JPH0213028B2 - - Google Patents
Info
- Publication number
- JPH0213028B2 JPH0213028B2 JP29862085A JP29862085A JPH0213028B2 JP H0213028 B2 JPH0213028 B2 JP H0213028B2 JP 29862085 A JP29862085 A JP 29862085A JP 29862085 A JP29862085 A JP 29862085A JP H0213028 B2 JPH0213028 B2 JP H0213028B2
- Authority
- JP
- Japan
- Prior art keywords
- metal
- mixture
- ceramic molded
- coated
- reaction
- 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.)
- Expired
Links
- 239000000203 mixture Substances 0.000 claims description 34
- 229910052751 metal Inorganic materials 0.000 claims description 33
- 239000002184 metal Substances 0.000 claims description 32
- 239000000919 ceramic Substances 0.000 claims description 27
- 238000000034 method Methods 0.000 claims description 24
- 238000006243 chemical reaction Methods 0.000 claims description 18
- 238000002844 melting Methods 0.000 claims description 18
- 150000002484 inorganic compounds Chemical class 0.000 claims description 16
- 229910010272 inorganic material Inorganic materials 0.000 claims description 16
- 230000008018 melting Effects 0.000 claims description 14
- 239000011247 coating layer Substances 0.000 claims description 13
- 239000010410 layer Substances 0.000 claims description 13
- 238000003786 synthesis reaction Methods 0.000 claims description 12
- 238000000576 coating method Methods 0.000 claims description 10
- 230000006835 compression Effects 0.000 claims description 9
- 238000007906 compression Methods 0.000 claims description 9
- 229910052796 boron Inorganic materials 0.000 claims description 8
- 239000011248 coating agent Substances 0.000 claims description 8
- 230000015572 biosynthetic process Effects 0.000 claims description 4
- 230000000737 periodic effect Effects 0.000 claims description 4
- 150000001540 azides Chemical class 0.000 claims description 3
- 150000002736 metal compounds Chemical class 0.000 claims description 3
- 229910052698 phosphorus Inorganic materials 0.000 claims description 3
- 230000000644 propagated effect Effects 0.000 claims description 3
- 229910052710 silicon Inorganic materials 0.000 claims description 3
- 229910052717 sulfur Inorganic materials 0.000 claims description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 15
- 239000010936 titanium Substances 0.000 description 12
- 229910052719 titanium Inorganic materials 0.000 description 12
- 239000000843 powder Substances 0.000 description 9
- 238000002485 combustion reaction Methods 0.000 description 7
- 239000007789 gas Substances 0.000 description 6
- QYEXBYZXHDUPRC-UHFFFAOYSA-N B#[Ti]#B Chemical compound B#[Ti]#B QYEXBYZXHDUPRC-UHFFFAOYSA-N 0.000 description 5
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 5
- 229910033181 TiB2 Inorganic materials 0.000 description 5
- 239000002131 composite material Substances 0.000 description 5
- 229910052755 nonmetal Inorganic materials 0.000 description 5
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 5
- PXIPVTKHYLBLMZ-UHFFFAOYSA-N Sodium azide Chemical compound [Na+].[N-]=[N+]=[N-] PXIPVTKHYLBLMZ-UHFFFAOYSA-N 0.000 description 4
- 239000000376 reactant Substances 0.000 description 4
- 239000002344 surface layer Substances 0.000 description 4
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 description 3
- 238000005304 joining Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 229910026551 ZrC Inorganic materials 0.000 description 2
- OTCHGXYCWNXDOA-UHFFFAOYSA-N [C].[Zr] Chemical compound [C].[Zr] OTCHGXYCWNXDOA-UHFFFAOYSA-N 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 229910002804 graphite Inorganic materials 0.000 description 2
- 239000010439 graphite Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 150000001247 metal acetylides Chemical class 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 150000004767 nitrides Chemical class 0.000 description 2
- 229910021332 silicide Inorganic materials 0.000 description 2
- 229910052708 sodium Inorganic materials 0.000 description 2
- 239000011734 sodium Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 230000002194 synthesizing effect Effects 0.000 description 2
- 150000003568 thioethers Chemical class 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 229910001369 Brass Inorganic materials 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 229910007948 ZrB2 Inorganic materials 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- VWZIXVXBCBBRGP-UHFFFAOYSA-N boron;zirconium Chemical compound B#[Zr]#B VWZIXVXBCBBRGP-UHFFFAOYSA-N 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- -1 carbides Chemical class 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- VNTLIPZTSJSULJ-UHFFFAOYSA-N chromium molybdenum Chemical compound [Cr].[Mo] VNTLIPZTSJSULJ-UHFFFAOYSA-N 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000000280 densification Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000002706 hydrostatic effect Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 239000012774 insulation material Substances 0.000 description 1
- 238000011068 loading method Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000011812 mixed powder Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 150000002843 nonmetals Chemical class 0.000 description 1
- 238000005240 physical vapour deposition Methods 0.000 description 1
- 229910052697 platinum Inorganic materials 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000002230 thermal chemical vapour deposition Methods 0.000 description 1
- 238000007751 thermal spraying Methods 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/4505—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements characterised by the method of application
- C04B41/455—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements characterised by the method of application the coating or impregnating process including a chemical conversion or reaction
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Chemically Coating (AREA)
Description
【発明の詳細な説明】
産業上の利用分野
本発明は、高融点無機化合物、例えば周期律表
第2、第3、第4、第5、第6および第7周期金
属の炭化物、ホウ化物、ケイ化物、リン化物、硫
化物、窒化物、酸化物およびこれらの複合化合物
を各種金属あるいはセラミツクス成形体の表面に
厚肉コーテイングを行う方法に関するものであ
る。DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application The present invention relates to high melting point inorganic compounds, such as carbides, borides, The present invention relates to a method for applying thick coatings of silicides, phosphides, sulfides, nitrides, oxides, and composite compounds thereof to the surfaces of various metal or ceramic molded bodies.
従来の技術
従来、金属あるいはセラミツクス成形体の表面
に高融点無機化合物をコーテイングする方法とし
て溶射法、CVD法、PVD法などがある。これら
の方法はコーテイング層の形成に時間がかかるた
め薄膜のコーテイングに有効ではあるが、1mm以
上の厚肉コーテイングの技術としては作業効率上
適当ではない。また金属あるいはセラミツクス成
形体の表面に厚肉のセラミツクスを形成させる方
法として、あらかじめ成形したセラミツクスを接
合させる方法がある。これらの方法はセラミツク
ス成形体の間に接合用のインサート材を挿入して
熱処理することにより結合させたり、ろう付けに
よる方法が知られているが、あらかじめ接合する
セラミツクスを製造しておく必要があり接合面が
複雑な形状を有している場合には必ずしも満足し
うる方法とはいえない。BACKGROUND TECHNOLOGY Conventionally, thermal spraying, CVD, and PVD methods have been used to coat the surface of a metal or ceramic molded body with a high-melting point inorganic compound. Although these methods are effective for coating thin films because it takes time to form a coating layer, they are not suitable from the viewpoint of work efficiency as techniques for coating thicker layers of 1 mm or more. Further, as a method for forming thick ceramics on the surface of a metal or ceramic molded body, there is a method of bonding preformed ceramics. These methods include inserting a bonding insert material between ceramic molded bodies and bonding by heat treatment, or brazing, but it is necessary to manufacture the ceramics to be bonded in advance. This method is not necessarily satisfactory when the joint surface has a complicated shape.
燃焼工程を開始させるに充分な温度に金属−非
金属混合物の表面層の小部分を強熱することによ
り(この場合、一層から他層への燃焼帯の伝播は
出発成分間の反応の結果として放出される熱およ
び熱伝達に基づく)金属と非金属の反応を開始さ
せ高融点無機化合物を合成する方法が公知であ
る。(特公昭56−27441)反応は燃焼帯として知ら
れる混合物の薄層で進行し、この場合温度は2000
〜4000Kという高い温度になる。燃焼帯は混合物
中に1〜15cm/sの速度で広がる。このような高融
点無機化合物の合成時に遠心力や静ガス圧または
静水圧で圧縮することにより高密度の成形体を得
る方法が提案されている。(例えば特願昭53−
5212、特願57−500289)
発明が解決しようとする問題点
本発明の目的は金属−非金属混合物の局部に着
火することにより反応を開始させ燃焼帯の進行と
ともに高融点無機化合物を合成する方法において
高融点無機化合物を合成すると同時に金属あるい
はセラミツクス成形体の表面に接合することによ
り、簡単な構造の装置を用いて安価にできる高融
点無機化物の厚肉コーテイングを行う方法を提供
することにある。 By igniting a small portion of the surface layer of the metal-nonmetal mixture to a temperature sufficient to initiate the combustion process, in which case the propagation of the combustion zone from one layer to the other occurs as a result of the reaction between the starting components. Methods are known to initiate reactions between metals and non-metals (based on released heat and heat transfer) to synthesize high melting point inorganic compounds. (Special Publication No. 56-27441) The reaction proceeds in a thin layer of the mixture known as the combustion zone, where the temperature is 2000
The temperature is as high as ~4000K. The combustion zone spreads through the mixture at a speed of 1-15 cm/s. A method has been proposed in which a high-density molded body is obtained by compressing such a high-melting-point inorganic compound using centrifugal force, static gas pressure, or hydrostatic pressure during synthesis. (For example, patent application 1973-
5212, Patent Application No. 57-500289) Problems to be Solved by the Invention The purpose of the present invention is to provide a method for synthesizing a high melting point inorganic compound as the combustion zone progresses by starting a reaction by locally igniting a metal-nonmetal mixture. An object of the present invention is to provide a method for producing a thick coating of a high melting point inorganic compound at a low cost using a device with a simple structure, by simultaneously synthesizing the high melting point inorganic compound and bonding it to the surface of a metal or ceramic molded body. .
問題点を解決するための手段
本発明に従えば周期律表第2、第3、第4、第
5、第6および第7周期から選ばれる金属または
金属化合物の少なくとも一種、非金属元素C、
B、Si、P、Sまたはアジ化物の少なくとも一種
を充分混合し、コーテイングの対象となる金属ま
たはセラミツクス成形体の表面に上記混合物を加
圧圧縮し、真空または0.1〜200atmの不活性雰囲
気下で混合物の端部に強熱着火して発熱反応を開
始させ、その反応がさらに混合物の次の層への熱
伝達によつて伝播される条件下で自己増殖的に合
成反応を加圧方向とほぼ平行な方向に進展させ、
圧縮バネの伸長力を利用することによつて合成と
同時に金属あるいはセラミツクス成形体の表面に
接合することによつてその目的を達成することが
できる。Means for Solving the Problems According to the present invention, at least one metal or metal compound selected from the second, third, fourth, fifth, sixth and seventh periods of the periodic table, a nonmetallic element C,
At least one of B, Si, P, S, or azide is thoroughly mixed, and the mixture is pressurized and compressed onto the surface of a metal or ceramic molded object to be coated, and the mixture is heated under vacuum or an inert atmosphere of 0.1 to 200 atm. The end of the mixture is ignited by ignition to initiate an exothermic reaction, and under conditions where the reaction is further propagated by heat transfer to the next layer of the mixture, the synthesis reaction proceeds in a self-propagating manner approximately in the direction of pressure. develop in parallel directions,
This purpose can be achieved by bonding to the surface of a metal or ceramic molded body at the same time as synthesis by utilizing the stretching force of a compression spring.
本発明方法における接合は投錨効果といわれる
機械的な作用をその主な要因とする接合法を利用
するものである。コーテイングする高融点無機化
合物が合成反応の際に高熱を発生するもの(例え
ば二ホウ化チタンTiB2や二ホウ化ジルコニウム
ZrB2)であり、またコーテイングの対象となる
金属またはセラミツクス成形体の熱伝導特性が小
さいため、あるいは融点が低いために高熱により
表層が一部溶解するものであるならば、特にコー
テイングする高融点無機化合物とコーテイングの
対象となる金属あるいはセラミツクス成形体の間
に別の高発熱混合物層を設ける必要はない。しか
しながらコーテイングする高融点無機化合物が合
成反応の際に発生した熱が少なく、あるいはコー
テイングの対象となる金属またはセラミツクス成
形体の熱伝導特性が良いかあるいは融点が高いた
めに表層が一部溶解する条件にない場合には高発
熱混合物層をコーテイングする高融点無機化合物
とコーテイングの対象となる金属あるいはセラミ
ツクス成形体の間にあらかじめ設けておき、合成
反応の際に高発熱混合物層の反応の結果生じた高
熱を接合に利用する必要がある。さらに、あらか
じめコーテイングの対象となる金属またはセラミ
ツクスの表面を平面でなく凹凸状に加工すること
によつて、効果的に接合強度の高いコーテイング
を行うことができる。 The joining in the method of the present invention utilizes a joining method whose main factor is a mechanical action called an anchoring effect. The high melting point inorganic compound to be coated is one that generates high heat during the synthesis reaction (e.g. titanium diboride TiB2 or zirconium diboride).
ZrB 2 ), and if the metal or ceramic molded object to be coated has low thermal conductivity or has a low melting point, and the surface layer will partially melt due to high heat, the high melting point to be coated is particularly important. There is no need to provide a separate layer of a high exothermic mixture between the inorganic compound and the metal or ceramic molded body to be coated. However, there are conditions in which the surface layer partially melts because the high melting point inorganic compound to be coated generates little heat during the synthesis reaction, or the metal or ceramic molded object to be coated has good thermal conductivity or has a high melting point. If the layer does not exist, it should be provided in advance between the high melting point inorganic compound to be coated with the high exothermic mixture layer and the metal or ceramic molded object to be coated, and a layer formed as a result of the reaction of the high exothermic mixture layer during the synthesis reaction. It is necessary to use high heat for bonding. Further, by processing the surface of the metal or ceramic to be coated in advance to have an uneven surface instead of a flat surface, it is possible to effectively coat the surface with high bonding strength.
本発明方法の特徴は、コーテイングの対象とな
る金属またはセラミツクス成形体の表面に金属−
非金属混合物を加圧圧縮し、真空または0.1〜
200atmの不活性ガスに置換した容器内において、
混合物の端部に強熱着火して発熱反応を開始さ
せ、自己増殖的な合成反応が加圧方向とほぼ平行
な方向に進展し反応がコーテイングの対象となる
金属またはセラミツクス成形体の表面に達した時
に合成物と金属またはセラミツクスとが強固に接
合するように、圧縮バネの伸張力によつて接合に
必要な圧力が持続的に加えられる点にある。した
がつて圧縮バネの役割は混合物の圧粉と合成物の
接合を可能ならしめることであり、圧縮バネはそ
の目的に合致するバネ定数と圧縮強度および伸張
長さを有するものではなくてはならない。これら
の条件はコーテイングする高融点無機化合物の収
縮距離、圧縮断面積、コーテイングの対象となる
金属またはセラミツクスの材質等によつてその最
適条件を決定することができる。 The feature of the method of the present invention is that the metal or ceramic molded object to be coated has a metal layer on the surface thereof.
Non-metallic mixtures are compressed under pressure, vacuum or 0.1~
In a container purged with 200 atm inert gas,
The end of the mixture is ignited with high heat to start an exothermic reaction, and a self-propagating synthesis reaction progresses in a direction almost parallel to the direction of pressure, and the reaction reaches the surface of the metal or ceramic molded object to be coated. The point is that the pressure necessary for bonding is continuously applied by the tension force of the compression spring so that the composite and the metal or ceramics are firmly bonded when the composite is bonded to the metal or ceramic. Therefore, the role of the compression spring is to enable the joining of the powder mixture and the composite, and the compression spring must have a spring constant, compressive strength, and extension length that meet this purpose. . The optimum conditions for these conditions can be determined depending on the shrinkage distance of the high melting point inorganic compound to be coated, the compressed cross-sectional area, the material of the metal or ceramic to be coated, etc.
本発明方法における着火方法は確実な着火のた
めと、加圧圧縮方向とほぼ平行な方向に反応を進
展させるために、混合物の端部に接するように2
本のタングステンあるいは同等の高融点金属の導
線を配し2本の導線の間に例えば0.2mm径の白金
線を接続する着火治具を用いる。タングステン線
に電流を通じることによつて白金線を通電加熱さ
せ、あるいは電流を通じることによつて蒸発飛散
した白金がその後の電流の経路となることによつ
て混合物に強熱を与え確実な着火に導く。2本の
導線の間に細線を接続するかわりに高周波電流を
通じることによつてイオン化したガスを電流の経
路として混合物に強熱を与えることも可能であ
る。このような確実な着火方法を備えることによ
り、本発明方法は高融点無機化合物の厚肉コーテ
イング方法として極めて実用性に優れたものとな
る。 The ignition method in the method of the present invention is such that two parts are placed in contact with the end of the mixture in order to ensure ignition and to allow the reaction to progress in a direction substantially parallel to the direction of pressurization and compression.
An ignition jig is used in which conductive wires made of tungsten or an equivalent high-melting point metal are arranged, and a platinum wire with a diameter of 0.2 mm, for example, is connected between the two conductors. By passing an electric current through the tungsten wire, the platinum wire is heated by electricity, or by passing an electric current, the platinum that evaporates and scatters becomes a path for the subsequent current, which gives the mixture intense heat and ensures reliable ignition. lead to. Instead of connecting a thin wire between the two conductive wires, it is also possible to pass a high-frequency current through the ionized gas and apply intense heat to the mixture using the ionized gas as the current path. By providing such a reliable ignition method, the method of the present invention becomes extremely practical as a thick coating method for high-melting point inorganic compounds.
発明の効果
本発明方法に従えば、周期律表第2、第3、第
4、第5、第6および第7周期から選ばれる金属
の炭化物、ホウ化物、ケイ化物、リン化物、硫化
物、窒化物、酸化物およびこれらの複合化合物を
金属またはセラミツクスの表面に極めて簡単な装
置および操作で短時間のうちに厚肉コーテイング
することができ、本発明方法は極めて実用性に優
れたものである。また本発明方法に従えばほとん
どあらゆる金属またはセラミツクスの表面にコー
テイングすることが可能となる。コーテイング層
の厚さは1mm以上が可能であり、最大厚さの限界
は事実上ない。一度にコーテイングできる面積は
1mm2以上が可能であり、装置を工夫することによ
つて面積の限界も事実上存在しない。適宜最適方
法を検討することによつて、コーテイング面が複
雑な形状を有しているような場合にも対応するこ
とができる。次に実施例によつて本発明をさらに
詳細に説明する。Effects of the Invention According to the method of the present invention, carbides, borides, silicides, phosphides, sulfides of metals selected from the second, third, fourth, fifth, sixth and seventh periods of the periodic table, The method of the present invention is highly practical, as it is possible to coat the surface of metal or ceramics with nitrides, oxides, and their composite compounds in a short time using extremely simple equipment and operations. . Furthermore, according to the method of the present invention, it is possible to coat almost any metal or ceramic surface. The thickness of the coating layer can be 1 mm or more, and there is virtually no limit to the maximum thickness. The area that can be coated at one time is 1 mm 2 or more, and by devising the equipment, there is virtually no limit to the area. By appropriately considering the optimum method, it is possible to cope with cases where the coating surface has a complicated shape. Next, the present invention will be explained in more detail with reference to Examples.
実施例 1
図1に示すように、真空にできる容器内に黒鉛
で熱遮断したクロムモリブデン鋼製の鋳型を設置
し、鋳型内にチタンとホウ素の粉末をモル比で1
対2の割合で充分混合した混合物を充填し、その
上にコーテイングの対象となるチタン棒をのせ
る。コーテイング面積は1cm2、混合粉末は2gで
ある。上下より500Kg/cm2の圧力をかけ、バネを圧
縮させると同時に圧粉を行う。容器内を真空引き
し余分なガスを排出する。あらかじめ装着した着
火治具(2本のタングステン線の端部に0.2mm径
の白金線を溶接したもの)に電流を瞬時流してコ
ーテイング層の外側から接合面に向つて反応を開
始させる。反応が圧粉体の端部から進展するに従
つて3000℃に加熱された燃焼帯において、ニホウ
化チタン(TiB2)の合成反応と同時にち密化が
進行し、反応によつて収縮した距離はバネの伸張
によつて遂次補なわれる。燃焼帯がチタン棒の端
面に達すると高熱によりチタン棒の表層が溶解し
ニホウ化チタンの厚肉コーテイング層と強固に結
合される。反応終了後冷却した試料を鋳型より取
り出しチタン表面にニホウ化チタンをコーテイン
グした接合体の製造を完了する。得られたコーテ
イング層は密度4.4g/cm3、厚さ4.5mm、接合強度
は400Kg/cm2であつた。Example 1 As shown in Figure 1, a mold made of chromium-molybdenum steel heat-insulated with graphite was placed in a container that could be evacuated, and titanium and boron powders were placed in the mold at a molar ratio of 1.
A well-mixed mixture in a 2:2 ratio is filled, and a titanium rod to be coated is placed on top of the mixture. The coating area was 1 cm 2 and the mixed powder was 2 g. A pressure of 500Kg/cm 2 is applied from above and below to compress the spring and at the same time compact the powder. Vacuum the inside of the container to remove excess gas. A current is instantaneously passed through a pre-installed ignition jig (a platinum wire with a diameter of 0.2 mm is welded to the ends of two tungsten wires) to initiate a reaction from the outside of the coating layer toward the joint surface. As the reaction progresses from the edge of the compact, densification progresses simultaneously with the synthesis reaction of titanium diboride (TiB 2 ) in the combustion zone heated to 3000℃, and the distance contracted by the reaction is This is successively compensated for by the expansion of the spring. When the combustion zone reaches the end face of the titanium rod, the surface layer of the titanium rod is melted by high heat and is firmly bonded to the thick coating layer of titanium diboride. After the reaction is complete, the cooled sample is removed from the mold and the titanium surface is coated with titanium diboride to complete the production of a joined body. The resulting coating layer had a density of 4.4 g/cm 3 , a thickness of 4.5 mm, and a bonding strength of 400 Kg/cm 2 .
実施例 2
反応物が200Kg/cm2の圧力下で型内で圧縮される
点を除き、実施例1において述べたと同一の方法
で黄銅表面にホウ化チタン(TiB)がコーテイン
グされるる。鋳型内に充填するチタンとホウ素の
粉末はモル比で1対1の割合で充分混合した混合
物2gを用いる。得られたコーテイング層は密度
4.5g/cm3、厚さ4.4mm、接合強度は400Kg/cm2であ
つた。Example 2 Titanium boride (TiB) is coated onto a brass surface in the same manner as described in Example 1, except that the reactants are compressed in a mold under a pressure of 200 Kg/cm 2 . As for the titanium and boron powders to be filled into the mold, 2 g of a mixture sufficiently mixed at a molar ratio of 1:1 is used. The resulting coating layer has a density
The weight was 4.5g/cm 3 , the thickness was 4.4mm, and the bonding strength was 400Kg/cm 2 .
実施例 3
反応物が200Kg/cm2の圧力下で型内で圧縮される
点、チタンとホウ素の粉末をモル比で1対2の割
合で混合した高発熱混合物を0.2gをあらかじめコ
ーテイング層とコーテイングの対象となるチタン
棒の間に充填する点を除き実施例1において述べ
たと同一の方法でチタン表面にホウ化チタン
(TiB)がコーテイングされる。鋳型内に充填す
るチタンとホウ素の粉末はモル比で1対1対の割
合で充分に混合した混合物2gを用いる。得られ
たコーテイング層は、密度4.5g/cm3、厚さ5mm、
接合強度は400Kg/cm2であつた。Example 3 The reactant was compressed in a mold under a pressure of 200 kg/ cm2 , and 0.2 g of a high exothermic mixture of titanium and boron powders mixed at a molar ratio of 1:2 was added to the coating layer in advance. Titanium boride (TiB) is coated on the titanium surface in the same manner as described in Example 1 except that it is filled between the titanium rods to be coated. As the powders of titanium and boron to be filled into the mold, 2 g of a mixture sufficiently mixed at a molar ratio of 1:1 is used. The resulting coating layer had a density of 4.5 g/cm 3 and a thickness of 5 mm.
The bonding strength was 400Kg/cm 2 .
実施例 4
反応物が500Kg/cm2の圧力下で型内で圧縮される
点、チタンとホウ素の粉末をモル比で1対2の割
合で混合した高発熱混合物0.2gをあらかじめコー
テイング層とコーテイングの対象となるステンレ
ス鋼(SUS304)の間に充填する点を除き実施例
1において述べたと同一の方法で、ステンレス鋼
の表面に炭化ジルコニウム(ZrC)がコーテイン
グされる。鋳型内に充填するジルコニウムと炭素
の粉末はモル比で1対1の割合で充分混合した混
合物2gを用いる。得られたコーテイング層は密
度6.1g/cm3、厚さ3.6mm、接合強度は300Kg/cm2であ
つた。Example 4 The reactant is compressed in a mold under a pressure of 500 Kg/cm 2 , and 0.2 g of a high exothermic mixture of titanium and boron powders mixed at a molar ratio of 1:2 is coated with the coating layer in advance. Zirconium carbide (ZrC) is coated on the surface of stainless steel in the same manner as described in Example 1 except that it is filled between the stainless steel (SUS304) to be coated. The zirconium and carbon powders to be filled into the mold are 2 g of a mixture sufficiently mixed at a molar ratio of 1:1. The resulting coating layer had a density of 6.1 g/cm 3 , a thickness of 3.6 mm, and a bonding strength of 300 Kg/cm 2 .
実施例 5
反応物が200Kg/cm2の圧力下で型内で圧縮される
点を除き、実施例1において述べたと同一の方法
でアルミニウム金属の表面に窒化チタン(TiN)
がコーテイングされる。鋳型内に充填するチタン
とアジ化ナトリウム(NaN3)の粉末はモル比で
3対1の割合で充分に混合した混合物2gを用い
る。チタンとアジ化ナトリウムの反応により窒化
チタンとナトリウムが生成し、ナトリウムはガス
状となつて鋳型の外へ排出され、窒化チタンのコ
ーテイング層がアルミニウム表面に形成される。
得られたコーテイング層は密度5.3g/cm3、厚さ
3.4mm、接合強度は200Kg/cm2であつた。Example 5 Titanium nitride (TiN) was deposited on the surface of aluminum metal in the same manner as described in Example 1, except that the reactants were compressed in a mold under a pressure of 200 Kg/ cm2 .
is coated. The powder of titanium and sodium azide (NaN 3 ) to be filled into the mold is 2 g of a mixture sufficiently mixed at a molar ratio of 3:1. The reaction between titanium and sodium azide produces titanium nitride and sodium, and the sodium is discharged out of the mold as a gas, forming a coating layer of titanium nitride on the aluminum surface.
The resulting coating layer has a density of 5.3 g/cm 3 and a thickness of
3.4 mm, and the bonding strength was 200 Kg/cm 2 .
第1図は本発明方法によつて高融点無機化合物
の厚肉コーテイングを行なうための装置及び金属
−非金属混合物とコーテイングの対象となる金属
の装填の一例を示す立面図であり、図中符号1は
圧縮装置の一部、2は真空容器、3は真空排出
口、4はアルゴンガス導入口、5は着火のための
電流印加装置、6は圧縮バネ、7はクロムモリブ
デン鋼製の鋳型、8は黒鉛製の熱絶縁材、9はタ
ングステン線、10は金属−非金属混合物、11
はコーテイングの対象となる金属である。
FIG. 1 is an elevational view showing an example of an apparatus for applying a thick coating of a high melting point inorganic compound according to the method of the present invention, and an example of loading a metal-nonmetal mixture and a metal to be coated. 1 is a part of the compression device, 2 is a vacuum container, 3 is a vacuum outlet, 4 is an argon gas inlet, 5 is a current application device for ignition, 6 is a compression spring, and 7 is a mold made of chrome-molybdenum steel. , 8 is a thermal insulation material made of graphite, 9 is a tungsten wire, 10 is a metal-nonmetal mixture, 11
is the metal to be coated.
Claims (1)
び第7周期から選ばれる金属または金属化合物の
少なくとも一種、非金属元素C、B、Si、P、S
またはアジ化物の少なくとも一種を充分混合し、
コーテイングの対象となる金属またはセラミツク
ス成形体表面に上記混合物を加圧圧縮し、真空ま
たは0.1〜200atmの不活性雰囲気下で混合物の端
部に強熱着火して発熱反応を開始させ、その反応
がさらに混合物の次の層への熱伝達によつて伝播
される条件下で自己増殖的に合成反応を加圧方向
とほぼ平行な方向に進展させ圧縮バネの伸張力を
利用することによつて合成と同時に金属またはセ
ラミツクス成形体の表面に高融点無機化合物の厚
肉コーテイングを行う方法。 2 周期律表第2、第3、第4、第5、第6およ
び第7周期から選ばれる金属または金属化合物の
少なくとも一種、非金属元素C、B、Si、P、S
またはアジ化物の少なくとも一種を充分混合し、
コーテイングの対象となる金属またはセラミツク
ス成形体の表面に上記混合物を加圧圧縮する際に
更に反応によつて合成される厚肉コーテイング層
と金属またはセラミツクス成形体の間に高発熱混
合物の層を設け、真空または0.1〜200atmの不活
性雰囲気下で混合物の端部に強熱着火して発熱反
応を開始させ、その反応がさらに混合物の次の層
への熱伝達によつて伝播される条件下で自己増殖
的に合成反応を加圧方向とほぼ平行な方向に進展
させ圧縮バネの伸張力を利用することによつて合
成と同時に金属またはセラミツクス成形体の表面
に高融点無機化合物の厚肉コーテイングを行う方
法。[Claims] 1. At least one metal or metal compound selected from periods 2, 3, 4, 5, 6, and 7 of the periodic table, nonmetallic elements C, B, Si, P, S
or sufficiently mixed with at least one azide,
The above mixture is pressurized and compressed onto the surface of the metal or ceramic molded object to be coated, and the end of the mixture is ignited with high heat in a vacuum or an inert atmosphere of 0.1 to 200 atm to start an exothermic reaction. Furthermore, under conditions propagated by heat transfer to the next layer of the mixture, the synthesis reaction progresses in a self-propagating manner in a direction approximately parallel to the direction of pressure, and synthesis is performed by utilizing the tension force of the compression spring. At the same time, a method in which a thick coating of a high melting point inorganic compound is applied to the surface of a metal or ceramic molded body. 2 At least one metal or metal compound selected from the 2nd, 3rd, 4th, 5th, 6th and 7th periods of the periodic table, non-metallic elements C, B, Si, P, S
or sufficiently mixed with at least one azide;
When the above-mentioned mixture is pressurized and compressed on the surface of the metal or ceramic molded body to be coated, a layer of the high exothermic mixture is further provided between the thick coating layer synthesized by reaction and the metal or ceramic molded body. , under vacuum or an inert atmosphere of 0.1 to 200 atm, under conditions where the end of the mixture is ignited to initiate an exothermic reaction, which is further propagated by heat transfer to the next layer of the mixture. By allowing the synthesis reaction to progress in a self-propagating manner in a direction almost parallel to the direction of pressure, and by utilizing the tension of a compression spring, a thick coating of a high-melting point inorganic compound can be applied to the surface of a metal or ceramic molded body at the same time as synthesis. How to do it.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP29862085A JPS62156271A (en) | 1985-12-27 | 1985-12-27 | Thick coating method with inorganic compound having high melting point |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP29862085A JPS62156271A (en) | 1985-12-27 | 1985-12-27 | Thick coating method with inorganic compound having high melting point |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS62156271A JPS62156271A (en) | 1987-07-11 |
| JPH0213028B2 true JPH0213028B2 (en) | 1990-04-03 |
Family
ID=17862083
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP29862085A Granted JPS62156271A (en) | 1985-12-27 | 1985-12-27 | Thick coating method with inorganic compound having high melting point |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62156271A (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2717541B2 (en) * | 1988-04-21 | 1998-02-18 | 株式会社小松製作所 | Method of forming ceramic layer on metal body |
| US5376421A (en) * | 1991-08-30 | 1994-12-27 | University Of Cincinnati | Combustible slurry for joining metallic or ceramic surfaces or for coating metallic, ceramic and refractory surfaces |
| AU7312494A (en) * | 1994-02-16 | 1995-09-04 | University Of Cincinnati, The | Method for joining ceramic and metal-ceramic heating elements to electrical terminals by micropyretic synthesis, compositions for electrical terminals and heaters comprising the same |
-
1985
- 1985-12-27 JP JP29862085A patent/JPS62156271A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS62156271A (en) | 1987-07-11 |
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