CN106007804B - A kind of high temperature resistant high impedance surface radar absorbing and preparation method thereof - Google Patents

A kind of high temperature resistant high impedance surface radar absorbing and preparation method thereof Download PDF

Info

Publication number
CN106007804B
CN106007804B CN201610330896.9A CN201610330896A CN106007804B CN 106007804 B CN106007804 B CN 106007804B CN 201610330896 A CN201610330896 A CN 201610330896A CN 106007804 B CN106007804 B CN 106007804B
Authority
CN
China
Prior art keywords
high temperature
temperature resistant
impedance surface
high impedance
preparation
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
CN201610330896.9A
Other languages
Chinese (zh)
Other versions
CN106007804A (en
Inventor
刘海韬
郝璐
�田�浩
杨晓树
戴全辉
程海峰
黄文质
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.)
National University of Defense Technology
Beijing Research Institute of Mechanical and Electrical Technology
Original Assignee
National University of Defense Technology
Beijing Research Institute of Mechanical and Electrical Technology
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 National University of Defense Technology, Beijing Research Institute of Mechanical and Electrical Technology filed Critical National University of Defense Technology
Priority to CN201610330896.9A priority Critical patent/CN106007804B/en
Publication of CN106007804A publication Critical patent/CN106007804A/en
Application granted granted Critical
Publication of CN106007804B publication Critical patent/CN106007804B/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
    • 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
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03CCHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
    • C03C8/00Enamels; Glazes; Fusion seal compositions being frit compositions having non-frit additions
    • C03C8/02Frit compositions, i.e. in a powdered or comminuted form
    • C03C8/10Frit compositions, i.e. in a powdered or comminuted form containing lead
    • 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
    • C04B41/5072Coating 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 with oxides or hydroxides not covered by C04B41/5025
    • 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
    • C04B41/86Glazes; Cold glazes
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K3/00Materials not provided for elsewhere
    • 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
    • C04B2111/00Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
    • C04B2111/00241Physical properties of the materials not provided for elsewhere in C04B2111/00
    • C04B2111/00258Electromagnetic wave absorbing or shielding 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
    • 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
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5208Fibers
    • C04B2235/5216Inorganic
    • C04B2235/522Oxidic
    • C04B2235/5232Silica or silicates other than aluminosilicates, e.g. quartz

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Structural Engineering (AREA)
  • Inorganic Chemistry (AREA)
  • Geochemistry & Mineralogy (AREA)
  • General Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Glass Compositions (AREA)
  • Compositions Of Oxide Ceramics (AREA)

Abstract

The invention discloses a kind of high temperature resistant high impedance surface radar absorbings, are double-layer structure, include the medium substrate layer in bottom and the high impedance surface layer in surface layer, the medium substrate layer, which is oxide fibre, enhances oxide-base composite material;The high impedance surface layer in the high temperature resistant resistance coating of periodic patterns mainly by forming.The present invention preparation method include:It first chooses and preparation media substrate, then the coating of high temperature resistant resistance coating is printed on by medium substrate surface using silk-screen printing technique, to get to the high temperature resistant high impedance surface radar absorbing after drying and sintering.The high temperature resistant high impedance surface radar absorbing of the present invention can be resistant at least 1000 DEG C of high temperature, have preferable heat-resisting quantity and excellent inoxidizability.

Description

A kind of high temperature resistant high impedance surface radar absorbing and preparation method thereof
Technical field
The present invention relates to radar absorbing field more particularly to a kind of high temperature resistant high impedance surface radar absorbing and Preparation method.
Background technology
Radar absorbing can be divided into room temperature (temperature in use is less than 200 DEG C) and high temperature two according to service temperature range Major class.In comparison, the research comparative maturity of current ambient temperature radar absorbing, and also to the research of high temperature radar absorbing In trying to explore.
It has disclosed at present and reports several high temperature microwave-absorbing ceramic structures and preparation method thereof.No. ZL201110052115.1 Chinese patent discloses a kind of composite material of silicon carbide microwave-absorbing ceramic of three-decker and preparation method thereof, the suction wave pottery of this report Porcelain is made of matching layer, depletion layer and reflecting layer, need to have different dielectric properties according to each functional layer of design requirement, preparation Reflectivity of the microwave-absorbing ceramic in 8GHz~18GHz frequency ranges is smaller than -9dB.ZL201110053460.7 Chinese patents disclose A kind of composite material of silicon carbide microwave-absorbing ceramic of four-layer structure and preparation method thereof, the microwave-absorbing ceramic of this report by matching layer, Depletion layer, dielectric layer and reflecting layer composition, need to have different dielectric properties, the suction wave of preparation according to each functional layer of design requirement Reflectivity in ceramic room temperature 8GHz~18GHz frequency ranges is smaller than -8dB, and under 700 DEG C of high temperature examinations, reflectivity is less than -8dB Bandwidth still have nearly 10GHz or so.But high temperature microwave-absorbing ceramic disclosed above is wanted according to the different electrical property of each functional layer The silicon carbide fibre of different resistivity need to be prepared by asking, and realization acquires a certain degree of difficulty, and cost is higher;And suction wave reported above Ceramics are multilayered structure, and the process is more complicated, and technological requirement is higher.For the above patent there are the problem of, ZL201410128311.6 Chinese patents disclose microwave-absorbing ceramic and its preparation of a kind of single layer structure composite material of silicon carbide Method, simple in structure, thinner thickness, but the Modulatory character of dielectric constant is not strong, is only capable of realizing the suction wave energy of specific band, Can design space it is smaller.
Invention content
The technical problem to be solved by the present invention is to overcome the shortcomings of to mention in background above technology and defect, provide one Kind high temperature resistant high impedance surface radar absorbing and preparation method thereof;Utilize high impedance surface and ceramic matric composite technology It is combined the high temperature resistant high impedance surface absorbing material being prepared into, the electromagnetic property that can both utilized high impedance surface excellent makes suction Wave material absorbing property has stronger designability and better absorbing property;Ceramic matric composite body can be utilized again Being advantage makes absorbing material have preferable heat-resisting quantity and mechanical property.
In order to solve the above technical problems, technical solution proposed by the present invention is:
A kind of high temperature resistant high impedance surface radar absorbing is double-layer structure, includes the medium substrate layer in bottom With the high impedance surface layer in surface layer, the medium substrate layer, which is oxide fibre, enhances oxide-base composite material;It is described High impedance surface layer in the high temperature resistant resistance coating of periodic patterns mainly by forming.Depend on the high impedance table of medium substrate layer The absorption to electromagnetic wave and decaying may be implemented in face.
Above-mentioned absorbing material, it is preferred that the oxide fibre enhancing oxide-base composite material includes quartz fibre Enhancing silica matrix composites, aluminosilicate fibre enhancing aluminosilicate based composites, mullite fiber enhances mullite Composite material or alumina fibre enhance alumina matrix composite.The these types of continuous oxidation fibres enhancing that the present invention chooses Oxide composite can not only ensure the mechanical property and thermal shock resistance that absorbing material product has had, moreover it is possible to ensure to inhale Wave material has high temperature resistant, antioxygenic property, after the high temperature resistant resistance coating covering on upper layer, still has required electrical Energy.
Above-mentioned absorbing material, it is preferred that the material system of the high temperature resistant resistance coating is ruthenic oxide system glass base Resistive coating.It is excellent that ruthenic oxide system glass base resistive coating can ensure that there is absorbing material high temperature resistant and resistance characteristic to stablize Gesture.
Above-mentioned absorbing material, it is preferred that the periodic patterns of the high temperature resistant resistance coating refer to being distributed in matrix form Square patch pattern, the length of side of matrix unit where aforementioned square patch is 12mm~21mm, the square patch The length of side and matrix unit the length of side ratio be 0.5~0.8.
Above-mentioned absorbing material, it is preferred that the thickness of the high temperature resistant resistance coating is 0.01~0.04mm;The medium The thickness of basal layer is 2~5mm.Select the thickness of the resistive coating that can ensure that resistance value is met the requirements;Choose the medium base The thickness of bottom can not only ensure that absorbing material is light, thin, and also ensure the high impedance table for being attached to the medium substrate layer Face layer can be best its high temperature resistant of performance and absorbing property.
The inventive concept total as one, the present invention also provides a kind of preparation method of above-mentioned absorbing material, including it is following Step:
(1) it chooses and preparation media substrate:Choosing suitable continuous oxidation fibres according to design requirement enhances oxide Based composites then prepare corresponding composite material as media substrate materials, finally, thick according to the design of medium substrate Degree is machined composite material, obtains required medium substrate;
(2) high impedance surface layer is prepared:Using silk-screen printing technique, the painting of the high temperature resistant resistance coating will be used to prepare The medium substrate surface that material is printed on step (1) preparation obtains the high temperature resistant high impedance surface radar after drying and sintering Absorbing material.
Above-mentioned preparation method, it is preferred that in the step (2), the preparation method of high temperature resistant resistance coating is as follows:By glass Through 1300 DEG C~1500 DEG C of temperature melting 1h~3h after glass material powder is uniformly mixed, then obtained glass melt is poured into Quenching is carried out in deionized water, obtains glass, then glass marble is worn into elder generation and RuO after glass powder2Powder after mixing again with have Airborne body is uniformly mixed and high temperature resistant resistance coating is made;
The mass percent of each chemical constituent is respectively in the wherein described glass raw material powder:
SiO230%~50%;
Al2O310%~25%;
PbO 12%~25%;
MgO 5%~15%;
CaO 5%~10%;
ZnO 3~10%;
BaO 2%~8% and B2O31%~5%.
The process that above-mentioned glass marble wears into glass powder carries out ball milling, ball milling in agate jar by ball-milling medium of acetone Technical process in, ball material mass ratio be (2~3):1, rotational speed of ball-mill be 380r/min~450r/min, Ball-milling Time be 6h~ 12h;Powder after ball milling crosses the mesh sieve of 200 mesh~400.
Above-mentioned glass powder and RuO2The mixed process of powder mixes in planetary gravity mixer, planetary gravity blender Revolution speed 1280rpm~1500rpm, rotational velocity be revolution speed 30%~60%, 60~120min of mixing time.
Above-mentioned glass and RuO2Mixed powder and the mixed process of organic carrier carried out in three-roll grinder, three rollers are ground The rotating speed of grinding machine is 250~450r/min, and grinding mixing time is 3~6h.
Above-mentioned preparation method, it is preferred that in the step (2), RuO2Powder accounts for glass powder and RuO2Powder gross mass 45%~85%, the mass fraction of organic carrier is 25%~20% in the high temperature resistant resistance coating;Organic carrier mainly by Mass fraction is 80%~90% tributyl citrate, 2%~5% nitrocellulose, 10%~15% lecithin composition.
Above-mentioned preparation method, it is preferred that in the step (2), use during silk-screen printing technique meshcount for 180~300 mesh, printing pass are 1~3 time;Temperature in drying process is 150 DEG C~250 DEG C, and drying time is 2h~4h; Peak firing temperature in sintering process is 1000 DEG C~1050 DEG C, and the heating rate in sintering process is 15 DEG C/min~20 DEG C/min, sintering time is 10min~120min.
Above-mentioned preparation method, it is preferred that in the step (2), high temperature resistant resistance dope viscosity is 170~300pa s。
Compared with the prior art, the advantages of the present invention are as follows:
(1) high temperature resistant high impedance surface radar absorbing of the invention is multiple with continuous oxidation fibres enhancing oxide Condensation material is medium substrate, and high impedance surface layer is very thin and sintering is on medium substrate surface, utilizes high impedance surface and ceramics Based composites technology, which is combined, is prepared into high temperature resistant high impedance surface absorbing material, on the one hand, can utilize high impedance surface Excellent electromagnetic property makes absorbing material absorbing property have stronger designability and better absorbing property;Another party Face can utilize ceramic matric composite system advantage that absorbing material is made to have preferable temperature tolerance and mechanical property, thus have There are preferable mechanical property and thermal shock resistance, so as to realize the integration for inhaling the multi-functionals such as wave, carrying and solar heat protection.
(2) high temperature resistant high impedance surface radar absorbing of the invention can be resistant at least 1000 DEG C of high temperature, have Preferable heat-resisting quantity and excellent inoxidizability.
(3) high temperature resistant high impedance surface radar absorbing of the present invention has surmounted traditional material microstructure composition and has determined The pattern of macro property can control the electromagnetic performance of material by adjusting the electromagnetic structure of sub-wavelength, can thickness compared with Realize that required absorbing property meets the lightweight demand of component to alleviate the weight of product in the case of small.
(4) the high temperature resistant high impedance surface radar absorbing that the present invention obtains is simple in structure, entire step of preparation process Simply, industrialized production can be efficiently applied to.
Description of the drawings
Fig. 1 is the structural schematic diagram of high temperature resistant high impedance surface radar absorbing of the present invention.
Fig. 2 is the high temperature resistant resistance coating photo prepared in the embodiment of the present invention 1.
Fig. 3 is the high temperature resistant high impedance surface radar absorbing tablet sample photo prepared in the embodiment of the present invention 1.
Fig. 4 be the embodiment of the present invention 1 in prepare high temperature resistant high impedance surface radar absorbing room temperature, 1000 DEG C with And restore the reflectance curve of room temperature after 1000 DEG C of examinations.
Specific implementation mode
To facilitate the understanding of the present invention, it is done more entirely below in conjunction with Figure of description and preferred embodiment to inventing herein Face meticulously describes, but protection scope of the present invention is not limited to specific embodiment.
Unless otherwise defined, all technical terms used hereinafter are generally understood meaning phase with those skilled in the art Together.Technical term used herein is intended merely to the purpose of description specific embodiment, is not intended to the limitation present invention's Protection domain.
Unless otherwise specified, various raw material, reagent, the instrument and equipment etc. used in the present invention can pass through city Field is commercially available or can be prepared by existing method.
Embodiment 1:
A kind of high temperature resistant high impedance surface radar absorbing of the present invention, as shown in Figure 1, including the medium in bottom Substrate and high impedance surface layer in surface layer, medium substrate are located at reflection by lining;Wherein, media substrate materials, which are chosen, does not come Mineral wool enhances mullite composite material, thickness d=3.0mm of medium substrate;High impedance surface layer is by being in periodic patterns High temperature resistant resistance coating (using ruthenic oxide as ruthenic oxide system glass base electricity that conductive phase, lead borosilicate glass are binder Resistance coating) composition, thickness 0.02mm;The periodic patterns of high temperature resistant resistance coating are the square patch in matrix form distribution Pattern, the length of side a=13.32mm of matrix unit, the length of side of square patch and the length of side of matrix unit where square patch Ratio be x=0.63.
The preparation method of the high temperature resistant high impedance surface radar absorbing of the present embodiment, includes the following steps:
(1) preparation media substrate:Choosing mullite fiber according to design requirement enhances mullite composite material as medium Base material, then, preparing mullite fiber using sol-gel technology enhances mullite composite material, and to composite material It is machined, obtains the medium substrate that thickness is 3.0mm;
(2) high temperature resistant resistance coating is prepared:
(a) smelting glass:It is respectively SiO by each chemical constituent content245%, Al2O315%, PbO12%, MgO 8%, CaO 5%, ZnO 7%, BaO 5%, B2O33% glass raw material powder is uniformly mixed, and is fitted into platinum crucible, then set together In Muffle furnace, 1400 DEG C, melting 3h are raised to the heating rate of 20 DEG C/min, then, the glass melt after fusing is poured into Quenching is carried out in deionized water, obtains glass dregs;
(b) glass is crushed:Obtained glass dregs are subjected to ball milling in agate jar, using acetone as ball-milling medium, ball Expect that mass ratio is 2:100 DEG C of drying 1h after the completion of ball milling, 1, rotating speed 450r/min, Ball-milling Time 8h cross 250 mesh sieve, obtain To glass powder;
(c) batch mixing:By obtained glass powder and RuO2Powder is 45 according to mass ratio:55 ratio is in planetary gravitational agitation The revolution speed of batch mixing in machine, blender is 1460rpm, and rotational velocity is the 30% of revolution speed, mixing time 120min;
(d) coating is prepared:First by tributyl citrate, nitrocellulose and lecithin according to 80:5:15 mass ratio It is configured to organic carrier, then, by glass obtained and RuO in above-mentioned steps (c)2Mixed powder presses 75 with organic carrier:25 Mass ratio mixing, then grind batch mixing in three-roll grinder, three-roll grinder rotating speed is 300r/min, and three-roll grinder is mixed The material time is 3h, obtains high temperature resistant resistance coating (viscosity of coating is 250Pas), photo is as shown in Figure 2;
(3) high impedance surface layer is prepared:Using silk-screen printing technique (250 mesh of meshcount is printed 1 time), by step (2) The medium substrate surface that the high temperature resistant resistance coating of preparation is printed on step (1) preparation then (is kept the temperature through drying at 250 DEG C 2h) and sintering process (1000 DEG C of peak firing temperature, heating rate be 20 DEG C/min, sintering time 10min), high impedance surface Layer is just sintered that (high impedance surface layer thickness is 0.02mm, and it is in matrix form to have on high temperature resistant resistance coating on medium substrate surface The square patch pattern of distribution, the length of side of matrix unit where square patch are 13.32mm, the length of side of square patch with The ratio of the length of side of matrix unit be 0.63) to get to the present invention high temperature resistant high impedance surface radar absorbing, tablet Photo is as shown in Figure 3.
The high temperature resistant high impedance surface radar absorbing of the present embodiment is tested within the scope of 4~8GHz, room temperature, 1000 DEG C, be returned to reflectivity under three state of temperatures of room temperature after 1000 DEG C of examinations, as shown in figure 4, test result is found, inhale wave material For material under three state of temperatures, the reflectivity within the scope of 4~8GHz is respectively less than -5.5dB.
Embodiment 2:
A kind of high temperature resistant high impedance surface radar absorbing of the present invention, as shown in Figure 1, including the medium in bottom Substrate and high impedance surface layer in surface layer, medium substrate are located at reflection by lining;Wherein, media substrate materials choose oxidation Aluminum fiber enhances alumina matrix composite, thickness d=2.6mm of medium substrate;High impedance surface layer is by being in periodic patterns High temperature resistant resistance coating (using ruthenic oxide as ruthenic oxide system glass base electricity that conductive phase, lead borosilicate glass are binder Resistance coating) composition, the thickness of resistive coating is 0.03mm;The periodic patterns of high temperature resistant resistance coating are distributed in matrix form Square patch pattern, the length of side a=18.87mm of matrix unit, the length of side and matrix of square patch where square patch The ratio of the length of side of unit is x=0.74.
The preparation method of the high temperature resistant high impedance surface radar absorbing of the present embodiment, includes the following steps:
(1) preparation media substrate:Choosing alumina fibre according to design requirement enhances alumina composite material as medium Base material, then, preparing alumina fibre using sol-gel technology enhances alumina composite material, and to composite material It is machined, obtains the medium substrate that thickness is 2.6mm;
(2) high temperature resistant resistance coating is prepared:
(a) smelting glass:It is respectively SiO by each chemical constituent content238%, Al2O322%, PbO12%, MgO 8%, CaO 7%, ZnO 5%, BaO 4%, B2O34% glass raw material powder is uniformly mixed according to a ratio, and is fitted into platinum crucible, then It is placed in Muffle furnace together, is raised to 1450 DEG C, melting 2.5h with 20 DEG C/min, then, the glass melt after fusing is poured into Quenching is carried out in ionized water, obtains glass dregs;
(b) glass is crushed:Glass dregs are subjected to ball milling, ball material mass ratio in agate jar by ball-milling medium of acetone It is 2:1, rotating speed 450r/min, Ball-milling Time 12h, ball milling dry 1h in 100 DEG C, cross 300 mesh sieve after the completion, obtain glass Powder;
(c) batch mixing:By glass powder and RuO2Powder is according to mass ratio 48:52 ratio is mixed in planetary gravity mixer The revolution speed of material, planetary gravity blender is 1500rpm, and rotational velocity is the 40% of revolution speed, and mixing time is 120min;
(d) coating is prepared:First by tributyl citrate, nitrocellulose and lecithin according to 80:5:15 mass ratio It is configured to organic carrier.Then, by glass obtained and RuO in above-mentioned steps (c)2Mixed powder presses 78 with organic carrier:22 Mass ratio mixing, then grind batch mixing in three-roll grinder, three-roll grinder rotating speed is 300r/min, grinds mixing time For 3h, obtain high temperature resistant resistance coating (viscosity of coating is 300Pas);
(3) high impedance surface layer is prepared:Using silk-screen printing technique (300 mesh of meshcount is printed 2 times), by step (2) The medium substrate surface that the high temperature resistant resistance coating of middle preparation is printed on step (1) preparation then (is kept the temperature through drying at 250 DEG C 2h) and sintering process (1000 DEG C of peak firing temperature, heating rate be 20 DEG C/min, sintering time 30min), high impedance surface Layer is just sintered that (thickness of high impedance surface layer is 0.03mm, on high impedance surface layer in medium substrate surface prepared by step (1) With the square patch pattern being distributed in matrix form, the length of side 18.87mm of matrix unit where square patch, square patch The ratio 0.74 of the length of side of piece and the length of side of matrix unit) to get to the present invention high temperature resistant high impedance surface radar-wave absorbing material Material.
High temperature resistant high impedance surface radar absorbing made from the present embodiment is tested within the scope of 8~12GHz, room temperature, 1000 DEG C, be returned to reflectivity under three state of temperatures of room temperature after 1000 DEG C of examinations, test result is found, in three temperature Under state, -10dB is respectively less than within the scope of 8~12GHz.

Claims (7)

1. a kind of high temperature resistant high impedance surface radar absorbing, which is characterized in that the absorbing material is double-layer structure, including Medium substrate layer in bottom and the high impedance surface layer in surface layer, the medium substrate layer, which is oxide fibre, enhances oxygen Compound based composites;The high impedance surface layer in the high temperature resistant resistance coating of periodic patterns mainly by forming;The oxygen Compound fiber reinforcement oxide-base composite material includes quartz fibre enhancing silica matrix composites, aluminosilicate fibre enhancing aluminium Silicate-based composite material, mullite fiber enhancing mullite composite material or alumina fibre enhance alumina base composite wood Material;The material system of the high temperature resistant resistance coating is ruthenic oxide system glass base resistive coating;The high temperature resistant resistance coating By being prepared for high temperature resistant resistance coating, the preparation method of high temperature resistant resistance coating is as follows:Glass raw material powder is mixed equal Through 1300 DEG C~1500 DEG C of temperature melting 1h~3h after even, then obtained glass melt is poured into deionized water and is quenched It is cold, obtain glass, then glass marble is worn into elder generation and RuO after glass powder2Powder is uniformly mixed system with organic carrier again after mixing At high temperature resistant resistance coating;
The mass percent of each chemical constituent is respectively in the wherein described glass raw material powder:
SiO230%~50%;
Al2O310%~25%;
PbO 12%~25%;
MgO 5%~15%;
CaO 5%~10%;
ZnO 3~10%;
BaO 2%~8% and B2O31%~5%.
2. absorbing material as described in claim 1, which is characterized in that the periodic patterns of the high temperature resistant resistance coating refer to In the square patch pattern that matrix form is distributed, the length of side of matrix unit is 12mm~21mm, institute where aforementioned square patch The ratio for stating the length of side of square patch and the length of side of matrix unit is 0.5~0.8.
3. absorbing material as described in claim 1, which is characterized in that the thickness of the high temperature resistant resistance coating be 0.01~ 0.04mm;The thickness of the medium substrate layer is 2~5mm.
4. a kind of preparation method of such as claims 1 to 3 any one of them absorbing material, which is characterized in that including following step Suddenly:
(1) it chooses and preparation media substrate:
(2) high impedance surface layer is prepared:Using silk-screen printing technique, the coating for being used to prepare the high temperature resistant resistance coating is printed Brush is inhaled after drying and sintering to get to the high temperature resistant high impedance surface radar in medium substrate surface prepared by step (1) Wave material.
5. preparation method as claimed in claim 4, which is characterized in that in the step (2), RuO2Powder account for glass powder and RuO2The 45%~85% of powder gross mass, the mass fraction of organic carrier is 20%~25% in the high temperature resistant resistance coating.
6. preparation method as claimed in claim 4, which is characterized in that in the step (2), using silk-screen printing technique process Middle meshcount is 180~300 mesh, and printing pass is 1~3 time;Temperature in drying process is 150 DEG C~250 DEG C, when dry Between be 2h~4h;Peak firing temperature in sintering process is 1000 DEG C~1050 DEG C, and the heating rate in sintering process is 15 DEG C/min~20 DEG C/min, sintering time is 10min~120min.
7. preparation method as claimed in claim 4, which is characterized in that in the step (2), high temperature resistant resistance dope viscosity is 170~300Pa s.
CN201610330896.9A 2016-05-18 2016-05-18 A kind of high temperature resistant high impedance surface radar absorbing and preparation method thereof Active CN106007804B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610330896.9A CN106007804B (en) 2016-05-18 2016-05-18 A kind of high temperature resistant high impedance surface radar absorbing and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610330896.9A CN106007804B (en) 2016-05-18 2016-05-18 A kind of high temperature resistant high impedance surface radar absorbing and preparation method thereof

Publications (2)

Publication Number Publication Date
CN106007804A CN106007804A (en) 2016-10-12
CN106007804B true CN106007804B (en) 2018-10-02

Family

ID=57098438

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610330896.9A Active CN106007804B (en) 2016-05-18 2016-05-18 A kind of high temperature resistant high impedance surface radar absorbing and preparation method thereof

Country Status (1)

Country Link
CN (1) CN106007804B (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107555968B (en) * 2017-08-30 2020-03-24 中国人民解放军国防科技大学 High-temperature-resistant wave-absorbing wedge and preparation method thereof
CN109956667A (en) * 2017-12-26 2019-07-02 北京有色金属研究总院 A kind of alkali corrosion resistance glass coating resistant to high temperatures and preparation method thereof
CN109830809A (en) * 2019-02-21 2019-05-31 南京邮电大学 A kind of multi-layer annular Terahertz Meta Materials wave absorbing device
CN109720027B (en) * 2019-03-05 2019-12-27 中南大学 High-temperature-resistant structural wave-absorbing material based on metal coating and preparation method thereof
CN111170753B (en) * 2020-01-21 2022-05-17 烟台大学 Circuit-screen-containing ceramic wave-absorbing material with high-temperature resistance and preparation method thereof
CN111733595B (en) * 2020-06-30 2023-01-03 中国人民解放军国防科技大学 High-temperature oxidation-resistant flexible conductive oxide ceramic fiber fabric composite material and preparation method thereof
CN114621728A (en) * 2020-12-10 2022-06-14 南京航空航天大学 High-temperature-resistant broadband wave-absorbing structure composite material and preparation method thereof
CN114603937B (en) * 2022-03-09 2023-03-31 电子科技大学 High-temperature-resistant radar infrared compatible stealth material and preparation method thereof
CN115073005B (en) * 2022-07-21 2022-11-08 西安宏星电子浆料科技股份有限公司 Anti-precipitation LTCC insulating medium slurry

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103158299A (en) * 2013-03-12 2013-06-19 中国人民解放军国防科学技术大学 Radar-infrared combined stealth material and preparation method thereof
CN104876616A (en) * 2015-04-20 2015-09-02 中国人民解放军国防科学技术大学 Heat-resistant wave-absorbing material and preparation method thereof

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103158299A (en) * 2013-03-12 2013-06-19 中国人民解放军国防科学技术大学 Radar-infrared combined stealth material and preparation method thereof
CN104876616A (en) * 2015-04-20 2015-09-02 中国人民解放军国防科学技术大学 Heat-resistant wave-absorbing material and preparation method thereof

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
高温结构吸波材料综述;刘海韬 等;《材料导报》;20091031;第23卷(第10期);第24~27页 *

Also Published As

Publication number Publication date
CN106007804A (en) 2016-10-12

Similar Documents

Publication Publication Date Title
CN106007804B (en) A kind of high temperature resistant high impedance surface radar absorbing and preparation method thereof
CN106042515B (en) A kind of high temperature resistant radar absorbing of sandwich and preparation method thereof
CN106007799B (en) Radar & infrared stealth materials and preparation method thereof based on double-layer frequency selective surfaces
CN106003864B (en) High temperature resistant radar & infrared stealth materials based on frequency-selective surfaces and preparation method thereof
CN106427115B (en) A kind of infrared compatible camouflage materials of high temperature resistant radar and preparation method thereof based on the double-deck Meta Materials
CN101104567B (en) Metal composite layer on aluminum oxide ceramic surface and composite technique thereof
CN103145336B (en) A kind of borosilicate glass and ball-aluminium oxide LTCC green band and preparation method thereof
CN111807704B (en) Matte glaze applied to sanitary ceramics, sanitary ceramics applying matte glaze and preparation method of sanitary ceramics
CN106630979B (en) A kind of high temperature resistant frequency selection transparent structure and preparation method thereof
CN107747080B (en) Radar and infrared compatible stealth coating capable of resisting temperature of 600 ℃ and preparation method thereof
CN101314549B (en) Metallic glaze composition
CN102795894A (en) Surface metallization layer of high-purity alumina ceramics and compounding technology thereof
CN103601370B (en) A kind of environmental protection is without the preparation method of acid pollution frosting powder, its preparation method and mat glass
CN107039778B (en) A kind of high temperature resistant radar absorbing and preparation method thereof based on the double-deck Meta Materials
CN102276151B (en) Technological method for preparing LTCC (low temperature co-fired ceramic) amorphous glass ceramic powder with microwave plasma torch
CN110950538B (en) Preparation method of low-expansion high-temperature-resistant environment-friendly medium-low-temperature transparent glass glaze
CN109180006A (en) A kind of low-temperature co-burning ceramic material and preparation method thereof
CN100427438C (en) Electro-magnetic induction vortex heating composite coating having both far infrared transmission and reflection functions
US5518778A (en) Single-layer high temperature coating on a ceramic substrate and its production
CN114603937B (en) High-temperature-resistant radar infrared compatible stealth material and preparation method thereof
JP2002187768A (en) Low temperature sintering dielectric material for high frequency and sintered body of the same
El-Kheshen et al. Densification, phase composition, and properties of borosilicate glass composites containing nano-alumina and titania
CN107759094A (en) Thick film circuit dielectric paste microcrystalline glass powder of stainless steel substrate and preparation method thereof
CN107540375A (en) A kind of low-temperature high-strength devitrified glass and its diamond composite
CN107324766A (en) China clay and production technology, product that a kind of Tao Yin is combined

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant