CN116639990B - Manufacturing process of composite layer graphite sagger - Google Patents

Manufacturing process of composite layer graphite sagger Download PDF

Info

Publication number
CN116639990B
CN116639990B CN202310932322.9A CN202310932322A CN116639990B CN 116639990 B CN116639990 B CN 116639990B CN 202310932322 A CN202310932322 A CN 202310932322A CN 116639990 B CN116639990 B CN 116639990B
Authority
CN
China
Prior art keywords
sagger
composite layer
mixing
layer graphite
phenolic resin
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202310932322.9A
Other languages
Chinese (zh)
Other versions
CN116639990A (en
Inventor
何江
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Changsha Zhongci New Material Technology Co ltd
Original Assignee
Changsha Zhongci New Material Technology Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Changsha Zhongci New Material Technology Co ltd filed Critical Changsha Zhongci New Material Technology Co ltd
Priority to CN202310932322.9A priority Critical patent/CN116639990B/en
Publication of CN116639990A publication Critical patent/CN116639990A/en
Application granted granted Critical
Publication of CN116639990B publication Critical patent/CN116639990B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/66Monolithic refractories or refractory mortars, including those whether or not containing clay
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/01Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
    • C04B35/16Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on silicates other than clay
    • C04B35/18Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on silicates other than clay rich in aluminium oxide
    • C04B35/195Alkaline earth aluminosilicates, e.g. cordierite or anorthite
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/009After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/45Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
    • C04B41/50Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/80After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
    • C04B41/81Coating or impregnation
    • C04B41/85Coating or impregnation with inorganic materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27DDETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D5/00Supports, screens, or the like for the charge within the furnace
    • F27D5/0068Containers
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/34Non-metal oxides, non-metal mixed oxides, or salts thereof that form the non-metal oxides upon heating, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
    • C04B2235/3409Boron oxide, borates, boric acids, or oxide forming salts thereof, e.g. borax
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/34Non-metal oxides, non-metal mixed oxides, or salts thereof that form the non-metal oxides upon heating, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
    • C04B2235/3427Silicates other than clay, e.g. water glass
    • C04B2235/3463Alumino-silicates other than clay, e.g. mullite
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/40Metallic constituents or additives not added as binding phase
    • C04B2235/402Aluminium
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/42Non metallic elements added as constituents or additives, e.g. sulfur, phosphor, selenium or tellurium
    • C04B2235/422Carbon
    • C04B2235/425Graphite
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/48Organic compounds becoming part of a ceramic after heat treatment, e.g. carbonising phenol resins
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/60Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
    • C04B2235/602Making the green bodies or pre-forms by moulding
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/656Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/656Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
    • C04B2235/6567Treatment time
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
  • Structural Engineering (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Inorganic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Battery Electrode And Active Subsutance (AREA)

Abstract

The invention discloses a process for manufacturing a composite layer graphite sagger, which belongs to the technical field of sagger production and comprises the following steps: grinding cordierite, mullite, aluminum powder, spinel and graphite powder, uniformly mixing, adding an adhesive, mixing to obtain a mixture, adding water, continuously stirring, stamping, forming, and sintering at 1350-1390 ℃ for 18-24 hours to obtain a blank; secondly, placing the green body in a vacuum drying oven for dipping treatment: vacuumizing, injecting impregnating solution, and carrying out pressure maintaining soaking and normal pressure soaking; taking out and drying at room temperature, and then putting into an oven, and drying at 110 ℃; and repeating the dipping treatment process for 2-3 times to obtain the composite layer graphite sagger. And a protective layer is formed on the surface of the green body through dipping treatment, so that the erosion resistance of the sagger is further improved in the subsequent processing and use process of the positive electrode material.

Description

Manufacturing process of composite layer graphite sagger
Technical Field
The invention belongs to the technical field of sagger production, and particularly relates to a composite layer graphite sagger manufacturing process.
Background
The production process of the lithium battery anode material mainly comprises the steps of filling raw materials such as blended powder into a sagger, sintering the sagger at high temperature through a roller kiln, discharging the sagger containing the raw materials out of the furnace, crushing the anode material, and finally packaging the product. Wherein, the sagger discharged from the furnace is continuously filled with blended powder, and then enters a roller kiln for sintering, so that the sagger is reciprocated.
As the sagger is a carrier for the reaction of the lithium battery anode material, the sagger can be subjected to phenomena of corner falling, peeling, cracking, deformation and the like after being sintered at high temperature for tens of periods. Li with extremely strong permeability can be generated in the sintering process of the positive electrode material of the lithium battery 2 O, limited by kiln exhaust, li 2 O cannot be completely discharged during the reaction. As the sintering process of the material proceeds, the sintering temperature gradually increases, and Li is accelerated 2 O diffuses to make it enter the bottom of the sagger along the air hole to react with the material to generate Li 4 SiO 4 、β-LiAlSiO 4 And LiAlO 2 Causing erosion of the sagger. With the cyclic sintering of the sagger, the sagger is continuously eroded, so that the porosity of the sagger is increased, and Li is increased 2 The O diffusion path can pass through the bottom of the sagger to reach the contact surface with the roller rod, so that the sagger, the roller rod and Li are caused 2 The crystallization generated by the O reaction is attached to the surface of the roller and the bottom of the sagger, so that the sagger is scrapped.
Disclosure of Invention
The invention aims to provide a manufacturing process of a composite layer graphite sagger, which aims to solve the problem of poor corrosion resistance in the use process of the sagger.
The aim of the invention can be achieved by the following technical scheme:
the manufacturing process of the composite layer graphite sagger comprises the following steps:
grinding cordierite, mullite, aluminum powder, spinel and graphite powder, uniformly mixing, adding an adhesive, mixing to obtain a mixture, adding water, continuously stirring, stamping, forming, and sintering at 1350-1390 ℃ for 18-24 hours to obtain a blank;
secondly, placing the green body in a vacuum drying oven for dipping treatment: vacuumizing, injecting impregnating solution, and carrying out pressure maintaining soaking and normal pressure soaking; taking out and drying at room temperature, and then putting into an oven, and drying at 110 ℃; and repeating the dipping treatment process for 2-3 times to obtain the composite layer graphite sagger.
Further, 30-32% of cordierite, 15-16% of mullite, 15-16% of aluminum powder, 20-22% of spinel, 2-2.5% of graphite powder and the balance of adhesive in the mixture according to weight percentage.
Further, the water in the first step is added in an amount of 21-23% of the mass of the mixture.
Further, the pressure maintaining soaking time is 5-10min, and the normal pressure soaking time is 25-30min.
Further, in the second step, drying at room temperature until the weight is unchanged; and drying at 110 ℃ to constant weight.
Further, the adhesive is POSS modified phenolic resin and boric oxide according to the mass ratio of 7:3, mixing, ball milling and sieving with a 200-mesh sieve.
Further, the POSS modified phenolic resin is prepared by the following steps:
and (3) mixing and diluting the aqueous phenolic resin and deionized water in equal volume, adding the octaepoxycyclohexylethyl-cage-shaped POSS, and mixing to obtain the POSS modified phenolic resin. The dosage ratio of the aqueous phenolic resin to the octaepoxycyclohexylethyl-cage POSS is 20:1.
further, the impregnating solution is prepared by the following steps:
mixing aluminum sol and a silane coupling agent, stirring and reacting for 3 hours at the temperature of 60 ℃ to obtain pretreated aluminum sol, adding saturated boric acid solution into the pretreated aluminum sol, stirring and mixing, and concentrating under reduced pressure at the temperature of 35 ℃ until the volume is unchanged to obtain impregnating solution.
Further, the silane coupling agent is one of propyl trimethoxy silane and butyl trimethoxy silane.
Further, the dosage mass ratio of the aluminum sol to the silane coupling agent to the saturated boric acid is 1:0.02:0.1.
the invention has the beneficial effects that:
the invention provides a process for manufacturing a composite layer graphite sagger, which forms a protective layer on the surface of a green body through dipping treatment, and further improves the erosion resistance of the sagger in the subsequent processing and using process of a positive electrode material.
Impregnating solution permeates into the blank body in the impregnation process, forming a layer of protective film on the surface of the blank body after repeated impregnation treatment to obtain a sagger, and forming the protective film on the surface of the sagger and Li in the use process of the sagger 2 O will react and consume Li 2 O, thereby improving the permeation resistance of the sagger. Boric acid in the impregnation solution generates boron oxide at high temperature, which dissolves many basic metal oxides (e.g. Li 2 O) for Li that has permeated into the sagger 2 O can react with the impregnating solution penetrating into the sagger and is accompanied by volumeThe expansion, the reaction product blocks the pores, and the apparent porosity after molding is further reduced.
The adhesive is obtained by mixing POSS modified phenolic resin and boron oxide, the adhesive, cordierite, mullite, aluminum powder, spinel and graphite powder are used as mixture to prepare a blank, the POSS modified phenolic resin and the graphite powder are used as carbon sources to react with the boron oxide by a carbothermic reduction method, and high-temperature resistant substances such as boron carbide are generated to exist in a reaction matrix, so that gas holes can be blocked, pore channels are narrowed, and Li is reduced 2 O penetrates into the material, thereby improving the erosion resistance of the material. Compared with the water-based phenolic resin, the POSS modified phenolic resin in the adhesive can increase the number of hydrophilic groups, improve the dispersion effect, and meanwhile, epoxy groups can be copolymerized with hydroxymethyl groups in the phenolic resin, so that the crosslinking degree is properly improved, cracking caused by brittleness of the cured phenolic resin is improved, and the stability of a product is improved.
Detailed Description
The technical solutions of the embodiments of the present invention will be clearly and completely described below in conjunction with the embodiments of the present invention, and it is apparent that the described embodiments are only some embodiments of the present invention, not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
Example 1
The embodiment provides a POSS modified phenolic resin, which is prepared through the following steps:
mixing 10g of phenol, 1.2g of sodium hydroxide and 10mL of deionized water, adding 15g of formaldehyde at 60 ℃, stirring and reacting for 2 hours, heating to 80 ℃ after the reaction is finished, continuously stirring for 30 minutes, adding 5g of formaldehyde, keeping the temperature unchanged, continuously stirring and reacting for 30 minutes, adding 10mL of deionized water and 2, 4-xylenol, and continuously stirring for 30 minutes to obtain the water-based phenolic resin; and (3) mixing and diluting the aqueous phenolic resin and deionized water in equal volume, adding the octaepoxycyclohexylethyl-cage-shaped POSS, and mixing to obtain the POSS modified phenolic resin. The dosage ratio of the aqueous phenolic resin to the octaepoxycyclohexylethyl-cage POSS is 20:1.
example 2
The embodiment provides an impregnating solution prepared by the following steps:
mixing aluminum sol (commercial product with solid content of 20.67%) and propyl trimethoxy silane, stirring at 60deg.C for 3 hr to obtain pretreated aluminum sol, adding saturated boric acid solution into the pretreated aluminum sol, stirring, mixing, and concentrating under reduced pressure at 35deg.C until volume is unchanged to obtain soaking solution. The dosage mass ratio of the aluminum sol to the propyl trimethoxy silane to the saturated boric acid is 1:0.02:0.1.
example 3
The embodiment provides an impregnating solution prepared by the following steps:
mixing aluminum sol (commercial product with solid content of 20.67%) and butyl trimethoxy silane, stirring at 60 ℃ for 3 hours to obtain pretreated aluminum sol, adding saturated boric acid solution into the pretreated aluminum sol, stirring and mixing, and concentrating under reduced pressure at 35 ℃ until the volume is unchanged to obtain the impregnating solution. The dosage mass ratio of the aluminum sol to the butyl trimethoxy silane to the saturated boric acid is 1:0.02:0.1.
example 4
The manufacturing process of the composite layer graphite sagger comprises the following steps:
firstly, POSS modified phenolic resin prepared in example 1 and boron oxide are mixed according to a mass ratio of 7:3 mixing, ball milling, sieving with a 200-mesh sieve to obtain an adhesive, grinding 30% of cordierite, 15% of mullite, 15% of aluminum powder, 20% of spinel and 2% of graphite powder according to weight percentage, uniformly mixing, adding 18% of adhesive, mixing to obtain a mixture, adding water, continuously stirring, stamping and forming, and sintering at 1350-1390 ℃ for 18h to obtain a green body, wherein the addition amount of water is 21% of the mass of the mixture;
secondly, placing the green body in a vacuum drying oven for dipping treatment: vacuumizing, injecting the impregnating solution in the embodiment 3, and carrying out pressure maintaining soaking for 5min and normal pressure soaking for 30min; taking out, drying at room temperature until the weight is unchanged, then putting into an oven, and drying at 110 ℃ until the weight is constant; the dipping treatment process is repeated for 2 times to obtain the composite layer graphite sagger.
Comparative example 1
In this comparative example, the binder was replaced with the aqueous phenolic resin of example 1, as compared with example 4. The remaining raw materials and preparation process remain the same as in example 3. The apparent porosity was measured according to GB/T2997-2015 and the test results are shown in Table 1 below:
from the test results, the sagger porosity prepared by the POSS modified phenolic resin prepared by the invention is lower.
Example 5
The manufacturing process of the composite layer graphite sagger comprises the following steps:
firstly, POSS modified phenolic resin prepared in example 1 and boron oxide are mixed according to a mass ratio of 7:3 mixing, ball milling, sieving with a 200-mesh sieve to obtain an adhesive, grinding 31% of cordierite, 15% of mullite, 15% of aluminum powder, 21% of spinel and 2% of graphite powder according to weight percentage, uniformly mixing, adding 16% of adhesive, mixing to obtain a mixture, adding water, continuously stirring, stamping and forming, and sintering at 1350-1390 ℃ for 22 hours to obtain a green body, wherein the addition amount of water is 22% of the mass of the mixture;
secondly, placing the green body in a vacuum drying oven for dipping treatment: vacuumizing, injecting the impregnating solution prepared in the example 2, and carrying out pressure maintaining soaking for 10min and normal pressure soaking for 30min; taking out, drying at room temperature until the weight is unchanged, then putting into an oven, and drying at 110 ℃ until the weight is constant; the dipping treatment process is repeated for 3 times to obtain the composite layer graphite sagger.
Example 6
The manufacturing process of the composite layer graphite sagger comprises the following steps:
firstly, POSS modified phenolic resin prepared in example 1 and boron oxide are mixed according to a mass ratio of 7:3 mixing, ball milling, sieving with a 200-mesh sieve to obtain an adhesive, grinding 32% of cordierite, 16% of mullite, 16% of aluminum powder, 20% of spinel and 2% of graphite powder according to weight percentage, uniformly mixing, adding 14% of adhesive, mixing to obtain a mixture, adding water, continuously stirring, stamping and forming, and sintering at 1350-1390 ℃ for 24 hours to obtain a green body, wherein the addition amount of water is 23% of the mass of the mixture;
secondly, placing the green body in a vacuum drying oven for dipping treatment: vacuumizing, injecting the impregnating solution prepared in the example 3, and carrying out pressure maintaining soaking for 10min and normal pressure soaking for 25min; taking out, drying at room temperature until the weight is unchanged, then putting into an oven, and drying at 110 ℃ until the weight is constant; the dipping treatment process is repeated for 3 times to obtain the composite layer graphite sagger.
Comparative example 2
In this comparative example, compared with example 6, the impregnation liquid was changed to an alumina sol (commercially available, solid content of 20.67%), and the remaining raw materials and the preparation process were the same as in example 6.
Comparative example 3
In this comparative example, compared with comparative example 1, the impregnation liquid was changed to an alumina sol (commercially available, solid content of 20.67%), and the remaining raw materials and the preparation process were kept the same as in comparative example 1.
Examples 5 to 6 and comparative examples 2 to 3 were tested and the apparent porosity was measured according to GB/T2997-2015. When lithium cobalt oxide, a positive electrode material of a lithium battery, was synthesized at 1050 ℃, the number of cycles of a plurality of sets of saggers (the end of the cycle with the occurrence of flaking of the saggers) was recorded, and the results are shown in table 2:
as can be seen from Table 2, the sagger prepared by the invention has good recycling effect and better corrosion resistance.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. The manufacturing process of the composite layer graphite sagger for the lithium battery anode material is characterized by comprising the following steps of:
grinding cordierite, mullite, aluminum powder, spinel and graphite powder, uniformly mixing, adding an adhesive, mixing to obtain a mixture, adding water, continuously stirring, stamping, forming, and sintering at 1350-1390 ℃ for 18-24 hours to obtain a blank; 30-32% of cordierite, 15-16% of mullite, 15-16% of aluminum powder, 20-22% of spinel, 2-2.5% of graphite powder and the balance of adhesive in the mixture according to weight percentage; the adhesive is POSS modified phenolic resin and boric oxide according to the mass ratio of 7:3, mixing, ball milling and sieving with a 200-mesh sieve to obtain the product;
secondly, mixing aluminum sol and a silane coupling agent, stirring and reacting for 3 hours at the temperature of 60 ℃ to obtain pretreated aluminum sol, adding saturated boric acid solution into the pretreated aluminum sol, stirring and mixing, and concentrating under reduced pressure at the temperature of 35 ℃ until the volume is unchanged to obtain impregnating solution; the dosage mass ratio of the aluminum sol to the silane coupling agent to the saturated boric acid is 1:0.02:0.1;
placing the green body in a vacuum drying oven for dipping treatment: vacuumizing, injecting impregnating solution, and carrying out pressure maintaining soaking and normal pressure soaking; taking out and drying at room temperature, and then putting into a baking oven for baking; and repeating the dipping treatment process for 2-3 times to obtain the composite layer graphite sagger for the lithium battery anode material.
2. The process for manufacturing the composite layer graphite sagger for the positive electrode material of the lithium battery, which is disclosed in claim 1, is characterized in that the water addition amount in the first step is 21-23% of the mass of the mixture.
3. The process for manufacturing the composite layer graphite sagger for the positive electrode material of the lithium battery, which is disclosed in claim 1, is characterized in that the pressure maintaining soaking time is 5-10min and the normal pressure soaking time is 25-30min.
4. The process for manufacturing a composite layer graphite sagger for a positive electrode material of a lithium battery according to claim 1, wherein in the second step, the composite layer graphite sagger is dried at room temperature until the weight is unchanged; the temperature is set in the oven and is 110 ℃ to be dried to constant weight.
5. The process for manufacturing a composite layer graphite sagger for a lithium battery anode material according to claim 1, wherein the POSS modified phenolic resin is prepared by the following steps:
mixing and diluting the water-based phenolic resin and deionized water in equal volume, adding octaepoxycyclohexylethyl-cage-shaped POSS, and mixing to obtain POSS modified phenolic resin; the dosage ratio of the aqueous phenolic resin to the octaepoxycyclohexylethyl-cage POSS is 20:1.
6. the process for manufacturing a composite layer graphite sagger for a lithium battery anode material according to claim 1, wherein the silane coupling agent is one of propyl trimethoxysilane and butyl trimethoxysilane.
CN202310932322.9A 2023-07-27 2023-07-27 Manufacturing process of composite layer graphite sagger Active CN116639990B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202310932322.9A CN116639990B (en) 2023-07-27 2023-07-27 Manufacturing process of composite layer graphite sagger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202310932322.9A CN116639990B (en) 2023-07-27 2023-07-27 Manufacturing process of composite layer graphite sagger

Publications (2)

Publication Number Publication Date
CN116639990A CN116639990A (en) 2023-08-25
CN116639990B true CN116639990B (en) 2023-12-12

Family

ID=87643862

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202310932322.9A Active CN116639990B (en) 2023-07-27 2023-07-27 Manufacturing process of composite layer graphite sagger

Country Status (1)

Country Link
CN (1) CN116639990B (en)

Citations (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05201781A (en) * 1991-10-30 1993-08-10 Hitachi Chem Co Ltd Production of carbon material converted into boron carbide and produced carbon material converted into boron carbide
US5330838A (en) * 1988-07-29 1994-07-19 Air Products And Chemicals, Inc. Coated carbonaceous articles and method for making same
JPH1087373A (en) * 1996-09-11 1998-04-07 Shikoku Chem Corp Fireproof heat insulating material
CN1370136A (en) * 1999-06-07 2002-09-18 联合矿物产品公司 Lightweight dry refractory
JP2003221283A (en) * 2002-01-31 2003-08-05 Kawasaki Refract Co Ltd Oxidation-resistant carbon raw material and monolithic refractory using the same
CN104693392A (en) * 2015-03-09 2015-06-10 中国科学院化学研究所 Catechol boric acid ester etherified thermoplastic phenolic resin, and preparation method and application thereof
CN105924177A (en) * 2016-04-25 2016-09-07 北京理工大学 Hot pressing-reaction sintering method for preparing boron carbide-based multiphase ceramic
CN106946553A (en) * 2017-04-01 2017-07-14 武汉理工大学 A kind of ceramic saggar of low-cost long-life and preparation method thereof
CN108546093A (en) * 2018-04-08 2018-09-18 凤阳爱尔思轻合金精密成型有限公司 Short fine magnesium oxide-based crucible of enhancing of a kind of aluminium oxide and preparation method thereof
CN108892760A (en) * 2018-06-29 2018-11-27 西安交通大学 A kind of epoxy cage type sesquialter siloxane phenol-formaldehyde resin modified and preparation method thereof
CN113698219A (en) * 2021-07-30 2021-11-26 中国航空工业集团公司济南特种结构研究所 Silicon nitride fiber reinforced ceramic matrix composite and preparation method thereof
CN113773067A (en) * 2021-11-11 2021-12-10 长沙中瓷新材料科技有限公司 Sagger based on cordierite and production process thereof
CN114195533A (en) * 2021-12-14 2022-03-18 广州粤瓷新材料有限公司 Sagger for lithium ion battery anode material and preparation method thereof
KR20220043055A (en) * 2020-09-28 2022-04-05 엘지전자 주식회사 Casing for sintering cathode active material used in lithium secondary battery and method for manufacturing the same
CN114538903A (en) * 2022-04-25 2022-05-27 湖南立达高新材料有限公司 High-strength chrome corundum ramming mass and preparation method thereof
WO2022127314A1 (en) * 2020-12-15 2022-06-23 广东邦普循环科技有限公司 Saggar for sintering lithium transition metal oxide, and preparation method therefor
JP7283026B1 (en) * 2022-02-24 2023-05-30 日本イットリウム株式会社 Materials for sintered bodies and sintered bodies

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005314215A (en) * 2004-03-29 2005-11-10 Ngk Insulators Ltd Dense cordierite sintered body and method of manufacturing the same

Patent Citations (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5330838A (en) * 1988-07-29 1994-07-19 Air Products And Chemicals, Inc. Coated carbonaceous articles and method for making same
JPH05201781A (en) * 1991-10-30 1993-08-10 Hitachi Chem Co Ltd Production of carbon material converted into boron carbide and produced carbon material converted into boron carbide
JPH1087373A (en) * 1996-09-11 1998-04-07 Shikoku Chem Corp Fireproof heat insulating material
CN1370136A (en) * 1999-06-07 2002-09-18 联合矿物产品公司 Lightweight dry refractory
JP2003221283A (en) * 2002-01-31 2003-08-05 Kawasaki Refract Co Ltd Oxidation-resistant carbon raw material and monolithic refractory using the same
CN104693392A (en) * 2015-03-09 2015-06-10 中国科学院化学研究所 Catechol boric acid ester etherified thermoplastic phenolic resin, and preparation method and application thereof
CN105924177A (en) * 2016-04-25 2016-09-07 北京理工大学 Hot pressing-reaction sintering method for preparing boron carbide-based multiphase ceramic
CN106946553A (en) * 2017-04-01 2017-07-14 武汉理工大学 A kind of ceramic saggar of low-cost long-life and preparation method thereof
CN108546093A (en) * 2018-04-08 2018-09-18 凤阳爱尔思轻合金精密成型有限公司 Short fine magnesium oxide-based crucible of enhancing of a kind of aluminium oxide and preparation method thereof
CN108892760A (en) * 2018-06-29 2018-11-27 西安交通大学 A kind of epoxy cage type sesquialter siloxane phenol-formaldehyde resin modified and preparation method thereof
KR20220043055A (en) * 2020-09-28 2022-04-05 엘지전자 주식회사 Casing for sintering cathode active material used in lithium secondary battery and method for manufacturing the same
WO2022127314A1 (en) * 2020-12-15 2022-06-23 广东邦普循环科技有限公司 Saggar for sintering lithium transition metal oxide, and preparation method therefor
CN113698219A (en) * 2021-07-30 2021-11-26 中国航空工业集团公司济南特种结构研究所 Silicon nitride fiber reinforced ceramic matrix composite and preparation method thereof
CN113773067A (en) * 2021-11-11 2021-12-10 长沙中瓷新材料科技有限公司 Sagger based on cordierite and production process thereof
CN114195533A (en) * 2021-12-14 2022-03-18 广州粤瓷新材料有限公司 Sagger for lithium ion battery anode material and preparation method thereof
JP7283026B1 (en) * 2022-02-24 2023-05-30 日本イットリウム株式会社 Materials for sintered bodies and sintered bodies
CN114538903A (en) * 2022-04-25 2022-05-27 湖南立达高新材料有限公司 High-strength chrome corundum ramming mass and preparation method thereof

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
锂电池正极材料合成用堇青石-莫来石质匣钵研究进展;段雪珂;王新福;刘国齐;王龙光;陈红伟;钱凡;;耐火材料(第02期);全文 *
除氧处理对碳化硼陶瓷性能的影响;刘维良;谭金刚;谈军;张海滨;葛昌纯;;陶瓷学报(第03期);全文 *

Also Published As

Publication number Publication date
CN116639990A (en) 2023-08-25

Similar Documents

Publication Publication Date Title
KR102652593B1 (en) Resistant saggar for firing cathode active material for lithium secondary batteries and manufacturing method thereof
CN108585905A (en) A kind of high-strength carborundum ceramics and preparation method thereof
CN107602127B (en) SiC hollow sphere and preparation method thereof
CN111233478A (en) Layered slurry preparation method of titanium carbide gradient porous ceramic
CN108484173A (en) SiCf/ SiC ceramic matrix composite material and preparation method thereof
CN115466123A (en) Preparation method of silicon carbide ceramic wafer boat
CN110937892A (en) High-temperature absorbent, ultrathin high-temperature wave-absorbing material and preparation method thereof
CN116639990B (en) Manufacturing process of composite layer graphite sagger
CN107814590A (en) A kind of preparation method of fusedsalt reactor graphite surface SiC coatings
CN112751140B (en) Diaphragm functional coating material for improving liquid retention capacity and safety performance of lithium ion battery electrolyte
CN114736400B (en) Ceramizable phenolic aerogel and preparation method thereof
CN104072190A (en) Preparation method of SiC porous ceramic
CN115849928A (en) Injection-condensation-molded alumina fiber reinforced composite material containing lanthanum phosphate interface layer and preparation method thereof
CN114105671B (en) Coal gangue-quartz-based ceramic support and preparation method thereof
CN112851394B (en) Preparation method of porous silicon carbide ceramic
CN112898022B (en) Ultralow temperature sintered microwave dielectric material Ca2V2O7-H3BO3And method for preparing the same
CN114907133A (en) Silicon-based ceramic core material, preparation method and silicon-based ceramic core
CN111848154B (en) Ceramic capacitor medium and preparation method thereof
CN109133976B (en) Preparation method of porous alumina
CN113149680A (en) Carbon fiber reinforced silicon-boron-carbon-nitrogen-based ceramic composite material and preparation method thereof
CN109721381A (en) The preparation method of silicon nitride shell reinforcing silicon nitride foam ceramic
CN114195547B (en) High-strength porous silicon carbide ceramic material and preparation method thereof
CN115340413B (en) Porous ceramic plate, porous composite ceramic plate and preparation method thereof
CN115974536B (en) Alumina fiber reinforced ceramic matrix composite containing lanthanum phosphate interface layer and preparation method thereof
CN116003158B (en) Method for preparing mullite porous ceramic by utilizing lithium slag, mullite porous ceramic and application

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant