JPH01127659A - Method for making sprayed deposit dense - Google Patents
Method for making sprayed deposit denseInfo
- Publication number
- JPH01127659A JPH01127659A JP28504587A JP28504587A JPH01127659A JP H01127659 A JPH01127659 A JP H01127659A JP 28504587 A JP28504587 A JP 28504587A JP 28504587 A JP28504587 A JP 28504587A JP H01127659 A JPH01127659 A JP H01127659A
- Authority
- JP
- Japan
- Prior art keywords
- temp
- sprayed deposit
- micropores
- sprayed coating
- composite material
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 14
- 239000000463 material Substances 0.000 claims abstract description 18
- 239000007791 liquid phase Substances 0.000 claims abstract description 4
- 239000011248 coating agent Substances 0.000 claims description 35
- 238000000576 coating method Methods 0.000 claims description 35
- 239000002131 composite material Substances 0.000 claims description 20
- 239000007790 solid phase Substances 0.000 claims description 4
- 239000007789 gas Substances 0.000 abstract description 5
- 238000001513 hot isostatic pressing Methods 0.000 abstract description 3
- 239000002184 metal Substances 0.000 abstract description 3
- 229910052751 metal Inorganic materials 0.000 abstract description 3
- 238000007751 thermal spraying Methods 0.000 abstract 3
- 239000007788 liquid Substances 0.000 abstract 2
- 239000007787 solid Substances 0.000 abstract 2
- 239000010953 base metal Substances 0.000 abstract 1
- 238000011282 treatment Methods 0.000 description 8
- 238000005507 spraying Methods 0.000 description 4
- 239000000956 alloy Substances 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000002775 capsule Substances 0.000 description 3
- 230000007547 defect Effects 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 238000013001 point bending Methods 0.000 description 3
- 239000000758 substrate Substances 0.000 description 3
- 230000007423 decrease Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 238000010998 test method Methods 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000007872 degassing Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000006193 liquid solution Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000012071 phase Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
Landscapes
- Coating By Spraying Or Casting (AREA)
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野)
本発明は溶射被膜が形成された複合材料の該溶射被膜の
緻密化を図り、その品質を改善する方法に関する。DETAILED DESCRIPTION OF THE INVENTION (Industrial Application Field) The present invention relates to a method for densifying a thermally sprayed coating of a composite material on which a thermally sprayed coating has been formed and improving its quality.
(従来の技術)
金属製基材の表面に溶射被膜を形成し、耐摩耗性や耐食
性等を向上させた複合材料がある。前記溶射被膜にはミ
クロポアーが多数存在しているため、溶射被膜の特性を
充分発揮させることができず、また被膜強度が低下する
欠点がある。(Prior Art) There is a composite material that has improved wear resistance, corrosion resistance, etc. by forming a thermal spray coating on the surface of a metal base material. Since the thermal spray coating has a large number of micropores, the thermal spray coating cannot fully exhibit its characteristics, and has the disadvantage that the strength of the coating decreases.
かかる欠陥を除去して溶射被膜の品質を向上させる方法
として、フュージング法や熱間等方向加圧(以下、HI
Pという。)法がある。フュージング法は、溶射被膜を
ガスバーナ等の加熱手段で再溶融させ、被膜中の欠陥を
浮上させたり、溶かし込んだりして欠陥を除去する方法
である。一方、HIP法は、複合材料を塑性変形容易な
薄板で形成されたカプセルに封入脱気した後、あるいは
前記カプセルに圧媒と共に封入した後、HIP処理を施
し、被膜中のミクロポアーを圧潰緻密化する方法である
。The fusing method and hot isostatic pressing (hereinafter referred to as HI) are methods for removing such defects and improving the quality of the sprayed coating.
It's called P. ) There is a law. The fusing method is a method in which a thermally sprayed coating is remelted using a heating means such as a gas burner, and defects in the coating are lifted or melted to remove the defects. On the other hand, in the HIP method, the composite material is encapsulated in a capsule made of a thin plate that is easily plastically deformed, deaerated, or encapsulated with a pressure medium in the capsule, and then subjected to HIP treatment to crush and densify the micropores in the coating. This is the way to do it.
(発明が解決しようとする問題点)
しかしながら、フュージング法は、ミクロポアーの除去
が充分行われず、作業者の熟練度によって品質が左右さ
れ易く、またガスバーナ等で再溶融するために溶射材料
として低融点の自溶性合金を用いなければならないとい
う制約がある。更に、溶射被膜が厚肉の場合、再溶融さ
れない部分が存在し、品質の向上が図れないという問題
がある。(Problems to be Solved by the Invention) However, with the fusing method, micropores are not removed sufficiently, the quality is easily affected by the skill level of the operator, and since it is remelted with a gas burner, it has a low melting point as a thermal spray material. There is a restriction that a self-fusing alloy must be used. Furthermore, when the sprayed coating is thick, there are parts that are not remelted, making it impossible to improve the quality.
また、HIP法では、複合材料をカプセルに封入する等
の煩雑な作業があり、生産性の低下、コスト高の要因と
なっている。Furthermore, the HIP method involves complicated operations such as encapsulating the composite material in a capsule, which causes a decrease in productivity and an increase in costs.
本発明はかかる問題点に鑑みなされたもので、複合材料
の溶射被膜中に存在するミクロポアーを簡単容易に除去
し、溶射被膜の品質の改善を図ることができる方法を提
供することを目的とする。The present invention was made in view of such problems, and an object of the present invention is to provide a method that can easily and easily remove micropores present in a thermally sprayed coating of a composite material and improve the quality of the thermally sprayed coating. .
(問題点を解決するための手段)
上記目的を達成するためになさ・れた本発明の溶射被膜
の緻密化方法は、溶射被膜が形成された複合材料を、真
空中でかつ溶射材料の液相と固相との共存温度域で保持
して前記溶射被膜の表面のみを溶融した後、溶射材料の
固相線温度以下の温度に降温し、次いで前記複合材料を
そのまま熱間等方向加圧することを発明の構成とするも
のである。(Means for Solving the Problems) In order to achieve the above object, the method for densifying a thermally sprayed coating of the present invention is to densify a composite material on which a thermally sprayed coating has been formed in a vacuum and in a liquid solution of a thermally sprayed material. After melting only the surface of the thermally sprayed coating by maintaining it in a temperature range where the phase and solid phase coexist, the temperature is lowered to a temperature below the solidus temperature of the thermally sprayed material, and then the composite material is hot isostatically pressed as it is. This is the structure of the invention.
(作 用)
溶射被膜が形成された複合材料を、望ましくはI X
10− ’ torr以下の真空中でかつ溶射材料の液
相と固相との共存温度域(望ましくは液相が10%以下
の温度域)で保持するので、溶射被膜を保形状態におい
たまま、該被膜中のミクロポアー内の酸素(空気)を排
除すると共に被膜表面を再溶融して表面の開孔を封止す
ることができる。(Function) The composite material on which the sprayed coating is formed is desirably IX
Since it is maintained in a vacuum of 10-' torr or less and in a temperature range where the liquid phase and solid phase of the sprayed material coexist (preferably in a temperature range where the liquid phase is 10% or less), the sprayed coating remains in its shape-retaining state. , it is possible to eliminate oxygen (air) in the micropores in the coating and to re-melt the coating surface to seal the openings on the surface.
溶射被膜の表面のみを溶融し、表面の開孔を封止した後
、溶射材料の固相線温度以下の温度に複合材料を降温す
るので、溶射被膜の内部のミクロポアーが真空(はぼ無
酸素)状態とされかつ表面が溶射材料の被膜によって密
封された複合材料が得られる。このため、HIP処理に
際して、複合材料の封缶脱気処理が不要となる。After melting only the surface of the sprayed coating and sealing the openings on the surface, the temperature of the composite material is lowered to below the solidus temperature of the sprayed material, so that the micropores inside the sprayed coating are in a vacuum ) and whose surface is sealed by a coating of sprayed material is obtained. Therefore, during HIP treatment, sealing and degassing of the composite material becomes unnecessary.
次いで、該複合材料にそのままHIP処理を施すことに
より、溶射被膜内部のミクロポアーが圧潰され緻密化が
図られると共に、溶射被膜が複合材料基材に強固に拡散
接合される。尚、HIP処理条件は従来と同様であり、
通常、処理温度Tは固相線温度をTsとすると Ts≧
T≧Q、8XTs。Next, by directly subjecting the composite material to HIP treatment, the micropores inside the thermally sprayed coating are crushed and densified, and the thermally sprayed coating is firmly diffusion bonded to the composite material base material. The HIP processing conditions are the same as before.
Usually, the processing temperature T is Ts≧, where Ts is the solidus temperature.
T≧Q, 8XTs.
圧力は700kg/cJ以上とされる。Tsを越えてH
IP処理すると、凝固時に再びミクロポアーが発生する
ので好ましくない。The pressure is set to be 700 kg/cJ or more. H over Ts
IP treatment is not preferable because micropores will be generated again during solidification.
尚、以上の処理は、HIP炉中に複合材料を装入し、通
常のHIP処理操作のほか、温度調整するだけで簡単に
行うことができ、作業性が極めて優れる。The above treatment can be easily carried out by simply charging the composite material into a HIP furnace and adjusting the temperature in addition to normal HIP treatment operations, resulting in extremely high workability.
(実施例)
断面が方形状の金属基板(材質335C)に下記組成の
Ni基自溶性合金(固相線温度: 1030℃、液相線
温度: 1070°C)を粉末ガス溶射法により溶射し
、膜厚3mlの溶射被膜を形成した複合材料を製作した
。(Example) A Ni-based self-fusing alloy with the following composition (solidus temperature: 1030°C, liquidus temperature: 1070°C) was sprayed onto a metal substrate (material 335C) with a rectangular cross section by a powder gas spraying method. A composite material with a thermally sprayed coating having a thickness of 3 ml was manufactured.
・Ni基自溶性合金組成(重量%)
C:0.6%、 St : 4.0%、 Fe : 3
.5%、Cr : 16%、 B:3.0%、 Co:
実質的残部前記複合材料をHIP炉に装入して、lXl
0−’torr、 1045℃にて30分間保持した後
、850°Cに降温した。・Ni-based self-fusing alloy composition (wt%) C: 0.6%, St: 4.0%, Fe: 3
.. 5%, Cr: 16%, B: 3.0%, Co:
Substantially the remainder of the composite material is charged into a HIP furnace and
After holding at 1045°C for 30 minutes at 0-'torr, the temperature was lowered to 850°C.
次いで、975°Cにて、Arガスを圧媒として100
0kg/C1aまで加圧し、2時間保持した後、炉冷し
た。Next, at 975°C, Ar gas was used as a pressure medium for 100°C.
The pressure was increased to 0 kg/C1a, maintained for 2 hours, and then cooled in a furnace.
以上の処理を施した実施例試料から、2mm厚×4mm
幅×30flII11長さの溶射被膜1をワイヤーカッ
ト放電加工によって切り出し、第1図の要領で4点曲げ
試験を行った。また、第2図に示す様に、基板3に溶射
被膜の一部2を残し、他は基板表面(接合面)から除去
して接合面においでせん断試験を行った。第1図および
第2図中の寸法単位は閣である。上記結果を下記第1表
および第2表に示す。尚、同表には、同複合材料の溶射
被膜にフュージングを施した従来例試料の試験結果を併
せて示す。From the example sample treated above, 2mm thick x 4mm
A thermally sprayed coating 1 having a width of 30 fl II and a length of 11 mm was cut out by wire-cut electric discharge machining, and a four-point bending test was conducted as shown in FIG. Further, as shown in FIG. 2, a part 2 of the sprayed coating was left on the substrate 3, and the rest was removed from the substrate surface (joint surface), and a shear test was conducted on the joint surface. The dimensional unit in Figures 1 and 2 is ka. The above results are shown in Tables 1 and 2 below. The same table also shows the test results of conventional samples in which the thermally sprayed coating of the same composite material was subjected to fusing.
(次 葉)
第1表 4点曲げ試験結果
第2表 せん断試験結果
第1表および第2表より、本発明実施例は従来例に対し
て、抗折強度が30%程度、せん断強度が40%程度向
上し、またデータのばらつきも極めて少ないことが知ら
れる。(Next page) Table 1 4-point bending test results Table 2 Shear test results From Tables 1 and 2, the bending strength of the embodiment of the present invention is about 30% and the shear strength is 40% compared to the conventional example. %, and it is known that the variation in data is extremely small.
(発明の効果)
以上説明した通り、本発明の溶射被膜の緻密化方法によ
れば、複合材料に形成された溶射被膜は、真空中でかつ
その表面のみが溶融され、固化されるので、溶射被膜内
のミクロボアーが真空状態とされて、溶射被膜表面の開
孔が封止され、これをそのままHIP処理することが可
能となる。従って、従来のように、HIP処理するに際
し、複合材料の封入脱気処理等の煩雑な作業が不要とな
り、作業の簡単容易化が図られる。(Effects of the Invention) As explained above, according to the method for densifying a thermally sprayed coating of the present invention, the thermally sprayed coating formed on the composite material is melted and solidified only on its surface in vacuum. The microbore within the coating is evacuated, the openings on the surface of the thermally sprayed coating are sealed, and this can be subjected to HIP treatment as is. Therefore, unlike in the past, when performing HIP processing, complicated operations such as enclosing and deaerating the composite material are no longer necessary, and the operations can be simplified.
そして、HIP処理により、溶射被膜中のミクロボアー
は圧潰され、溶射被膜の緻密化、品質の向上を図ること
ができる。Then, by the HIP treatment, the microbore in the sprayed coating is crushed, making it possible to make the sprayed coating denser and improve its quality.
第1図は4点曲げ試験要領説明図、第2図は接合面にお
けるせん断試験要領説明図である。
第1図
j12 図FIG. 1 is an explanatory diagram of a four-point bending test procedure, and FIG. 2 is an explanatory diagram of a shear test procedure on a joint surface. Figure 1j12 Figure
Claims (1)
溶射材料の液相と固相との共存温度域で保持して前記溶
射被膜の表面のみを溶融した後、溶射材料の固相線温度
以下の温度に降温し、次いで前記複合材料をそのまま熱
間等方向加圧することを特徴とする溶射被膜の緻密化方
法。(1) The composite material on which the thermal sprayed coating has been formed is held in a temperature range where the liquid phase and solid phase of the thermal sprayed material coexist to melt only the surface of the thermal sprayed coating, and then the solid phase of the thermal sprayed material is melted. 1. A method for densifying a sprayed coating, comprising lowering the temperature to a temperature below the line temperature, and then subjecting the composite material to hot iso-directional pressing as it is.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62285045A JPH07122130B2 (en) | 1987-11-10 | 1987-11-10 | Densification method of thermal spray coating |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62285045A JPH07122130B2 (en) | 1987-11-10 | 1987-11-10 | Densification method of thermal spray coating |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH01127659A true JPH01127659A (en) | 1989-05-19 |
JPH07122130B2 JPH07122130B2 (en) | 1995-12-25 |
Family
ID=17686452
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP62285045A Expired - Lifetime JPH07122130B2 (en) | 1987-11-10 | 1987-11-10 | Densification method of thermal spray coating |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH07122130B2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113796945A (en) * | 2021-10-29 | 2021-12-17 | 苏州海宇新辰医疗科技有限公司 | Cryoablation tube |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS60110862A (en) * | 1983-11-22 | 1985-06-17 | Mitsubishi Heavy Ind Ltd | Manufacture of thruster |
JPS61159566A (en) * | 1985-01-08 | 1986-07-19 | Daido Steel Co Ltd | Coating method of metallic or ceramic base material |
-
1987
- 1987-11-10 JP JP62285045A patent/JPH07122130B2/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS60110862A (en) * | 1983-11-22 | 1985-06-17 | Mitsubishi Heavy Ind Ltd | Manufacture of thruster |
JPS61159566A (en) * | 1985-01-08 | 1986-07-19 | Daido Steel Co Ltd | Coating method of metallic or ceramic base material |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113796945A (en) * | 2021-10-29 | 2021-12-17 | 苏州海宇新辰医疗科技有限公司 | Cryoablation tube |
CN113796945B (en) * | 2021-10-29 | 2023-08-18 | 苏州海宇新辰医疗科技有限公司 | Cryoablation tube |
Also Published As
Publication number | Publication date |
---|---|
JPH07122130B2 (en) | 1995-12-25 |
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