OA18250A - Composite lubricating material, engine oil, grease, and lubricating oil. - Google Patents
Composite lubricating material, engine oil, grease, and lubricating oil. Download PDFInfo
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- OA18250A OA18250A OA1201700084 OA18250A OA 18250 A OA18250 A OA 18250A OA 1201700084 OA1201700084 OA 1201700084 OA 18250 A OA18250 A OA 18250A
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- 239000000463 material Substances 0.000 title claims abstract description 52
- 239000002131 composite material Substances 0.000 title claims abstract description 33
- 230000001050 lubricating Effects 0.000 title claims abstract description 30
- 239000004519 grease Substances 0.000 title claims abstract description 22
- 239000010705 motor oil Substances 0.000 title claims abstract description 11
- 239000010687 lubricating oil Substances 0.000 title 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 354
- 229910002804 graphite Inorganic materials 0.000 claims abstract description 148
- 239000010439 graphite Substances 0.000 claims abstract description 148
- 239000003575 carbonaceous material Substances 0.000 claims abstract description 81
- 238000002441 X-ray diffraction Methods 0.000 claims abstract description 22
- 239000000314 lubricant Substances 0.000 claims abstract description 14
- 239000002199 base oil Substances 0.000 claims description 37
- 239000000654 additive Substances 0.000 claims description 10
- 239000000941 radioactive substance Substances 0.000 claims description 6
- 230000000996 additive Effects 0.000 claims description 5
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- 238000002485 combustion reaction Methods 0.000 claims description 3
- 239000012530 fluid Substances 0.000 claims description 3
- 238000005096 rolling process Methods 0.000 claims description 3
- 230000001590 oxidative Effects 0.000 claims description 2
- 238000003786 synthesis reaction Methods 0.000 claims description 2
- 230000002194 synthesizing Effects 0.000 claims description 2
- 238000002050 diffraction method Methods 0.000 abstract 2
- 229910021389 graphene Inorganic materials 0.000 description 197
- OZAIFHULBGXAKX-UHFFFAOYSA-N precursor Substances N#CC(C)(C)N=NC(C)(C)C#N OZAIFHULBGXAKX-UHFFFAOYSA-N 0.000 description 99
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- 238000010586 diagram Methods 0.000 description 22
- 239000000203 mixture Substances 0.000 description 18
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- KXGVEGMKQFWNSR-LLQZFEROSA-N Deoxycholic acid Chemical compound C([C@H]1CC2)[C@H](O)CC[C@]1(C)[C@@H]1[C@@H]2[C@@H]2CC[C@H]([C@@H](CCC(O)=O)C)[C@@]2(C)[C@@H](O)C1 KXGVEGMKQFWNSR-LLQZFEROSA-N 0.000 description 2
- 241000196324 Embryophyta Species 0.000 description 2
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerol Natural products OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 2
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- 206010040844 Skin exfoliation Diseases 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N ZrO2 Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
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- ALYNCZNDIQEVRV-UHFFFAOYSA-N 4-Aminobenzoic acid Chemical compound NC1=CC=C(C(O)=O)C=C1 ALYNCZNDIQEVRV-UHFFFAOYSA-N 0.000 description 1
- 241001674808 Biastes Species 0.000 description 1
- CJZGTCYPCWQAJB-UHFFFAOYSA-L Calcium stearate Chemical compound [Ca+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O CJZGTCYPCWQAJB-UHFFFAOYSA-L 0.000 description 1
- BHQCQFFYRZLCQQ-OELDTZBJSA-N Cholic acid Chemical compound C([C@H]1C[C@H]2O)[C@H](O)CC[C@]1(C)[C@@H]1[C@@H]2[C@@H]2CC[C@H]([C@@H](CCC(O)=O)C)[C@@]2(C)[C@@H](O)C1 BHQCQFFYRZLCQQ-OELDTZBJSA-N 0.000 description 1
- 239000004380 Cholic acid Substances 0.000 description 1
- 229910002483 Cu Ka Inorganic materials 0.000 description 1
- USIUVYZYUHIAEV-UHFFFAOYSA-N Diphenyl ether Chemical class C=1C=CC=CC=1OC1=CC=CC=C1 USIUVYZYUHIAEV-UHFFFAOYSA-N 0.000 description 1
- 230000036499 Half live Effects 0.000 description 1
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- NRNCYVBFPDDJNE-UHFFFAOYSA-N Pemoline Chemical compound O1C(N)=NC(=O)C1C1=CC=CC=C1 NRNCYVBFPDDJNE-UHFFFAOYSA-N 0.000 description 1
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- HCWPIIXVSYCSAN-IGMARMGPSA-N Radium-226 Chemical compound [226Ra] HCWPIIXVSYCSAN-IGMARMGPSA-N 0.000 description 1
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- 238000003917 TEM image Methods 0.000 description 1
- 125000005037 alkyl phenyl group Chemical group 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminum Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
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- OYPRJOBELJOOCE-UHFFFAOYSA-N calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
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- 150000001720 carbohydrates Chemical group 0.000 description 1
- 239000006229 carbon black Substances 0.000 description 1
- 239000004359 castor oil Substances 0.000 description 1
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- 125000002091 cationic group Chemical group 0.000 description 1
- 150000001768 cations Chemical class 0.000 description 1
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- LFQSCWFLJHTTHZ-UHFFFAOYSA-N ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- RTZKZFJDLAIYFH-UHFFFAOYSA-N ether Substances CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 1
- 150000002170 ethers Chemical class 0.000 description 1
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- 239000010419 fine particle Substances 0.000 description 1
- 229910003472 fullerene Inorganic materials 0.000 description 1
- 239000012208 gear oil Substances 0.000 description 1
- 150000008131 glucosides Chemical class 0.000 description 1
- 239000010720 hydraulic oil Substances 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
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- 238000001746 injection moulding Methods 0.000 description 1
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- KEAYESYHFKHZAL-UHFFFAOYSA-N sodium Chemical compound [Na] KEAYESYHFKHZAL-UHFFFAOYSA-N 0.000 description 1
- 229910052708 sodium Inorganic materials 0.000 description 1
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- 239000011780 sodium chloride Substances 0.000 description 1
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- 239000003760 tallow Substances 0.000 description 1
- 239000011032 tourmaline Substances 0.000 description 1
- 229940070527 tourmaline Drugs 0.000 description 1
- 229910052613 tourmaline Inorganic materials 0.000 description 1
- RYFMWSXOAZQYPI-UHFFFAOYSA-K trisodium phosphate Chemical class [Na+].[Na+].[Na+].[O-]P([O-])([O-])=O RYFMWSXOAZQYPI-UHFFFAOYSA-K 0.000 description 1
- WMYJOZQKDZZHAC-UHFFFAOYSA-H trizinc;dioxido-sulfanylidene-sulfido-$l^{5}-phosphane Chemical compound [Zn+2].[Zn+2].[Zn+2].[O-]P([O-])([S-])=S.[O-]P([O-])([S-])=S WMYJOZQKDZZHAC-UHFFFAOYSA-H 0.000 description 1
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Abstract
Provided are a composite lubricating material, engine oil, grease and lubricant, excellent in lubricity. The composite lubricating material comprises at least a graphite-based carbon material and/or graphene-like graphite exfoliated from the graphite-based carbon material dispersed in a base material. The graphite-based carbon material is characterized by having a rhombohedral graphite layer (3R) and a hexagonal graphite layer (2H), wherein a Rate (3R) of the rhombohedral graphite layer (3R) and the hexagonal graphite layer (2H), based on an Xray diffraction method, which is defined by following Equation 1 is 31% or more: Rate (3R) = P3/(P3+P4)xl00 •••• Equation 1 wherein P3 is a peak intensity of a (101) plane of the rhombohedral graphite layer (3R) based on the Xray diffraction method, and P4 is a peak intensity of a (101) plane of the hexagonal graphite layer (2H) based on the X-ray diffraction method
Description
COMPOSITE LUBRICATING MATERIAL, ENGINE OIL, GREASE, AND LUBRICANT, AND METHOD OF PRODUCING A COMPOSITE LUBRICATING MATERIAL {Technical Field} {0001}
The présent invention relates to a composite lubricating material, engine oil, grease, and lubricant, and method of producing a composite lubricating material.
{Background Art} {0002}
In recent years, addition of various nanomaterials to a driving mechanism, such as an engine, and a transmission mechanism, such as a transmission gear and a réduction gear, has been studied for purposes of improving fuel consumption, reducing friction, and the like. In particular, for environmental or resource problems, carbon materials such as graphene, CNT (carbon nanotube) and fullerene hâve attracted attention as nonmetal nanomaterials.
{0003}
Taking engine oil as an example, addition of molybdenum disulfide (M0S2) or flaky graphite having a layered crystal structure, which exhibit low shearing résistance, and the
I like has been known (Non Patent Literature 5). Further, a sliding member in which a friction loss is further reduced on a sliding surface by using graphite in a particulate form has been studied {Patent Literature 1).
On the other hand, as for lubricants, for a purpose of prolonging the life of a lubricant by suppressing détérioration of the base oil itself caused by a température change, oxidation, and the like, addition of carbon materials, such as carbon fibers and carbon nanotubes, having an antioxidative effect and a decomposition/deterioration préventive effect for base oil, and radioactive substances generating a négative ion and the like has been studied (Patent Literatures 2, 3 and 4) .
{Citation List} {Patent Literature} {0004}
PTL | 1: | JP-A-2013-203905 | {[0091] | and | [0120]) |
PTL | 2: | JP-A-2008-298097 | ([0015]) | ||
PTL | 3: | JP-T-2013-538914 | ([0074] | and | [0090]) |
PTL | 4: | JP-A-2007-277500 | {[0002]- | [0003]) | |
PTL | 5: | WO 2014/064432 ( [0040]) |
{Non Patent Literature} {0005} »
NPL 1: Structural Change of Graphite with Griding; authors: Michio INAGAKI, Hisae MUGISHIMA, and Kenji HOSOKAWA; February lat, 1973 (Received)
NPL 2: Changes of Probabilities Pl, PABA, PABC with Heat Treatment of Carbons; authors: Tokiti NODA, Masaaki IWATSUKI, and Michio INAGAKI; September 16th, 1966 (Received) NPL 3: Spectroscopic and X-ray diffraction studies on fluid deposited rhombohedral graphite from the Eastern Ghats Mobile Belt, India; G.Parthasarathy, Current Science, Vol.90, No. 7, 10 April 2006
NPL 4: Classification of solid carbon materials and their structural characteristics; Nagoya Institute of Technology; Shinji KAWASAKI
NPL 5: Catalog Carbon Products for Mechanical Applications,
Toyo Tanso Co., Ltd. (Date of issue: Sep. 12, 2013)
NPL 6: Tribological properties of monolayer graphene oxide sheets as water-based lubricant additives; H. Kinoshita, Y. Nishina, A.A. Alias, M. Fujii; Carbon, Volume 66, Jan 2014, Pages 720-723 {Summary of Invention) {Technical Problem) {0006}
However, there is a problem in the methods disclosed in Patent Literature 1, namely, a sliding part is directly coated with graphite, thus making reapplication of the graphite difficult. Further, the methods disclosed in Patent Literatures 2 and 3 show that carbon fibers and carbon nanotubes are dispersed in base oil, and that performing this dispersion is effective in improving sliding performance, preventing oxidation, and suppressing changes in viscosity caused by température changes. However these effects are not significant. The methods disclosed in Patent
Literature 4 are intended to prevent oxidation and decomposition/deterioration of lubricant by adding tourmaline powders, however it is not clear if this contributes to improving lubricity.
{0007}
Further, regarding lubricity, performed by using oxidized graphene, from experiments it is shown that a lubricating agent comprising an aqueous dispersion of graphene has better lubricity than a conventional lubricating agent (Non Patent Literature 6) . Thus utilizing graphene in a lubricating agent is considered.
However, there has been a problem that an amount of the graphene that is exfoliated is normally small by processing natural graphite without any treatments. However, as a resuit of earnest studies, by carrying out predetermined treatments to graphite serving as a source material, there was obtained a graphite-based carbon material (a graphene »
precursor), from which graphene was easily exfoliated, the graphene being able to be dispersed at a high concentration or to a high degree. A part or whole of the graphene precursor is exfoliated by ultrasonic waves, stirring and sliding to produce a mixed material being graphene-like graphite, containing material from the graphene precursor to graphene. A size, thickness, etc. of the graphene-like graphite are not limited since they are variable depending on an addition amount, a process time, etc. of the graphene precursor, however, it is preferred that the graphene-like graphite is more flaked. That is, in other words, the graphite-based carbon material (the graphene precursor) is graphite capable of being easily exfoliated and dispersed as graphene-like graphite by sliding using a driving unit, such as an engine, a transmission gear, and a réduction gear.
It was found that lubricity could be improved by dispersing a small amount of the graphene precursors and/or the graphene-like graphite in a base material. Moreover, it was found that the composite lubricating material could be produced without using a spécifie production method. Regarding lubricity, for example, réduction of a friction coefficient, réduction of frictional résistance, radiation of sliding heat, prévention of oxidation and decomposition/deterioration of base oil, and the like can be
I improved, and as a resuit, this contributes to, for example, improving fuel consumption and the like.
{0008}
The invention has been completed focusing on such problems, and an object of the invention is to provide a composite lubricating material, engine oil, grease, and 1ubricant and method of producing a composite lubricating material, excellent in lubricity.
Another object of the invention is to provide a composite lubricating material capable of exhibiting desired characteristics even though an amount of the graphene-like graphite dispersed/added in a base material is small.
Yet another object of the invention is to provide a composite lubricating material excellent in lubricity by utilizing a conventional production process.
{Solution to Problem) {0009}
In order to solve the above-described problems, a composite lubricating material of the présent invention comprises at least a graphite based carbon material and/or graphene-like graphite exfoliated from the graphite-based carbon material dispersed in a base material, the graphite-based carbon material characterized by having a rhombohedral graphite layer <3R) and a hexagonal t
graphite layer (2H), wherein a Rate C3R) of the rhombohedral graphite layer (3R) and the hexagonal graphite layer (2H), based on an X-ray diffraction method, which is defined by following Equation 1 is 31% or more:
Rate (3R) = P3/(P3+P4)*100 ···· Equation 1 wherein
P3 is a peak intensity of a (101) plane of the rhombohedral graphite layer (3R) based on the X-ray diffraction method, and
P4 is a peak intensity of a (101) plane of the hexagonal graphite layer (2H) based on the X-ray diffraction method.
According to the features, the composite material is excellent in lubricity. This is because, it is speculated that, at least one of a graphite based carbon material and graphene-like graphite is dispersed in a base material, and as sliding is performed by a sliding part, the graphite based carbon material or the graphene-like graphite is further flaked, thereby increasing an absolute number of pièces of the graphene-like graphite. As a resuit, a density of the graphene-like graphite is increased over time and lubricity is improved.
It is noted that, in this spécification, a graphitebased carbon material and/or graphene-like graphite exfoliated from the graphite-based carbon material (are) dispersed means that at least any one of a graphite-based carbon material and graphene-like graphite exfoliated from the graphite-based carbon material is dispersed.
{0010}
A weight ratio of the graphite-based carbon material to the base material is characterized by being 1/10,000 or more to less than 1.
According to the feature, a lubrication function of added products can be sufficiently exerted.
{0011}
The base material is characterized by being at least one or more of base oil derived from minerai, synthesis, plants or animais.
According to the feature, a composite lubricating material excellent in lubricity can be obtained.
{0012}
The composite lubricating material is characterized by comprising at least one or more kinds of additives for a purpose of preventing oxidative détérioration.
According to the feature, the composite lubricating material is not only excellent in lubricity, but also can fully exert a lubrication function for a long time.
{0013}
The additives are characterized by comprising a radioactive substance.
According to the feature, a négative ion generated by the radioactive substance suppresses active oxygen that causes oxidation and décomposition of base oil, thus the life of a composite lubricating material can be further prolonged.
{0014}
Engine oil is characterized by comprising the composite lubricating material.
According to the feature, engine oil excellent in lubricity used for an internai combustion engine or the like can be obtained.
{0015}
Grease is characterized by comprising the composite lubricating material.
According to the feature, grease excellent in lubricity used for a sliding member such as a rolling bearing can be obtained.
{0016}
Lubricant is characterized by comprising the composite lubricating material.
According to the feature, lubricant used for an operating part such as a fluid bearing can be obtained.
{Brief Description of Drawings} {0017} {Fig. 1} Fig. 1 is a figure which shows a crystal structure of graphite, where (a) refers to a crystal structure of hexagonal crystals, and (b) refers to a crystal structure of rhombohedral crystals.
{Fig. 2) Fig. 2 is a diagram which shows an X-ray diffraction profile of general natural graphite.
(Fig. 3} Fig. 3 is a diagram which illustrâtes a production apparatus A using a jet mill and plasma of Example 1.
(Fig. 4} Fig. 4 is a figure which illustrâtes a production apparatus B using a bail mill and magnetron of Example 1, where (a) is a diagram which illustrâtes a pulverizing state, and (b) is a diagram which illustrâtes a state where graphite-based carbon materials (precursors) are collected.
{Fig. 5} Fig. 5 is a diagram which shows an X-ray diffraction profile of a graphite-based carbon material of Sample 5 produced by the production apparatus B according to Example 1.
{Fig. 6} Fig. 6 is a diagram which shows an X-ray diffraction profile of a graphite-based carbon material of Sample 6 produced by the production apparatus A according to Example 1.
{Fig. 7) Fig. 7 is a diagram which shows an X-ray diffraction profile of a graphite-based carbon material of Sample 1 indicating a comparative example.
{Fig. 8} Fig. 8 is a diagram which shows a dispersionproducing apparatus which produces a dispersion using a graphite-based carbon material as a precursor.
{Fig. 9} Fig. 9 is a diagram which shows dispersing states of dispersions produced by using graphite-based carbon materials of Sample 1 indicating a comparative example, and Sample 5 produced by the production apparatus B of Example 1.
{Fig. 10} Fig. 10 is a TEM image of a graphite-based carbon material {graphene) dispersed in a dispersion.
{Fig. 11} Fig. 11 is a figure which shows distribution states of a graphite-based carbon material dispersed in a dispersion which was produced using a graphite-based carbon material (precursor) of Sample 5, where (a) is a diagram which shows an average size distribution, while (b) is a diagram which shows a distribution of the number of layers.
{Fig. 12} Fig. 12 is a figure which shows a distribution state of a graphite-based carbon material dispersed in a dispersion which was produced using a graphite-based carbon material of Sample 1 indicating the comparative example, where (a) is a diagram showing an average size distribution, and (b) is a diagram showing a distribution of the number of layers.
{Fig. 13} Fig. 13 is a diagram which shows distributions of the number of layers of graphite-based carbon materials each dispersed in dispersions that were produced using Samples 1 to 7 as precursors.
{Fig. 14} Fig. 14 is a diagram which shows proportions of graphene having 10 layers or less to a content of 5 rhombohedral crystals dispersed in a dispersion.
{Fig. 15} Fig. 15 is a figure which shows a distribution state of graphite when varying conditions for producing a dispersion using a graphite-based carbon material (precursor) of Sample 5 according to Example 2, where (a) is 10 a diagram showing a distribution in a case where an ultrasonic treatment and a microwave treatment were combined, while (b) is a diagram showing a distribution of the number of layers in a case where an ultrasonic treatment was conducted.
{Fig. 16} Fig. 16 is a diagram which shows a résistance value when a graphite-based carbon material of Example 3 was dispersed in a conductive ink.
{Fig. 17} Fig. 17 is a diagram which shows a tensile strength when a graphite-based carbon material of Example 4 was 20 kneaded with a resin.
{Fig. 18} Fig. 18 is a diagram which shows an elastic modulus when a graphite-based carbon material of Example 5 was kneaded with a resin.
{Fig. 19} Fig. 19 is a diagram which shows distribution 25 states of graphite-based carbon materials in a dispersion, dispersed in N-methylpyrrolidone (NMP), for providing a supplementary description of a dispersing state of Example 5, where (a) is a distribution state of sample 12, and (b) is a distribution state of sample 2.
{Fig. 20} Fig. 20 is a diagram which illustrâtes a friction abrasion testing device of Example 6.
{Fig. 21} Fig. 21 is a graph which shows a friction coefficient of a test piece of Example 6.
{Fig. 22} Fig. 22 is a graph which shows an abrasion depth of the test piece of Example 6.
{Fig. 23} Fig. 23 is a SEM photographed image (plan view) of a graphene precursor.
{Fig. 24} Fig. 24 is a SEM photographed image (side view) of a graphene precursor.
{Fig. 25} Fig. 25 is a graph which shows a friction coefficient of a test piece of Example 7.
{Fig. 26} Fig. 26 is a graph which shows an abrasion depth of the test piece of Example 7.
{Fig. 27} Fig. 27 is a graph which shows a friction coefficient of a test piece of Example 8.
(Fig. 28} Fig. 28 is a graph which shows an abrasion depth of the test piece of Example 8.
(Fig. 29} Fig. 29 is a graph which shows a friction coefficient of a test piece of Example 9.
{Fig. 30} Fig. 30 is a graph which shows an abrasion depth of the test piece of Example 9.
(Description of Embodiments} {0018}
The invention focuses on a crystal structure of graphite, and, at first, matters relating to the crystal structure will be explained. It has been known that natural graphite is classified into three types of crystal structures, namely hexagonal crystals, rhombohedral crystals and disordered crystals, depending on an overlapping manner of layers. As shown in Fig. 1, hexagonal crystals hâve a crystal structure in which layers are arranged in the order of ABABAB··, while rhombohedral crystals hâve a crystal structure in which layers are arranged in the order of ABCABCABC··.
{0019}
In natural graphite, there are almost no rhombohedral crystals in a stage where natural graphite is excavated. However, about 14% of rhombohedral crystals exist in general natural graphite-based carbon materials because pulverization or the like is carried out in a purification stage. In addition, it has been known that a proportion of rhombohedral crystals converges on about 30% even when pulverization is carried out during purification for a long time (Non-Patent Literatures 1 and 2).
Moreover, a method in which graphite is expanded by heating, rather than with physical forces such as pulverization, thereby flaking the graphite. However, even when graphite is treated with a heat of 1600 K (about l,300°C), a proportion of rhombohedral crystals is about 25% (Non-Patent Literature 3) . Furthermore, the proportion is up to about 30% even when heat of an extremely high température of 3000°C is applied thereto (Non-Patent Literature 2).
Thus, although it is possible to increase a proportion of rhombohedral crystals by treating natural graphite with physical forces or heat, the upper limit is about 30%. (0020}
Hexagonal crystals (2H), which are included in natural graphite at a high level, are very stable, and an interlayer van der Waals’ force between their graphene layers is shown by Equation 3 (Patent Literature 5). By applying an energy exceeding this force, graphene is exfoliated. An energy required for the exfoliation is inversely proportional to the cube of the thickness. Therefore, in a thick state where numerous layers are overlapped, graphene is exfoliated by a weak physical force such as by very feeble ultrasonic waves. However, in a case where graphene is exfoliated from somewhat thin graphite, a very large energy is required. In other words, even if graphite is treated for a long time, only weak parts of the surface are exfoliated, and large parts remain not exfoliated.
{0021}
Fvdw = H-A/{6n*t3) ···· Equation 3
Fvdw: Van der Waals' force
H: Hamaker constant
A: Surface area of graphite or graphene t: Thickness of graphite or graphene {0022}
The présent inventors succeeded in increasing a proportion of rhombohedral crystals (3R), which had been increased to only about 30% by treatments of pulverization or heating to an extremely high température, to 30% or more by carrying out predetermined treatments, as shown below, to natural graphite. The following findings were obtained as results of experiments and studies. That is, when a content of rhombohedral crystals (3R) in a graphite-based carbon material is higher, particularly when the content is 31 % or more, there is a tendency that graphene is easily exfoliated by use of such a graphite-based carbon material as a precursor, thereby easily obtaining a highly concentrated and dispersed graphene dispersion or the like. For the reason, it is considered that, when a shear force or the like is applied to rhombohedral crystals (3R), a deformation occurs between layers, i.e. a deformation in the entire structure of the graphite becomes large, and graphene is easily exfoliated independently of the van der Waals' force. Accordingly, in the invention, a graphite-based carbon material, from which graphene is easily exfoliated by carrying out predetermined treatments to natural graphite, and which makes it possible to disperse graphene at a high concentration or to a high degree, is called a graphene precursor. Hereinafter, a method of producing a graphene precursor showing predetermined treatments, a crystal structure of the graphene precursor, and a graphene dispersion using the graphene precursor will be described in that order in examples below.
{0023}
Here, in the spécification, a graphene refers to a flake-like or sheet-like graphene which is a crystal of a mean size of 100 nm or more but which is not a fine crystal of a mean size of several nanometers to tens of nanometers, and which has 10 layers or less.
Additionally, since graphene is a crystal with a mean size of 100 nm or more, when artificial graphite and carbon black, which are amorphous (microcrystal) carbon materials other than natural graphite, are even treated, graphene cannot be obtained (Non-Patent Literature 4).
Further, in the spécification, a graphene composite means a composite which is produced by using the graphitebased carbon material useful as a graphene precursor according to the invention, i.e. a graphite-based carbon material having a Rate (3R) of 31% or more (e.g. Samples 27 of Example 1, samples 2, 21, ··· of Example 5 described below).
{0024}
Hereinafter, examples for carrying out the composite lubricating material, the engine oil, the grease, and the lubricant, according to the présent invention, will be described.
{Example 1} {0025} <As to production of a graphite-based carbon material useful as a graphene precursor>
A method for obtaining a graphite-based carbon material useful as a graphene precursor by a production apparatus A using a jet mill and plasma shown in Fig. 3 will be explained. As an example, the production apparatus A refers to a case in which plasma is applied for the radiowave-force-based treatment and in which the jet mill is used for the physicalforce-based treatment.
{0026}
In Fig. 3, the symbol 1 refers to a particle of 5 mm or less of a natural graphite material (flaky graphite ACB-50 manufactured by Nippon Graphite Industries, ltd.); the symbol 2 refers to a hopper which stores the natural graphite material 1; the symbol 3 refers to a Venturi nozzle which discharges the natural graphite material 1 from the hopper 2; the symbol 4 refers to a jet mill which jets the air which has been pumped from a compressor 5, while being divided into eight places, to thereby allow the natural graphite material to collide against the inside of a chamber by a jet biast; and the symbol 7 refers to a plasma generator which sprays a gas 9, such as oxygen, argon, nitrogen or hydrogen, through a nozzle 8 from a tank 6 and which applies a voltage to a coil 11, wound around the outer periphery of the nozzle 8, from a high-voltage power supply 10, thereby generating plasma inside the chamber of the jet mill 4, and the plasma generator is provided in each of four places inside the chamber. The symbol 13 refers to a pipe which connects the jet mill 4 and a dust collector 14 to one another; the symbol 14 refers to a dust collector; the symbol 15 refers to a collection container; the symbol 16 refers to a graphitebased carbon material (graphene precursor); and the symbol 17 refers to a blower.
{0027}
Next, the production method will be explained. Conditions for the jet mill and plasma are as follows.
The conditions for the jet mill are as follows. Pressure: 0.5 MPa
Air volume: 2.8 m3/min
Nozzle inner Diameter: 12 mm
Flow rate: about 410 m/s
The conditions for plasma are as follows.
Output: 15 W
Voltage: 8 kV
Gas species: Ar (purity 99.999 vol%)
Gas flow rate: 5 L/min {0028}
It is considered that the natural graphite materials 1, which hâve been charged into the chamber of the jet mill 4 from the Venturi nozzle 3, are accelerated to the sonie velocity or higher inside the chamber, and are pulverized by impact between the natural graphite materials 1 or by impact of them against the wall, and that, simultaneously, the plasma 12 discharges an electric current or excites the natural graphite materials 1, acts directly on atoms (électrons), and increases deformations of crystals, thereby promoting the pulverization. When the natural graphite materials 1 turn into fine particles of a certain particle diameter (about 1 to 10 pm), their mass is reduced, the centrifugal force is weakened, and, consequently, the natural graphite materials 1 are pumped out from the pipe 13 which is connected to the center of the chamber.
{0029}
A gas including graphite-based carbon materials (graphene precursors), which hâve been flowed from the pipe 13 into a cylindrical container of the chamber of the dust collector 14, forms a spiral flow, and drops the graphitebased carbon materials 16, which collide with the internai wall of the container, to a collection container 15 below, while an ascending air current generates in the center of the chamber due to a tapered container part of the downside of the chamber, and the gas is emitted from the blower 17 (so-called cyclone effects). According to the production apparatus A in this example, about 800 g of a graphene precursor from 1 kg of the raw materials, i.e. natural graphite materials 1, is used. The graphite-based carbon material (graphene precursors) 16 was obtained (recovery efficiency: about 80%).
{0030}
Next, based on the production apparatus B using a bail mill and microwaves shown in Fig. 4, a method for obtaining a graphite-based carbon material useful as a graphene precursor will be described. The apparatus B refers to, as an example, a case where microwaves are applied as the radiowave-force-based treatment and where a bail mill is used for the physical-force-based treatment.
{0031}
In Fig. 4 (a) and (b), the symbol 20 refers to the bail mill; the symbol 21 refers to a microwave generator (magnetron) ; the symbol 22 refers to a wave guide; the symbol 23 refers to a microwave inlet; the symbol 24 refers to a media; the symbol 25 refers to particles of 5 mm or less of a natural graphite material (flaky graphite ACB-50 manufactured by Nippon Graphite Industries, ltd.); the symbol 26 refers to a collection container; the symbol 27 refers to a filter; and the symbol 28 refers to graphitebased carbon material (graphene precursors).
{0032}
Next, the production method will be explained. Conditions for the bail mill and the microwave generator are as follows.
The conditions for the bail mill are as follows.
Rotational speed: 30 rpm
Media size: <p5 mm
Media species: zirconia balls
Pulverization time: 3 hours
The conditions for the microwave generator (magnetron) are as follows.
Output: 300 W
Frequency: 2.45 GHz
Irradiation method: Intermittent {0033} kg of natural graphite carbon raw materials 25 and
800 g of media 24 are charged into the chamber of the bail mill 20, the chamber is closed, and the mixture is treated at a rotational speed of 30rpm for 3 hours. During the treatment, microwaves are irradiated intermittently (for 20 seconds every 10 minutes) to the chamber. It is considered that the microwave irradiation acts directly on atoms {électrons) of the raw materials, thus increasing deformations of the crystals. After the treatment, media 24 are removed by the filter 27, and thus, powder of about 10 pm of graphite-based carbon materials (precursors) 28 can be collected in the collection container 26.
{0034} <As to an X-ray diffraction profile of graphite-based carbon materials (graphene precursors)>
With reference to Figs. 5 to 7, X-ray diffraction profiles and crystal structures will be described with respect to graphite-based natural materials (Samples 6 and
5) produced by the production apparatuses A and B, and the powder of about 10 pm of graphite-based natural materials (Sample 1: a comparative example) obtained by using only the bail mill of the production apparatus B.
The measurement conditions for the X-ray diffraction apparatus are as follows.
Source : Cu Ka ray
Scanning speed : 20 ’ / min
Tube voltage : 40kV
Tube current : 30mA
According to the X-ray diffraction method (horizontalsample-mounting-model multi-purpose X-ray diffractometer Ultima IV manufactured by Rigaku Corporation), each sample shows peak intensities PI, P2, P3 and P4 in the planes (100), (002) and (101) of hexagonal crystals 2H and in the plane (101) of rhombohedral crystals 3R. Therefore, these peak intensities will be explained.
Here, the measurements of X-ray diffraction profile hâve been used the so-called standardized values at home and abroad in recent years. This horizontal-sample-mountingmodel multi-purpose X-ray diffractometer Ultima IV manufactured by Rigaku Corporation is an apparatus which can measure X-ray diffraction profile in accordance with JIS R 7651:2007 Measurement of lattice parameters and crystallite sizes of carbon materials. In addition, Rate (3R) is the ratio of the diffraction intensity obtained by the Rate (3R) = P3 / (P3 + Ρ4)χ 100, even if the value of the diffraction intensity is changed, the value of Rate (3R) is not changes. Means that the ratio of the diffraction intensity is t
standardized, it is commonly used to avoid performing the identification of the absolute value substance and its value does not dépend on measurement devices.
{0035}
As shown in Fig. 5 and Table 1, Sample 5 produced by the production apparatus B, which applies a treatment with a bail mill and a microwave treatment, had high rates of peak intensifies P3 and Pl, and a Rate (3R) defined by Equation 1 showing a rate of P3 to a sum of P3 and P4 was 46%. Additionally, the intensity ratio P1/P2 was 0.012.
Rate (3R) = P3/(P3+P4)*100 ···· Equation 1 wherein
Pl is a peak intensity of a (100) plane of the hexagonal graphite layer (2H) based on the X-ray diffraction method,
P2 is a peak intensity of a (002) plane of the hexagonal graphite layer (2H) based on the X-ray diffraction method,
P3 is a peak intensity | of a | (101) | plane of the |
rhombohedral graphite layer | (3R) | based | on the X-ray |
diffraction method, and | |||
P4 is a peak intensity of a | (101) | plane of the hexagonal |
graphite layer (2H) based on the X-ray diffraction method.
{0036} {Table 1}
Peak intensities [counts·deg] (2Θ [°]) | |
Hexagonal crystals 2H (100) [Pl] | 162 (42.33) |
Hexagonal crystals 2H (002) [P2] | 13157 (26.50) |
Rhombohedral crystals 3R (101) [P3] | 396 (43.34) |
Hexagonal crystals 2H (101) (P4J | 466 (44.57) |
{0037}
In the same manner, as shown in Fig. 6 and Table 2,
Sample 6 produced by the production apparatus A, which applies a treatment based on the jet mill and a treatment 5 based on plasma, had high rates of peak intensities P3 and
Pl, and the Rate (3R) was 51%. In addition, the intensity ratio P1/P2 was 0.014.
{0038} (Table 2}
Peak intensities [countS’deg] (20 [°] ) | |
Hexagonal crystals 2H (100) [PU | 66 {42.43} |
Hexagonal crystals 2H (002) [P2] | 4,675 (26.49) |
Rhombohedral crystals 3R (101) [P31 | 170 (43.37) |
Hexagonal crystals 2H (101) [P4] | 162 ¢44.63) |
{0039}
Furthermore, as shown in Fig. 7 and Table 3, Sample 1 indicating a comparative example produced with only the bail mill had a small rate of a peak intensity P3, compared with Samples 5 and 6, and the Rate (3R) was 23%. In addition, 5 the intensity ratio P1/P2 was 0 .008.
{0040} {Table 3}
Peak intensities [counts *deg] (2Θ[°]) | |
Hexagonal crystals 2H (100) [Pl] | 120 (42.4) |
Hexagonal crystals 2H (002) [P2] | 15,000 (26.5) |
Rhombohedral crystals 3R (101) [P3] | 50 (43.3) |
Hexagonal crystals 2H (101) [P4] | 160 (44.5) |
{0041}
Thus, Sample 5 produced by the production apparatus B of Example 1, and Sample 6 produced by the production apparatus A of Example 1 had Rates (3R) of 46% and 51%, respectively, and it was shown that their Rates (3R) were 40% or more, or 50% or more, compared with the natural graphite shown in Fig. 2 and Sample 1 indicating a comparative example.
Next, graphene dispersions were produced using the 10 above-produced graphene precursors, and their easiness in exfoliation of graphene was evaluated.
* {0042} <As to graphene dispersions>
A method for producing a graphene dispersion will be explained with reference to Fig. 8. Fig. 8 shows, as an example, a case where an ultrasonic treatment and a microwave treatment are combined in a liquid when a graphene dispersion is produced.
(1) 0 .2 g of a graphite-based carbon material useful as a graphene precursor and 200 ml of N-methylpyrrolidone (NMP) which serves as dispersing medium are charged to a beaker 40.
{2} The beaker 40 is put into a chamber 42 of a microwave generator 43, and an ultrasonic trembler 44A of an ultrasonic horn 44 is inserted into dispersing medium 41 from the upper direction.
(3) The ultrasonic horn 44 is activated, and ultrasonic waves of 20 kHz (100 W) are continuously applied thereto for 3 hours.
(4) While the above ultrasonic horn 44 is actuated, the microwave generator 43 is activated to apply microwaves of
2.45 GHz (300 W) intermittently (irradiation for 10 seconds every 5 minutes) thereto.
{0043}
I
Fig. 9 refers to appearances of graphene dispersions produced in the above-described way when 24 hours had passed.
Although a portion of the graphene dispersion 30 using Sample 5 produced by the production apparatus B was deposited, a product entirely showing a black color was observed. For this, it is considered that a large portion of the graphite-based carbon materials used as graphene precursors are dispersed in a state where graphene is exfoliated from them.
In the dispersion 31 using Sample 1 indicating a comparative example, most of the graphite-based carbon materials were deposited, and it was confirmed that a portion thereof floated as a supernatant. From the facts, it is considered that graphene was exfoliated from a small portion thereof and that they floated as the supernatant.
{0044}
Furthermore, the graphene dispersion produced in the above-described way was diluted to an observable concentration, was coated onto a sample stage (TEM grid), and the grid was dried. Thus, the size and the number of layers of graphene was observed in the captured image of a transmission électron microscope (TEM), as shown in Fig. 10. In addition, the grid coated with the diluted supernatant was used for Sample 1. For example, in the case of Fig. 10, the size corresponds to a maximum length L of a flake 33, »
which was 600 nm, based on Fig. 10 (a). As for the number of layers, the end face of the flake 33 was observed in Fig.
(b), and overlapping graphene layers were counted, thereby calculating the number of layers as 6 layers (a portion indicated by the symbol 34). In this way, the size and the number of layers were measured with respect to each flake (N indicates the number of flakes), and the numbers of graphene layers and the sizes shown in Figs. 11 and 12 were obtained.
{0045}
With reference to Fig. 11 (a), a particle size distribution (distribution of sizes) of thin flakes included in the graphene dispersion of Sample 5 (Rate (R3) of 46%) produced by the production apparatus B of Example 1 was a distribution having a peak of 0.5 pm. In addition, in Fig.
(b), as to the number of layers, a distribution which had a peak in 3 layers and in which graphene having 10 layers or less were 68% was observed.
With reference to Fig. 12, a particle size distribution (distribution of sizes) of thin flakes included in the dispersion of Sample 1 (Rate (R3) of 23%) of the comparative example was a distribution having a peak of 0.9 pm. In addition, as for the number of layers, a distribution in which those having 30 layers or more occupied the greater portion and in which graphene having 10 layers or less were 10% was observed.
From the results, it was revealed that, when the product of Sample 5 produced by the production apparatus B was used as a graphene precursor, a highly-concentrated graphene dispersion which contains plenty of graphene of 10 layers or less and which has excellent dispersibility of graphene can be obtained.
{0046}
Next, with reference to Fig. 13, a relation between the Rate (3R) of the graphene precursor and the number of layers in the graphene dispersion will be described. Samples 1, 5 and 6 in Fig. 13 are those described above. Samples 2, 3 and 4 were produced by the production apparatus B which carried out a treatment based on a bail mill and a microwave treatment, and were graphene dispersions produced using graphene precursors which had been produced by making the irradiating time of microwaves shorter than that for Sample 5. In addition, Sample 7 was produced by the production apparatus A which carried out a treatment based on a jet mill and a plasma treatment, and was a graphene dispersion produced by using a graphene precursor which had been produced by applying plasma of a higher output than that for Sample 6.
{0047}
From Fig. 13,as to Samples 2 and 3 showing Rates (3R) of 31% and 38%, respectively, the distributions of the number of layers hâve peaks at around 13 as the number of layers;
that is, the shapes of the distributions are close to that of a normal distribution (dispersions using Samples 2 and
3). As to Samples 4 to 7 showing Rates (3R) of 40% or more, the distributions of the number of layers hâve peaks at several as the number of layers (thin graphene); that is, the shapes of the distributions are those of a so-called 10 lognormal distribution. On the other hand, as to Sample 1 having a Rate (3R) of 23%, the distribution thereof has a peak at 30 or more as the number of layers (a dispersion using Sample 1) . That is, it is understood as follows: there is a tendency that, in cases where the Rate (3R) reaches 31% 15 or more, the shapes of the layer number distributions differ from those for cases where the Rate (3R) is less than 31%;
and further, in cases where the Rate (3R) reaches 40% or more, the shapes of the layer number distributions clearly differ from those for cases where the Rate (3R) is less than 20 40%. In addition, it can be understood that, as to proportions of graphene of 10 layers or less, the Rate (3R) of the dispersion using Sample 3 is 38%, while the Rate (3R) of the dispersion using Sample 4 is 62%, and that, when the
Rate (3R) reaches 40% or more, a proportion of graphene of 25 10 layers or less rapidly increases.
I » {0048}
From these facts, it can be considered that graphene of 10 layers or less are easily exfoliated in cases where the Rate (3R) is 31% or more, and that, as the Rate (3R) increases to 40%, 50% and 60%, graphene of 10 layers or less are more easily exfoliated. In addition, focusing on the intensity ratio P1/P2, Samples 2 to 7 show values within a comparatively narrow range of 0.012 to 0.016, and any of them are préférable because they exceed 0.01 where it is considered that graphene is easily exfoliated since crystal structures will be deformed.
{0049}
Furthermore, results obtained by comparing Rates (3R) and proportions of graphene of 10 layers or less included therein are shown in Fig. 14. With reference to Fig. 14, it was revealed that, when the Rate (3R) reached 25% or more, around 31%, graphene of 10 layers or less started to increase (showing an ever-increasing slope). Further, it was revealed that, around 40%, graphene of 10 layers or less rapidly increased (as to proportions of graphene of 10 layers or less, whereas the Rate (3R) of the dispersion using Sample 3 was 38%, the Rate (3R) of the dispersion using Sample 4 was 62%, and the proportion of graphene of 10 layers or less rapidly increased by 24% as the Rate (3R) increased by 4%), and that a percentage of graphene of 10 layers or less
I against the total graphene was 50% or more. In addition, the points of black squaree in Fig. 14 each correspond to different samples, and above-described Samples 1 to 7 and other samples are included therein.
{0050)
From the facts, when a sample showing a Rate (3R) of 31% or more is used as a graphene precursor to produce a graphene dispersion, the proportion of distributed graphene of 10 layers or less starts increasing; further, when a sample showing a Rate (3R) of 40% or more is used as a graphene precursor to produce a graphene dispersion, 50% or more of graphene of 10 layers or less are produced. In other words, a graphene dispersion in which graphene is highly concentrated and highly dispersed can be obtained. Furthermore, because almost no graphite-based carbon materials (precursors) included in the dispersion deposit as described above, a concentrated graphene dispersion can easily be obtained. According to this method, even a graphene dispersion whose graphene concentration exceeded 10% can be produced without concentrating it. Particularly, the Rate (3R) is preferably 40% or more from a view point that the proportion of dispersed graphene of 10 layers or less sharply increases to 50% or more.
{0051} r
The above description clarifies the following: when the Rate (3R) is 31% or more, preferably 40% or more, and further preferably 50% or more, séparation into graphene of 10 layers or less and thin graphite-based carbon materials of around 10 layers occurs in a greater proportion in many cases; and in the case where these graphite-based carbon materials are used as graphene precursors, a highly-concentrated graphene dispersion that has excellent dispersibility of graphene can be obtained. Still further, Example 5 to be described below clarifies that, in the case where the Rate (3R) is 31% or more, graphite-based carbon materials are useful as a graphene precursor.
{0052}
Furthermore, an upper limit for the Rate (3R) is considered that the upper limit is not particularly defined. However, it is préférable that the upper limit is defined such that the intensity ratio P1/P2 simultaneously satisfies 0.01 or more, because graphene precursors are easily exfoliated when a dispersion or the like is produced. In addition, in cases of production methods using production apparatuses A and B, the upper limit is about 70%, from a viewpoint that graphene is easily produced. Also, a method combining a treatment based on the jet mill of the production apparatus A and a plasma treatment is more préférable, because a graphene precursor having a higher Rate (3R) can t
easily be obtained. Additionally, the Rate (3R) as long as it reaches 31% or more by combining the physical-force-based treatment and the radiowave-force-based treatment.
{Example 2} {0053}
In Example 1, a case where the ultrasonic treatment and the microwave treatment were combined for obtaining a graphene dispersion is explained. In Example 2, only an ultrasonic treatment was carried out while a microwave treatment was not carried out, and other conditions were the same as those for Example 1.
Fig. 15 (b) shows a distribution of a number of layers with respect to a graphene dispersion which was obtained by carrying out an ultrasonic treatment using the graphene precursor of Sample 5 (Rate (3R) = 46%) produced by the production apparatus B. In addition, Fig. 15 (a) is the same as the distribution shown in Fig. 11 (b) of Sample 5 produced by the production apparatus B of Example 1.
As a resuit, although the tendency of the distribution of the number of layers was almost similar, a proportion of graphene of 10 layers or less was 64%, and was slightly decreased, compared with 68% of Example 1. From the fact, it was revealed that it was more effective to simultaneously carry out two of the treatments based on a physical force and a radiowave force for producing a graphene dispersion.
{Example 3) {0054}
In Example 3, an example used for a conductive ink will be described.
Sample 1 (Rate (3R) = 23%), Sample 3 (Rate (3R) = 38%), Sample 5 (Rate (3R) = 46%) and Sample 6 (Rate (3R) = 51%) of Example 1 were used as graphene precursors in mixture solution of water and an alcohol of the carbon number of 3 or less, which severed as a conductivity-imparting agent, at concentrations adopted for conductive inks, thus producing INK1, INK3, INK5 and INK6, and their résistance values were compared. Based on the results, as the Rates (3R) became higher, the résistance values were lower.
{Example 4} {0055}
In Example 4, an example in which a graphene precursor was kneaded with a resin will be explained.
When a resin sheet, in which graphene was dispersed, was produced, the tensile strength was very superior although glass fibers were added thereto. Therefore, a factor for this was studied, and, consequently, a finding that a t
compatibilizer added simultaneously with the glass fibers contributed to formation of graphene from the precursor could be obtained. Therefore, products obtained by mixing dispersing agents and a compatibilizer into a resin were studied.
wt% of Sample 5 (Rate (3R) = 46%) of Example 1 was added as a precursor directly to LLDPE (polyethylene), and the mixture was kneaded while applying shear (a shearing force) thereto with a kneader, two-shaft kneader (extruder) or the like.
It has been publicly known that, when a graphite-based carbon materials turned into graphene, being highly dispersed in a resin, the tensile strength increases. Therefore, by measuring a tensile strength of the resin, degrees of exfoliating into graphene and dispersion can relatively be estimated. The tensile strength was measured with an exact tabletop general-purpose testing machine (AUTOGRAPH AGS-J) manufactured by Shimadzu Corporation under a condition of test speed of 500 mm/min.
(0056}
In addition, in order to compare degree of exfoliating into graphene and dispersibility depending on the presence or absence of additives, the following comparisons of three types of (a), (b) and (c) were carried out.
(a) No additives (b) a general dispersing agent (zinc stéarate) (c) a compatibilizer (a graft-modified polymer) {0057}
With reference to Fig. 17 showing the measurement results, the results will be explained. In addition, in Fig. 17, circles refer to resin materials using Sample 1 of the comparative example, and squares refer to resin materials using Sample 5 of Example 1.
In case (a) where no additive was added, a différence of the tensile strengths was small.
In case (b) where the dispersing agent was added, it was revealed that formation of graphene was promoted to a certain degree in the graphene precursor of Sample 5.
In case (c) where the compatibilizer was added, it was revealed that that formation of graphene was significantly promoted in the graphene precursor of Sample 5. This is because it is considered that, besides effects to disperse graphene, the compatibilizer binds the graphene layer-bound bodies and the resin, and acts on them such that the graphene layer-bound bodies are stripped therefrom, when applying shear in that state. {0058}
Zinc stéarate is explained above as an example of the dispersing agent. However, those suited for compounds may be selected. As examples of the dispersing agent, anionic (anion} surfactants, cationic (cation) surfactants,
I zwitterionic surfactants, and nonionic surfactants can be mentioned. In particular, anion surfactants and nonionic surfactants are préférable for graphene. Nonionic surfactants are more préférable. Since nonionic surfactants are surfactants which do not dissociate into ions and which show hydrophilic properties by hydrogen bonds with water, as observed in oxyethylene groups, hydroxyl groups, carbohydrate chains such as glucoside, and the like, there is a merit that they can be used in nonpolar solvents, although they do not hâve a strength of hydrophilicity as high as ionic surfactants. Further, this is because, by varying chain lengths of their hydrophilic groups, their properties can freely be changed from lipophilie properties to hydrophilic properties. As anionic surfactants, X acid salts (as for the X acid, for example, cholic acid, and deoxycholic acid), for example, SDC: sodium deoxycholate, and phosphate esters, are préférable. Furthermore, as nonionic surfactants, glycerol fatty acid esters, sorbitan fatty acid esters, fatty alcohol ethoxylates, polyoxyethylene alkyl phenyl ether, alkyl glycosides, and the like are préférable.
{Example 5} {0059}
In order to further verify that those obtained when the Rate (3R) is 31% or more are bénéficiai as graphene precursors, which is described above in Example 1, an example in which a graphene precursor was kneaded with a resin will be further explained in Example 5. The following explains elastic moduli of resin molded articles in which graphitebased carbon materials containing Samples 1 to 7 in Example 1, having Rates (3R) plotted in Fig. 14, were used as precursors, {0060} (1) Using the above-described graphite-based carbon material as a precursor, 5wt% of LLDPE (polyethylene: 20201J produced by Prime Polymer Co., Ltd.) and lwt% of a dispersant (nonionic surfactant) were mixed in an ion-exchanged water, and the above-described device illustrated in Fig. 8 was actuated under the same conditions, whereby graphene dispersions containing 5wt% of graphene and graphite-based carbon materials were obtained.
(2) 0.6 kg of the graphene dispersion obtained in (1) was immediately kneaded into a resin of 5.4 kg using a kneader (pressing-type kneader WDS7-30 produced by Moriyama Co., Ltd.), whereby pellets were produced. The kneading conditions are to be described below. It should be noted that the mixing ratio between the resin and the dispersion was selected so that the amount of the graphene and graphitet based carbon matériels mixed therein was eventually 0.5wt%.
(3) The pellets produced in (2) were formed into a test piece according to JIS K7161 1A (length: 165 mm, width: 20 mm, thickness: 4 mm) by an injection molding machine.
(4) The elastic modulus (Mpa) of the test piece produced in (3) was measured under a condition of a test speed of 500 mm/min according to JIS K7161 by a table-top type précision universal tester produced by Shimadzu Corporation (AUTOGRAPH AGS-J).
(0061)
The kneading conditions were as follows.
Kneading température: 135°C
Rotor rotation speed: 30 rpm
Kneading time: 15 minutes '
Pressurization in furnace: applying 0.3 MPa for 10 minutes after start, and depressurizing to atmospheric pressure after the 10 minutes elapsed {0062}
Here, the dispersion of the above-described graphene dispersion into a resin is considered as follows. As the melting point of a resin is generally 100°C or higher, water evaporates in atmosphère, but in a pressing-type kneader, the inside of a furnace can be pressurized. In the inside of the furnace, the boiling point of water is raised so that the dispersion is kept in a liquid form, whereby an émulsion
I of the dispersion and the resin can be obtained. After applying pressure for a predetermined time, the inside is gradually depressurized, which causes the boiling point of water to decrease, thereby allowing water to evaporate. Here, graphene confined in water are left in the resin. This causes graphene and graphite-based carbon materials to be dispersed at a high concentration in the resin.
Further, since the graphene and graphite-based carbon materials tend to precipitate in the graphene dispersion as time elapses, the graphene dispersion is kneaded into the resin preferably immediately after the graphene dispersion is obtained.
{0063}
It should be noted that the following may be used as the means for obtaining the émulsion of the dispersion and the resin, other than the pressing kneader: a chemical thruster; a vortex mixer; a homomixer; a high-pressure homogenizer; a hydroshear; a flow jet mixer; a wet jet mill; and an ultrasonic generator.
Further, the following may be used as a solvent for the dispersion, other than water: 2-propanol (IPA); acetone; toluene; N-methylpyrrolidone (NMP); and N,N-dimethyl formamide (DMF).
{0064}
Table 4 illustrâtes the relationship between the Rates (3R) of around 30% and the elastic moduli of resin molded articles. It should be noted that Sample 00 in Table 4 is a blank Sample in which no precursor was kneaded, Samples 11 and 12 hâve Rates (3R) between that of Sample 1 and that of 5 Sample 2, and Sample 21 has a Rate (3R) between that of
Sample 2 and that of Sample 3.
{0065} (Table 4}
Sample No. | 00 | 1 | 11 | 12 | 2 | 21 | 3 | 4 |
P3/(P3+P4) | - | 23% | 25% | 28% | 31% | 35% | 38% | 42% |
Elastic modulus (MPa) (Average in 5 times) | 175 | 197 | 196 | 199 | 231 | 249 | 263 | 272 |
Différence from blank | - | 12.4 % | 12.0 % | 13.9 % | 31.7 % | 42.1 % | 50.0 % | 55.6 % |
Under-10 layers upon dispersion in NM P (Reference) | - | 10% | 12% | 25% | 25% | 30% | 38% | 62% |
{0066}
Fig. 18 and Table 4 prove that the différence of the elastic modulus with respect to that of Sample 00 (blank) (increase ratio of the elastic modulus) is approximately uniform around 10% until the Rate (3R) reaches 31%; after 15 the Rate (3R) reaches 31%, the différence sharply increases to 32%; while the Rate (3R) increases from 31% to 42%, the différence monotonously increases to 50%; and after the Rate (3R) reaches 42%, the différence slightly increases and a
converges to around 60%. In this way, when the Rate (3R) is 31% or more, a resin molded article having an excellent elastic modulus can be obtained. Further, since the amount of graphene and graphite-based carbon materials contained in a resin molded article is 0.5wt%, which is small, influence on properties that the resin originally possesses is small. {0067}
It is considered that this tendency attributes to a sharp increase in a thin graphite-based carbon material containing graphene having 10 or less layers in contact with a resin after the Rate (3R) reaches 31%. Here, in Example 5, it is impossible to détermine the number of layers of graphene by observation with TEM due to influences of a dispersant used for dispersion in water. Then, only for reference, the reason for the sharp increase described above is considered based on the distribution of the numbers of layers of the graphite-based carbon material illustrated in Table 4 upon dispersion in NMP. Sample 12 and Sample 2 are compared with each other, and it is found that both of the proportions of graphene (the number of layers are 10 or less) were 25%. On the other hand, as illustrated in Fig. 19, as to Sample 2, the proportion of thin ones having less than 15 layers was greater as compared with Sample 12; in other words, the graphite-based carbon material dispersed as a precursor had a larger surface area, which means that the t
area thereof in contact with the resin sharply increased.
In this way, Example 5 clearly indicates that when the
Rate (3R) is 31% or more, a graphite-based carbon material used as a graphene precursor tends to be separated into graphene having 10 or less layers and a thin graphite-based carbon material.
{Example 6} {0068}
Experiments were performed by adding the graphene precursors produced by the above methods to base oil.
{0069} <Various conditions>
Base oil (minerai oil): Daphné Mechanic Oil 32 (ISO viscosity grade of VG32 manufactured by Idemitsu Kosan. Co., Ltd.) (for industry),
Testing device: Friction abrasion testing device TRBS-DU-0000 (manufactured by CSM Instruments), «Ball-on-disk method»
Bail (diameter: 06 mm, material: SUJ2, hardness
HV780),
Disk (diameter: 030, thickness: 2 mm, material:
SUS440C, hardness: HV240, surface roughness 0.3 pmRzjis), <Frictional condition 1: rotational speed: 100 rpm, radius: 10 mm, load: 5 N, oil température: 80°C 30 min>
<Conforming to JIS R 1613 and DIN50324, as well as ASTM and IS0>
Surface roughness measuring device: SV-3000CNC (manufactured by Mitutoyo Corp.) <Measuring condition: Speed of 0.1 mm/sec, tip radius of 2 pm, measurement force of 0.75 mN, conforming to JIS B0651:2001>
Graphite-based carbon material: graphene precursor (produced by the above methods),
Mixer (ARE-310 manufactured by THINKY), <Mixing condition 1: Normal température of 25°C, mixing at 2,000 rpm x 10 min, defoaming after mixing at 2,100 rpm x 30 sec)
Comparative material: molybdenum disulfide powder (M-5 manufactured by Daizo Corp. Average diameter of 0.45 pm) (0070) <Experimental procedures>
Step 1. To base oil (990 g), 10 g of graphene precursors (see Samples 1, 2, 21, and 4 (Samples used in Examples 1 and 5)) are added, and, under the mixing condition 1, the graphene precursors are exfoliated and dispersed to obtain a dispersion 62 having a concentration of lwt%.
Step 2. 600 g of the dispersion 62 was put into a liquid holder 61 of a testing device 60 and a friction test was performed by rotating a disk 64 while being contacted with a bail 63 under the frictional condition 1.
Step 3. In a 30 min-long test, average values of a friction coefficient (μ) for the last 30 sec before the end of the 5 test were read and plotted in Fig. 21.
Step 4. By using a surface roughness measuring device, five worn parts on a surface of the disk 64 caused by a contact with the bail 63 were measured, and an abrasion depth was obtained from average values of this measurement and plotted 10 in Fig. 22.
{0071)
In order to confirm an effect of graphene-like graphite, experiments were performed with a Rate (3R) of 23% (Sample 1), 31% (Sample 2), 35% (Sample 21), and 42% (Sample 4) with 15 a mixture ratio shown in Table 5.
Comparative example 6-2 | | Comparative example 6-1 | Example 6-4 | Example 6-3 | | Example 6-2 | | Example 6-1 | | ||
LD LD | 100 | KD KD | LD LD | 99 | 99 | Base oil | Mixture ratio (wt%) |
1— | 1 | 1 | 1 | 1 | 1 | 2 o ω Kl | |
1 | 1 | 1 | 1 | 1 | 1— | 23% (Sample 1) | Graphene precursor Rate (3R) |
1 | 1 | ( | 1— | en P LJ ΰ B ΙΌ o*> l-· Φ | |||
1 | 1 | 1 | H* | 1 | 1 | 35% (Sample 21) | |
1 | 1 | l·— | 1 | 1 | 1 | en . ω & ΐ B M Ό <*> 1— Φ | |
o * o LD G) | 0.125 | 0.022 | 0.025 | | 0.041 | | 0.095 | Friction coefficient (μ) | |
9.2 | 1— H» | 2.0 | M ίο | 3.1 | 7.2 | Abrasion depth (pm) |
{0072}
LD
I {0073} From Table 5 and Figs. 21 and 22, it was observed that a friction coefficient in Examples 6-2, 6-3, and 6-4 was lower than in Example 6-1 and Comparative examples 6-1 and 6-2, in other words, sliding properties were improved. In particular, when the Rate (3R) of the graphene precursor reached 31% or more, it was observed that a friction coefficient had a remarkable tendency of becoming significantly low, as compared with cases of the Rate (3R) being 0% (Comparative example 6-1) (strictly speaking, this is not the same as Rate (3R) = 0%. Since a graphene precursor was not added, the 0% data shouldn't be plotted to the same graph. Nevertheless the data is plotted at the position of 0% for convenience. Hereinafter, 0% has the same meaning, including a case of M0S2 being used.), the Rate (3R) being 23% (Example 6-1), and Comparative example 6-2 where M0S2 was added.
{0074}
Further, it was observed that an abrasion depth in Examples 6-2, 6-3, and 6-4 was shallower than in Example 61 and Comparative examples 6-1 and 6-2, in other words, abrasion was reduced. Moreover, it was observed that an abrasion depth tended to be shallow when a graphene precursor was added regardless of a Rate (3R) of the graphene precursor. An abrasion depth in Comparative example 6-2 where MoS2 was added was deeper than in Example 6-1. This t
is because, it is speculated that, M0S2 having a Mohs hardness of 1 is softer than graphene-like graphite having hardness comparable to a diamond (Mohs hardness of 10) , or has less lubricity than graphene-like graphite.
{0075}
When the graphene precursors having the Rate (3R) of 31% or more (Examples 6-2, 6-3, and 6-4) are dispersed in the base oil, a friction coefficient is lowered and an abrasion depth becomes shallow. This is because, it is speculated that, more graphene-like graphite was exfoliâted from the graphene precursors or the graphene-like graphite by shearing force generated between the bail 63 and the disk 64, and at the same time, a surface of the disk was protected by the graphene-like graphite adsorbed on a sliding part, as a resuit, a friction coefficient was lowered and an abrasion depth became shallow.
When the Rate (3R) is less than 31% (Example 6-1), it is considered that an amount of graphene-like graphite that is exfoliated by the shearing force is too small so that an effect of adding the graphene precursor is not sufficiently exerted.
(0076}
In contrast, when the Rate (3R) is 35% or more (Examples
6-3 and 6-4), an excellent effect is obtained by having a lower friction coefficient and a shallower abrasion depth, as compared with cases of the Rate (3R) being equal to or lower than that. It is considered that this is because the number of pièces of graphene-like graphite was increased as compared with the case of the Rate (3R) being 31% {Example 6-2) .
{0077}
For reference, an explanation is given on photographed images of graphene precursors taken by a scanning électron microscope (SEM). The graphene precursors obtained in Example 1 are a laminate of flaky graphite having a length of 7 pm and a thickness of 0.1 pm as shown for example in Figs. 23 and 24 .
{Example 7} {0078}
Experiments were performed by adding the graphene precursors produced by the above methods to base oil.
{0079} <Various conditions>
Base oil (synthetic oil): Exxon Mobil 1 0W-20 (SAE viscosity grade of OW-20 manufactured by Exxon Mobil Corp.) (for automobile),
Except for base oil, experimental conditions and the like are the same as in Example 6.
Comparative example 7-2 | Comparative example 7-1 | Example 7-4 | Example 7-3 | Example 7-2 | Example 7-1 | ||
100 | kO kO | 99 | | 99 | | 99 | Base oil | Mixture ratio (wt%) | |
M | 1 | 1 | 3 o ω | ||||
1 | 1 | 1 | H* | 23% (Sample 1) | Graphene precursor Rate (3R) | ||
1 | 1 | 1 | H* | 31% (Sample 2) | |||
1 | 1 | H* | 1 | 1 | 35% (Sample 21) | ||
1 | 1 | k-* | 1 | 1 | 1 | en ûj ·* ΐ 3 M TJ dp I-» œ | |
0.065 | 0.083 | 0.013 1 | 0.015 | 0.023 | 0.062 | Friction coefficient (μ) | |
6.2 | 8.2 | 2.0 | 2.4 | 2.5 | 3.2 | α 1 O P |
(08001 en ω {0081}
From Table 6 and Figs. 25 and 26, it was observed that a friction coefficient in Examples 7-2, 7-3, and 7-4 was lower than in Example 7-1 and Comparative examples 7-1 and
7-2. In particular, when the Rate (3R) of the graphene precursors reached 31% or more, it was observed that a friction coefficient had a remarkable tendency of becoming significantly low, as compared with cases of the Rate (3R) being 0% (Comparative example 7-1), the Rate (3R) being 23% (Example 7-1), and Comparative example 7-2 where M0S2 was included.
{0082}
Further, similarly in the case of a friction coefficient, it was observed that an abrasion depth in Examples 7-2, 7-3, and 7-4 was shallower than in Example 71 and Comparative examples 7-1 and 7-2. Moreover, it was observed that an abrasion depth tended to be shallow when a graphene precursor was added regardless of the Rate (3R) of the graphene precursor. An abrasion depth in Comparative example 7-2 where M0S2 was included was deeper than in Example
7-1. This is because, it is speculated that, M0S2 having a Mohs hardness of 1 is softer than graphene-like graphite having hardness comparable to a diamond (Mohs hardness of 10), or has less lubricity than graphene-like graphite.
{0083}
B
It is considered that a friction coefficient and an abrasion depth are improved for the same reason as explained in Example 6.
{0084}
From Examples 6 and 7, it was observed that a friction coefficient was lowered and an abrasion depth became shallow regardless of the kind of base oil. When the graphene precursors having the Rate (3R) of 23% were used (Examples 6-1 and 7-1), it was observed that an abrasion depth became shallow and a friction coefficient was slightly lowered regardless of base oil as compared with the cases where graphene precursors were not added (Comparative examples 62 and 7-2), while when the graphene precursors having the Rate (3R) of 31% or more were used, it was observed that a friction coefficient was lowered and an abrasion depth became shallow in a striking manner (both were greatly improved).
{Example 8) {0085}
Experiments were performed by adding the graphene precursors produced by the above methods to base oil.
{0086} <Various conditions>
Base oil (minerai oil): Daphné Eponex Grease No.l (NLGI No. No.l manufacturée! by Idemitsu Kosan Co., Ltd.) (for industry), <Frictional condition 2: rotational speed: 100 rpm, radius: 10 mm, load: 5 N, oil température: 80°C, 10 min>
Except for base oil and frictional conditions, experimental conditions and the like are the same as in Example 6.
(0087)
Step 1. To 500 g of base oil, 5 g of graphene precursors (see Samples 1, 2, 21, and 4 (Samples used in Examples 1 and 5)) are added, and, under the mixing condition 1, the graphene precursors are exfoliated and dispersed to obtain grease 62 having a concentration of lwt%. (For convenience of explanation, a reference sign 62 in Fig. 20 refers to grease in Example 8.)
Step 2. 100 g of the grease 62 was put into a liquid holder 61 of a testing device 60 and a friction test was performed by rotating a disk 64 while being contacted with a bail 63 under the frictional condition 2.
Step 3. In a 30 min-long test, average values of a friction coefficient (μ) for the last 30 sec before the end of the test were read and plotted in Fig. 27.
Step 4. By using a surface roughness measuring device, five worn parts on a surface of the disk 64 caused by a contact with the bail 63 were measured, and an abrasion depth was obtained from average values of this measurement and plotted in Fig. 28.
Comparative example 8-2 | Comparative example 8-1 | Example 8-4 | Example 8-3 | Example 8-2 | Example 8-1 | | ||
99 | 100 | 99 | LO | 66 | 99 | Base oil | Mixture ratio (wt%) |
H» | 1 | 1 | 1 | 1 | 1 | K o to N | |
1 | 1 | 1 | 1 | h-· | w - § ΰ TJ <*> H» Φ | Graphene precursor Rate (3R) | |
1 | 1 | 1 | 1 | w | 31% (Sample 2) | ||
1 | 1 | M | 1 | 1 | 35% (Sample 21) | ||
1 | H* | 1 | 1 | 1 | to ± § M *0 dp »-· (D | ||
0.102 | 0.132 | 0.041 | 0.044 | 0.069 | 0.103 | Friction coefficient (μ) | |
5.2 | 7.9 | 2.2 | 2.4 | 3.1 | CD | Abrasion depth (gm) |
{Table 7} en
CD
I {0089}
As shown in Table 7 and Figs. 27 and 28, it was observed that a friction coefficient in Examples 8-2, 8-3, and 8-4 was lower than in Example 8-1 and Comparative examples 8-1 and 8-2. In particular, when the Rate (3R) of the graphene precursors reached 31% or more, it was observed that a friction coefficient had a remarkable tendency of becoming significantly low as compared with cases of the Rate (3R) being 0% (Comparative example 8-1), the Rate (3R) being 23% (Example 8-1), and Comparative example 8-2 where M0S2 was included.
{0090}
Further, similarly in the case of a friction coefficient, it was observed that an abrasion depth in Examples 8-2, 8-3, and
8-4 was shallower than in Example 8-1 and Comparative examples
8-1 and 8-2. Moreover, it was observed that an abrasion depth tended to be shallow when a graphene precursor was added regardless of a Rate (3R) of the graphene precursor. An abrasion depth in Comparative example 8-2 where M0S2 was included was deeper than in Example 8-1. This is because, it is speculated that, M0S2 having a Mohs hardness of 1 is softer than graphenelike graphite having hardness comparable to a diamond (Mohs hardness of 10), or has less lubricity than graphene-like graphite.
{0091}
It is considered that a reason for improvements such as a low friction coefficient and a shallow abrasion depth is the same as explained in Example 6.
{0092}
From Examples 6, 7, and 8, improvements such as a low friction coefficient and a shallow abrasion depth were observed regardless of the kind of base oil. When the graphene precursors having the Rate (3R) of 23% were used (Examples 6-1, 7-1, and 81) , it was observed that an abrasion depth became swallow and a friction coefficient was slightly lowered regardless of base oil as compared with the cases where graphene precursors were not added (Comparative examples 6-2, 7-2, and 8-2), while when the graphene precursors having the Rate (3R) of 31% or more were used, it was observed that a friction coefficient was lowered and an abrasion depth became swallow in a striking manner (both were greatly improved).
{Example 9} {0093}
Next, experiments were performed by adding the graphene precursors produced by the above methods to base oil. The experiments were performed with a mixture ratio of the graphene precursors having the Rate (3R) of 31% to base oil under conditions shown in Table 8. Other experimental conditions and the like are the same as in Example 6.
{0094} {Table 8}
Mixture ratio (wt%) | Friction coefficient (μ) | Abrasion depth (μπ>) | ||
Base oil | Graphene precursor | |||
Rate (3R) - 31% (Sample 2) | ||||
Exemple 6-1 | 99 | 1 | 0.0952 | 6.5 |
Example 9-1 | 98 | 2 | 0.0792 | 5.9113 |
Example 9-2 | 97 | 3 | 0.0652 | 5.2 |
Example 9-3 | 95 | 5 | 0.0434 | 4.2 |
Example 9-4 | 93 | 7 | 0.0352 | 3.7 |
Example 9-5 | 91 | 9 | 0.0321 | 3.6 |
Example 9-6 | 89 | 11 | 0.0325 | 3.^U |
Example 9-7 | 87 | 13 | 0.0357 | 3.7 |
Example 9-8 | 85 | 15 | 0.0389 | 3.5 |
Example 9-9 | 99.2 | 0.8 | 0.0998 | 7.3 |
Example 9-10 | 99.5 | 0.5 | 0.1082 | 8.2 |
Example 9-11 | 99.7 | 0.3 | 0.1127 | 9.^b |
Example 9-12 | 99.9 | 0.1 | 0.1201 | 10 |
Comparative example 6-1 | 100 | - | 0.1253 | 11 |
{0095}
From Table 8 and Figs. 29 and 30, when the mixture ratio of the graphene precursors to the base oil was in the vicinity of 1/10 (Example 9-5), it was observed that a friction and abrasion stayed at the same Further, coefficient an depth mostly values and their characteristics became saturated. when the mixture ratio of the graphene precursors is 1/10 or more, it was observed that a friction coefficient was conversely increased. On the other hand, when the mixture ratio was 1/200 (Example 9-10), it was observed that a friction coefficient was lowered by 10% or more and an abrasion depth became shallow by 20% or more, as compared with Comparative example 6-1 where a graphene precursor was not added. Moreover, it was observed that a friction coefficient was sharply lowered when the mixture ratio was 1/50 sharply became 9-10) or more.
Based on 1/10,000 or preferably 1/200 or more, than 1, preferably less than 1/10 than 1/50.
(Example 9-1) or more, shallow when the these, a lower more, preferably and while an abrasion depth mixture ratio was 1/200 (Example limit of the mixture ratio is 1/1,000 or more, an upper limit , and further and further thereof is less preferably less {0096}
Further, in Example 6-9, an additive may be added for a purpose of preventing oxidation of base oil. In this case, an additive shall be included in a mixture ratio (wt%) of base oil. Examples of such an additive include ZnDTP (zinc dithiophosphate), phénols, amines, sulfides, and radioactive substances. Particularly préférable are radioactive substances that émit négative ions having a suppressing effect of radical groups (activity) acting as an oxidation factor. Of these, Bad Gastein ores (place of origin: Austria) that contain radium 226 having a long half-life are préférable.
{0097}
This paragraph describes a mechanism of oxidation. Oxidation factors include oxygen, température, worn métal powders, moisture, blow-by gas, and the like, and when these factors are interacted with a hydrocarbon group contained in base oil, the hydrocarbon group (RH) is decomposed into R (activity) and H (hydrogen). Subsequently, the decomposed R is changed to form a peroxide, such as (ROO) and (ROOH), by binding to oxygen (O2) . This peroxide reacts with another hydrocarbon group contained in base oil to induce a chain reaction, thereby causing a rapid oxidation reaction.
{0098}
Moreover, in Example 6-9, the graphene precursors are produced by a radiowave force-based treatment and/or a physical force-based treatment as described above, thus it is not necessary to perform an oxidation/reduction treatment. Further since a réduction treatment is not necessary to produce a mixture with base oil, high température or drying to a powder is not required, as a resuit, kneading with base oil is readily performed.
{0099}
The foregoing explained the embodiments of the présent invention using drawings, however it should be understood that the spécifie constitutions are not at ail restricted to these embodiments, and changes and additions are also included in the présent invention without departing from the gist of the présent invention.
{0100}
Examples of a base material for dispersing a graphite-based carbon material include the following. It is noted that a mixture ratio of a base material may be smaller than that of a graphite-based carbon material.
{0101}
As base oil, minerai oils such as paraffin-based oils and naphthenic oil are included. Further included are synthetic oils based on esters, such as aolefin (PAO), polyol esters, diesters, and complex esters, synthetic hydrocarbons, ethers, phenyl ethers, silicones, and the like. Further included are oils derived from plants, such as castor oil, rapeseed oil, and wax. Oils derived from animais, such as oil of sperm whale and oil of beef tallow, are also included.
{0102}
As grease included are grease based on calcium soap, grease based on calcium complex, grease based on sodium soap, grease based on aluminum soap, grease based on lithium soap, non-soap based grease, silicone grease, fluoroether grease, and the like. {0103}
In addition, as an example of natural graphite for producing a graphite-based carbon material useful as a graphene precursor, particles of 5 mm or less of a natural graphite material (flaky graphite ACB-50 manufactured by Nippon Graphite Industries, ltd.) is described above. However, as for the natural graphite, products which are flaky graphite, being pulverized into 5 mm or less, and which hâve a Rate (3R) of less than 25% and an intensity ratio P1/P2 of less than 0.01 are préférable, from a viewpoint that they are easily-available. Corresponding to recent technology development, natural graphite-like graphite {in which crystals are stacked in layers) can be artificially synthesized, thus raw materials for graphene and graphene-like graphite are not limited to natural graphite (minerai) . Artificial graphite having a high degree of purity is preferably used for a purpose of controlling a métal content. Further as long as a Rate (3R) is 31% or more, artificial graphite, which is not produced by a radiowave force-based treatment or a physical force-based treatment described above, may be used.
It should be noted that a graphite-based carbon material useful as a graphene precursor is generally referred to as graphene, a graphene precursor, a graphene nanoplatelet (GNP), few-layer graphene (FLG) , nanographene, and the like, however it is not particularly limited thereto.
Industrial Applicability {0104}
The présent invention covers a composite lubricating material having lubricity, and an application field thereof is not limited. For example, the following fields are included in the présent invention.
(1) Engine oil
For internai combustion engines of automobiles, etc.
(2) Sliding surface oil
For sliding surfaces of machine tools.
(3) Turbine oil
For turbines of thermal power génération, water power génération, nuclear power génération, ships, air planes, etc.
(4) Hydraulic oil
For hydraulic Systems that operate oil pressure of heavy machines, etc.
(5) Bearing oil
For bearings, rolling bearings, etc.
(6) Lubricant for mist oil supply
For cooling during annealing, release agents, etc.
(7) Gear oil
For bevel gears, worm gears, etc.
(8) Compressor oil
For air compressors, etc.
t (9) Base oil for refrigerator oil
For chillers, air conditioners, etc.
(10) Vacuum pump oil
For oil rotation type vacuum pumps, oil mist pumps, etc.
(11)
Transmission oil
For transmissions such as CVT
Claims (8)
1- A composite lubricating material comprising at least a graphite-based carbon material and/or graphene-like exfoliated from the graphite-based carbon material dispersed in a base material, the graphite-based carbon material having a rhombohedral graphite layer (3R) and a hexagonal graphite layer (2H), wherein a Rate (3R) of the rhombohedral graphite layer (3R) and the hexagonal graphite layer (2H), based on an X-ray diffraction method, which is defined by following Equation 1 is 31% or more:
Rate (3R) = P3/(P3+P4)*100 ···· Equation 1 wherein
P3 is a peak intensity of a (101) plane of the rhombohedral graphite layer (3R) based on the X-ray diffraction method, and
P4 is a peak intensity of a (101) plane of the hexagonal graphite layer (2H) based on the X-ray diffraction method.
2- The composite lubricating material according to claim 1, wherein a weight ratio of the graphite-based carbon material to the base material is 1/10,000 or more to less than 1.
3- The composite lubricating material according to claim 1, wherein the base material is at least one or more of base oil derived from minerai, synthesis, plants or animais.
4- The composite lubricating material according to claim 1, comprising one or more kinds of additives for a purpose of preventing oxidative détérioration.
5- The composite lubricating material according to claim 4, wherein the additive is a radioactive substance.
6- Engine oil for use in an internai combustion engine or the like, comprising the composite lubricating material according to claim 1.
7- Grease for use in a rolling bearing, a sliding part, or the like, comprising the composite lubricating material according to claim 1.
8- Lubricant for use in a fluid bearing, a gear, or the like, comprising the composite lubricating material according to claim 1.
Publications (1)
Publication Number | Publication Date |
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OA18250A true OA18250A (en) | 2018-09-17 |
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