JPH0357178B2 - - Google Patents
Info
- Publication number
- JPH0357178B2 JPH0357178B2 JP11559182A JP11559182A JPH0357178B2 JP H0357178 B2 JPH0357178 B2 JP H0357178B2 JP 11559182 A JP11559182 A JP 11559182A JP 11559182 A JP11559182 A JP 11559182A JP H0357178 B2 JPH0357178 B2 JP H0357178B2
- Authority
- JP
- Japan
- Prior art keywords
- vanadium
- resistance
- alloy
- yttrium
- thermal
- 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
- 239000000956 alloy Substances 0.000 claims description 14
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 12
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 8
- 229910052804 chromium Inorganic materials 0.000 claims description 8
- 239000011651 chromium Substances 0.000 claims description 8
- 229910052727 yttrium Inorganic materials 0.000 claims description 8
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 7
- 229910052782 aluminium Inorganic materials 0.000 claims description 7
- 238000007751 thermal spraying Methods 0.000 claims description 6
- 229910052684 Cerium Inorganic materials 0.000 claims description 5
- 229910052746 lanthanum Inorganic materials 0.000 claims description 5
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 claims description 5
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- 239000007921 spray Substances 0.000 claims description 2
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 claims 1
- 230000007797 corrosion Effects 0.000 description 14
- 238000005260 corrosion Methods 0.000 description 14
- 229910052720 vanadium Inorganic materials 0.000 description 14
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 13
- 229910045601 alloy Inorganic materials 0.000 description 11
- 230000003647 oxidation Effects 0.000 description 9
- 238000007254 oxidation reaction Methods 0.000 description 9
- 230000000694 effects Effects 0.000 description 7
- 239000000463 material Substances 0.000 description 7
- 239000011248 coating agent Substances 0.000 description 5
- 238000000576 coating method Methods 0.000 description 5
- 239000000843 powder Substances 0.000 description 5
- 230000035939 shock Effects 0.000 description 5
- ZMIGMASIKSOYAM-UHFFFAOYSA-N cerium Chemical compound [Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce] ZMIGMASIKSOYAM-UHFFFAOYSA-N 0.000 description 4
- 239000003921 oil Substances 0.000 description 4
- 238000005507 spraying Methods 0.000 description 4
- 229910018138 Al-Y Inorganic materials 0.000 description 3
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 3
- 229910052717 sulfur Inorganic materials 0.000 description 3
- 239000011593 sulfur Substances 0.000 description 3
- 229910000669 Chrome steel Inorganic materials 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000000295 fuel oil Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004584 weight gain Effects 0.000 description 2
- 235000019786 weight gain Nutrition 0.000 description 2
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- WAIPAZQMEIHHTJ-UHFFFAOYSA-N [Cr].[Co] Chemical compound [Cr].[Co] WAIPAZQMEIHHTJ-UHFFFAOYSA-N 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical group [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000007750 plasma spraying Methods 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 229910052761 rare earth metal Inorganic materials 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Coating By Spraying Or Casting (AREA)
Description
本発明は耐熱性溶射用合金材料、特に高温腐食
に強い溶射用合金粉末に関するものである。
近年石油価格の上昇は著しく、また品質につい
ても硫黄、バナジウムの含有量が多い低品質油が
増加している。このような状況においては省エネ
ルギー技術とともに低品質油の活用技術が非常に
重要になつている。
ところで、燃料として重油を使用するガスター
ビンの燃焼室、石油精製装置用加熱炉などの高温
下で使用される部品の多くは、耐熱性の他に高温
での耐食性が要求されている。特に硫黄やバナジ
ウム含有量の多い重油を使わざるを得ない状況に
おいては、従来使用されていたクロム鋼やニツケ
ル・クロム鋼では高温における耐蝕性が不充分で
あり、使用範囲が制約される難点がある。
この難点を克服するため溶射加工法が著しい進
歩を示しており、高温で使用する部材の表面に高
温耐食材料を溶射被覆し、部材の寿命を延長する
技術が採用されている。具体的な例としてはNi
基のNi−Cr−Al−Y合金が提案されており、一
部の用途では効果を発揮している。
しかしながらNi基のNi−Cr−Al−Y合金はバ
ナジウム濃度が高く、しかも高温度の環境におい
て使用される場合には、必ずしも耐食性が充分で
はなく、保護被膜としての機能を保つことができ
ないのでしばしば問題となつている。
本発明はバナジウム濃度の高い高温腐食環境に
対しても、充分な耐食性を示す溶射用合金粉末材
料を提供するものである。
すなわち、本発明はバナジウムアタツクに強い
クロムを主成分とし、これにアルミニウムおよび
イツトリウムを添加し、残部がニツケルから成る
ことを第1の特徴とし、さらに高温度における皮
膜の靭性と密着性を改善するため該合金にランタ
ン、セリウムのうち少くとも1種以上を添加した
ことを第2の特徴とする。
本発明の各成分の含有量を前記の如く定めた理
由は皮膜の耐熱性、耐食性、耐熱衝撃性、靭性お
よび皮膜と母材との密着性を検討した上、有効範
囲として定めたものである。
即ち、クロムは本発明合金の耐熱性、耐食性を
付与するのに必要なものであり、特に高温でのバ
ナジウムアタツクに対抗させるためクロム基合金
とする。クロムが50%未満では高温におけるバナ
ジウムによる腐食に対して充分な効果が得られ
ず、70%を越えると皮膜が脆弱となり、母材との
密着性が弱くなり実用的でなくなる。
アルミニウムはクロムとのあいだで金属間化合
物を形成し、耐酸化性および高温での硫黄による
腐食に対して効果的である。添加量が2%未満で
はその効果が弱く、一方15%を越えると溶射皮膜
が脆化するためである。
イツトリウムはアルミニウムと同時に添加する
ことにより、溶射皮膜の耐食耐酸化性に対して効
果を有する。添加量は0.1%未満では効果が不充
分であり、3.0%を越えても効果の伸長は認めら
れず経済的でないからである。
残余をニツケルとしたのは耐熱性および耐食性
を損うことなく溶射皮膜に靭性を与え、母材との
密着性を良くするためである。
さらに選択元素のランタンやセリウムはイツト
リウムと性質の類似し希土類元素であるが、イツ
トリウムと同時に添加することにより皮膜の靭性
を改善し、特に皮膜の割れの防止や耐剥離性の向
上に対して効果的であることが判明した。添加量
はランタン、セリウムのうち少くとも1種を0.1
%〜3.0%とするのが適当である。0.1%未満では
その効果は弱く、3%を越えても効果の向上は認
められない。
次に本発明の実施例をあげて詳述する。
実施例
表1に示す組成の合金を通常の溶融細粒化法に
より粉末にした後、分級して10〜44μmの粒度範
囲に調整して溶射用材料とした。これらの合金粉
末材料を使用してプラズマ溶射により40mm角2mm
厚のハステロイCの試験片の両面に0.3mm厚の溶
射被覆を施した。
溶射条件は次のとおりであつた。
アークガス:Ar:Hr=3:1、50/min
電 圧:34V
電 流:800A
粉末供給量:30g/min
次にこれらの試験片について高温でのバナジウ
ムアタツク試験、酸化試験、熱衝撃試験を実施し
た。バナジウムアタツク試験は85%V2O5−15%
Na2SO4溶液を塗布後電気炉中で1050℃に3時間
保持した後取出し、再び塗布加熱を3回くり返し
てから脱スケール処理を行ない、試験前後の重量
変化により腐食度合を調べた。酸化試験について
は試験片を大気雰囲気の炉中で1100℃で100時間
保持し、経時的に酸化増量を測定した。熱衝撃試
験は試料を1050℃の炉中で3時間保持した後水冷
する処理をくり返し、溶射皮膜が剥離するまでの
くり返し回数を調らべた。バナジウムアタツク試
験および耐熱衝撃試験の結果を表1に、酸化試験
結果を第1図に示した。尚、比較例として従来使
用されていたNi−Cr−Al−Y合金(No.5)およ
びCr−Ni合金(No.6)で溶射被覆し、同様の試
験をした結果を併記した。
The present invention relates to a heat-resistant thermal spraying alloy material, particularly to a thermal spraying alloy powder that is resistant to high-temperature corrosion. Oil prices have risen markedly in recent years, and low-quality oil with high sulfur and vanadium contents is on the rise. Under these circumstances, energy saving technology and technology to utilize low-quality oil have become extremely important. By the way, many of the parts used at high temperatures, such as combustion chambers of gas turbines that use heavy oil as fuel, heating furnaces for oil refineries, etc., are required to have corrosion resistance at high temperatures in addition to heat resistance. Particularly in situations where heavy oil with high sulfur and vanadium contents must be used, the conventionally used chrome steel and nickel chrome steel have insufficient corrosion resistance at high temperatures, which limits the range of use. be. In order to overcome this difficulty, thermal spray processing methods have shown remarkable progress, and techniques have been adopted to extend the service life of parts by thermally spraying them with high-temperature corrosion-resistant materials on the surfaces of parts used at high temperatures. A specific example is Ni
Ni-Cr-Al-Y based alloys have been proposed and have been effective in some applications. However, Ni-based Ni-Cr-Al-Y alloys have a high vanadium concentration, and when used in high-temperature environments, they do not necessarily have sufficient corrosion resistance and cannot maintain their function as a protective film. It's becoming a problem. The present invention provides an alloy powder material for thermal spraying that exhibits sufficient corrosion resistance even in a high-temperature corrosive environment with a high vanadium concentration. That is, the first feature of the present invention is that the main component is chromium, which is resistant to vanadium attack, to which aluminum and yttrium are added, and the remainder is nickel, and further improves the toughness and adhesion of the film at high temperatures. The second feature is that at least one of lanthanum and cerium is added to the alloy in order to achieve this. The content of each component of the present invention was determined as described above because it was determined as an effective range after considering the heat resistance, corrosion resistance, thermal shock resistance, toughness, and adhesion between the film and the base material of the film. . That is, chromium is necessary to impart heat resistance and corrosion resistance to the alloy of the present invention, and in particular, a chromium-based alloy is used to resist vanadium attack at high temperatures. If the chromium content is less than 50%, sufficient effect against corrosion by vanadium at high temperatures will not be obtained, and if it exceeds 70%, the film will become brittle and the adhesion to the base material will weaken, making it impractical. Aluminum forms an intermetallic compound with chromium and is effective against oxidation and corrosion by sulfur at high temperatures. If the amount added is less than 2%, the effect will be weak, while if it exceeds 15%, the sprayed coating will become brittle. When added at the same time as aluminum, yttrium has an effect on the corrosion and oxidation resistance of the sprayed coating. This is because if the amount added is less than 0.1%, the effect is insufficient, and if it exceeds 3.0%, no extension of the effect is observed and it is not economical. The reason why the remainder was made of nickel was to impart toughness to the thermal sprayed coating without impairing its heat resistance and corrosion resistance, and to improve its adhesion to the base material. Furthermore, the selective elements lanthanum and cerium are rare earth elements with similar properties to yttrium, but when added at the same time as yttrium, they improve the toughness of the film, and are particularly effective in preventing cracking and improving peeling resistance of the film. It turned out to be true. Addition amount is 0.1 of at least one of lanthanum and cerium.
% to 3.0% is appropriate. If it is less than 0.1%, the effect is weak, and if it exceeds 3%, no improvement in the effect is observed. Next, the present invention will be described in detail with reference to examples. EXAMPLE An alloy having the composition shown in Table 1 was made into a powder by a conventional melt-refining method, and then classified to adjust the particle size to a range of 10 to 44 μm to obtain a material for thermal spraying. 40mm square 2mm by plasma spraying using these alloy powder materials.
A 0.3 mm thick thermal spray coating was applied to both sides of a thick Hastelloy C test piece. The thermal spraying conditions were as follows. Arc gas: Ar: Hr = 3:1, 50/min Voltage: 34 V Current: 800 A Powder supply rate: 30 g/min Next, these specimens were subjected to vanadium attack tests, oxidation tests, and thermal shock tests at high temperatures. carried out. Vanadium attack test is 85%V 2 O 5 -15%
After applying the Na 2 SO 4 solution, it was kept at 1050°C for 3 hours in an electric furnace, then taken out, and the application and heating were repeated 3 times, followed by descaling treatment, and the degree of corrosion was examined by weight changes before and after the test. For the oxidation test, the test piece was held at 1100°C for 100 hours in a furnace in an atmospheric atmosphere, and the oxidation weight gain was measured over time. In the thermal shock test, the sample was kept in a furnace at 1050°C for 3 hours and then cooled with water repeatedly, and the number of repetitions until the thermal spray coating peeled off was determined. The results of the vanadium attack test and the thermal shock test are shown in Table 1, and the results of the oxidation test are shown in FIG. In addition, as a comparative example, the results of a similar test performed by thermal spray coating with conventionally used Ni-Cr-Al-Y alloy (No. 5) and Cr-Ni alloy (No. 6) are also shown.
【表】
表1の結果からクロムを50%以上含み、アルミ
ニウムとイツトリウムを同時に含んでいるNo.1〜
No.4およびNo.7は耐バナジウムアタツクに優れて
いることがわかる。たゞしアルミニウム含有量の
多いNo.7は皮膜が脆くなつて剥離し易くなるので
適当でない。またランタン、セリウムを添加した
No.3、No.4は耐バナジウムアタツクに加え、耐熱
衝撃性が著しく向上することが認められる。
第1図によればイツトリウムの添加されていな
いNo.6およびNo.8はかなりの酸化増量がみられ
る。またアルミニウム含有量の多いNo.7では被覆
に割れが発生したため、異常酸化を起こしたもの
である。
以上説明したとおり、本発明によれば特に高温
での耐バナジウム腐食性にすぐれた強固な溶射皮
膜が得られる。[Table] From the results in Table 1, No. 1 ~ containing 50% or more chromium and simultaneously containing aluminum and yttrium
It can be seen that No. 4 and No. 7 have excellent vanadium attack resistance. However, No. 7, which has a high aluminum content, is not suitable because the film becomes brittle and easily peels off. Also added lanthanum and cerium.
In addition to vanadium attack resistance, No. 3 and No. 4 were found to have significantly improved thermal shock resistance. According to FIG. 1, in No. 6 and No. 8 to which yttrium was not added, a considerable increase in oxidation weight was observed. Furthermore, in No. 7, which had a high aluminum content, cracks occurred in the coating, which caused abnormal oxidation. As explained above, according to the present invention, a strong thermal sprayed coating with excellent vanadium corrosion resistance particularly at high temperatures can be obtained.
第1図は本発明による耐熱性溶射合金で被覆し
た試片の高温酸化増量の経時変化を示す図であ
る。
FIG. 1 is a diagram showing the change over time in high-temperature oxidation weight gain of a specimen coated with the heat-resistant sprayed alloy according to the present invention.
Claims (1)
ウム2〜15%、イツトリウム0.1〜3.0%および残
部がニツケルから成ることを特徴とする耐熱性溶
射性溶射用合金材料。 2 重量パーセントでクロム50〜70%、アルミニ
ウム2〜15%、イツトリウム0.1〜3.0%、ランタ
ンまたはセリウムのうち少くとも1種を0.1〜3.0
%および残部がニツケルから成ることを特徴とす
る耐熱性溶射用合金材料。[Claims] 1. A heat-resistant thermal spray alloy material, characterized in that it consists of 50 to 70% chromium, 2 to 15% aluminum, 0.1 to 3.0% yttrium, and the balance nickel. 2. Contains at least one of 50-70% chromium, 2-15% aluminum, 0.1-3.0% yttrium, and 0.1-3.0% lanthanum or cerium by weight.
A heat-resistant alloy material for thermal spraying, characterized in that % and the remainder are made of nickel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11559182A JPS596352A (en) | 1982-07-05 | 1982-07-05 | Heat resistant alloy material for plasma spray |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11559182A JPS596352A (en) | 1982-07-05 | 1982-07-05 | Heat resistant alloy material for plasma spray |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS596352A JPS596352A (en) | 1984-01-13 |
| JPH0357178B2 true JPH0357178B2 (en) | 1991-08-30 |
Family
ID=14666389
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP11559182A Granted JPS596352A (en) | 1982-07-05 | 1982-07-05 | Heat resistant alloy material for plasma spray |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS596352A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2003147464A (en) | 2001-11-02 | 2003-05-21 | Tocalo Co Ltd | Member with high-temperature strength |
-
1982
- 1982-07-05 JP JP11559182A patent/JPS596352A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS596352A (en) | 1984-01-13 |
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