JP2952341B2 - Heat resistant material and method for producing the same - Google Patents
Heat resistant material and method for producing the sameInfo
- Publication number
- JP2952341B2 JP2952341B2 JP8103904A JP10390496A JP2952341B2 JP 2952341 B2 JP2952341 B2 JP 2952341B2 JP 8103904 A JP8103904 A JP 8103904A JP 10390496 A JP10390496 A JP 10390496A JP 2952341 B2 JP2952341 B2 JP 2952341B2
- Authority
- JP
- Japan
- Prior art keywords
- powder
- intermetallic compound
- weight
- oxidation resistance
- sic
- 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 - Lifetime
Links
- 239000003779 heat-resistant material Substances 0.000 title claims description 17
- 238000004519 manufacturing process Methods 0.000 title claims description 6
- 229910000765 intermetallic Inorganic materials 0.000 claims description 37
- 239000000843 powder Substances 0.000 claims description 35
- 230000003647 oxidation Effects 0.000 claims description 34
- 238000007254 oxidation reaction Methods 0.000 claims description 34
- 229910010038 TiAl Inorganic materials 0.000 claims description 31
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 10
- 239000000203 mixture Substances 0.000 claims description 10
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 6
- 238000000498 ball milling Methods 0.000 claims description 6
- 229910052786 argon Inorganic materials 0.000 claims description 5
- 239000011261 inert gas Substances 0.000 claims description 4
- 238000000465 moulding Methods 0.000 claims description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 2
- 229910001873 dinitrogen Inorganic materials 0.000 claims description 2
- 239000001307 helium Substances 0.000 claims description 2
- 229910052734 helium Inorganic materials 0.000 claims description 2
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 2
- 238000010276 construction Methods 0.000 claims 1
- 238000000034 method Methods 0.000 description 22
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 8
- 238000010438 heat treatment Methods 0.000 description 8
- 239000001301 oxygen Substances 0.000 description 8
- 229910052760 oxygen Inorganic materials 0.000 description 8
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 7
- 238000005245 sintering Methods 0.000 description 7
- 229910010413 TiO 2 Inorganic materials 0.000 description 6
- 239000002245 particle Substances 0.000 description 6
- 229910001069 Ti alloy Inorganic materials 0.000 description 4
- 230000007423 decrease Effects 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 239000011159 matrix material Substances 0.000 description 4
- 238000009792 diffusion process Methods 0.000 description 3
- 239000010419 fine particle Substances 0.000 description 3
- 238000005551 mechanical alloying Methods 0.000 description 3
- 230000000704 physical effect Effects 0.000 description 3
- 239000010936 titanium Substances 0.000 description 3
- 229910052719 titanium Inorganic materials 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 238000003801 milling Methods 0.000 description 2
- 239000011812 mixed powder Substances 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 229910052758 niobium Inorganic materials 0.000 description 2
- 239000010955 niobium Substances 0.000 description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 229910000601 superalloy Inorganic materials 0.000 description 2
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- QVYYOKWPCQYKEY-UHFFFAOYSA-N [Fe].[Co] Chemical compound [Fe].[Co] QVYYOKWPCQYKEY-UHFFFAOYSA-N 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- UQZIWOQVLUASCR-UHFFFAOYSA-N alumane;titanium Chemical compound [AlH3].[Ti] UQZIWOQVLUASCR-UHFFFAOYSA-N 0.000 description 1
- 238000005269 aluminizing Methods 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000003245 coal Substances 0.000 description 1
- 239000011362 coarse particle Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 238000000748 compression moulding Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- -1 for example Substances 0.000 description 1
- TXFYZJQDQJUDED-UHFFFAOYSA-N germanium nickel Chemical compound [Ni].[Ge] TXFYZJQDQJUDED-UHFFFAOYSA-N 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 238000007569 slipcasting Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Powder Metallurgy (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Description
【0001】[0001]
【発明の属する技術分野】本発明は、新規な耐熱性材料
及びその製造方法に関するものである。さらに詳しくい
えば、本発明は、軽量でかつ耐熱性に優れるとともに、
高温における耐酸化性を向上させたTiAl金属間化合
物系耐熱性材料、及びこのものを効率よく製造する方法
に関するものである。The present invention relates to a novel heat-resistant material and a method for producing the same. More specifically, the present invention is lightweight and excellent in heat resistance,
The present invention relates to a TiAl intermetallic compound heat-resistant material having improved oxidation resistance at high temperatures, and a method for efficiently producing the same.
【0002】[0002]
【従来の技術】チタン合金は軽くて強く、かつ比較的耐
熱性が良好なことから、航空機用材料などとして広く使
用されているが、その使用温度限界は673〜873K
程度であって、これより高い温度になると定常的な応力
がかかる部位ではクリープ現象が激しいという欠点があ
り、用途が制限されるのを免れない。このため、耐クリ
ープ性に優れるチタン合金の開発が進められているが、
通常の合金では十分に満足しうるものが得られていな
い。2. Description of the Related Art Titanium alloys are widely used as aircraft materials because they are light and strong and have relatively good heat resistance. However, their operating temperature limit is 673 to 873K.
However, at a temperature higher than this, there is a disadvantage that a creep phenomenon is severe at a portion where a steady stress is applied, and it is unavoidable that the application is restricted. For this reason, titanium alloys with excellent creep resistance are being developed.
Satisfactory ones have not been obtained with ordinary alloys.
【0003】ところで、近年、チタン−アルミニウム
系、ニッケル−アルミニウム系、ニッケル−ゲルマニウ
ム系、鉄−コバルト系などの金属間化合物が、耐熱性材
料として注目されている。通常の合金は、結晶の各格子
位置を異種原子が不規則に占めているが、金属間化合物
は、各構成原子の占める位置が特定され、いわゆる規則
構造を形成しており、その結果、異常強化現象などの金
属間化合物の特異な変形挙動をもたらす。一般に、変形
温度が上昇すると金属材料の強度は低下するが、金属間
化合物は、ある温度領域まで変形温度の上昇に伴い、逆
にその強度が増加する、いわゆる異常強化現象を示すも
のが多く、これが金属間化合物が耐熱性材料として注目
される理由の一つとなっている。In recent years, intermetallic compounds such as titanium-aluminum, nickel-aluminum, nickel-germanium, and iron-cobalt have attracted attention as heat-resistant materials. In ordinary alloys, the heterogeneous atoms occupy each lattice position of the crystal irregularly, but in the intermetallic compound, the positions occupied by the constituent atoms are specified, forming a so-called ordered structure. This leads to a unique deformation behavior of the intermetallic compound such as a strengthening phenomenon. In general, when the deformation temperature increases, the strength of the metal material decreases.However, intermetallic compounds often exhibit the so-called abnormal strengthening phenomenon, in which the strength increases with an increase in the deformation temperature up to a certain temperature range, This is one of the reasons why the intermetallic compound attracts attention as a heat-resistant material.
【0004】このような金属間化合物の中でTiAl
は、アルミニウムを多量に含んでいるため、Ni基超合
金やコバルト基超合金に比べて低比重で、高い比強度を
有し、しかも優れた高温強度を有していることから、軽
量耐熱性材料として期待されている。また、ヤング率も
他のチタン合金より大きく、低剛性であるため、チタン
合金のもう1つの欠点も補っている。Among such intermetallic compounds, TiAl
Has a low specific gravity, high specific strength, and excellent high-temperature strength compared to Ni-based superalloys and cobalt-based superalloys because it contains a large amount of aluminum. It is expected as a material. In addition, it has a higher Young's modulus and lower rigidity than other titanium alloys, thereby compensating for another disadvantage of titanium alloys.
【0005】しかしながら、このTiAl金属間化合物
は常温延性が乏しく、機械加工性が劣る上、1073K
以上の高温における耐酸化性が低いという欠点を有して
おり、実用上の大きな障害となっている。したがって、
常温延性を改善するために、これまで精力的に研究が行
われ、例えばクロム、マンガン、ニオビウム、ケイ素、
スズ、タングステンなどの元素を第三成分として添加す
る方法、相変態を利用して組織を制御する方法、粉末冶
金法(メカニカルアロイングや急冷プロセス)を用いて
組織を超微細化する方法など、種々の方法が試みられて
おり、その成果が徐々に実りつつある。[0005] However, this TiAl intermetallic compound has poor room temperature ductility, poor machinability, and 1073K
It has the disadvantage that the oxidation resistance at high temperatures is low, which is a major obstacle in practical use. Therefore,
In order to improve the cold ductility, intensive research has been carried out so far, for example, chromium, manganese, niobium, silicon,
Such as a method of adding elements such as tin and tungsten as a third component, a method of controlling the structure using phase transformation, and a method of ultra-fine structure using powder metallurgy (mechanical alloying or quenching process). Various methods have been tried and the results are gradually paying off.
【0006】一方、高温における耐酸化性を改善するた
めに、例えばケイ素、モリブデン、ニオビウム、リン、
マンガン、クロム、イットリウムなどの元素を第三成分
として添加する方法、低酸素分圧下で熱処理する方法、
CoCrAlやCOCrAlYなどで表面コーティング
する方法、アルミニウムの拡散浸透処理法(アルミナイ
ジング処理法)など、外的因子を制御する方法や、結晶
粒径、表面状態及び内部組織などの材料の内的因子を制
御する方法などが試みられている。On the other hand, in order to improve oxidation resistance at high temperatures, for example, silicon, molybdenum, niobium, phosphorus,
Manganese, chromium, a method of adding an element such as yttrium as a third component, a method of heat treatment under a low oxygen partial pressure,
A method of controlling external factors such as a method of surface coating with CoCrAl or COCrAlY, a diffusion infiltration treatment method of aluminum (aluminizing treatment method), and a method of controlling internal factors of a material such as a crystal grain size, a surface state, and an internal structure. Control methods have been attempted.
【0007】しかしながら、これらの方法は操作が煩雑
であったり、十分な耐酸化性が得られなかったり、また
耐酸化性が得られても、他の物性が低下するなどの欠点
があり、必ずしも満足しうるものではなかった。However, these methods have drawbacks such as complicated operation, insufficient oxidation resistance, and deterioration of other physical properties even if oxidation resistance is obtained. It was not satisfactory.
【0008】[0008]
【発明が解決しようとする課題】本発明はこのような事
情のもとで、軽量でかつ耐熱性に優れ、しかも高温での
耐酸化性が著しく向上したTiAl金属間化合物系耐熱
性材料を提供することを目的としてなされたものであ
る。Under these circumstances, the present invention provides a TiAl intermetallic compound heat-resistant material which is lightweight, has excellent heat resistance, and has remarkably improved oxidation resistance at high temperatures. It was done for the purpose of doing.
【0009】[0009]
【課題を解決するための手段】本発明者らは、TiAl
金属間化合物の高温での耐酸化性を向上させるために鋭
意研究を重ねた結果、TiAl金属間化合物のマトリッ
クスにSiC微粒子を特定の割合で分散させることによ
り、TiAl金属間化合物が本来有する優れた特性をそ
こなうことなく、高温での耐酸化性を著しく向上させう
ることを見出し、この知見に基づいて本発明を完成する
に至った。Means for Solving the Problems The present inventors have proposed TiAl
As a result of intensive studies to improve the oxidation resistance of the intermetallic compound at high temperatures, by dispersing the SiC fine particles at a specific ratio in the matrix of the TiAl intermetallic compound, the excellent properties inherent in the TiAl intermetallic compound have been obtained. It has been found that the oxidation resistance at high temperatures can be significantly improved without deteriorating the characteristics, and the present invention has been completed based on this finding.
【0010】 すなわち、本発明はTiAl金属間化合
物粉末とSiC粉末との重量比100:0.5ないし1
00:50の混合物の焼結体から成る1273K〜14
73Kの温度範囲における耐酸化性が優れていることを
特徴とする耐熱性材料、及びボールミリンしてTiAl
金属間化合物粉末を形成させ、次いでこの粉末100重
量部に対し、SiC粉末0.5〜50重量部を配合し、
加圧成形後、30MPa以上の圧力下、1200〜15
00Kの温度において焼結することを特徴とするTiA
l金属間化合物粉末とSiC粉末との重量比100:
0.5ないし100:50の混合物の焼結体から成る1
273K〜1473Kの温度範囲における耐酸化性が優
れている耐熱性材料の製造方法、を提供する。 That is, the present invention relates to a TiAl intermetallic compound.
Weight ratio of material powder to SiC powder 100: 0.5 to 1
1273K-14 consisting of a sintered body of a 00:50 mixture
Excellent oxidation resistance in the temperature range of 73K
Characteristic heat-resistant material, and ball milling TiAl
An intermetallic compound powder is formed and then 100
0.5 to 50 parts by weight of SiC powder with respect to parts by weight,
After pressure molding, under a pressure of 30 MPa or more, 1200 to 15
TiA characterized by sintering at a temperature of 00K
l Weight ratio of intermetallic compound powder to SiC powder 100:
1 consisting of a sintered body of a mixture of 0.5 to 100: 50
Excellent oxidation resistance in the temperature range of 273K to 1473K
A method for producing a heat-resistant material.
【0011】[0011]
【発明の実施の形態】本発明の耐熱性材料は、TiAl
金属間化合物のマトリックスに、SiC微粒子を分散さ
せたものであり、このSiCの量は、TiAl金属間化
合物100重量部に対し、0.5〜50重量部の範囲に
あることが必要である。この量が0.5重量部未満では
高温における耐酸化性の向上効果が十分に発揮されない
し、50重量部を超えるとTiAl金属間化合物として
の性質がそこなわれるおそれがある。TiAl金属間化
合物としての性質を十分に維持するとともに、高温にお
ける耐酸化性をより優れたものにするには、このSiC
の含有量は、TiAl金属間化合物100重量部に対
し、5〜30重量部の範囲にあるのが特に好ましい。DETAILED DESCRIPTION OF THE INVENTION The heat-resistant material of the present invention is TiAl
SiC fine particles are dispersed in a matrix of an intermetallic compound, and the amount of SiC needs to be in the range of 0.5 to 50 parts by weight based on 100 parts by weight of TiAl intermetallic compound. If the amount is less than 0.5 part by weight, the effect of improving oxidation resistance at high temperatures is not sufficiently exhibited, and if it exceeds 50 parts by weight, the properties as a TiAl intermetallic compound may be impaired. In order to sufficiently maintain the properties as a TiAl intermetallic compound and to improve the oxidation resistance at high temperatures, it is necessary to use SiC.
Is particularly preferably in the range of 5 to 30 parts by weight based on 100 parts by weight of the TiAl intermetallic compound.
【0012】TiAl金属間化合物の耐酸化性は、金属
チタンより良好であるが、1073K以上の高温におい
ては低下すること、そしてこの耐酸化性が低い原因の1
つとして、TiO2の成長が耐酸化性の優れたAl2O3
の成長より著しく速いことにあることが知られている。
TiO2の基本的な成長機構は、その中の酸素空孔を介
しての酸素の拡散であり、したがって、本発明のよう
に、SiCを添加するとTiO2中の酸素空孔濃度が減
少し、その成長速度が遅くなってAl2O3が形成されや
すくなり、その結果、耐酸化性が向上するものと考えら
れる。The oxidation resistance of the TiAl intermetallic compound is better than that of titanium metal, but decreases at a high temperature of 1073 K or higher. One of the causes of the low oxidation resistance is as follows.
First, the growth of TiO 2 is due to Al 2 O 3 having excellent oxidation resistance.
Is known to be significantly faster than the growth of
The basic growth mechanism of TiO 2 is the diffusion of oxygen through the oxygen vacancies therein, thus, as in the present invention, the addition of SiC reduces the oxygen vacancy concentration in TiO 2 , It is considered that the growth rate is slowed and Al 2 O 3 is easily formed, and as a result, oxidation resistance is improved.
【0013】本発明の耐熱性材料の製造方法に従えばま
ず、チタン粉末とアルミニウム粉末との等モル混合物を
用いてTiAl金属間化合物粉末を形成させる。この際
用いられるチタン粉末及びアルミニウム粉末の大きさに
ついては特に制限はないが通常平均粒径が10〜200
μmの範囲にあるものが用いられる。この粉末混合物を
用いてTiAl金属間化合物を形成させるには、例えば
メカニカルアロイング法を採用するのが有利であり、具
体的には、適当なミル容器内において、減圧下又は不活
性ガス雰囲気下に、前記粉末混合物のボールミリングを
行う。このミル容器については特に制限はなく、従来メ
カニカルアロイング法において慣用されているものを用
いることができるが、例えば高エネルギー撹拌ミルであ
るアトライターや量産のための大型化が容易な回転ボー
ルミルなどの使用が効率的で有利である。また、ボール
ミリングを減圧下で行う場合、圧力は、原料粉末の酸化
を防止するために50Pa以下、好ましくは20Pa以
下が望ましい。一方、不活性ガス雰囲気下で行う場合、
不活性ガスとしては、例えばアルゴンやヘリウム、ある
いはこれらに少量の窒素ガスを混入させたガスなどが好
ましく用いられる。According to the method for producing a heat-resistant material of the present invention, first, TiAl intermetallic compound powder is formed using an equimolar mixture of titanium powder and aluminum powder. The size of the titanium powder and the aluminum powder used at this time is not particularly limited, but usually has an average particle size of 10 to 200.
Those having a range of μm are used. In order to form a TiAl intermetallic compound using this powder mixture, it is advantageous to employ, for example, a mechanical alloying method. Specifically, in a suitable mill container, under reduced pressure or under an inert gas atmosphere. Next, ball milling of the powder mixture is performed. The mill container is not particularly limited, and those conventionally used in the mechanical alloying method can be used. Examples thereof include an attritor that is a high-energy stirring mill and a rotary ball mill that can be easily enlarged for mass production. Is efficient and advantageous. When the ball milling is performed under reduced pressure, the pressure is preferably 50 Pa or less, more preferably 20 Pa or less in order to prevent oxidation of the raw material powder. On the other hand, when performing in an inert gas atmosphere,
As the inert gas, for example, argon or helium, or a gas obtained by mixing a small amount of nitrogen gas with them is preferably used.
【0014】このようにして、十分にボールミリングを
行うことにより、通常平均粒径10〜70μm程度のT
iAl金属間化合物粉末が得られる。次に、この粉末1
00重量部に対し、SiC粉末0.5〜50重量部、好
ましくは5〜30重量部を配合したのち、所望形状に加
圧成形する。このSiC粉末としては、TiAl金属間
化合物のマトリックス中に均質に分散して、耐酸化性及
び耐クリープ性などに優れる耐熱性材料が得られ、かつ
経済性の点から、平均粒子径0.5〜20μmの範囲に
あるものが好適である。また、加圧成形法としては、例
えばプレス法、押出し法、等方圧縮成形法、スリップキ
ャスティング法、延伸加圧法、直接圧延法などがあり、
いずれも用いることができるが、これらの中で、通常プ
レス法が好ましく用いられる。By performing ball milling sufficiently in this manner, a T having an average particle size of about 10 to 70 μm is usually obtained.
An iAl intermetallic compound powder is obtained. Next, this powder 1
After mixing 0.5 to 50 parts by weight, preferably 5 to 30 parts by weight of SiC powder with respect to 00 parts by weight, the mixture is pressure-molded into a desired shape. As the SiC powder, a heat-resistant material having excellent oxidation resistance and creep resistance can be obtained by being homogeneously dispersed in a matrix of a TiAl intermetallic compound, and from the viewpoint of economy, an average particle size of 0.5 Those having a range of 2020 μm are preferred. Examples of the pressure molding method include, for example, a press method, an extrusion method, an isotropic compression molding method, a slip casting method, a stretching pressure method, a direct rolling method, and the like.
Any of them can be used, but among them, the press method is preferably used.
【0015】次に、このようにして得られた加圧成形体
を、30MPa以上の圧力下、1200〜1500Kの
温度において焼結し、所望の耐熱性材料を作製する。圧
力が30MPa未満や温度が1200Kより低い場合、
焼結が十分に行われず、所望の物性を有する焼結体が得
られないおそれがある。また、1500Kを超える高い
温度で焼結する必要はなく、それ以下の温度で焼結は十
分に進行し、1500Kを超えるとむしろ所望の物性を
有する焼結体が得られにくくなる。焼結装置については
特に制限はなく、従来TiAl金属間化合物焼結体の製
造に慣用されている装置を用いることができるが、例え
ば放電プラズマ焼結装置の使用が効率的で有利である。Next, the thus obtained pressure-formed body is sintered at a temperature of 1200 to 1500 K under a pressure of 30 MPa or more to produce a desired heat-resistant material. When the pressure is lower than 30 MPa or the temperature is lower than 1200 K,
Sintering may not be performed sufficiently, and a sintered body having desired physical properties may not be obtained. Further, it is not necessary to perform sintering at a high temperature exceeding 1500K, and sintering proceeds sufficiently at a temperature lower than 1500K, and when it exceeds 1500K, it becomes difficult to obtain a sintered body having desired physical properties. The sintering apparatus is not particularly limited, and an apparatus conventionally used for producing a TiAl intermetallic compound sintered body can be used. For example, a discharge plasma sintering apparatus is efficient and advantageous.
【0016】[0016]
【発明の効果】本発明の耐熱性材料は、TiAl金属間
化合物のマトリックス中にSiC微粒子が均質に分散し
たものであって、軽量で、かつ耐熱性に優れるととも
に、高温における耐酸化性が良好であり、比強度の高い
軽量耐熱性材料として航空機などに好適に用いられる。The heat-resistant material of the present invention is obtained by uniformly dispersing SiC fine particles in a matrix of a TiAl intermetallic compound, is lightweight, has excellent heat resistance, and has good oxidation resistance at high temperatures. It is suitably used for aircraft and the like as a lightweight heat-resistant material having high specific strength.
【0017】[0017]
【実施例】次に、本発明を実施例によりさらに詳細に説
明するが、本発明は、これらの例によってなんら限定さ
れるものではない。EXAMPLES Next, the present invention will be described in more detail with reference to examples, but the present invention is not limited to these examples.
【0018】実施例 チタン粉末(純度99.9%、粒子径150μm以下)
とアルミニウム粉末(純度99.9%、粒子径150μ
m以下)をモル比1:1になるように配合した粉末82
2gを、内径300mm、内側長さ350mmのステン
レス鋼(SUS304)製円筒型ミル容器に、直径1
2.7mmのボールベアリング用の鋼球(SUJ−2)
41.1kgと共に充てんして密封した。この際、ボー
ル充てん量はミル容器内容積に対して33%、粉末/ボ
ール重量比は1/50であった。Example Titanium powder (purity 99.9%, particle size 150 μm or less)
And aluminum powder (purity 99.9%, particle size 150μ)
m or less) in a molar ratio of 1: 1.
2 g was placed in a stainless steel (SUS304) cylindrical mill container having an inner diameter of 300 mm and an inner length of 350 mm in a diameter of 1 mm.
2.7mm ball for ball bearing (SUJ-2)
Filled with 41.1 kg and sealed. At this time, the ball filling amount was 33% based on the volume in the mill container, and the powder / ball weight ratio was 1/50.
【0019】次いで、ミル容器をロータリーポンプで排
気後、高純度アルゴンガスを導入し、回転速度7.43
rad/秒(71.0rpm)にて転動ボールミリング
を400時間行ったのち、粉末をミル容器内壁とボール
表面に付着して回収できないものを除いて全量回収し
た。回収した粉末は、未反応の粗大な粒子を取り除くた
め、目開き75μmのJIS標準ふるいを用いてふるい
分けし、TiAl金属間化合物粉末(ふるい通過分)を
得た。Next, after the mill container was evacuated with a rotary pump, high-purity argon gas was introduced, and the rotation speed was 7.43.
After rolling ball milling was performed at rad / sec (71.0 rpm) for 400 hours, the entire amount of the powder was recovered except for those that could not be recovered by adhering to the inner wall of the mill container and the ball surface. The recovered powder was sieved using a JIS standard sieve having a mesh size of 75 μm to remove unreacted coarse particles to obtain a TiAl intermetallic compound powder (sieve passing amount).
【0020】次に、このTiAl金属間化合物粉末10
0重量部に対し、SiC粉末(純度99%以上、粒子径
2〜3μm)を0.5、10及び15重量部の割合で、
それぞれ配合し、各混合粉末を遠心式ボールミル(FR
ISCH,P−6)によりアルゴンガス中で次のように
してミリングを行った。すなわち、各混合粉末を、それ
ぞれ直径20.0mmのタングステン−カーバイド製ミ
リングボール5個と共に、容量80mlのタングステン
−カーバイド製円筒型ミル容器に入れ、アルゴンガス中
にてミリングを行った。この際ボールと粉末の重量比は
1/11.7であった。Next, the TiAl intermetallic compound powder 10
With respect to 0 parts by weight, SiC powder (purity: 99% or more, particle diameter: 2 to 3 μm) was added in a ratio of 0.5, 10 and 15 parts by weight
Each mixed powder is mixed with a centrifugal ball mill (FR
Milling was performed as follows in an argon gas according to ISCH, P-6). That is, each mixed powder was put together with five tungsten-carbide milling balls each having a diameter of 20.0 mm in a tungsten-carbide cylindrical mill container having a capacity of 80 ml, and milled in argon gas. At this time, the weight ratio between the ball and the powder was 1 / 11.7.
【0021】3時間ミリングを行ったのち、粉末をボー
ルとミル容器に付着し、回収できないものを除いて全量
回収した。次いで、この粉末を内径20mmのカーボン
製モールドに充てんし、40MPaの圧力で予備成形し
たのち、放電プラズマ焼結装置[住友石炭鉱業(株)
製,SPS−1020]により、圧力56MPa、温度
1323〜1373Kの条件で焼結した。After milling for 3 hours, the powder was adhered to a ball and a mill container, and all powder was recovered except for those that could not be recovered. Next, the powder is filled in a carbon mold having an inner diameter of 20 mm, and is preformed at a pressure of 40 MPa. Then, a discharge plasma sintering apparatus [Sumitomo Coal Mining Co., Ltd.]
Manufactured by SPS-1020] at a pressure of 56 MPa and a temperature of 1323 to 1373K.
【0022】このようにして得られた焼結体について、
X線回折による相の同定、走査型電子顕微鏡(Scan
ning Electron Microscorp
e:SEM)とEDS(Energy Dispers
ive X−ray Spectrometer)によ
る微細組織、酸化物の成分と分布などの観察を行い、さ
らに熱重量分析装置(Thermogravimetr
ic analysis:TGA)を用いて、大気中、
1373Kと1473K温度において、連続的に60時
間高温酸化試験を行った。With respect to the sintered body thus obtained,
Phase identification by X-ray diffraction, scanning electron microscope (Scan)
Ning Electron Microcorp
e: SEM) and EDS (Energy Dispers)
The microstructure, the composition and distribution of oxides, and the like were observed by an X-ray spectrometer, and a thermogravimetric analyzer (Thermogravimeter)
ic analysis (TGA), in air,
At 1373K and 1473K temperatures, high temperature oxidation tests were performed continuously for 60 hours.
【0023】図1は、TiAlに対し、SiC 15重
量%を添加した焼結体の大気中酸化試験において、加熱
温度が1373Kの場合(実線)と1473Kの場合
(破線)の加熱時間と重量増加との関係を示すグラフで
ある。FIG. 1 shows the heating time and weight increase when the heating temperature was 1373K (solid line) and 1473K (dashed line) in the atmospheric oxidation test of a sintered body in which 15% by weight of SiC was added to TiAl. 6 is a graph showing a relationship with the graph.
【0024】図1から、酸化による重量増加は加熱時間
の増大とともにわずかに増加したのち、飽和する傾向を
示すことが分かる。長時間大気中に曝しても酸化による
重量増加が小さいことはSiCの添加により、試料表面
に耐酸化性に優れたAl2O3皮膜が均一に形成され耐酸
化性が向上するものと推測される。この耐酸化性の向上
はAl2O3がチタンの酸化を抑制する一種のバリアーの
役割と、酸素に対する大きな表面積をもつことによる保
護性酸化皮膜の生成を促進させることによるものと考え
られる。From FIG. 1, it can be seen that the weight increase due to the oxidation slightly increases with the increase of the heating time and then tends to saturate. The small increase in weight due to oxidation even when exposed to the air for a long time is presumed to be due to the fact that the addition of SiC forms an Al 2 O 3 film with excellent oxidation resistance uniformly on the sample surface and improves the oxidation resistance. You. It is considered that this improvement in oxidation resistance is due to the role of Al 2 O 3 as a kind of barrier for suppressing the oxidation of titanium and the promotion of the formation of a protective oxide film due to its large surface area against oxygen.
【0025】比較例 実施例と同様にしてTiAl金属間化合物粉末を得た
後、この粉末を、SiC粉末を添加することなく、その
まま実施例と同様にして予備成形後、焼結し、TiAl
金属間化合物焼結体を製造した。Comparative Example After obtaining a TiAl intermetallic compound powder in the same manner as in the example, this powder was preformed as it was in the same manner as in the example without adding SiC powder, and then sintered.
An intermetallic compound sintered body was manufactured.
【0026】次に、このTiAl金属間化合物焼結体に
ついて、熱重量分析装置を用い、大気中、1273Kの
温度において、連続的に60時間高温酸化試験を行っ
た。図2は、TiAl焼結体の大気中酸化試験(127
3K)における、加熱時間と重量増加との関係を示すグ
ラフである。この図2から、加熱時間の増大に伴って、
酸化による重量増加が著しく起こることが分かる。Next, the TiAl intermetallic compound sintered body was subjected to a high-temperature oxidation test continuously at a temperature of 1273 K in the atmosphere for 60 hours using a thermogravimetric analyzer. FIG. 2 shows an atmospheric oxidation test of a TiAl sintered body (127
It is a graph in 3K) which shows the relationship between heating time and weight increase. From FIG. 2, as the heating time increases,
It can be seen that the weight increase due to oxidation significantly occurs.
【0027】このように、TiAl金属間化合物の耐酸
化性が悪い原因の1つは、TiO2の成長がAl2O3の
成長より極めて速いことにある。TiO2の基本的な成
長機構は、その中の酸素空孔を介しての酸素の拡散であ
るので、原子価制御の原理を適用してチタンより価数の
大きい元素をドーピングすればTiO2中の酸素空孔濃
度が減少し、その成長速度が小さくなることが期待で
き、Al2O3層ができやすくなると考えられる。したが
って、このような考えに基づき、実施例のようにSiC
を添加することにより、均一なAl2O3層を形成させ、
耐酸化性を向上させることができた。As described above, one of the causes of the poor oxidation resistance of the TiAl intermetallic compound is that the growth of TiO 2 is much faster than the growth of Al 2 O 3 . The basic growth mechanism of the TiO 2 is because it is the diffusion of oxygen through the oxygen vacancies therein, by applying the principle of valence control of TiO 2 when doping the valence of larger elements of titanium It can be expected that the concentration of oxygen vacancies in the Al 2 O 3 layer will decrease, and that the growth rate will decrease. Therefore, based on such an idea, the SiC
To form a uniform Al 2 O 3 layer,
Oxidation resistance could be improved.
【図1】 本発明の耐熱性材料の1例における大気中で
の加熱時間と重量増加との関係を示すグラフ。FIG. 1 is a graph showing the relationship between heating time in air and weight increase in one example of the heat-resistant material of the present invention.
【図2】 TiAl金属間化合物の1例における大気中
での加熱時間と重量増加との関係を示すグラフ。FIG. 2 is a graph showing the relationship between heating time in air and weight increase in one example of a TiAl intermetallic compound.
Claims (2)
との重量比100:0.5ないし100:50の混合物
の焼結体から成る1273K〜1473Kの温度範囲に
おける耐酸化性が優れていることを特徴とする耐熱性材
料。1. An excellent oxidation resistance in a temperature range of 1273K to 1473K which is a sintered body of a mixture of TiAl intermetallic compound powder and SiC powder in a weight ratio of 100: 0.5 to 100: 50. Characterized heat resistant material.
ル混合物を用い、減圧下又はアルゴンやヘリウム若しく
はこれらに少量の窒素ガスを混入させた不活性ガス雰囲
気下でボールミリンしてTiAl金属間化合物粉末を形
成させ、次いでこの粉末100重量部に対し、SiC粉
末0.5〜50重量部を配合し、加圧成形後、30MP
a以上の圧力下、1200〜1500Kの温度において
焼結することを特徴とするTiAl金属間化合物粉末と
SiC粉末との重量比100:0.5ないし100:5
0の混合物の焼結体から成る1273K〜1473Kの
温度範囲における耐酸化性が優れている耐熱性材料の製
造方法。 2. An isomorph of titanium powder and aluminum powder.
Mixture under reduced pressure or argon or helium
Is an inert gas atmosphere mixed with a small amount of nitrogen gas.
Ball milling under air to form TiAl intermetallic compound powder
Then, 100 parts by weight of this powder was mixed with SiC powder.
0.5 to 50 parts by weight of powder, and after pressure molding, 30MP
a at a pressure of 1200 to 1500K
TiAl intermetallic compound powder characterized by being sintered
Weight ratio to SiC powder: 100: 0.5 to 100: 5
1273K-1473K consisting of a sintered body of a mixture of
Production of heat-resistant materials with excellent oxidation resistance in the temperature range
Construction method.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8103904A JP2952341B2 (en) | 1996-03-29 | 1996-03-29 | Heat resistant material and method for producing the same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8103904A JP2952341B2 (en) | 1996-03-29 | 1996-03-29 | Heat resistant material and method for producing the same |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH09268336A JPH09268336A (en) | 1997-10-14 |
| JP2952341B2 true JP2952341B2 (en) | 1999-09-27 |
Family
ID=14366421
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP8103904A Expired - Lifetime JP2952341B2 (en) | 1996-03-29 | 1996-03-29 | Heat resistant material and method for producing the same |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2952341B2 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108277374A (en) * | 2018-02-09 | 2018-07-13 | 兰州理工大学 | A kind of Al-Ti-C-Y composite crystal grain fining agents, alloy and preparation method thereof |
| CN117535562A (en) * | 2023-11-15 | 2024-02-09 | 江苏浩景智能制造科技有限公司 | TiAl porous composite material, preparation method and application |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH01129938A (en) * | 1987-11-16 | 1989-05-23 | Mitsubishi Heavy Ind Ltd | Composite material and its manufacture |
| JPH0578762A (en) * | 1991-05-23 | 1993-03-30 | Sumitomo Light Metal Ind Ltd | Tial-based composite material having excellent strength and its production |
| JPH0790414A (en) * | 1993-09-20 | 1995-04-04 | Sumitomo Light Metal Ind Ltd | Ti-Al intermetallic compound intake / exhaust valve having excellent wear resistance and method of manufacturing the same |
-
1996
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