortion, raise the temperature to 450 ° C., hold for 1 hour, and then cool to room temperature (In the atmosphere). Further, as a heat treatment simulating the thermal history of AIP, the temperature was raised to 450 ° C., held for 6 hours, and then cooled to room temperature (in the atmosphere). Then, the dimensional change rate of the piston ring was obtained by measuring the ring outer diameter after the strain relief heat treatment and the ring outer diameter after the AIP simulation heat treatment with calipers as shown in the above equation 2. During the coiling molding, no stretching treatment was performed. As shown in FIG. 6, the ring outer diameter was measured at three locations d ₁ , d ₂ , and d ₃ for one piston ring, and measured for 10 piston rings. FIG. 10 shows the calculation result of the ring diameter change rate based on the arithmetic average value of the ring dimension measurement results and the arithmetic average value of the Vickers hardness (HV0.5) after the AIP simulated heat treatment for 10 piston rings. Show. The horizontal axis in FIG. 10 is the tempering temperature (° C.). For comparison, FIG. 10 also shows data of C (test material 1, Si—Cr steel) in FIG. 9, but the Vickers hardness (HV 0. 5) is clearly lower than that of specimen 2.

As is apparent from FIG. 10, it can be seen that by tempering the specimen 2 to 450 to 515 ° C., the hardness increases and the rate of change in the ring diameter (thermal deformation amount) decreases.
b. Heat treatment temperature for strain relief Specimen material 2 in the steel types shown in Table 1 was melted, and a cold wire with a wire diameter of 3.5 mm was obtained by the same process. Further, the wire was kept at 700 ° C. for 4 hours and then air-cooled. Next, after rolling the wire to a rectangular section of 2.0 mm thickness × 4.8 mm width, the temperature was raised to 850 ° C. and held for 4 minutes, then oil cooled, tempered to 450 ° C. and held for 8 minutes, Air cooled. Then, after coiling the wire so that the outer diameter becomes 80 mm, it is cut into the shape of the piston ring 15 as shown in FIG. 5, and the temperature is raised to 450 to 600 ° C. and held for 1 hour to remove distortion. Cooled to (in air). Further, as a heat treatment simulating the thermal history of AIP, the temperature was raised to 450 ° C., held for 6 hours, and then cooled to room temperature (in the atmosphere). Then, the dimensional change rate of the piston ring was obtained by measuring the ring outer diameter after the strain relief heat treatment and the ring outer diameter after the AIP simulation heat treatment with calipers as shown in the above equation 2. During the coiling molding, no stretching treatment was performed. As shown in FIG. 6, the ring outer diameter was measured at three locations d ₁ , d ₂ , and d ₃ for one piston ring, and measured for 10 piston rings. The results of calculating the ring diameter change rate based on the arithmetic average value of the above ring dimension measurement results and the standard deviation of the ring diameter change rate are shown in FIGS. Moreover, the arithmetic average value of the Vickers hardness (HV0.5) after AIP simulation heat processing about 10 piston rings is shown in FIG.

  As apparent from FIG. 11 (a), the ring diameter change rate (%) decreases when the strain relief temperature is increased, but the reduction amount of the ring diameter change rate decreases even when the temperature is increased to 550 ° C. or higher. . Further, as can be seen from FIG. 11 (b), it can be seen that the standard deviation of the ring diameter change rate (%) becomes the smallest when the strain relief heat treatment temperature is 520 to 550 ° C. Furthermore, as can be seen from FIG. 12, the Vickers hardness (HV0.5) increases as the strain relief heat treatment temperature decreases, but the Vickers hardness (HV0.5) exceeds 500 even at a strain relief temperature of 550 ° C. It can be seen that it is extremely hard. However, when the heat treatment temperature for strain relief exceeds 550 ° C., the Vickers hardness (HV0.5) is lowered and may not be able to withstand actual use.

To summarize the above test results, in order to suppress the decrease in hardness and change in ring diameter (thermal deformation) even when subjected to long-time heat treatment accompanying ion plating treatment, typical compositions are shown as steel types. It is preferable to employ a specimen 2 composed of the components as shown in FIG. 1, and subject the specimen 2 to melting, hot rolling, primary wire drawing, intermediate heat treatment, secondary wire drawing according to a predetermined process, It can be said that the most preferable heat treatment step is a step of quenching from 450 ° C. to 515 ° C. after the rectangular cross-section processing, tempering to 450 to 515 ° C., and performing a heat treatment for removing strain at 520 to 550 ° C. after coiling.
(5) Vickers hardness and ring diameter change rate The test material 2 in the steel types shown in Table 1 was dissolved, and a cold wire with a wire diameter of 3.5 mm was obtained by the same process. Further, the wire was kept at 700 ° C. for 4 hours and then air-cooled. Next, after rolling the wire to a rectangular section of 2.0 mm thickness × 4.8 mm width, the temperature was raised to 850 ° C. and held for 4 minutes, then oil cooled, tempered to 450 ° C. and held for 8 minutes, Air cooled. Then, after coiling the wire so that the outer diameter becomes 80 mm, it is cut into the shape of the piston ring 15 as shown in FIG. 5, and the temperature is raised to 450 to 600 ° C. and held for 1 hour to remove distortion. Cooled to (in air). Further, as a heat treatment simulating the thermal history of AIP, the temperature was raised to 450 ° C., held for 6 hours, and then cooled to room temperature (in the atmosphere). For various Vickers hardnesses after strain relief annealing, the ring outer diameter after strain relief heat treatment and the ring outer diameter after AIP simulated heat treatment are measured with calipers, as shown in the above equation 2, The dimensional change rate of the ring was obtained. During the coiling molding, no stretching treatment was performed. As shown in FIG. 6, the ring outer diameter was measured at three locations d ₁ , d ₂ , and d ₃ for one piston ring, and measured for 10 piston rings. FIG. 13 shows the result of calculating the ring diameter change rate based on the arithmetic average value of the above ring dimension measurement results.

  As is apparent from FIG. 13, when the Vickers hardness (HV0.5) after strain relief annealing exceeds 550, the ring diameter change rate (%) increases.

It is principal part sectional drawing of a diesel engine. It is the schematic which shows the state which inserts the piston ring which consists of Si-Cr steel which gave Cr plating into a piston ring groove | channel. It is the schematic which shows the state which inserts the piston ring which consists of martensitic stainless steel which performed the nitriding process into a piston ring groove | channel. It is the schematic which shows the state which inserts the piston ring which consists of martensitic stainless steel which performed the ion plating process after the nitriding process in a piston ring groove | channel. It is a perspective view of a piston ring. It is a figure explaining the outer diameter measuring method of a piston ring. It is a figure which shows the ring diameter change rate at the time of the distortion removal heat processing in the test material 3. FIG. It is a figure which shows the ring diameter change rate at the time of AIP simulation heat processing in the test material 3. FIG. It is a figure which compares and shows the ring diameter change rate and the Vickers hardness at the time of AIP simulated heat processing in each steel type. It is a figure which shows the relationship between the tempering temperature in the test material 2, the ring diameter change rate at the time of AIP simulation heat processing, and Vickers hardness. FIG. 11A is a diagram showing the relationship between the strain relief heat treatment temperature in the test material 2 and the ring diameter change rate during the AIP simulated heat treatment, and FIG. 11B is the strain relief heat treatment temperature in the test material 2 and the AIP simulated heat treatment. It is a figure which shows the relationship of the standard deviation of the ring diameter change rate at the time. It is a figure which shows the relationship between the distortion removal heat processing temperature in the test material 2, and the Vickers hardness after AIP simulation heat processing. It is a figure which shows the relationship between the Vickers hardness after distortion removal annealing in the test material 2, and the ring diameter change rate at the time of AIP simulated heat processing.

Explanation of symbols

DESCRIPTION OF SYMBOLS 1 Top ring 2 Second ring 3 Piston ring groove 4 Piston ring groove 5 Oil ring 6 Cylinder wall 7 Spring 8 Hard chromium plating 9 Nitriding process 10 Hard ceramic coating 11 Piston ring 12 Piston ring 13 Piston ring 14 Piston ring groove 15 Piston ring

Claims (1)

C is 0.45 to 0.80 mass%, Si is 0.80 to 2.50 mass%, Mn is 0.10 to 1.00 mass%, Cr is 0.30 to 1.20 mass%, Ni is 0.20 to 1.50 mass%, V is 0.05 to 0.50 mass%, Cu is 0.15 mass% or less , and the balance is Fe. In a method of manufacturing a piston ring by plastic processing to a rectangular cross section, processing into a piston ring shape after quenching and tempering, applying stress plating to the piston ring and then ion plating,
The tempering temperature is 450-515 ° C.,
A method for producing a piston ring, wherein the strain relief annealing temperature is 520 to 550 ° C.

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