JP2008128476A - Bearing - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide a refrigerant compressor using a bearing having improved wear resistance while shortening a time for machining the bearing and reducing material loss. <P>SOLUTION: The bearings 2c, 4a each use a carbon graphite base material which is obtained by baking such a molded product that kneaded material containing inorganic filler is molded into an approximate usable shape. The carbon graphite base material has an area porosity of 15% or less when found under a microscope, contains ash, and is filled with α solid solution of phosphor copper or copper containing phosphor. <P>COPYRIGHT: (C)2008,JPO&INPIT

Description

  The present invention relates to a bearing.

  Three scroll compressor bearings (carbon bearing and winding bush) are used for the main bearing and the slewing bearing, and are designed to be in a fluid lubrication state in steady operation, but especially in severe transient operating environments. A local load concentrates on the upper end of the main bearing, and a frictional wear phenomenon that closely resembles the wear mark of boundary lubrication occurs.

For the bearing, a bronze-filled carbon material, which is an isotropic carbon graphite base material filled with 50% or more of bronze (BC3) in an isotropic carbon graphite base material, and PTFE (polyethylene) on a steel plate sintered with bronze. For example, a wound bush material obtained by forming a composite material coated with (tetrafluoroethylene) resin into a cylindrical shape is used.
And as an isotropic carbon graphite base material, the carbon graphite base material by which 20-50 mass% of graphite is conventionally contained as a raw material is disclosed (for example, refer patent document 1 and patent document 2).
JP 2002-213356 A JP 2003-314448 A

  Conventionally disclosed carbon graphite base materials as bearing base materials possessed by refrigerant compressors have prescribed the form of graphite related to wear resistance in the raw material composition, but in practice, graphite at the time of firing Progresses and the crystallinity of graphite changes. In fact, although it is important to evaluate the degree of crystallinity of graphite crystallites using X-ray diffraction with respect to the carbon graphite base material after firing, it has not been sufficiently studied. Therefore, there is a problem in wear resistance due to insufficient management of the form of graphite in the final form of the bearing. In addition, graphite and carbon materials have the characteristic that the standard electrode potential is noble, and the filling metal has the characteristic that Zn (zinc) is base when Cu (copper) and Sn (tin) are excluded. Lack of consideration for corrosion. Further, BC3 (bronze) filled in the conventional carbon graphite base material contains 1 to 3% of base Zn (zinc), which is inferior in corrosion resistance and easily causes corrosion wear. Furthermore, conventionally, a cylindrical bearing is formed from a carbon graphite base material formed into a block shape by cutting, but the carbon graphite base material has high hardness and is difficult to cut, so processing takes time. In addition, there is a problem that there are many material losses because there are many parts to be scraped off.

  As described above, the conventionally disclosed bearing using the carbon graphite base material mainly specifies the composition (graphite component) and hardness (shore) of the raw material, and other characteristics are sufficiently studied. Therefore, there is a problem that the mechanical strength such as wear resistance during the operation of the refrigerant compressor is not sufficiently considered, and there is no provision for the amount of wear of the bearing during the operation. In addition, there is a problem that it takes a long time to form the bearing and there is a lot of material loss.

  Therefore, the object of the present invention is to provide a bearing that is superior in mechanical strength such as wear resistance and that can reduce the time required for processing the bearing and reduce material loss compared to a conventional bearing. There is to do.

  In order to solve the above problems, the present invention uses a carbon graphite base material obtained by firing a molded product obtained by molding a mixture of carbon graphite aggregate and binder into a shape close to the shape to be used. A bearing was used. The carbon graphite base material includes 0.5 to 10% by mass of ash, and hollow open pores are formed so that the area porosity determined by microscopic observation is 15% or less. More than half of the open pores are filled with copper α solid solution, and the copper α solid solution contains phosphorous copper or phosphorus, and the phosphorus content is 0.05 to 7.5 mass%. Features.

  The bearing of the present invention provides a bearing that is excellent in mechanical strength such as wear resistance and the like, and that can shorten the time required for processing the bearing and reduce material loss compared to a conventional bearing. it can.

  One example of a compressor used in an air conditioner or a refrigeration apparatus is a positive displacement refrigerant compressor. This positive displacement refrigerant compressor has a structure in which a motor drive unit and a compression machine unit are coupled by a single shaft, and a bearing supports a load. The shaft and the bearing are required to have mechanical and chemical practical strength in an environment of lubricating oil in which refrigerant and refrigeration oil coexist. For example, when the friction coefficient is increased, the mechanical loss is increased, and when the wear amount (ΔW) is increased, noise and vibration are caused. When the sealability of the compressor chamber due to misalignment is deteriorated, the volume efficiency is decreased.

In general, an inverter control method or a multi-refrigerant sealing method is adopted for the operation of the shaft and bearing of the refrigerant compressor, and the viscosity (η) of the lubricating oil, the peripheral speed (v) of the shaft, and the shaft load (P). When the engine speed fluctuates over a wide range and starts up rapidly, an oil supply delay phenomenon occurs. For this reason, the lubrication mode of the shaft and the bearing portion shifts from fluid lubrication at steady state to intermediate mixed lubrication and the most severe boundary lubrication. Therefore, a refrigerant compressor having high reliability for a long time corresponding to the lubrication mode is required.
The present embodiment provides a bearing material and a bearing that can cope with these severe lubrication modes.

Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings as appropriate.
FIG. 1 is a schematic sectional view of a scroll type refrigerant compressor. FIG. 2 is a partially enlarged view of a portion surrounded by a one-dot chain line in FIG.

  As shown in FIG. 1, the scroll-type refrigerant compressor SC has a compression mechanism unit by disposing a compression mechanism unit, which will be described later, inside the scroll sealed container 1 and an electric mechanism unit motor 7 below. The fixed scroll member 3 and the motor 7 which is an electric mechanism part are connected via a crankshaft (shaft member) 5.

  The compression mechanism includes a fixed scroll member 3 in which a spiral wrap 3b is erected on a base plate 3a, and a revolving scroll member 2 in which a spiral wrap 2b is erected on a base plate 2a. The fixed scroll member 3 and the orbiting scroll member 2 are arranged so that the spiral wrap 3b and the spiral wrap 2b mesh with each other. A suction port 3c is formed in the outer peripheral portion of the fixed scroll member 3, and a discharge port 3d is formed in the central portion.

  As shown in FIG. 2, the crankshaft 5 is supported by a bearing 4 a (main bearing) disposed at the center of the frame 4. A crank 5 a protruding from the tip of the crankshaft 5 is inserted into a bearing 2 c (orbiting bearing) of the orbiting scroll member 2 and engaged with the orbiting scroll member 2.

  The Oldham joint 6 serving as a rotation prevention mechanism is a joint that allows the orbiting scroll member 2 to perform a revolving motion without rotating relative to the fixed scroll member 3. The Oldham joint 6 engages with the rear key groove 2 d of the base plate 2 a of the orbiting scroll member 2 and with the base key groove 4 d of the frame 4.

The operation of such a scroll type refrigerant compressor SC will be described with reference to FIGS.
In this scroll-type refrigerant compressor SC, when the crankshaft 5 is rotated by the motor 7, the orbiting scroll member 2 performs the orbiting motion with respect to the fixed scroll member 3 without rotating due to the eccentric rotation of the crank 5a. As a result, the refrigerant gas sucked from the suction port 3c is compressed in the compression chamber 3e formed by meshing the spiral wrap 3d and the spiral wrap 2d. The compressed refrigerant gas is discharged above the fixed scroll member 3 from the protrusion 3d. Then, the compressed refrigerant gas reaches from the upper side of the fixed scroll member 3 to the lower side of the frame 4 through the communication hole 3g and is discharged from the discharge port 3f to the outside of the scroll hermetic container 1.

As described above, the scroll type refrigerant compressor SC as described above is provided with the bearing 2c on the base plate 2a and the bearing 4a on the frame 4 respectively. And the circulating lubricating oil (refrigerating machine oil containing a refrigerant | coolant) is supplied to both the bearing 2c and the bearing 4a. In such a bearing 2c and bearing 4a, when the scroll-type refrigerant compressor SC is started or when the discharge pressure of the refrigerant is high, supply of lubricating oil is insufficient and damage such as wear and seizure is likely to occur.
However, as shown in FIG. 2, the bearings 2 c and 4 a of the present embodiment are press-fitted and fixed to predetermined positions of the base plate 2 a and the frame 4 of the orbiting scroll member 2, respectively. The reliability and durability of the SC can be improved.
Of course, at this time, the bearings 2c and 4a may be attached to predetermined positions of the base plate 2a and the frame 4 by means of shrink fitting, cold fitting, screw fitting, fitting, adhesive, or the like. Since the pressure crushing strength (crushing load) at the time of press-fitting is required to be 18.6 MPa (150 N) or more, the crushing strength of the bearings 2c and 4a is sufficient to withstand a load higher than this. Is set. The crushing strength referred to here is obtained by the sintered bearing-crushing strength test method shown in JIS Z 2507. Specifically, in the bearings 2c and 4a used in the scroll-type refrigerant compressor SC shown in FIG. 1, for example, the size is an outer diameter Φ19 mm, an inner diameter Φ16 mm, and a height 14.3 mm. The crushing load of the bearings 2c and 4a is 150 N or more, and the crushing strength is 18.6 MPa or more.

  Next, an example in which the bearing of this embodiment is used in a rotary type refrigerant compressor different from the scroll type refrigerant compressor SC (see FIG. 1) will be described with reference to the drawings as appropriate. FIG. 3 is a schematic cross-sectional view of a rotary type refrigerant compressor. 4 is a partially enlarged view of a portion surrounded by a one-dot chain line in FIG.

As shown in FIG. 3, the rotary type refrigerant compressor RC is different from the scroll type refrigerant compressor SC (see FIG. 1) in that the compression mechanism portion 9 is disposed below the frame 14 in the rotary sealed container 8. In addition, the motor unit 10 as an electric mechanism unit is disposed above the frame 14. And the rolling piston 13 eccentrically attached to the crankshaft 12 driven by the motor unit 10 is configured to suck and compress the refrigerant.
The compressed refrigerant is discharged from a discharge port (not shown) to become a high-temperature and high-pressure gaseous refrigerant, and is discharged to the heat exchanger side (condenser and evaporator) constituting the refrigeration cycle via the discharge pipe 11. The The heat-exchanged refrigerant is sucked into the rolling piston 13 through the suction port 13a and is compressed again by the rolling piston 13.
As shown in FIG. 4, the bearing 15 is a bearing of the crankshaft 12 and is attached to the frame 14 by means such as press fitting, shrink fitting, cold fitting, screw fitting, fitting, coupling, adhesive, or the like. It has been.

The bearing 15 is set to a strength that can withstand a load of 150 N (18.6 MPa) or more as a pressure ring load (pressure ring strength) at the time of press-fitting.
Bearings 2c, 4a (see FIG. 2) and bearing 15 (see FIG. 4) used in the scroll type refrigerant compressor SC (see FIG. 1) and the rotary type refrigerant compressor RC (see FIG. 3) [ Hereinafter, it may be simply referred to as “bearing”] is a material in which a predetermined metal described later is included in an anisotropic carbon graphite base material, as will be described later in the method of manufacturing the bearing.

Such a scroll-type refrigerant compressor SC and a rotary-type refrigerant compressor RC (hereinafter, sometimes simply referred to as “refrigerant compressor”) move (circulate) the refrigerant in the refrigeration cycle and the heat medium of the refrigeration oil. Is used to cool or heat the room. At this time, the kind of refrigerant and refrigerating machine oil used in the refrigerant compressor described above is very important in relation to the bearing. Specifically, the material eluted from the bearing into the mixture of the refrigerant and the refrigerating machine oil, more specifically, the carbon graphite base material to be described later, which is a component of the bearing, is 1% by mass or less, and the flock point It is desirable that no precipitate is deposited in the mixture.
Here, “the precipitate does not precipitate in the mixture” means a state in which the precipitate is not visually detected in the flock point test. The flock point test is performed in accordance with ASTM or JIS K 2211. For example, a test piece is placed in 90% by mass of refrigerant and 10% by mass of refrigerating machine oil, and is extracted by heating under specified conditions. This is a test for cooling to −40 ° C. after the treatment and evaluating the presence or absence of the precipitated substance.
Examples of the refrigerant that realizes such a combination include at least one selected from a halogenated hydrocarbon refrigerant, a hydrocarbon refrigerant, and a natural refrigerant. That is, these refrigerant | coolants can be used individually or in combination as appropriate.
Examples of the halogenated hydrocarbon refrigerant include a fluorinated hydrocarbon refrigerant, a fluorinated bromide hydrocarbon refrigerant, a fluorinated iodohydrocarbon refrigerant, and the like.
Among these refrigerants, preferred are fluorinated hydrocarbon (HFC) refrigerants such as R410A, R404A, R407C, and R134a, fluorinated iodocarbon refrigerants such as CF ₃ I, and carbonization such as R600a and R290. Examples thereof include hydrogen refrigerants, natural refrigerants such as R744 and R717, and the like. In particular, a fluoroiodohydrocarbon refrigerant is preferable in that it has a low environmental load.
The refrigerating machine oil that realizes such a combination includes, for example, mineral oil, polyol ester (POE) oil, polyalkylene glycol (PAG) oil, polyvinyl ether (PVE) oil, polyalphaolefin (PAO) oil, and hard oil. Examples thereof include at least one selected from alkylbenzene (HAB) oils. That is, these refrigerating machine oils can be used alone or in appropriate combination.

Next, a bearing manufacturing method will be described mainly with reference to FIG. FIG. 5 is a process diagram for explaining the bearing manufacturing method according to the present embodiment. In FIG. 5, comparison with a conventional process is also described in order to clarify differentiation from the present embodiment. Incidentally, in FIG. 5, the conventional process is shown as “current material manufacturing method” surrounded by a one-dot chain line.
In this manufacturing method, as shown in FIG. 5, first, an inorganic filler serving as an aggregate, graphite (artificial graphite, natural graphite, etc.), coke (coal, petroleum, etc.) and a binder serving as a binder (coal or For example, coal tar pitch obtained from petroleum is mixed at a ratio of 3 parts by mass of binder to 7 parts by mass of aggregate (Step 1). In this mixing, although not shown, it is desirable to add a coupling agent (a silane coupling agent, a titanium coupling agent, etc.) for uniformly dispersing the inorganic filler.

In Step 1, the inorganic filler, graphite, and coke constituting the aggregate are mixed with a mixer or the like. In this mixing, the above coupling agent is put into a mixer or the like. This coupling agent contains, for example, carbide easily forming elements such as Si, Ti, Zr, Al, Cr, and Mo. Specifically, the above-described silane coupling agent, titanium coupling agent, etc. Is mentioned.
The coupling agent can uniformly disperse the solid substance in the binder (petroleum pitch, etc.) by coating the surface of the solid substance (coke, graphite, inorganic filler). When the solid material is uniformly dispersed in this way, the torque of the kneader described later becomes less resistant and the workability is further improved.

Moreover, the abrasion resistance at the time of a heavy load can be improved by mix | blending an inorganic substance moderately. When the inorganic content is small, the bearing is too soft for the Fe-based shaft, and the bearing is likely to be worn. On the other hand, when the amount is large, the bearing is too hard for the Fe-based shaft and the shaft is shaved. For this reason, the bearing of this embodiment prescribes | regulates the moderate inorganic compounding range. In addition, wear resistance at high loads can be improved by appropriately blending an inorganic material so as to have an appropriate hardness with respect to the Fe-based shaft. That is, if the hardness is low, the bearing is damaged by the load of the shaft. Conversely, if the hardness is high, the shaft is scratched and worn.
For this reason, in this embodiment, as described above, an inorganic filler is blended in the aggregate.

  Examples of the inorganic filler include those containing at least one oxide selected from Si, Fe, Mg, Al, and Ca. The inorganic filler has a Mohs hardness of 3 or less, preferably 1 to 3 when the raw material containing it is fired to form a carbon graphite base material. It is blended as follows.

  In Step 2, the aggregate mixed in Step 1, the above-described binder constituting the binder, and the above-described coupling agent are mixed. This mixing is performed at a temperature of 150 to 160 ° C., for example. As a result, the aggregate is dispersed and mixed in the binder, whereby a bulky kneaded material is obtained.

Next, in Step 3, the bulk kneaded material is subjected to a pulverizer and a granulator to be subjected to particle size classification to obtain raw material pellets.
And in Step4, it mixes so that the magnitude | size of the particle | grains (raw material pellet) which carried out the particle size classification may become suitable. As a result, raw material pellets suitable for fluidity and mold filling (hereinafter, simply referred to as “raw material”) are obtained.

Next, in N-Step 5, the following mold powder molding is performed. That is, in this N-Step 5, a molded product obtained by molding the raw material into a shape close to a shape used as a bearing, for example, a bearing according to the present embodiment is obtained. The “shape close to the shape used” here includes a so-called “near net shape”, and may be a shape close to the shape of the target bearing, or a plurality of target bearings may be included. The shape may be close to a continuous long raw material. In the case of a long length, a predetermined length is cut out from the raw material, and the bearing is manufactured. Further, the “shape close to the shape to be used” may be a columnar shape when the bearing is cylindrical. It will be formed in a shape.
Incidentally, in the manufacturing method according to the present embodiment, the raw materials are molds one by one using a powder molding machine such that the raw material has a cylindrical shape with an outer diameter of Φ20.5 mm, an inner diameter of Φ11.5 mm, and a height of 25 mm. Molded. For this molding, a uniaxial pressing method from the vertical direction is employed. In this uniaxial pressing method, for example, an ejection method molding method having upper and lower punches, a withdraw wall molding method, or the like is used.

  Both of these molding methods improve the density distribution of the green compact. Both of these molding methods utilize upper and lower punches in order to prevent a decrease in density of the corner portion on the side opposite to the punch, which was a problem with conventional unidirectional die hydraulic presses. Here, the orientation of the graphite crystal when the upper and lower punches are used will be described with reference to the drawings as appropriate. FIG. 6 to be referred to is an explanatory view of a graphite polycrystalline aggregate model included in the bearing, (a) is a diagram showing a conventional random graphite aggregate, and (b) is a diagram showing an aligned plate-like graphite aggregate. It is.

  As shown in FIG. 6 (a), the conventional one that does not use the upper and lower punches forms a random graphite aggregate in which the orientations of the graphite crystals are randomly arranged. On the other hand, when the above-described upper and lower punches are used, the random graphite aggregate is an aligned plate-like graphite aggregate in which the orientations of the graphite crystals are aligned (aligned) as shown in FIG. Become. By making good use of the orientation direction, the performance of the bearing described later is further improved. FIG. 7 referred to here is a perspective view showing a graphite crystal structure.

  As shown in FIG. 7, the graphite crystal is an aggregate represented by a hexagonal crystal. The net plane [(004) plane] of this crystal has a small friction coefficient and acts as a solid lubricant. The reason why the friction coefficient is small is that the gaps between the crystals are wide and the crystals easily slip. On the other hand, the (110) plane orthogonal to the (004) plane of the hexagonal crystal is hard and has a high-strength chemical bond. Therefore, the bearing described later according to the present embodiment uses this (110) surface as a sliding surface (thrust surface) of the bearing.

  Next, in N-Step 6 shown in FIG. 5, the mold powder molded body (green molded body) which is the molded product obtained in N-Step 5 is fired. This firing is performed in a non-oxidizing atmosphere, for example, at 1000 ° C. for 0.5 months. The above-described carbon graphite base material is obtained by this firing. This carbon graphite base material has substantially the same shape as the bearing because the mold powder compact before firing has a shape close to the shape of the bearing. Further, since the carbon graphite base material is thin, there is no temperature difference between inside and outside in the firing process. As a result, there is no cracking or chipping due to distortion. And, for example, the reactive substance produced by the reaction between carbon and the inorganic filler is not left on the carbon graphite base material. In addition, the time required for firing is halved compared to the prior art.

In the carbon graphite base material thus obtained, the binder (binder) chemically completes the carbonization reaction, and becomes 90 to 99% by mass of fixed carbon and 0.5 to 10% by mass of ash. The binder before firing contains 36 to 60% by mass of fixed carbon.
Further, the volatile content of the carbon graphite base material is 1% by mass or less.
Incidentally, the fixed carbon can be measured in accordance with JIS R 7212 or JIS K 2425. Ash content can be measured according to JIS R 7223, JIS M 8812, JIS M 8511, or JIS K 2425. The volatile content of the carbon graphite base material can be measured according to JIS R 7212, JIS M 8812, or JIS M 8511.
The above-mentioned ash is mainly composed of an inorganic substance contained in graphite, coke and the like, and an ash of an inorganic filler blended for improving the function.

  The ash content can be adjusted, for example, by estimating in advance the ash content of coke or graphite used as a raw material and the ash content of the inorganic filler. Such estimation may be performed so that the ash content converted from the oxide of the inorganic filler is 0.5 to 10% by mass.

  Incidentally, the ash content of coke is 0.19% by mass, the ash content of artificial graphite is 0.1% by mass or less, the ash content of scaly graphite is 1.12% by mass, and the ash content of earthy graphite is 19.6%. The ash content of the highly crystalline graphite is 0.1% by mass or less, and the ash content of the amorphous graphite is 0.33% by mass. These graphites may be used alone or in any combination.

  On the other hand, the mechanical strength and frictional wear characteristics of the carbon graphite base material (or bearing) are improved by positively blending the inorganic filler. In other words, when a very small amount of undecomposed raw material other than fixed carbon remains in the carbon graphite base material, in the bearing incorporated in the refrigerant compressor, the undecomposed raw material softens and swells and the strength thereof decreases. The undecomposed raw material is eluted into the refrigerating machine oil and the refrigerant, and is precipitated in the refrigerant flow path to obstruct the refrigerant flow. From the above, in the bearing of this embodiment, it is important to completely eliminate the undecomposed raw material in the carbon graphite base material, and the carbon graphite base material used for the bearing of this embodiment is as described above. It consists of a range of fixed carbon and ash.

In addition, the binder from which petroleum pitch, coal pitch or the like is a raw material is generally a compound of carbon and hydrogen, the fixed carbon measured in accordance with JIS K 2425 is 55% by mass, and the rest is hydrogen or the like. It is. And a softening point is 73-92 degreeC.
Such binder undecomposed material after firing is softened in the usage environment of the refrigerant compressor and eluted into the refrigeration oil and refrigerant, thereby reducing the strength of the bearing and It causes troubles such as clogging of refrigerant piping due to deposition.

In N-Step 6 in the bearing manufacturing method of the present embodiment, in order to suppress the occurrence of these obstacles, the raw material containing the above-described binder is thermally decomposed while being gradually heated at 400 ° C. or higher, Finally, it is baked by being heated up to 800-2000 ° C. and completely coked.
In this production method, the temperature is raised to 800 to 2000 ° C., so that the inorganic filler as a raw material reacts with carbon to prevent generation of a substance that impairs the characteristics of the carbon graphite base material. it can. Incidentally, as a method for indirectly evaluating the characteristics of the carbon graphite base material, for example, a method of performing a flock point test or a method of performing a low temperature precipitation test by a shield tube test can be cited.

  And the carbon graphite base material obtained in this way is a carbon graphite base material having anisotropy. In other words, the mold powder molded body (green molded body) obtained in N-Step 5 is an aligned plate-like graphite aggregate in which the orientation of the graphite crystals is oriented. In the porous base material, graphite crystals have anisotropy.

The orientation of the graphite crystal in the carbon graphite substrate in this embodiment is 1.2 or more in terms of the anisotropic ratio (Ra) represented by the following formula (1).
Ra = I ₁ / I ₂ (1)
(In the above formula (1), I ₁ is the integral intensity ratio ((110) plane of the (004) plane and (110) plane) of the graphite crystal on the sliding surface with the shaft of the bearing. Integrated intensity / integrated intensity of (004) plane), and I ₂ is an integrated intensity ratio ((110) by X-ray diffraction of the (004) plane and (110) plane of the graphite crystal in a plane orthogonal to the sliding plane. ) Represents the integral intensity of the plane / (004) integral intensity of the plane))
The basis for the anisotropic ratio of 1.2 or more will be described later.

The carbon graphite base material in this embodiment has a crystallinity of 15 to 50% by X-ray diffraction.
The carbon graphite base material as described above preferably has a flexural strength of 50 MPa or more and a compressive strength of 180 MPa or more, and the average area porosity determined with a microscope of the pores is 15% or less. It is desirable that

  Next, in N-Step 7, the carbon graphite base material is put into a vacuum high-pressure filling furnace. At this time, after the vacuum high-pressure filling furnace containing the molten metal (copper α solid solution) is evacuated, the carbon graphite base material is immersed in the molten metal. Next, nitrogen gas is introduced into the vacuum high-pressure filling furnace and the inside of the vacuum high-pressure filling furnace is pressurized to 1 to 20 MPa. As a result, the voids (pores) of the carbon graphite base material are filled with molten metal. In addition, as for the filling rate of a molten metal, 10-50 mass% of a product (bearing mentioned later) is desirable.

Next, in N-Step 8, the carbon graphite base material after filling is finished into the final shape of the product. This finishing process is described as “bearing process 1” in FIG.
At this time, since the shape of the carbon graphite base material before filling is substantially the same as the shape of the bearing as described above, there is little material loss in this finishing process. And the bearing of a refrigerant compressor is obtained through such finishing.

  Next, a conventional method for manufacturing a bearing (current material manufacturing method), that is, a method for manufacturing a large number of bearings from a block molded body will be described with reference to FIG. Note that Step 1 to Step 4 in FIG. 5 are shared, but conventionally, only the amount of graphite is specified. Therefore, inorganic fillers and binders (including coupling agents) are not used in the processes corresponding to Step 1 to Step 4 in the conventional bearing manufacturing method. In other words, new characteristics due to the chemical change of the substance that is the feature of this embodiment (fixed carbon is 99.0% by mass or more, the strength is reduced under the use environment of the compressor, softening or swelling by refrigerating machine oil or refrigerant, or It does not give rise to the property of not producing an extract). In other words, the addition of the aggregate, binder and coupling agent of the present embodiment produces the above characteristics in the firing (N-Step 6) stage, and the bearing performance and reliability are improved when the bearing is processed at N-Step 8. Is done.

  As shown in FIG. 5, CIP molding is performed in O-Step 5 in the present method for producing a material. In this O-Step5, the raw materials that are appropriately mixed with the size of the particles classified in Step4 and matched to the fluidity and mold filling properties are filled into a rubber mold that makes a block material of about 200 mm x 400 mm x 800 mm, for example. The The rubber mold filled with this raw material is immersed in the liquid and is subjected to isotropic compression molding by applying hydraulic pressure from all directions. As a result, a block material precursor is formed.

  Next, in O-Step 6, the block material is baked to form the block material. The firing temperature and time are, for example, 1000 ° C. × 1 month. The graphite crystal contained in the block material thus obtained is a random graphite aggregate shown in FIG. 6A, which is a so-called isotropic carbon graphite base material.

  Next, in O-Step7, the block material is processed into a rectangular bar material in cross-sectional view. The equipment used at this time is a cutting machine such as a sawing machine. In addition, the bar material was cut to 23 mm × 23 mm × 300 mm, for example, and surface-finished so as to approximate the final shape of the bearing to 21 mm × 21 mm × 300 mm.

Next, in O-Step8, a molten metal filling process is performed in a vacuum high-pressure filling furnace as in N-Step7 except that the bar material is used instead of the carbon graphite base material used in N-Step7. Is done.
Next, the bearing is completed through bearing processing 1 of O-Step 9, bearing processing 2 of O-Step 10, and bearing processing 3 of O-Step 11. In the bearing processing 1, the bar material is processed into a cylindrical shape by a processing device such as an NC lathe. Further, in the bearing processing 2, the columnar bar material is processed into a cylindrical shape. Further, in the bearing processing 3, the bar material having a cylindrical shape is finished by a finishing device to become a target bearing.

  As described above, the current bearing molding method surrounded by the alternate long and short dash line has many processes, and the bearing material is made by cutting out from the bar material. There were problems such as bad material loss. Moreover, since the graphite crystal orientation is not considered in the firing stage, the performance and reliability of the bearing are insufficient unlike the bearing of the present embodiment.

Next, with reference to FIG. 8A, FIG. 8B, and FIG. 10, the porosity of the carbon graphite base material used in the bearing of this embodiment, the orientation of the graphite crystals, and the like will be described. FIG. 8A is a microscopic structure diagram of the carbon graphite base material of the present embodiment, and FIG. 8B is a diagram showing a distribution of pore diameters. FIG. 10 is a diagram showing the degree of crystallinity of the carbon graphite base material and the area ratio of the graphite structure by Raman analysis.
Here, reference numeral 16 shown in FIG. 8A indicates an inorganic filler containing Al, Si, etc., reference numeral 17 indicates open holes, reference numeral 18 indicates closed holes, and reference numeral 19 indicates carbon graphite. Show. Incidentally, the inorganic filler 16 may be blended in order to increase the hardness and wear resistance of the bearing, or may be contained as an impurity in a raw material such as graphite.
In the bearing of this embodiment, as described above, these inorganic fillers are collectively referred to as ash (0.5 to 10% by mass in terms of oxide).

  The open pores 17 are a gap through which a gas generated by thermal decomposition of the binder is released, and a gap formed between the raw material particles when metal powder molding is performed (see N-Step 8 in FIG. 5). There are holes left during sintering. These holes are continuous holes. As shown in FIG. 8B, these continuous holes are distributed in a diameter range of about 1 to 15 μm. These holes are filled with 50% by mass or more of metal.

  Next, Table 1 shows the relationship between the molding pressure of the powder molding machine and the area porosity.

  As shown in Table 1, the isotropic carbon graphite base material obtained when the molding pressure by the hydrostatic molding method is 100% has an average area porosity of 10.86% in a 100-fold microscope field of view. The anisotropic carbon graphite base material obtained when the molding pressure is 100% has an average area porosity of 9.07%.

Further, the anisotropic carbon graphite base material obtained when the molding pressure is 97% has an average area porosity of 14.13% and an molding area pressure of 95% has an average area porosity of 17.36%. It has become. This indicates that the molding load is transmitted to the contact surface of the raw material particles and further transmitted to the lower raw material particles.
Here, FIG. 9A is a distribution diagram showing a molding pressure distribution when a raw material is compression-molded only by an upper punch in a powder molding die, and a density distribution (porosity after firing) thereby.
When the raw material is compression-molded only with the upper punch, the raw material particles do not exhibit sufficient pressure transmission due to slip resistance of the mold wall surface. As a result, as shown in FIG. 9A, the bottom corner portion is a low-density and porous portion with a small pressure action. The porous portion having a low density deteriorates the mechanical strength and frictional wear resistance characteristics described later.

FIG. 9B is a distribution diagram showing a molding pressure distribution when a raw material is compression-molded by both an upper punch and a lower punch in a powder molding die, and a density distribution (porosity after firing) thereby. is there.
When the raw material is compression-molded by both the upper punch and the lower punch, the low-density porous portion, that is, the fragile portion generated when compression molding is performed only by the upper punch is eliminated, as shown in FIG. 9B. In addition, the porosity distribution is sound. In other words, the mechanical strength and frictional wear resistance quality of the bearing described later are greatly improved. In particular, the upper and lower parts, such as bearings, provide the punch pressure effect. For parts that require the strength required for assembly press-fitting of the compression mechanism and the concentrated load of the axial load of the compressor, the porosity and mechanical The intensity distribution works effectively. This part is filled with a metal described later at high pressure.

  Further, the closed hole 18 (see FIG. 8A) includes a binder (for example, coal tar pitch, coal pitch, petroleum pitch) and a coupling agent (for example, a silane coupling agent, a titanium coupling) serving as a binder. The gas generated by thermal decomposition of the agent) and the like remains in the structure and becomes independent vacancies. This independent hole is difficult to be filled with metal during filling.

The carbon graphite 19 (see FIG. 8 (a)) shows a structure after a kneaded body made of raw material graphite, coke, binder (binder), coupling agent and the like is fired. The rate is measured by Raman spectroscopy. The graphite crystallinity of this part can be specified by X-ray diffraction. FIG. 10 referred to here is a graph showing the relationship between the graphite crystallinity by X-ray diffraction in a carbon graphite base material and the graphite area ratio of the matrix by Raman analysis. The graphite area ratio was measured using a laser Raman spectroscopic analyzer manufactured by RENISHAW. This measurement was performed using a He—Ne laser under the conditions of a laser output of 25 mV, a wavelength of 682.8 mm ⁻¹ , a wavelength resolution of 0.2 cm ⁻¹ , and a spatial resolution of 1 μm (maximum 200 μm). The graphite crystallinity was measured using an Rigaku X-ray diffractometer (RINT2500HL). This measurement was performed using a Cu X-ray source and an X-ray output of 50 kV (250 mA). As an optical system in the X-ray diffraction apparatus, a concentrated beam with a monochromator was used, the slit DS was set to 0.5 deg, the slit RS was set to 0.15 mm, and the slit SS was set to 0.5 deg.
The degree of crystallinity of the carbon-graphite base material is obtained by comparison by preparing a standard sample with a known raw material in advance by the ratio of the crystalline graphite peak to the peak of amorphous coke, etc. by X-ray diffraction. Is possible. Thereby, it becomes possible to prescribe | regulate the quantity and characteristic of graphite which are required for the characteristic of a bearing. Thereby, it becomes possible to prescribe | regulate the quantity and characteristic of graphite which are required for a bearing characteristic.

In this embodiment, as shown in FIG. 10, the crystallinity of the carbon graphite base material is 15 to 50%. If the crystallinity is 15% or less, the lubricity of the bearing is poor, and the mating shaft material is worn. If the crystallinity is 50% or more, the wear characteristics of the bearing are inferior, which is not preferable as a bearing for a refrigerant compressor.
Moreover, the area ratio of the matrix of the carbon graphite base material by Raman spectroscopic analysis can distinguish amorphous coke and crystalline graphite by the magnitude | size of two types of peak waveforms. This area ratio is obtained by estimating the area ratio of graphite using a known standard sample. As described above, the graphite in the carbon graphite base material of the bearing used in the present embodiment is specified. This corresponds to 45 to 68% in terms of area ratio.

Next, when evaluated by a frictional wear test of a bearing obtained by using such a carbon graphite base material, it becomes as shown in FIGS.
FIG. 11 is a graph showing the relationship between the degree of graphite crystallinity and the amount of wear. FIG. 12 is a diagram showing the relationship between the average area porosity and the wear amount. FIG. 13 is a diagram showing the relationship between the anisotropic ratio and the amount of wear.
As shown in FIG. 11, when the degree of crystallinity of the graphite is less than 15% (for example, 45% in terms of the area ratio of the graphite structure), the hardness of the counterpart shaft material (hardness after quenching: H _V 450 or more) is high. Damage to the material is undesirable. On the other hand, when the degree of crystallinity exceeds 50% (for example, 58% in terms of the area ratio of the graphite structure), the wear amount is soft and exceeds the reference value.

  As shown in FIG. 12, when the area porosity is 15% or more, the wear amount of the bearing is increased and the wear amount of the shaft is also increased. This is considered to be due to the fact that the actual test surface pressure with the shaft increases as the porosity increases, and the bond strength between the particles of the bearing material decreases. Therefore, in the present embodiment, the area porosity is specified to be 15% or less. In FIG. 12, the circles indicate the values of the conventional isotropic carbon graphite base material.

In the frictional wear test in boundary lubrication with the refrigerant R410A, in the winter heating operation of a refrigeration apparatus such as an air conditioner, the refrigerant is unevenly distributed from the high temperature side indoor unit to the bottom of the refrigerant compressor of the low temperature side outdoor unit. Assume that a condition occurs. Further, in rapid start-up operation and defrosting operation, it is assumed that refrigerant or refrigeration oil in which a large amount of refrigerant is dissolved is supplied to the bearing portion with a slight delay.
Under the above operating conditions (test conditions), Conventional Example 6 in FIG. 23 is a bearing material that has been used. The amount of wear was 27 μm / 2h (13.5 μm / h). The amount of bearing wear is related to the sealing performance (leakage resistance) in the gap between the cylinder and piston of the rotary refrigerant compressor, the sealing performance of the shaft and bearing of the scroll type refrigerant compressor, that is, the sealing performance of the compression chamber. ing.
Therefore, this time, 20 μm / 2h (10 μm / h) is set as a target value in order to cope with severer operating conditions and aim for higher efficiency and higher reliability. This is a target value that is necessary for continuously maintaining the volumetric efficiency in the cylinder and the volumetric efficiency of the compression chamber over a long period of time. In other words, the wear amount of the bearing is 20 μm / 2h or less (10 μm / h) or less, that is, a test load of 9.8 MPa with respect to the short-term transient severe operating condition assumed by the wear test as described above. The target value is 10 μm / h or less.
Therefore, the anisotropic ratio corresponding to the wear amount of 10 μm / h requires 1.2 as shown in FIG.
As shown in FIG. 13, when the anisotropic ratio increases, the amount of wear decreases. A conventionally known isotropic carbon graphite base material has an anisotropic ratio of 1.0. As can be seen from FIG. 13, the specimen with an anisotropic ratio of 1.5 has a wear amount of 5.4 μm / h, whereas the conventional specimen with an anisotropic ratio of 1.0 becomes 13.6 μm / h, which is about 1 / 2.5. Double the amount of wear. Further, it was found that the one with an anisotropic ratio of 1.8 has a wear amount of about 1 / 4.6 times when the wear amount is 2.95 μm / h. As described above, the anisotropic ratio is preferably 1.2 or more.
Next, the anisotropic ratio indicating the orientation of the graphite crystal by X-ray diffraction of the carbon graphite test material was measured. The results are shown in Table 2. This measurement was performed using an Rigaku X-ray diffractometer (RINT2500HL). This measurement was performed under the condition of an X-ray output of 50 kV (250 mA) using a CuX ray source. As an optical system in the X-ray diffraction apparatus, a concentrated beam with a monochromator was used, the slit DS was set to 0.5 deg, the slit RS was set to 0.3 mm, and the slit SS was set to 0.5 deg. FIG. 14 referred to here is a perspective view of a test piece that makes the best use of the (110) plane of the graphite crystal formed when press molding.

The anisotropic ratio here is the X-ray diffraction when the integrated intensity ratio between the sliding test surface and its right-angle plane is determined by the peak integrated intensity and the integrated intensity ratio of the (004) plane and the (110) plane. Each ratio is defined as an anisotropic ratio. That is, the anisotropic ratio is obtained by the above-described formula (1).
As shown in Table 2, the block shape made of the isotropic carbon graphite base material of Conventional Example 1 has an anisotropic ratio of 1.025, whereas the cylindrical shaped product of Example 1 has 1. It was found to be 791.
Next, the frictional wear characteristics and the mechanical characteristics of the test piece collected from the cylindrical base material made of the carbon graphite base material used for the bearing of the present embodiment are the conventional isotropic carbon graphite base material. Contrast with

  Here, the test piece will be described first. FIG. 15 is a schematic diagram showing the sampling position of the test piece on the cylindrical base material. As shown in FIG. 15, the lateral A-plane whose test surface is indicated by diagonal lines is a plane in which the network surface of the graphite crystal is oriented with high density by press forming, and the (004) plane by X-ray diffraction is concentrated. Oriented surface.

  Next, the friction and wear characteristics and mechanical characteristics described above were evaluated for such a test piece T. First, a mating material (SCM) was formed in a cylindrical shape with the oblique line surface of each test piece T as a sliding surface, and a frictional wear test was performed in the gas of refrigerant R410A. The results are shown in Table 3. In addition, the test method of the friction wear test in the gas of R410A is the same as the friction wear evaluation test method of the metal-filled carbon graphite base material described later.

  As shown in Table 3, when the B surface is a sliding surface in Example 3 (molding pressure -3%), the wear amount of the test piece T is the test piece of the isotropic carbon graphite base material of Conventional Example 2. The wear amount of the counterpart material is equal to or less than 1/3 of that of the isotropic carbon graphite base material of the conventional example 2, but when the A surface is a sliding surface in Example 4, the wear of the test piece T The amount increases 1.65 times that of Conventional Example 2.

  Further, in Example 5 in which the molding surface is 5% and the B surface is a sliding surface, the wear amount of the test piece T is 2.2 times that of the conventional example 2, and the wear amount of the counterpart material is 2.5 times. . In addition, the friction coefficient of Example 5 at this time is 1.4 times larger than that of Conventional Example 2. As described with reference to FIG. 12, this occurs due to the porosity. That is, when the molding pressure is lowered from -3% to -5%, the density of the green powder decreases, the porosity increases, the mechanical strength decreases, the test surface pressure increases in the actual test, and the forced orientation degree of the graphite crystal decreases. It is thought to be.

  Further, the thermal conductivity (W / m · K) of the B surface of Example 3 is about 1.16 times better than that of Example A. This macroscopically represents the anisotropic ratio of graphite. Further, in Example 2 (molding pressure -0%), the wear amount of the test piece T is 1 / 1.5 compared with the test piece T of the isotropic carbon graphite base material of Conventional Example 2, The amount of wear was 1/3, confirming that it was excellent. This is the effect of the orientation of the graphite crystal, which is one of the features of this embodiment.

  Further, the mechanical properties of Example 2 (molding pressure-0%) are the same as the isotropic carbon graphite base material of Conventional Example 2 and the crushing load (crushing strength) is the same, and the bending strength and hardness are slightly higher. Although it was low, it turned out that it was a level which is satisfactory practically. Moreover, the regulation of bending strength and compressive strength required for the bearing is not clarified in the conventional one. That is, a bending strength of 50 MPa or more applied to the bearing during press-fitting corresponds to a crushing strength of 18.6 MPa (compression ring load 150 N) or more, and the bearing according to the present embodiment preferably has a strength that can withstand this crushing load. Further, the compressive strength of 180 MPa or more corresponds to the load resistance of the bearing and the shaft (shaft). That is, if the compressive strength is weak, the shaft (shaft) is broken and abnormal wear occurs. When strong, it was found that the damage can be kept very small, so that reliability can be secured.

Next, the result of the thermochemical stability test of the carbon graphite base material used for the bearing of this embodiment will be described.
A shield tube test (150 ° C., 40 days) was performed on a combination of a typical refrigerant used in an air conditioner, a refrigerator, a water heater, and the like and a refrigerating machine oil (viscosity grade). And the appearance, the low temperature precipitation property (−40 ° C.) of the eluate, the increase in the total acid value due to the deterioration of the refrigerating machine oil, and the change in the bending strength of the carbon graphite base material were studied. The results are shown in Table 4.

As shown in Table 4, in the evaluation of the compatibility of the HFC refrigerants of R410A, R134a, R407C, and R404A with ester oil (POE) and polyvinyl ether oil (PVE oil), both refrigeration oil, low temperature precipitation, and bending strength No abnormality is observed. In addition, no abnormality was observed in the combination of the hydrocarbon refrigerant of R600a or R290 and mineral oil (MO) as described above. Furthermore, a similar test was performed using a high-pressure vessel with a combination of R744 (CO ₂ ), R717 (NH ₃ ), PAG, and MO, and after taking out after the test, R134a was newly enclosed and a low-temperature precipitation test was performed. No abnormalities were found in the samples, which proved to be good. From these, it became clear that it is practically suitable as a bearing material for a refrigerant compressor used in the coexistence of the refrigerant and refrigeration oil.
Moreover, since the baked carbon graphite base material has voids, there is a problem that the frictional wear characteristic and the mechanical strength characteristic are lowered when the operation state is severe. This is presumably because the lubricating oil permeates through the holes and the hydraulic pressure distribution decreases.

Hereinafter, the improvement of this point will be described with reference to FIGS. 16 to 18. FIG. 16 is a conceptual diagram showing a bearing model of a porous carbon graphite base material, (a) is a conceptual diagram showing a model before metal filling, and (b) is a concept showing a model after metal filling. It is a figure, (c) is a figure showing the lubrication model of a journal bearing. FIG. 17 is a diagram illustrating a state diagram and mechanical properties of the filled metal. (A) is a copper - Mechanical properties of the solid solution of tin (tensile strength: sigma _B, Hardness: H _B, elongation: [delta]) is a diagram showing the relation, (b) copper - phosphorus - tin It shows a ternary metallic state, and is a diagram showing an area range of an α solid solution and an area range of α + Cu ₃ P of the present embodiment. FIG. 18 is a diagram showing the electrode potential of a typical filled metal.

  First, as shown in FIG. 16 (a), the bearing 20 is a bearing made by processing a carbon graphite base material having porous holes before metal filling, and the shaft 21 is a quench-hardened shaft. The bearing 20 rotates in the clockwise direction (clockwise) in a range from a low speed to a high speed (the rotation speed indicated by N in FIG. 16 is, for example, 800 to 8000 rpm). Reference numeral 22 denotes a lubricating oil mixed with refrigerating machine oil and a refrigerant, and this lubricating oil 22 is drawn between the shaft 21 and the bearing 20 by the rotation of the shaft 21 and has a wedge action, so that the shaft 21 is shown in FIG. Lift as shown in (a). If this lifting force overcomes the axial load P, so-called fluid lubrication occurs and metal contact can be prevented. That is, wear of the bearing due to contact can be prevented. However, when the axial load P is high or the lubricating oil viscosity is low, the hydraulic pressure due to the wedge action penetrates into the bearing, and the hydraulic pressure distribution decreases. In this state, sufficient fluid lubrication cannot be maintained. That is, as shown in FIG. 16C, a boundary lubrication region and a fluid lubrication region are mixed, and a so-called mixed lubrication region is entered. As described above, this state occurs due to a severe operation state or the like, and does not cause a problem during normal operation. The bearing 20a shown in FIG. 16 (b) of the present embodiment is one after the porous holes are filled with metal. When this bearing 20a is used, the penetration of the lubricating oil can be suppressed extremely small. That is, the hydraulic pressure distribution B is greatly improved as compared with the hydraulic pressure distribution A before filling (see FIG. 16A). This is shown in the hydraulic pressure distribution A and the hydraulic pressure distribution B (see FIGS. 16A and 16B).

  Next, a so-called severe operation that rapidly raises the refrigerant compressor to a high speed will be described. The refrigerant compressor is in a state where an oil film is not formed between the bearing and the shaft at the start of operation even if the oil supply method is different. When the shaft is rotated in the absence of this oil film (time lag), metal contact occurs and heat is generated, resulting in wear and galling. In the winter heating operation mode, since the refrigerant is condensed and unevenly distributed in the outdoor unit of the air conditioner, the refrigerant gathers at the lower part (bottom part) of the compressor to form a so-called sleeping state. The refrigerant present at the bottom is supplied between the shaft and the bearing through the shaft. Lubricating oil containing a large amount of this refrigerant has extremely low viscosity and extremely small oil film formation, resulting in boundary lubrication. When operating in this state, metal contact is caused and the refrigerant and refrigerating machine oil are decomposed as heat is generated, so-called corrosive wear and galling phenomenon occur. In order to eliminate such wear and galling phenomenon, in this embodiment, in the bearing 20a shown in FIG. 16 (b), long-term reliability is considered in consideration of wear resistance and corrosion resistance in the pores of the carbon graphite base material. The optimal metal that secures the properties is selected and filled. The conventional bearing is obtained by filling carbon graphite with one metal selected from Group IB, Group VIII excluding Fe, and Sn, or an alloy mainly composed of these metals.

Next, selection of a filling metal that ensures long-term reliability and improves wear resistance and corrosion resistance will be described.
Carbon graphite is a precious substance, and in the presence of trace amounts of moisture with base metals, such as refrigeration cycles and refrigerant compressors, it is thought that corrosion and refrigerant decomposition are accelerated by electrochemical action. It is done. Selection of the filling metal was conducted by examining chemical changes in the refrigerating machine oil when immersed in a refrigerating machine oil (ester type) containing 100 ppm of various filling candidate metals and kept at 250 ° C. for 1 hour. The results are shown in Table 5.

As shown in Table 5, it was found that Sn (tin) solder containing Pb (lead) and an active substance (flux) has an abnormally high fatty acid concentration and cannot be used. On the other hand, Al (aluminum) has a small amount of fatty acid, but reacts with the base material at the time of filling to produce a composite carbide, so it is not suitable as a filling metal. Further, Cu (copper) has a small amount of fatty acid but is soft, so that improvement in mechanical strength due to reinforcement is poor. Furthermore, Zn (zinc) and Sn (tin) have a fatty acid concentration that is about twice that of Cu (copper).
Also, solute metals in oil are 36 ppm for Pb (lead), 16 ppm for Sn solder, and all other metals are 0.1 ppm or less (out of detection limit). It was not possible to find a significant difference.

  In this embodiment, in order to increase the mechanical strength, which is a defect of Cu, and to prevent a chemical reaction with the carbon graphite base material, a metal such as Sn (tin), Zn (zinc), Si (silicon) or the like is used. In addition to alloying, in order to suppress the production of fatty acids, the range of α solid solution was specified and filled. As the α solid solution, Cu (copper) -2.3% Be (beryllium), Cu (copper) -5.0% Si (silicon), Cu (copper) -9.7% Al (aluminum), Cu (copper) ) -12% Sn (tin), Cu (copper) -29% Zn (zinc), etc., but Be (beryllium), Si (silicon) and Al (aluminum) are reactive with carbon graphite base materials at high temperatures. Therefore, it is necessary to devise a method to minimize the reaction when filling. Cu (copper), Sn (tin), and Zn (zinc) have very little reaction at the filling temperature near the melting point, and are suitable for work. Therefore, here, a Cu (copper) -Sn (tin) based alloy will be described.

FIG. 17 referred to here is a diagram showing a phase diagram and mechanical properties of the filled metal, and (a) shows mechanical properties (tensile strength: σ _B , hardness: H _{B in a} copper-tin based solid solution. (B) shows the copper-tin-phosphorus ternary metal state, and the area range of the α solid solution and the area range of α + Cu ₃ P in this embodiment. FIG. FIG. 18 is a diagram showing the electrode potential of a typical filled metal.
The Cu (copper) -Sn (tin) alloy has a relationship between the metal phase diagram shown in FIGS. 17A and 17B and the mechanical properties, and the α solid solution has about 12% Sn (tin). It becomes a range. At this time, the tensile strength σ _B is about 1.8 times, the hardness is about 1.6 times, and an improvement effect is obtained by filling the holes. On the other hand, since the α solid solution of Cu (copper) has a base metal such as elution Zn (zinc), Sn (tin), Si (silicon), etc. described above, dissolved in the structure of Cu (copper). As shown in FIG. 18, the corrosion potential of the object apparently becomes an electrode potential at the same level as that of pure copper. In other words, the α solid solution can greatly improve the mechanical strength and have the same corrosion resistance as that of pure copper. Especially in the refrigerant compressor and the refrigerating apparatus, the electrode potential of the carbon graphite substrate and the α of Cu (copper) The potential difference of the solid solution can be reduced, and the reliability with corrosion can be greatly improved. Furthermore, as shown in FIG.17 (b), the ratio of P (phosphorus) which can be contained in the α solid solution of Cu (copper) is 0.05 to 7.5 mass%.

Moreover, as shown in Table 5, bronze [Cu (copper) + Sn (tin)], phosphor bronze [Cu (copper) + Sn (tin) + P (phosphorus)], phosphorus, which can be used for the bearing of this embodiment. Copper [Cu (copper) + P (phosphorus)] can be kept at a low fatty acid concentration that approximates that of pure copper. Furthermore, as a means of enhancing the mechanical strength of the α solid solution, mechanical strength is obtained without impairing the properties of the carbon graphite base material by dissolving or partially depositing P (phosphorus) in the form of Cu ₃ P. Further, it is possible to improve the friction and wear resistance characteristics, and it is possible to obtain an alloy whose structure is strengthened so that the hardness becomes H _V 100 or more. One feature of the present embodiment is that the strength of the carbon graphite base material is increased by filling the carbon graphite base material with 20 to 70% by mass of the strengthened alloy. Note that typical copper alloys used in the filling experiments are JIS (Japanese Industrial Standards) BC3, PBC3, and BCuP2. In order to verify that 20 to 70% by mass of the metal whose structure has been strengthened is filled, for example, one of the bearings (see FIGS. 20A and 20B) before and after filling the metal described later. The amount of metal may be obtained by subtracting the mass before filling from the mass after filling to determine the amount of metal, and dividing this by the mass after filling. Here, the reason for prescribing 20 to 70% by mass is the result of selecting the best workability, and it is difficult to make ones exceeding 70% by mass and those having 20% by mass or less in the current filling furnace. Because. Moreover, when it becomes 20 mass% or less, workability | operativity will worsen of course, but it is because mechanical strength or a frictional wear characteristic falls significantly.

Next, means for filling a carbon graphite base material with a copper alloy that forms an α solid solution of Cu (copper) and material characteristics after filling will be described.
FIG. 19 is a copying diagram showing an example in which an alloy that forms an α solid solution of Cu (copper) is melted in a vacuum and high-pressure filling device, and the pores of the carbon graphite base material are high-pressure filled. FIG. 20 (a) is a schematic diagram showing a cross-section cut out from a block-shaped isotropic carbon graphite base material, and FIG. 20 (b) is a columnar or cylindrical anisotropic carbon graphite base. It is a schematic diagram which shows a material. FIG. 22A is a microstructural view before filling the metal of the anisotropic carbon graphite base material, and FIG. 22B is a microstructural view after the metal filling of the anisotropic carbon graphite base material.

First, a vacuum high pressure filling apparatus for filling a carbon graphite base material with a copper alloy will be described here.
As shown in FIG. 19, the vacuum high-pressure filling device 23 has a metal melting furnace 25, a hanging basket 26, and an elevator 27 in a vacuum container 24. Then, after setting the carbon graphite base material to be filled in the hanging cage 26, the vacuum high pressure filling device 23 is evacuated and the gas is discharged. Next, the copper alloy is heated and melted with an α solid solution of Cu (copper) in the metal melting furnace 25. Then, the carbon graphite base material to be filled is immersed in the suspension basket 26 using the elevator 27 in this heated and melted copper alloy bath.

Next, an inert gas such as nitrogen gas is injected from the injection port 28, and the pressure in the metal melting furnace 25 is increased to a high pressure of, for example, 10 MPa, and this high pressure is maintained. As a result, the vacant portion of the filled carbon graphite base material is forcibly filled with the copper alloy. As the pressure for pressurization and filling, for example, 20 MPa for a diameter of 1 μm and 10 MPa for 2 μm are required, corresponding to the hole distribution diagram of FIG. In normal performance, the gap filling rate is 62 to 90% at 10 MPa. When the molding pressure is small and the pores are large, about 50% filling is possible even at 1 MPa.
Thereafter, the hanging cage 26 is raised and cooled to a temperature below the solidus of the copper alloy, and the solidification of the metal is completed. Thereafter, high-pressure gas is discharged to the atmosphere, and the inside of the vacuum high-pressure filling device 23 is brought to normal pressure. In this state, the metal-filled carbon graphite base material is taken out from the vacuum high-pressure filling device 23.

  As shown in FIGS. 20 (a) and (b), for example, the bearing used for the refrigerant compressor is a bar when the outer diameter Φ is set to 19 mm, the inner diameter Φ is set to 16.0 mm, and the height (not shown) is set to 15 mm. Made from wood and cylindrical material. In the case shown in FIG. 20 (b), the bearing is fabricated by processing the cylindrical material so that the outer diameter is 20.5 mm, the inner diameter is 11.5 mm, and the height is 25 mm. In addition, the said dimension is the example added to the final shape in order to include a clamp margin. Incidentally, in the example shown in FIG. 20A, the step of processing a bar material into a column (see O-Step 9 in FIG. 5), the step of processing from a column into a cylinder (see O-Step 10 in FIG. 5), and the column An example is shown in which the final finished dimensions are obtained through a finishing step (see O-Step 10 in FIG. 5). That is, the phantom line shown with the dashed-two dotted line in Fig.20 (a) represents the final finishing dimension.

  When the bar material shown in FIG. 20 (a) is compared with the cylindrical material shown in FIG. 20 (b), the cylindrical material shown in FIG. 20 (b) has a metal filling ratio of the bar material shown in FIG. 20 (a). 1/5, the volume ratio is 2/5, and the effective area ratio of the filled metal in the carbon graphite base material is 13/60. And when comparing the bar material shown in FIG. 20 (a) and the cylindrical material shown in FIG. 20 (b), the amount of heat drawn out during immersion, the amount of metal taken out, the filling time, the production capacity, etc. It was demonstrated that the bearing manufacturing method of the embodiment (see FIG. 5) is excellent.

  Next, the mechanical and physical properties of the carbon graphite base material filled with metal will be described with reference to Table 6. Table 6 summarizes the mechanical and physical properties of the carbon graphite base material filled with metal.

  Conventional Example 3 in Table 6 is one in which isotropic carbon base material with an average area porosity of 10.86% shown in Table 1 is filled with bronze (BC3: P content 0), The area filling rate was 7.66%, and the area porosity corresponding to unfilled was 0.86%. The area void filling rate is 90%.

Hereinafter, as the carbon graphite base material according to the present embodiment, an example in which the average area porosity shown in Table 1 is 9.07% and a cylindrical anisotropic carbon graphite base material is filled with metal will be described. To do.
Example 6 was filled with bronze (BC3) and had an area filling rate of 6.49% and an area porosity of 1.31%. The area void filling factor is 83%.
Example 7 was filled with phosphor bronze (PBC3: P content 0.05 to 0.5 mass%), with an area filling factor of 4.82% and an area porosity of 2.98%. became. The area gap filling factor is 62%.
Example 8 was filled with phosphoric copper (BCuP2: P content 6.8 to 7.5% by mass), with an area filling factor of 6.10% and an area porosity of 1.54%. became. The area void filling factor is 80%.

Next, as the carbon graphite base material according to the present embodiment, an average area porosity shown in Table 1 is 9.07%, and an anisotropic carbon graphite base material of a cylindrical body is filled with a metal. explain.
Example 9 was filled with bronze (BC3), and had an area filling rate of 6.13% and an area porosity of 1.70%. The area void filling factor is 78%.
Example 10 was filled with phosphor bronze (PBC3) and had an area filling rate of 7.40% and an area porosity of 0.98%. The area void filling rate is 88%.
Example 11 was filled with phosphor copper (BCuP2), and the area filling rate was 6.52% and the area porosity was 1.63%. The area void filling factor is 80%.

  Further, as shown in Table 6, the bending strength, compressive strength, and crushing strength (crushing load) of Examples 6 to 11 are smaller in each item compared to Conventional Example 3 ( It can be confirmed that a bending strength of 50 MPa or more and a compressive strength of 180 MPa or more, which are targets for the bearing base material, are secured. Furthermore, it can also be confirmed that a crushing strength (crushing load) of 18.6 MPa (150 N by crushing load) or more is secured in a cylindrical test product having an outer diameter of Φ19 mm, an inner diameter of 16 mm, and a height of 14.3 mm.

  FIG. 21 is a microstructure diagram of Example 6 of the anisotropic carbon graphite substrate in Table 6 before (a) and after (b) filling with metal. In FIG. 21, black portions indicate pores and gray sea portions indicate carbon graphite base materials. In addition, the organization chart of Fig.21 (a) which shows the state before filling with a metal is B surface of an anisotropic carbon graphite base material when the shaping | molding pressure demonstrated in Example 2 of Table 3 is set to 100%. Is shown. FIG. 21 (b) shows the structure after filling with the metal, and the blank on the B surface of the anisotropic carbon graphite base material when the molding pressure described in Example 2 in Table 3 is 100%. The micrograph when a hole is filled with metal is shown. The white part indicates a filled metal, and the black part indicates an unfilled part. That is, it shows a state in which 62 to 90% of the metal is filled in the holes that are hindered with respect to the mechanical strength and the lubricating oil film.

  As described above, the anisotropic carbon graphite base material according to the present embodiment (Examples 6 to 11 shown in Table 6) has an area void filling rate of 62 to 90%, Since 62 to 90% of the holes that are hindering the lubricating oil film are filled with metal, the mechanical strength and performance of the lubricating oil film can be improved. It was confirmed that the mechanical strength (bending strength, compressive strength, crushing strength) satisfies the strength required for the bearing.

  Tables 7 and 8 evaluate the thermochemical stability of the carbon-graphite base material filled with metal against a mixture of refrigerant and refrigerating machine oil.

  The test conditions shown in Table 7 and Table 8 conform to the shield tube test specified by JIS K 2211 (refrigeration machine oil). That is, 5 mL of refrigerating machine oil (ester oil) containing 100 ppm of water, 0.5 g of refrigerant (R410A), and carbon graphite produced in a size (length 3 mm × width 4 mm × length 50 mm) that can be placed in a glass tube in advance. The base material was enclosed in a glass tube, and a heating test at 150 ° C. for 40 days, which was assumed as the usage environment of the bearing in the refrigerant compressor, was performed. And the reliability concerning the thermochemical stability after a heating test is evaluated. Example 12 in Table 7 is an anisotropic carbon graphite base material filled with phosphor bronze (PBC3), and Example 13 is an anisotropic carbon graphite base material filled with phosphor copper (BCuP2). . And, the amount of acidic substance which is a product when the refrigeration oil is chemically decomposed by a refrigerant, etc., a precipitation test of a solute that visually checks the appearance at room temperature and in a condition of being left in an environment of −40 ° C. for 4 hours. Each test of the total acid value test to be confirmed and the fatty acid test in which the amount of free fatty acid present in the refrigerating machine oil was analyzed by gas chromatography were performed before and after the heating test. As a result, it was confirmed that there was no significant difference in all test results before and after the heating test. This is equivalent to Conventional Example 4 (isotropic carbon graphite base material filled with bronze (BC3)). Moreover, also in the bending test using the carbon graphite base material concerning Examples 12 and 13, it has confirmed that there was no significant difference before and behind a heating test. From the above, it was confirmed that there was no problem in using the carbon graphite base material according to the present embodiment as a bearing material.

  Also, an anisotropic metal-filled carbon substrate (length 3 mm × width 4 mm × length 50 mm) and one of HFC refrigerants R134a, R407C, R404A or hydrocarbon (HC) refrigerants R600a, R290 (0.5 g), 5 mL of refrigeration oil (ester oil) containing 100 ppm or 500 ppm of moisture is sealed in a glass tube, and a heating test is performed at 150 ° C. for 40 days assuming the usage environment of the bearing in the refrigerant compressor. And the result of having evaluated the reliability concerning the thermochemical stability after a heating test is shown in Table 8. In Table 8, Examples 14 to 27 are described in the anisotropic carbon graphite group filled with the metal described in the column of packed metal, the refrigerant described in the column of refrigerant, and the column of refrigerating machine oil. It is shown to be tested in combination with a refrigerating machine oil. Also in these results, no abnormality was observed after the heating test in terms of hue change, presence / absence of appearance precipitates, bending strength, and total acid value, and it was confirmed that the bearing was practical. Moreover, in the analysis of the metal in refrigerating machine oil performed at the same timing as the evaluation shown in Table 7 and Table 8, Cu (copper), Sn (tin), and P (phosphorus) are below the detection limit (<0.01 ppm). And good corrosion resistance could be confirmed. This was not significantly different due to the difference in water content (100 ppm, 500 ppm) contained in the refrigerating machine oil, and it was confirmed that the same corrosion resistance was exhibited at any water content.

  To summarize the above, the carbon graphite base material according to the present embodiment includes an HFC refrigerant (R134a, R404A, R407C, etc.) represented by R410A, an ester refrigerator oil, an HC refrigerant represented by R600a, R290, and mineral oil ( MO) has high practical reliability in chemical stability.

Next, put CO ₂ refrigerant (R744), PAG refrigerating machine oil (water content 150ppm), and filled metal carbon graphite base material specimen into a metal pressure vessel, and thermochemical stability in the usage environment of the refrigerant compressor The reliability related to sex was evaluated. The amount of CO ₂ refrigerant used at this time was 40 g, the amount of refrigerating machine oil was 40 mL, and the test was a heating test at 150 ° C. × 40 days. Also in this test, no abnormality was observed in test items such as hue, bending strength, total acid value, etc., compared with a blank in which only refrigerator oil and refrigerant were enclosed in a glass tube. In addition, since the visual test of an external appearance check cannot be performed in the said metal container, the refrigerating machine oil and refrigerant | coolant (R134a) after a test are enclosed in the hard glass tube mentioned above, and the eluted substance is visually determined. Again, it was confirmed that there was no precipitate at room temperature and -40 ° C. Further, it has been found that the ammonia refrigerant has high reactivity with copper, and thus has poor appearance and low temperature precipitation and is not practical.

Hereinafter, with reference to FIGS. 22 to 25, the friction and wear characteristics of the metal-filled carbon graphite base material assuming the use environment of a refrigerant compressor such as an air conditioner and a refrigeration apparatus will be described.
FIG. 22 is a diagram showing the arrangement of the frictional wear test pieces. FIG. 23 is a diagram in which a frictional wear test using R410A as a gaseous refrigerant is performed, and the wear amount measured in this test is compared between the conventional example and this embodiment. FIG. 24 is a diagram in which a frictional wear test using R410A as a gas refrigerant is performed, and an average friction coefficient measured in this test is compared between the conventional example and this embodiment. FIG. 25 is a diagram in which a frictional wear test using CO ₂ as a gaseous refrigerant is performed, and the wear amount measured in this test is compared between the conventional example and this embodiment.

The frictional wear test piece is composed of a fixed piece 29 and a movable piece 30 as shown in FIG. The fixed piece 29 is assumed to be a bearing, and the movable piece 30 is assumed to be a shaft (steel of H _V 450 or higher: for example, carburizing and quenching of SCM415, surface accuracy Rz = 1.2 μm or lower). In addition, when performing an evaluation test using the fixed piece 29 and the movable piece 30, the shape and size of the frictional wear evaluation test can be performed under the high-pressure atmosphere of the refrigerant assuming the operating atmosphere of the refrigerant compressor. The fixed piece 29 and the movable piece 30 are formed.
Table 9 shows the test conditions for the evaluation test of the fixed piece 29 and the movable piece 30.

  This test condition is a severe acceleration test condition under boundary lubrication operation assuming a non-lubricating oil state. In other words, the test conditions are such that the test surface pressure corresponds to the bearing surface pressure, and the test condition is equivalent to the peripheral speed of the shaft. It is a condition that the lubricating oil does not reach the shaft and the bearing portion at the start-up or the like.

Next, as shown in FIG. 23, the anisotropic carbon graphite cylinders and columnar substrates of Examples 28 to 34 filled with bronze (BC), phosphor bronze (PBC), and phosphor copper (BCuP) In any case, it was found that the amount of wear was improved to about ½ as compared with the case where the isotropic carbon graphite base material of Conventional Example 5 was filled with bronze (BC). Further, the isotropic carbon graphite base material of Conventional Example 5 was also obtained by filling the block molded body of the isotropic carbon graphite base material of Examples 33 and 34 with phosphor bronze (PBC) and phosphor copper (BCuP). It was confirmed that the amount of wear was lower than that of the material filled with bronze (BC). This is a compounding effect of the copper alloy containing phosphorus (Cu ₃ P). That is, Conventional Example 5 is the same isotropic carbon graphite base material but does not contain phosphorus, so that the wear amount of the bearing is 6 μm / 2 h, whereas Example 33 is 5.1 μm / 2 h. is there. In addition, Example 34 was 3.4 μm / 2h. Therefore, it was found that the abrasion amount was improved in Examples 33 and 34 as compared with Conventional Examples 5 and 6. Furthermore, Conventional Example 6 has the above-described graphite crystallinity of 86% (Examples 28 to 34 have a graphite crystallinity of 15 to 50%) and a low mechanical strength. There is a difference in the amount of wear.

  Next, as shown in FIG. 24, the isotropic carbon graphite base material is phosphor bronze (PBC) as compared with the conventional example 5 in which the isotropic carbon graphite base material is filled with bronze (BC). Example 34 filled with phosphor, Example 33 filled with phosphor copper (BCuP), Example 32 filled with bronze (BC) in a cylindrical molded body of anisotropic carbon graphite base material, Filled with phosphor bronze (PBC) Example 31, Example 30 filled with phosphor copper (BCuP), Example 29 filled with a cylindrical molded body of anisotropic carbon graphite base material and bronze (BC), and phosphor bronze (PBC) In Example 28, the friction coefficient decreases in proportion to the content of P (phosphorus) in the filling metal. Therefore, it can be understood that the α solid solution of Cu (copper) containing P (phosphorus) is filled in the network pores of the carbon graphite base material, the material strength is increased, and the friction coefficient is reduced.

Next, as shown in FIG. 25, in the frictional wear test using the CO ₂ refrigerant as the gas refrigerant, the wear amount of the conventional isotropic carbon graphite base material is 2 μm / h or less. The amount of wear of the anisotropic carbon graphite base material of this embodiment is also 2 μm / h or less. In addition, an isotropic carbon graphite base material filled with bronze (infiltrated product) is almost the same as an anisotropic carbon graphite base material filled with bronze (infiltrated product), and the amount of wear is the same. Abnormally increases. When the test surface pressure as a condition of this friction and wear test is 20 MPa, a tribochemical reaction occurs between the refrigerant and the filled metal on the friction surface, and wear progresses. In this case, the unfilled base material alone is superior. I found out. Accordingly, it has been found that there is no significant difference in isotropicity and anisotropy between the base material and the filled product in terms of wear in the CO ₂ refrigerant, and it can be put to practical use.

  Next, test results obtained by performing the wear test by changing the test surface pressure using the anisotropic carbon graphite base material of the present embodiment as the fixed piece 29 (see FIG. 22) will be described with reference to the drawings as appropriate. FIG. 26 is a diagram showing a result of a wear test performed in R410A as a gaseous refrigerant by changing the test surface pressure in a range of 5 to 15 MPa. In addition, as above-mentioned as a refrigerant | coolant made into object by this embodiment, R134a, R410A, R407C, R404A etc. are mentioned, However, A constituent element is C (carbon), F (fluorine), H (hydrogen), Corrosion wear related to the tribochemical reaction under the environment is represented by R410A used as a refrigerant in this test.

  Moreover, as mentioned above, POE (ester oil), PVE (ether oil), etc. are mentioned as refrigerating machine oil made into object by this embodiment, However, POE was used as refrigerating machine oil in this test.

  In the above-described air wear test (see FIGS. 23 and 24), the test was performed at a constant speed of 1.2 m / s and a test surface pressure of 9.8 MPa in R410A as a gas refrigerant. The air wear test was performed at 5 MPa and 15 MPa before and after the above air wear test. Other conditions were set as shown in Table 10.

  In the load resistance test, the test piece was immersed in a mixed lubricating oil of refrigerant R410A and polyol ester refrigerating machine oil (VG68), and the test surface pressure was continuously increased in the range of 1.8 to 98 MPa. Then, when the test surface pressure reached 98 MPa (Max pressure), the load resistance test was finished and the amount of wear was measured. Other conditions are as described in Table 10.

  As shown in FIG. 26, in Conventional Example 7, when the test surface pressure becomes 9.8 MPa and the test surface pressure becomes 15 MPa, the amount of wear increases rapidly and reaches 16 μm / h. Further, in Conventional Example 8, the wear amount when the test surface pressure was 9.8 MPa was 12 μm / h, but when the test surface pressure was 15 MPa, the wear amount increased to 20 μm / h. In Example 35, the wear amount when the test surface pressure was 9.8 MPa was 2 μm / h or less, but the wear amount when the test surface pressure was 15 MPa was 14 μm / h. In Example 36, the wear amount at a test surface pressure of 9.8 MPa was 2 μm / h or less, but the wear amount at a test surface pressure of 15 MPa was 3.7 μm / h. 1/3 or less.

  FIG. 27 is a diagram showing a result of an abrasion test assuming mixed lubrication in a mixed liquid of refrigerant and refrigerating machine oil with the surface pressure changed from 1.8 to 98 MPa, (a) isotropic carbon. The figure which measured the relationship between the surface pressure of graphite (block), and a friction coefficient, (b) is the figure which measured the relationship between the surface pressure of anisotropic carbon graphite (cylinder), and a friction coefficient. 28 (a) and 28 (b) are diagrams showing the relationship between the surface pressure and the friction coefficient of the anisotropic carbon graphite of this embodiment filled with metal, and FIG. 28 (c) is a conventional isotropic filled with metal. It is a figure which shows the relationship between the surface pressure of a conductive carbon graphite, and a friction coefficient. FIG. 29 is a diagram showing a comparison test result of shaft and bearing wear amounts in the test result of FIG.

FIG. 27 (a) shows the load resistance of the isotropic carbon graphite base material. As shown in FIG. 27 (a), in this wear test, the friction coefficient increases rapidly from the test surface pressure of 23 MPa. As a result, the friction surface was broken, and the test piece itself was broken at a test surface pressure of 60 MPa.
FIG. 27 (b) shows the load resistance of the anisotropic carbon graphite base material. As shown in FIG. 27 (b), in this wear test, the test piece itself was broken at a test load of 75 MPa. In the wear test of FIG. 27B, the same characteristics as the isotropic carbon graphite base material are shown.

FIGS. 28 (a), (b) and (c) show load resistance when an anisotropic carbon graphite substrate is filled with a metal, and are shown in FIGS. 28 (a), (b) and (c). As described above, in this wear test, the friction coefficient of the anisotropic carbon graphite + phosphorus bronze, the anisotropic carbon graphite + phosphorus copper, and the isotropic carbon graphite + bronze was about 0.1 or less. In this abrasion test, it was found that the load resistance is drastically improved by the presence of the oil film surface.
FIG. 29 shows a representative example of the amount of wear at the completion of the test of FIG. 28 (a). As shown in FIG. 29, in the conventional example 9, the amount of wear of the fixed piece is 80 μm / 2h, and the movable piece Wear amount of the fixed piece is 352 μm / 2h, and wear amount of the movable piece is 3.2 μm / 2h.
In Example 37, the wear amount of the fixed piece is 5 μm / 2h and the wear amount of the movable piece is 1.2 μm / 2h. In Example 38, the wear amount of the fixed piece is 13 μm / 2h and the wear amount of the movable piece is It was 2.5 μm / 2h.

From the above test results, in the mixed lubrication state and boundary lubrication state under severe operating conditions of the refrigerant compressor, those in which the anisotropic carbon graphite base material is filled with bronze (BC) and phosphor bronze (PBC) are particularly It was confirmed to be excellent.
To summarize the above, a solid solution of Cu (copper) containing P (phosphorus) is filled in the gap between the raw material particles on the B surface of a molded body such as a column or cylinder of a carbon graphite base material. strength is high, for example bronze (BC) is _H V 117, phosphor bronze (PBC) is _H V 128, copper-phosphorus (BCuP) is _H V 105, these hard and brittle carbon graphite substrate _(H V 146 ˜211) is believed to reinforce the carbon graphite substrate.

  Next, about the test results when the example products having the above test results are incorporated into an R410A refrigerant compressor such as a refrigeration system, and a compressor is subjected to a limit strength test by a high-speed intermittent operation of inverter startup with a large amount of refrigerant enclosed. explain. In the test results, the conventional product (isotropic carbon graphite block molding base material + bronze (BC) filling) and the example (anisotropic carbon graphite cylindrical base material + phosphor bronze (PBC) filling) were used for shafts and bearings. Almost no trace of sliding was observed on each friction surface, and good results were shown in terms of wear amount and oil deterioration. Similarly, in the refrigerator, no abnormality was found as a result of the long-term reliability evaluation of the combination of R600a and mineral oil and the combination of R134a and ester oil using a reciprocating compressor. Furthermore, in the hot water heater, no abnormality was found as a result of long-term reliability evaluation in the combination of R744 and PAG oil using a scroll compressor. In other words, in a normal use state, the bearing according to the present embodiment satisfies the operating conditions of a conventional refrigeration apparatus or a compressor, and further has characteristics superior to those of conventional products in the severe test as described above. It was confirmed.

  Next, in order to clarify the bearing characteristics in the normal low load region, the refrigerant is stored in the refrigerant compressor having the characteristics shown in FIG. 16C while referring to FIGS. 30A and 30B. Sommerfeld number when the viscosity (η) at a predetermined temperature of the refrigeration oil in which the refrigerant is dissolved, the test surface pressure (P) of the shaft and the bearing, and the peripheral speed (v) are changed. The relationship of the friction coefficient with respect to (Stribeck curve) will be described by comparing the conventional carbon graphite substrate and the carbon graphite substrate according to the present embodiment.

Fig. 30 (a) is a diagram showing a Stribeck curve of an anisotropic carbon graphite substrate, and Fig. 30 (b) is a diagram showing a Stribeck curve of an isotropic carbon graphite substrate.
In this test for obtaining the Stribeck curve, the test load is 1 MPa, 2 MPa in a mixed practical atmosphere (viscosity η: 26 × 10 ⁻³ Pa · s) of 40 ° C., refrigerant (R410A), and refrigerating machine oil (ester type). A Stribeck curve at 3 MPa was determined. As is clear from FIGS. 30 (a) and 30 (b), in the case of a test load as low as 1 MPa, ηv / P is superior to the isotropic carbon graphite base material than the isotropic carbon graphite base material. I understand that. This is considered to be derived from the fact that the average porosity of the substrate is 10.86% isotropic and 9.07% anisotropy (see FIG. 8).

Next, with reference to FIGS. 31 (a) and 31 (b), a predetermined refrigerating machine oil in which refrigerant stored in the refrigerant compressor in the refrigerant compressor having the characteristics shown in FIG. 16 (c) is dissolved is dissolved. The relationship between the Sommerfeld number and the coefficient of friction (Stribeck curve) when the viscosity (η) at the temperature of the shaft, the test surface pressure (P) of the shaft and the bearing, and the peripheral speed (v) are changed. A comparison between a conventional carbon graphite substrate and the carbon graphite substrate according to the present embodiment will be described.
FIG. 31 (a) is a diagram showing a Stribeck curve of a conventional isotropic carbon graphite base material, and FIG. 31 (b) is a conventional isotropic carbon graphite base material + bronze (BC) metal filling. It is a figure which shows the Stribeck curve of an isotropic carbon graphite base material.
This test for obtaining the Stribeck curve is based on the above-mentioned conventional isotropic carbon graphite base material, or a bearing and shaft formed of a conventional metal-filled isotropic carbon graphite base material, and HFC refrigerant and refrigerating machine oil. This was performed assuming the case of sealing together with a predetermined amount of R410A representing the above.

At this time, the temperature of the refrigerating machine oil is limited to 40 ° C., 60 ° C., and 80 ° C., the test surface pressure is limited to 1 MPa, 2 MPa, and 3 MPa, and the peripheral speed is in the range of 0.012 to 1.2 m / s. limited to, was performed on the assumption that is limited to a range of practical viscosity ^{(η) 9.5 × 10 -3 ~26} × 10 -3 Pa · s of the refrigerant compressor. In this test, the fixed piece 29 and the movable piece 30 shown in FIG. 22 were used. The results of evaluating each obtained Stribeck curve were as follows.

  As shown in FIG. 31 (a), the coefficient of friction of the isotropic carbon graphite substrate increases rapidly when ηv / P becomes 10 [(Pa · s · m / s) / (GPa)] or less. However, the mechanical loss due to the friction of the bearing is large under the environmental conditions of high test surface pressure, low speed and low viscosity. It is desirable that ηv / P is 10 [(Pa · s · m / s) / (GPa)] or more.

  As shown in FIG. 31 (b), the metal-filled isotropic carbon graphite base material has ηv / P of 1.2 [(Pa · s · m / s) / (GPa) as in FIG. 31 (a). )] Use above is desirable.

FIG. 32A is a carbon graphite base material according to the present embodiment, and shows a Stribeck curve of an anisotropic carbon graphite base material + phosphorus bronze (PBC) metal-filled anisotropic carbon graphite base material. FIG.
As shown in FIG. 32 (a), this metal-filled anisotropic carbon graphite base material has an ηv / P of 0.9 [(Pa · s · m / s) / (GPa) at axial loads of 1 MPa and 2 MPa. )] Maintains a low friction region and enters a so-called fluid lubrication state to reduce the mechanical loss of the shaft and the bearing. Therefore, it is excellent in initial conformability and lubricating oil film retention, and can sufficiently withstand use under low viscosity, low speed rotation (for example, 1000 rpm) and high load.

FIG. 32 (b) shows that, among the test conditions for obtaining the Stribeck curve in FIG. 32 (a), the temperature 60 ° C. was changed to the temperature 80 ° C., and the viscosity 14 × 10 ⁻³ Pa · s was changed to the viscosity 9.5 ×. It is a figure which shows the Stribeck curve calculated | required when it changes to 10 ^<-3 > Pa * s. As can be seen from the measurement results of FIGS. 31 (b), 32 (a) and 32 (b), the lubricating condition of the working fluid in which the refrigerant and the refrigerating machine oil coexist is at least η (the Sommerfeld number of the shaft and the bearing). (Viscosity or viscosity coefficient) · v (peripheral speed) / P (load) is desirably 0.8 [(Pa · s · m / s) / (GPa)] or more. It was confirmed that it was small. In addition, the average surface pressure (axial load) of the Sommerfeld number of the shaft and the bearing in the lubrication condition of the working fluid in which the refrigerant and the refrigerating machine oil coexist is at least 0.15 to 20 MPa, and the amount of wear of the bearing is small. I understand. In the refrigerant compressor including the bearing manufactured based on the above results, the mechanical loss due to the friction of the bearing is reduced, and the amount of wear is also reduced. Therefore, according to this bearing, the noise and vibration of the refrigerant compressor are reduced, the sealing performance of the compressor chamber due to misalignment is improved, and the reduction in volumetric efficiency (ηv) can be prevented. As a result, according to this bearing, it is possible to obtain a refrigerant compressor and a refrigeration apparatus that can ensure power saving and reliability.

FIG. 33 is a diagram schematically showing the Stribeck curve of the carbon graphite base material. As shown in FIG. 33, the metal-filled product has a significantly improved friction coefficient when ηv / P is the same as that of the unfilled product, and a fluid lubrication region having a particularly low friction coefficient can be formed.
The bearings according to this embodiment are used. For example, refrigerators include home and commercial air conditioners, refrigerators, dehumidifiers, water heaters, washing and drying machines, showcases, refrigeration units, automobile air conditioners, and the like. is there.

Since the present embodiment has the configuration as described above, the following effects can be obtained.
As shown in FIG. 24, in the boundary lubrication conditions in the R410A gas refrigerant atmosphere, the friction coefficient can be reduced as the P (phosphorus) content increases. In the present embodiment, since the bearing is formed using a carbon graphite base material filled with phosphorous copper or a copper α solid solution containing 0.05 to 7.5 mass% of phosphorous, the friction coefficient is small and the friction is reduced. It has an excellent effect of providing a bearing with low loss.

  In the present embodiment, the bearing is formed using a carbon graphite base material having a crystallinity of 15 to 50% before being filled with metal. As shown in FIGS. 10 and 11, when the crystallinity is in the range of 15 to 50%, the area ratio of the graphite matrix is moderately suppressed, and the amount of wear is reduced. Therefore, it is possible to provide a bearing having excellent mechanical strength such as wear resistance.

Further, in the present embodiment, focusing on the fact that the Cu (copper) α solid solution apparently shows an electrode potential equivalent to that of Cu (copper), the semimetal P (phosphorus) is in the form of Cu ₃ P. The bearing is molded using a carbon graphite base material that contains, improves mechanical properties and corrosion resistance, and improves friction and wear resistance. Therefore, it is possible to provide a bearing with excellent wear resistance.

Further, in the present embodiment, an alloy in which Cu ₃ P is dispersed and precipitated in phosphorous copper or an α solid solution of Cu (copper) containing P (phosphorus) and the hardness is strengthened to H _V 100 or more is used. Since it is used as a bearing for a refrigerant compressor of a refrigerator in which 20 to 70% by mass of a carbon graphite base material is filled, the filled metal has good fluidity and easily penetrates into pores, and is a reaction product with carbonaceous material. A bearing is formed using a carbon graphite base material having improved friction and wear resistance without forming (intermetallic compound). Therefore, it is possible to provide a bearing with excellent wear resistance.

  Moreover, in this embodiment, it is an alpha solid solution of Cu (copper) containing phosphorous copper or P (phosphorus), and before the content of P (phosphorus) is 0.05 to 7.5 mass%. Since the carbon graphite base material is a bearing for a refrigerant compressor of a refrigerator having a graphite crystallinity of 15 to 50% by X-ray diffraction, mechanical characteristics, corrosion resistance, and friction resistance are not deteriorated in workability. It is possible to obtain a refrigerant compressor bearing for a refrigerator having excellent wear characteristics.

  Furthermore, in this embodiment, since the carbon graphite base material obtained by firing after being molded into a shape close to the usage shape of the bearing is processed into the bearing, the processing amount is small, and the time required for processing Can be shortened, and since the amount discarded as shavings is reduced, the material loss can be reduced.

It is a cross-sectional schematic diagram of the scroll-type refrigerant compressor in which the bearing which concerns on embodiment is integrated. It is the elements on larger scale of the location enclosed with the dashed-dotted line of FIG. It is a cross-sectional schematic diagram of the rotary type refrigerant compressor in which the bearing which concerns on embodiment is integrated. It is the elements on larger scale of the part enclosed with the dashed-dotted line of FIG. It is process drawing for demonstrating the manufacturing method of the bearing which concerns on embodiment. It is explanatory drawing of the graphite polycrystal aggregate | assembly model contained in a bearing, (a) is a figure which shows the conventional random graphite aggregate | assembly, (b) is a figure which shows an aligned graphite aggregate | assembly. It is a perspective view which shows a graphite crystal structure. (A) is a microscope organization chart of the carbon graphite base material in an embodiment, and (b) is a figure showing distribution of a hole diameter. (A) is a distribution diagram showing a molding pressure distribution when a raw material is compression-molded only with an upper punch in a powder molding die, and a density distribution (porosity after firing) thereby, (b) is a powder molding It is a distribution map which shows the molding pressure distribution at the time of carrying out the compression molding of the raw material by both the upper punch and lower punch in this metal mold | die, and the density distribution (void ratio after baking) by it. It is a figure which shows the crystallinity of a carbon graphite base material, and the area ratio of the graphite structure | tissue by a Raman analysis. It is a figure which shows the relationship between graphite crystallinity and the amount of wear. It is a figure which shows the relationship between an average area porosity and an abrasion loss. It is a figure which shows the relationship between an anisotropic ratio and the amount of wear. It is a perspective view of the test piece which utilized the (110) surface of the graphite crystal | crystallization formed when it press-molds to the maximum. It is the schematic diagram which showed the collection position of the test piece in a cylindrical body base material. It is a conceptual diagram which shows the bearing model of a porous carbon graphite base material, (a) is a conceptual diagram which shows the model before metal filling, (b) is a conceptual diagram which shows the model after metal filling, (c ) Is a diagram showing a lubrication model of a journal bearing. It is a figure showing the phase diagram and mechanical characteristic of a filling metal. (A) is a copper - Mechanical properties of the solid solution of tin (tensile strength: sigma _B, Hardness: H _B, elongation: [delta]) is a diagram showing the relation, (b) copper - phosphorus - tin shows the metallic state of the ternary diagrams showing the area range of area coverage and alpha + Cu 3 _P of alpha solid solution to be filled in the carbon graphite substrate. It is a figure which shows the electrode potential of a typical filling metal. It is a copying figure which shows an example which melts the alloy which forms alpha solid solution of Cu (copper) in a vacuum high-pressure filling device, and carries out high-pressure filling of the vacancy of a carbon graphite base material. (A) is a schematic diagram showing a rectangular bar material with a cross section cut out from a block-like isotropic carbon graphite base material, and (b) is a schematic diagram showing a columnar or cylindrical anisotropic carbon graphite base material. FIG. (A) is the microstructural view before the metal filling of the anisotropic carbon graphite base material, (b) is the microstructural view after the metal filling of the anisotropic carbon graphite base material. It is a figure which shows arrangement | positioning of a friction abrasion test piece. It is the figure which performed the friction abrasion test using R410A as a gaseous refrigerant | coolant, and compared the abrasion loss measured by this test with the conventional examples 5 and 6 and Examples 28-34. It is the figure which performed the friction abrasion test using R410A as a gaseous refrigerant | coolant, and compared the average friction coefficient measured by this test with the prior art examples 5 and 6 and Examples 28-34. Perform frictional wear test using CO ₂ as a gas refrigerant, it is a graph comparing the wear amount measured in this test with an isotropic carbon graphite substrate and the anisotropic carbon graphite substrate. It is a figure which shows the result of having changed the test surface pressure in the range of 5-15 MPa, and having done the abrasion test in R410A as a gaseous refrigerant. It is a figure which shows the result of the wear test supposing mixed lubrication in the liquid mixture of a refrigerant | coolant and refrigerating machine oil, changing a surface pressure to 1.8-98 MPa, (a) is isotropic carbon graphite (block) The figure which measured the relationship between the surface pressure of this, and a friction coefficient, (b) is the figure which measured the relationship between the surface pressure of anisotropic carbon graphite (cylinder) and a friction coefficient. (A) And (b) is a figure which shows the relationship between the surface pressure of the anisotropic carbon graphite with which the metal was filled, and a friction coefficient, (c) is the surface pressure and friction of the conventional isotropic carbon graphite with which the metal was filled. It is a figure which shows the relationship of a coefficient. It is a figure which shows the abrasion amount comparison test result of the axis | shaft and bearing in the test result of Fig.28 (a). (A) is a figure which shows the Stribeck curve of an anisotropic carbon graphite base material, (b) is a figure which shows the Stribeck curve of an isotropic carbon graphite base material. (A) is a figure which shows the Stribeck curve of the conventional isotropic carbon graphite base material, (b) is the metal filling isotropic carbon of the conventional isotropic carbon graphite base material + bronze (BC). It is a figure which shows the Stribeck curve of a graphite base material. (A) is a figure which shows the Stribeck curve of the metal filling anisotropic carbon graphite base material of anisotropic carbon graphite base material + phosphor bronze (PBC), (b) is the Stribeck curve of (a). Of the test conditions for which the temperature was changed from 60 ° C. to 80 ° C. and the viscosity was changed from 14 × 10 ⁻³ Pa · s to the viscosity of 9.5 × 10 ⁻³ Pa · s. It is a figure which shows a curve. It is the figure which modeled the Stribeck curve of a carbon graphite base material.

Explanation of symbols

DESCRIPTION OF SYMBOLS 1 Scroll sealed container 2 Orbiting scroll member 2a Base plate 2b Wrap 2c Bearing 2d Back keyway 3 Fixed scroll member 3a Base plate 3b Wrap 3c Suction port 3d Discharge port 4 Frame 4a Bearing 5 Crankshaft 5a Crank 6 Oldham joint 7 Motor 8 Sealed container for rotary 9 Compressor part 10 Motor part 11 Discharge pipe 12 Crankshaft 13 Rolling piston 13a Suction port 14 Frame 15 Bearing SC Scroll type refrigerant compressor RC Rotary type refrigerant compressor

Claims (4)

A bearing using a carbon graphite base material obtained by firing a molded product obtained by molding a mixture of carbon graphite aggregate and binder into a shape close to the shape to be used,
In the carbon graphite base material,
While containing ash content of 0.5-10% by mass,
Hollow open pores are formed so that the area porosity determined by microscopic observation is 15% or less,
More than half of the open pores are filled with copper α solid solution,
The said alpha solid solution of copper contains phosphorous copper or phosphorus, and the content of phosphorus is 0.05-7.5 mass%, The bearing characterized by the above-mentioned.   The bearing according to claim 1, wherein the kneaded material further includes an inorganic filler.   The carbon graphite base material in a state before the open pores are filled with the copper α solid solution has a graphite crystallinity of 15 to 50% by X-ray diffraction. The bearing according to claim 1 or claim 2. An alloy whose hardness is strengthened to H _V 100 or more by dispersing and precipitating Cu ₃ P in the α solid solution of copper is contained in the carbon graphite base material in an amount of 20 to 70% by mass. The bearing according to claim 1 or 2, wherein