JPH0361743B2 - - Google Patents

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Publication number
JPH0361743B2
JPH0361743B2 JP61269464A JP26946486A JPH0361743B2 JP H0361743 B2 JPH0361743 B2 JP H0361743B2 JP 61269464 A JP61269464 A JP 61269464A JP 26946486 A JP26946486 A JP 26946486A JP H0361743 B2 JPH0361743 B2 JP H0361743B2
Authority
JP
Japan
Prior art keywords
less
alloy
ductility
tial
alloys
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
Application number
JP61269464A
Other languages
Japanese (ja)
Other versions
JPS63125634A (en
Inventor
Yukio Nishama
Takuya Myashita
Toshiharu Noda
Susumu Isobe
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Daido Steel Co Ltd
Kawasaki Motors Ltd
Original Assignee
Daido Steel Co Ltd
Kawasaki Jukogyo KK
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Daido Steel Co Ltd, Kawasaki Jukogyo KK filed Critical Daido Steel Co Ltd
Priority to JP26946486A priority Critical patent/JPS63125634A/en
Priority to US07/120,070 priority patent/US4849168A/en
Priority to DE8787116728T priority patent/DE3781394T2/en
Priority to EP87116728A priority patent/EP0275391B1/en
Publication of JPS63125634A publication Critical patent/JPS63125634A/en
Publication of JPH0361743B2 publication Critical patent/JPH0361743B2/ja
Granted legal-status Critical Current

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  • Powder Metallurgy (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

発明の目的 purpose of invention

【産業上の利用分野】[Industrial application field]

本発明は、Ti−Al系合金、とくに金属間化合
物TiAlを主要構成相とする合合金の改良に関す
る。
The present invention relates to the improvement of Ti-Al alloys, particularly alloys containing the intermetallic compound TiAl as a main constituent phase.

【従来技術】[Prior art]

たとえばタービンブレードやエンジンバルブの
ように、回転または往復運動をする部品は、高性
能化すなわち高応答性および高出力の要請を受け
て、ますます軽量化される傾向にある。従つて、
これらの部品に使用する耐熱材料は、単なる強度
でなく比強度(強度/密度)が重要視され、その
向上に努力が注がれている。 このような状況の中で、Ti−Al系合金、とく
に金属間化合物TiAlを主要構成相とするものが
注目されている。TiAlは耐用温度(応力28.1Kg
f/mm2でクリープ破断寿命が1000時間に相当する
温度)が800℃であつて常用のTi合金(Ti−6Al
−4V)の550℃を上回り、しかも比重は3.8であ
つてTi合金の4.5よりはセラミツクス(gi3N4)の
3.2に近く、セラミツクスにはない加工性を有す
る上に、比強度はNi超合金(Inconel 713C)の
それを上回る。 とはいえ、TiAlを主要構成相とするTi−Al系
合金は、Ti合金やNi基超合金にくらべて延性が
低く、塑性加工が困難であるという弱点をもつ。
そこで、延性を改善する努力がなされている(た
とえば特開昭56−4344号は適量のVの添加を開示
している)が、未だ実用化には至つていない。
For example, components that rotate or reciprocate, such as turbine blades and engine valves, are becoming increasingly lightweight in response to demands for higher performance, ie, higher response and higher output. Therefore,
For the heat-resistant materials used in these parts, not just strength but specific strength (strength/density) is important, and efforts are being made to improve it. Under these circumstances, Ti--Al alloys, particularly those containing the intermetallic compound TiAl as a main constituent phase, are attracting attention. TiAl can withstand temperature (stress 28.1Kg
The temperature at which creep rupture life corresponds to 1000 hours at f/mm 2 ) is 800℃, and the commonly used Ti alloy (Ti-6Al
-4V) at 550℃, and the specific gravity is 3.8, which is higher than that of ceramics (gi 3 N 4 ) than 4.5 of Ti alloy.
3.2, it has workability not found in ceramics, and its specific strength exceeds that of Ni superalloy (Inconel 713C). However, Ti-Al alloys containing TiAl as the main constituent phase have the disadvantage that they have lower ductility than Ti alloys and Ni-based superalloys, and are difficult to plastically work.
Therefore, efforts have been made to improve the ductility (for example, JP-A-56-4344 discloses the addition of an appropriate amount of V), but this has not yet been put to practical use.

【発明が解決しようとする問題点】[Problems to be solved by the invention]

本発明は、上記した問題のひとつの解決策を提
案しようとの意図にもとづくものであつて、その
目的は、金属間化合物TiAlを主要構成相とする
Ti−Al系合金の延性を高めて、塑性加工を容易
にした軽量耐熱合金を提供することにある。 発余の構成
The present invention is based on the intention of proposing a solution to one of the above-mentioned problems, and its purpose is to use an intermetallic compound TiAl as the main constituent phase.
The object of the present invention is to provide a lightweight heat-resistant alloy that is easy to plastically work by increasing the ductility of a Ti-Al alloy. Composition of aftermath

【問題点を解決するための手段】[Means to solve the problem]

本発明の延性を改善した溶製材用Ti−Al系耐
熱合金は、Al:32〜38%に加えてB:0.005%〜
0.20%をを含有し、残部が不可避の不純物および
Tiからなる組成を有する。 好ましくは、上記の合金成分に対して、C:
0.2%以下、O:0.3%以下、N0.3%以下の1種ま
たは2種以上を有意な量、ただしO+N:0.4%
以下であるように添加し含有させる。 本発明のTi−Al系合金から所望の構成部品を
製造する手段としては、鋳造はもとより、鍜造も
採用できる。
The Ti-Al heat-resistant alloy for ingot material with improved ductility of the present invention has Al: 32 to 38% and B: 0.005% to
Contains 0.20%, the balance is unavoidable impurities and
It has a composition consisting of Ti. Preferably, for the above alloy components, C:
Significant amounts of one or more of the following: 0.2% or less, O: 0.3% or less, N0.3% or less, but O + N: 0.4%
It is added and contained as follows. As a means of manufacturing desired components from the Ti-Al alloy of the present invention, not only casting but also forging can be employed.

【作 用】[Effect]

本発明のTi−Al系合金において上記の成分組
成を選択した理由は、つぎのとおりである。 Al:32〜38% 金属間化合物Ti−Al(γ用)を与える化学量
論組成はTi−36%Alであつて、Ti−Al二元
合金においてTiAlが単相で存在するのは、
Al:34〜42%の範囲である。しかし、Alが
38%を超えると延性が低下して目的に反する
ので、これを上限とする。一方、34%より
Alが少ないTiリツチの組成になるとTi3Al
(α2相)が生成し、この化合物は微量であれ
ば延性の向上に役立つ。Ti3Alそれ自体は脆
いため、多量になると脆化が起るので、32%
を下限にえらんだ。 B:0.005〜0.20% BはTiAlの化合物の粒界を強化し、延性を
高めるとともに結晶粒を微細化して、強度の
向上にも寄与する。この効果は、0.005%と
いう少量の添加で得られる。一方、多量にな
ると脆いホウ化物の生成を招いて延性が低下
するので、0.20%の上限を定めた。 C:0.20%以下 CはTiと炭化物TiC形成し、合金の強度を高
める。その効果は次第に飽和し、かつ多量の
TiCは脆化の原因となるので、0.2%を上限
とした。 O:0.3%以下、N:0.3%以下、ただし O+N:0.4%以下 OもNも、TiAlに固溶してこれを強化する。
しかし、固溶量が上記の限界を超えると延性
が低下する。 〔実施例〕 表に示す組成のTi−Al系合金を溶製した。 溶解は、Arガス雰囲気でプラズマアークを熱
源とし、水冷銅ルツボをそなえたスカル炉を用い
て実施した。No.1〜5は第一の発明、No.6〜8は
第二の発明、そしてNo.9〜11は、比較のため挙げ
た既知の技術に従う例である。。 合金のインゴツトから試験片を切り出して、
900℃における引張試験を行なつた。結果を、表
にあわせて示す。それによれば、本発明の合金が
改善された延性を有することが明らかである。 No.2の合金については、1150℃において30%ま
たは50%の据込み加工を行行つた。 アプセツト量50%においても、試験片の表面に
ワレは認められなかつた。
The reason for selecting the above-mentioned composition in the Ti-Al alloy of the present invention is as follows. Al: 32-38% The stoichiometric composition that gives the intermetallic compound Ti-Al (for γ) is Ti-36% Al, and the reason why TiAl exists as a single phase in the Ti-Al binary alloy is because
Al: ranges from 34 to 42%. However, Al
If it exceeds 38%, the ductility decreases and defeats the purpose, so this is set as the upper limit. On the other hand, 34%
When the composition becomes Ti-rich with less Al, Ti 3 Al
( α2 phase) is formed, and this compound helps improve ductility in small amounts. Since Ti 3 Al itself is brittle, embrittlement will occur if the amount is large, so 32%
was chosen as the lower limit. B: 0.005 to 0.20% B strengthens the grain boundaries of the TiAl compound, increases ductility, and refines crystal grains, contributing to improved strength. This effect can be obtained by adding as little as 0.005%. On the other hand, if the amount is too large, brittle borides are formed and ductility is reduced, so an upper limit of 0.20% was set. C: 0.20% or less C forms carbide TiC with Ti and increases the strength of the alloy. The effect gradually becomes saturated and a large amount of
Since TiC causes embrittlement, the upper limit was set at 0.2%. O: 0.3% or less, N: 0.3% or less, however, O+N: 0.4% or less. Both O and N are dissolved in TiAl to strengthen it.
However, when the amount of solid solution exceeds the above limit, ductility decreases. [Example] A Ti-Al alloy having the composition shown in the table was melted. Melting was carried out in an Ar gas atmosphere using a plasma arc as a heat source and a skull furnace equipped with a water-cooled copper crucible. Nos. 1 to 5 are examples of the first invention, Nos. 6 to 8 are examples of the second invention, and Nos. 9 to 11 are examples according to known techniques cited for comparison. . Cut out a test piece from an alloy ingot,
A tensile test was conducted at 900°C. The results are also shown in the table. Thereby, it is clear that the alloys of the present invention have improved ductility. Alloy No. 2 was subjected to 30% or 50% upsetting at 1150°C. Even with an upset amount of 50%, no cracks were observed on the surface of the test piece.

【表】【table】

【表】 発明の効果 本発明により、高い耐熱性と比強度を有する
Ti−Al系合金の延性が高められ、塑性加工が容
易になつた。従つて、種々の回転系または往復動
系の機械部品、たとえば航空機用ジエツトエンジ
ンや産業用ガスタービンのブレード、単車または
自動車エンジンの吸気排気弁、ロツカーアーム、
コンロツド、ターボホイールなどが容易に製造で
きる。 塑性加工が容易であるということは、加工の困
難さがひきおこしていた製品の信頼性の問題を
も、著しく軽減することになる。
[Table] Effects of the invention The present invention has high heat resistance and specific strength.
The ductility of Ti-Al alloys has been increased, making plastic working easier. Therefore, various rotating or reciprocating mechanical parts, such as blades of aircraft jet engines and industrial gas turbines, intake and exhaust valves of motorcycle or automobile engines, rocker arms,
Conrods, turbo wheels, etc. can be manufactured easily. The ease of plastic working also significantly reduces the reliability problems of products caused by difficult working.

Claims (1)

【特許請求の範囲】 1 Al:32〜38%に加えてB:0.005〜0.20%を
含有し、残部が実質的にTiからなる溶製材用Ti
−Al系耐熱合金。 2 Al:32〜38%に加えてB:0.005〜0.2%を含
有し、さらにC:0.2%以下、O:0.3%以下、
N:0.3%以下の1種または2種以上を、有意な
量、ただしO+N:0.4%以下であるように添加
することにより含有し、残部が実質的にTiから
なる溶製材用Ti−Al系耐熱合金。
[Scope of Claims] 1. A Ti for ingot lumber containing 0.005 to 0.20% of B in addition to 32 to 38% of Al, with the remainder being substantially Ti.
-Al-based heat-resistant alloy. 2 Contains B: 0.005 to 0.2% in addition to Al: 32 to 38%, further C: 0.2% or less, O: 0.3% or less,
A Ti-Al system for melt-molded materials containing one or more N: 0.3% or less by adding a significant amount, but O + N: 0.4% or less, and the remainder substantially consisting of Ti. Heat resistant alloy.
JP26946486A 1986-11-12 1986-11-12 Ti-al alloy Granted JPS63125634A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP26946486A JPS63125634A (en) 1986-11-12 1986-11-12 Ti-al alloy
US07/120,070 US4849168A (en) 1986-11-12 1987-11-12 Ti-Al intermetallics containing boron for enhanced ductility
DE8787116728T DE3781394T2 (en) 1986-11-12 1987-11-12 TITAN ALUMINUM ALLOY.
EP87116728A EP0275391B1 (en) 1986-11-12 1987-11-12 Titanium-aluminium alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP26946486A JPS63125634A (en) 1986-11-12 1986-11-12 Ti-al alloy

Publications (2)

Publication Number Publication Date
JPS63125634A JPS63125634A (en) 1988-05-28
JPH0361743B2 true JPH0361743B2 (en) 1991-09-20

Family

ID=17472800

Family Applications (1)

Application Number Title Priority Date Filing Date
JP26946486A Granted JPS63125634A (en) 1986-11-12 1986-11-12 Ti-al alloy

Country Status (1)

Country Link
JP (1) JPS63125634A (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0261017A (en) * 1988-08-27 1990-03-01 Yakichirou Shiozaki Titanium-aluminum alloy
JP2960068B2 (en) * 1988-10-05 1999-10-06 大同特殊鋼株式会社 TiAl-Ti (3) Al-based composite material
JPH0818151B2 (en) 1988-11-11 1996-02-28 大同特殊鋼株式会社 Joining method and joining part of Ti-Al alloy and structural steel
US5252150A (en) * 1990-05-18 1993-10-12 Toyota Jidosha Kabushiki Kaishi Process for producing nitrogen containing Ti--Al alloy
JP3006120B2 (en) * 1990-05-18 2000-02-07 トヨタ自動車株式会社 Ti-Al alloy and method for producing the same
US5370839A (en) * 1991-07-05 1994-12-06 Nippon Steel Corporation Tial-based intermetallic compound alloys having superplasticity

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6270531A (en) * 1985-09-24 1987-04-01 Sumitomo Light Metal Ind Ltd Formation of ti-al intermetallic compound member
JPH0735554B2 (en) * 1986-10-31 1995-04-19 大同特殊鋼株式会社 Ti-Al based alloy for powder metallurgy

Also Published As

Publication number Publication date
JPS63125634A (en) 1988-05-28

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