JPH0372058A - Structural member made of titanium or titanium alloy - Google Patents
Structural member made of titanium or titanium alloyInfo
- Publication number
- JPH0372058A JPH0372058A JP20945489A JP20945489A JPH0372058A JP H0372058 A JPH0372058 A JP H0372058A JP 20945489 A JP20945489 A JP 20945489A JP 20945489 A JP20945489 A JP 20945489A JP H0372058 A JPH0372058 A JP H0372058A
- Authority
- JP
- Japan
- Prior art keywords
- surface layer
- layer part
- titanium
- structural member
- stabilizing element
- 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
- 229910001069 Ti alloy Inorganic materials 0.000 title claims abstract description 17
- 239000010936 titanium Substances 0.000 title claims abstract description 11
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 title claims abstract description 10
- 229910052719 titanium Inorganic materials 0.000 title claims abstract description 10
- 239000002344 surface layer Substances 0.000 claims abstract description 29
- 239000006104 solid solution Substances 0.000 claims abstract description 14
- 238000002844 melting Methods 0.000 claims abstract description 11
- 230000008018 melting Effects 0.000 claims abstract description 11
- 238000005275 alloying Methods 0.000 claims abstract description 10
- 230000000087 stabilizing effect Effects 0.000 claims description 12
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 239000002184 metal Substances 0.000 claims description 8
- 229910052804 chromium Inorganic materials 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 229910052748 manganese Inorganic materials 0.000 claims description 3
- 229910052750 molybdenum Inorganic materials 0.000 claims description 3
- 229910052759 nickel Inorganic materials 0.000 claims description 3
- 229910052720 vanadium Inorganic materials 0.000 claims description 2
- 238000002485 combustion reaction Methods 0.000 claims 1
- 239000000463 material Substances 0.000 abstract description 10
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 abstract description 8
- 229910002092 carbon dioxide Inorganic materials 0.000 abstract description 4
- 239000001569 carbon dioxide Substances 0.000 abstract description 4
- 239000003381 stabilizer Substances 0.000 abstract 2
- 239000000853 adhesive Substances 0.000 abstract 1
- 230000001070 adhesive effect Effects 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 9
- 239000000843 powder Substances 0.000 description 9
- 238000000034 method Methods 0.000 description 6
- 239000000203 mixture Substances 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 239000007789 gas Substances 0.000 description 3
- 239000000956 alloy Substances 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000010309 melting process Methods 0.000 description 2
- 238000004881 precipitation hardening Methods 0.000 description 2
- 238000007712 rapid solidification Methods 0.000 description 2
- 101100136092 Drosophila melanogaster peng gene Proteins 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Landscapes
- Valve-Gear Or Valve Arrangements (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Abstract
Description
【発明の詳細な説明】 A1発明の目的 (1) 産業上の利用分野 本発明はチタンまたはチタン合金製構造部材に関する。[Detailed description of the invention] A1 Purpose of the invention (1) Industrial application field The present invention relates to structural members made of titanium or titanium alloys.
(2)従来の技術
従来、この種構造部材として、その部材の摺動特性要求
部位を、金属組織が単一のβ相である溶製β型チタン合
金より構成したものが知られている(特開昭61−24
7806号公報参照)。(2) Prior Art Conventionally, as this type of structural member, there has been known a structural member in which the parts requiring sliding properties are made of a molten β-type titanium alloy whose metal structure is a single β phase ( Japanese Unexamined Patent Publication No. 61-24
(See Publication No. 7806).
(3)発明が解決しようとする課題
しかしながら、前記溶製β型チタン合金は、溶製α型お
よびα+β型チタン合金に比べて多少摺動特性が向上す
るもの\、高速、且つ高面圧下で使用される構造部材の
要求摺動特性を満たすことはできない。(3) Problems to be Solved by the Invention However, the forged β-type titanium alloy has somewhat improved sliding properties compared to the ingot-produced α-type and α+β-type titanium alloys. It is not possible to satisfy the required sliding characteristics of the structural members used.
本発明は前記に鑑み、金属組織を改質して、優れた摺動
特性および強度を持つ表層部を備えた前記チタンまたは
チタン合金製構造部材を提供することを目的とする。In view of the above, an object of the present invention is to provide a titanium or titanium alloy structural member having a surface layer portion having excellent sliding properties and strength by modifying the metal structure.
B1発明の構成
(1)課題を解決するための手段
本発明に係るチタンまたはチタン合金製構造部材は、高
密度エネルギ源を用いた局所熔融合金化処理により改質
された表層部を備え、前記表層部の金属組織は、全率固
溶型β安定化元素を含有する第1のβ相と、共析型β安
定化元素を含有する第2のβ相との二相を混在させて構
成されることを特徴とする。B1 Structure of the Invention (1) Means for Solving the Problems The titanium or titanium alloy structural member according to the present invention includes a surface layer portion modified by a local melting process using a high-density energy source. The metallographic structure of the surface layer is composed of a mixture of two phases: a first β phase containing a total solid solution β stabilizing element and a second β phase containing a eutectoid β stabilizing element. It is characterized by being
(2)作 用
前記局所溶融合金化処理を通用すると、溶融径自己冷却
による急速凝固作用が得られるので、表層部の金属組織
が微細で、且つ均質となり、また表層部は二種のβ相の
混在組織となっているので、その表層部の摺動特性が大
幅に向上する。これにより表層部は高速、且つ高面圧下
においても優れた耐久性を示し、また強度も高い。(2) Effect When the above-mentioned local melting alloying process is applied, a rapid solidification effect due to self-cooling of the melt diameter is obtained, so the metal structure in the surface layer becomes fine and homogeneous, and the surface layer has two types of β phases. Since it has a mixed structure, the sliding properties of the surface layer are greatly improved. As a result, the surface layer exhibits excellent durability even at high speeds and under high surface pressure, and also has high strength.
その上、前記局所溶融合金化処理による表層部は、母材
としてのチタンまたはチタン合金に対する密着力が強く
、高速、且つ高面圧下での摺動に際し、剥離するような
ことはない。Moreover, the surface layer formed by the local melting alloying treatment has strong adhesion to titanium or a titanium alloy as a base material, and does not peel off when sliding at high speed and under high surface pressure.
(3)実施例
第1図はチタン合金製構造部材としてのロッカアーム1
を示す、ロッカアーム1は内燃機関用動弁機構に用いら
れるもので、その一端部にカムと摺擦するスリッパ面2
を有する。(3) Example Figure 1 shows a rocker arm 1 as a titanium alloy structural member.
The rocker arm 1 shown in FIG.
has.
ロッカアーム1の製造に当っては、Tt−6Af−4V
の組成を有するα+β型チタン合金製素材が用いられ、
スリッパ面2を構成する表層部3は、素材に高密度エネ
ルギ源を用いた局所溶融合金化処理を施して改質された
ものである。When manufacturing rocker arm 1, Tt-6Af-4V
An α+β type titanium alloy material having the composition is used,
The surface layer 3 forming the slipper surface 2 is modified by subjecting the material to a local melting process using a high-density energy source.
表層部3の金属組織は、全率固溶型β安定化元素を含有
する第1のβ相と、共析型β安定化元素を含有する第2
のβ相との二相を混在させて構成される。The metal structure of the surface layer 3 consists of a first β phase containing a total solid solution type β stabilizing element and a second phase containing a eutectoid β stabilizing element.
It is composed of a mixture of two phases: the β phase and the β phase.
全率固溶型β安定化元素としては、MOおよびVの少な
くとも一種が該当する。また共析型β安定化元素として
は、Fe、Cr、Mn、、CoおよびNiから選択され
る少なくとも一種が該当する。At least one of MO and V is applicable as the total solid solution β stabilizing element. The eutectoid β-stabilizing element is at least one selected from Fe, Cr, Mn, Co, and Ni.
全率固溶型β安定化元素は、母材である前記α+β型チ
タン合金と全率固溶体をつくる。この元素を10重量%
以上含有させることによって、第1のβ相を室温まで持
ちきたすことができる。また、この元素は第1のβ相の
摺動特性および耐熱性を向上させる効果を有する。The total solid solution type β stabilizing element forms a total solid solution with the α+β type titanium alloy that is the base material. 10% by weight of this element
By containing the above amount, the first β phase can be brought to room temperature. Furthermore, this element has the effect of improving the sliding properties and heat resistance of the first β phase.
これらの効果を得るためのMOおよび■の具体的含有量
はMoの場合は10重量%以上、またVの場合は14.
9重量%である。In order to obtain these effects, the specific content of MO and (2) is 10% by weight or more in the case of Mo, and 14% in the case of V.
It is 9% by weight.
た\し、全率固溶型β安定化元素の単独添加では、第1
のβ相の硬さが低く、十分な耐摩耗性が得られない。However, when the total solid solution β stabilizing element is added alone, the first
The hardness of the β phase is low, and sufficient wear resistance cannot be obtained.
また共析型β安定化元素を3.5重量%以上含有させる
ことによって、第2のβ相の安定化が図られ、また析出
硬化作用を生しさせて第2のβ相の硬さを向上させるこ
とができる。In addition, by containing 3.5% by weight or more of the eutectoid β-stabilizing element, the second β phase is stabilized, and the hardness of the second β phase is increased by producing a precipitation hardening effect. can be improved.
これらの効果を得るためのFe、Cr、Mn、Coおよ
びNiの具体的含有量は、Feの場合は3.5〜15重
量%、Crの場合は6.3重量%以上、Mnの場合は6
.4重量%以上、Coの場合は7重量%以上、Niの場
合は9重量%以上である。The specific content of Fe, Cr, Mn, Co and Ni to obtain these effects is 3.5 to 15% by weight for Fe, 6.3% by weight or more for Cr, and 6.3% by weight or more for Mn. 6
.. The content is 4% by weight or more, 7% by weight or more for Co, and 9% by weight or more for Ni.
た父′シ、共析型β安定化元素の含有量が40重量%を
上回ると、この元素の固溶性が低いことに起因して、偏
析等を生じ、安定した第2のβ相が得られなくなる。し
たがって、この元素の含有量の上限は40重量%に設定
される。However, if the content of the eutectoid β-stabilizing element exceeds 40% by weight, segregation etc. will occur due to the low solid solubility of this element, making it difficult to obtain a stable second β phase. I won't be able to do it. Therefore, the upper limit of the content of this element is set at 40% by weight.
なお、全率固溶型β安定化元素を添加せずに、共析型β
安定化元素のみを添加すると、前記析出硬化作用に伴い
金属間化合物が形成されて第2のβ相が脆化する傾向に
あるが、この問題は全率固溶型β安定化元素を併用する
ことによって解消される。In addition, without adding any solid solution type β stabilizing elements, eutectoid type β
If only a stabilizing element is added, an intermetallic compound is formed due to the precipitation hardening effect, and the second β phase tends to become brittle. However, this problem can be solved by combining a completely solid solution β stabilizing element. It is resolved by this.
表層部3の耐摩耗性を向上させる上で、その表層部3に
硬質粒子を分散させることは有効な手段である。この硬
質粒子の分散に当っては、全率固溶型β安定化元素を含
むMo、C粉末を用い、局所溶融合金化処理におけるM
o、C→2Mo+C1Ti+C→T1Cの反応を利用し
て硬質粒子としてのTICを析出させるとよい。このM
oC粉末はMoI!!:Tiとの合金化を容易にする作
用をも有する。Dispersing hard particles in the surface layer 3 is an effective means for improving the wear resistance of the surface layer 3. In dispersing these hard particles, Mo and C powders containing solid solution β-stabilizing elements are used, and M
It is preferable to precipitate TIC as hard particles using the reaction of C→2Mo+C1Ti+C→T1C. This M
oC powder is MoI! ! : Also has the effect of facilitating alloying with Ti.
以下、ロッカアーム1の局所溶融合金化処理について説
明する。Hereinafter, the local melting alloying process of the rocker arm 1 will be explained.
第2図は粉末噴射による局所溶融合金化処理法を示シ、
前記母材(Ti−6AI!、−4V)よりなるロッカア
ーム用素材1゜を矢印方向へ移動させ、そのスリッパ面
対応部2゜に、オシレータ5より炭酸ガスレーザを照射
し、同時にガス供給ノズル6よりシールドガスであるヘ
ルウムガスを、また粉末供給ノズル7よりMoz C粉
末(全率固溶型β安定化元素)およびFe粉末(共析型
β安定化元素)をそれぞれ供給するものである。Figure 2 shows the local melting alloying process using powder injection.
The rocker arm material 1° made of the base material (Ti-6AI!, -4V) is moved in the direction of the arrow, and its slipper surface corresponding portion 2° is irradiated with a carbon dioxide laser from the oscillator 5, and at the same time from the gas supply nozzle 6. Helium gas, which is a shielding gas, is supplied from the powder supply nozzle 7, and Moz C powder (total solid solution type β-stabilizing element) and Fe powder (eutectoid type β-stabilizing element) are respectively supplied.
処理条件は次の通りである。The processing conditions are as follows.
ロッカアーム用素材1゜の移動速度(処理速度):30
0鵬/閉in
炭酸ガスレーザ:出力 5kW、スポット径2111、
振幅 5IIIII、パワー密度 5〜6X10’W/
cd
Mo、C粉末:直径 10〜44μm、供給量15.7
g/win ; F C粉末:純度 99%以上、
粒度 200メツシユ以下、供給量 4.6 g /m
in前記処理により、第1のβ相と第2のβ相との二相
を混在させた金属組織が得られる。Movement speed of rocker arm material 1° (processing speed): 30
0 Peng/closed carbon dioxide laser: output 5kW, spot diameter 2111,
Amplitude 5III, Power density 5~6X10'W/
cd Mo, C powder: diameter 10-44 μm, supply amount 15.7
g/win; FC powder: purity 99% or more,
Particle size: 200 mesh or less, supply amount: 4.6 g/m
By the above-mentioned treatment, a metal structure in which two phases, the first β phase and the second β phase are mixed, is obtained.
前記処理により得られた表層部3の平均組成は、T i
−27,1M o −7,9F e−3,3A l
−2,2Vである。The average composition of the surface layer 3 obtained by the above treatment is T i
-27,1M o -7,9F e-3,3A l
-2.2V.
炭酸ガスレーザといった高密度エネルギ源による局所溶
融合金化処理においては、溶融後自己冷却による急速凝
固作用が得られるので、金属組織が微細で、且つ均質と
なり、したがって安定した摺動特性および強度が得られ
る。また母材に対する表層部3の密着力も強い。In local melting alloy processing using a high-density energy source such as a carbon dioxide laser, rapid solidification is achieved by self-cooling after melting, resulting in a fine and homogeneous metal structure, resulting in stable sliding properties and strength. . Furthermore, the adhesion of the surface layer 3 to the base material is strong.
なお、前記局所溶融合金化処理法としては、索材1゜の
スリッパ面対応部2゜に予め粉末を設置しておく、ブリ
ブレイス法の適用も可能である。In addition, as the local melting alloying treatment method, it is also possible to apply the bribrace method, in which powder is placed in advance at the slipper surface corresponding portion 2° of the cable material 1°.
また、本発明はTi合金製構造部材にも適用される。Further, the present invention is also applied to structural members made of Ti alloy.
C1発明の効果
本発明によれば、表層部を得るための改質処理および表
層部の金属組織を前記のように特定することによって、
母材との密着力が高く、且つ優れた摺動特性および強度
を持つ表層部を備えたチタンまたはチタン合金製構造部
材を提供することができる。C1 Effect of the invention According to the invention, by specifying the modification treatment for obtaining the surface layer and the metal structure of the surface layer as described above,
It is possible to provide a titanium or titanium alloy structural member that has a surface layer that has high adhesion to the base material and has excellent sliding properties and strength.
【図面の簡単な説明】
第1図はロッカアームの要部破断正面図、第2図は局所
溶融合金化処理法の説明図である。
1・・・ロッカアーム(構造部材)、3・・・表層部第
1図
第2図BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a cutaway front view of the main part of the rocker arm, and FIG. 2 is an explanatory diagram of the local melting alloying process. 1... Rocker arm (structural member), 3... Surface layer Fig. 1 Fig. 2
Claims (4)
より改質された表層部を備え、前記表層部の金属組織は
、全率固溶型β安定化元素を含有する第1のβ相と、共
析型β安定化元素を含有する第2のβ相との二相を混在
させて構成されることを特徴とするチタンまたはチタン
合金製構造部材。(1) A surface layer portion modified by local melting alloying treatment using a high-density energy source, and the metal structure of the surface layer portion is a first β phase containing a solid solution type β stabilizing element. and a second β phase containing a eutectoid β stabilizing element.
%以上であり、また前記共析型β安定化元素の含有量は
3.5重量%以上、40重量%以下である、第(1)項
記載のチタンまたはチタン合金製構造部材。(2) The total content of the solid solution β-stabilizing element is 10% by weight or more, and the content of the eutectoid β-stabilizing element is 3.5% by weight or more and 40% by weight or less. , the titanium or titanium alloy structural member according to item (1).
少なくとも一種であり、また前記共析型β安定化元素は
、Fe、Cr、Mn、CoおよびNiから選択される少
なくとも一種である、第(1)または第(2)項記載の
チタンまたはチタン合金製構造部材。(3) The total solid solution β-stabilizing element is at least one of Mo and V, and the eutectoid β-stabilizing element is at least one selected from Fe, Cr, Mn, Co, and Ni. The titanium or titanium alloy structural member according to item (1) or item (2).
前記表層部はスリッパ面を構成している、第(1)、第
(2)または第(3)項記載のチタンまたはチタン合金
製構造部材。(4) the structural member is a rocker arm for an internal combustion engine;
The titanium or titanium alloy structural member according to item (1), item (2), or item (3), wherein the surface layer portion constitutes a slipper surface.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1209454A JP2797201B2 (en) | 1989-08-11 | 1989-08-11 | Titanium or titanium alloy structural members |
US07/563,660 US5139585A (en) | 1989-08-07 | 1990-08-07 | Structural member made of titanium alloy having embedded beta phase of different densities and hard metals |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1209454A JP2797201B2 (en) | 1989-08-11 | 1989-08-11 | Titanium or titanium alloy structural members |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH0372058A true JPH0372058A (en) | 1991-03-27 |
JP2797201B2 JP2797201B2 (en) | 1998-09-17 |
Family
ID=16573143
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1209454A Expired - Fee Related JP2797201B2 (en) | 1989-08-07 | 1989-08-11 | Titanium or titanium alloy structural members |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2797201B2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101102486B1 (en) * | 2011-05-11 | 2012-01-05 | 강릉원주대학교산학협력단 | Assistant apparatus for measuring speed of current and measuring method for speed of current using it |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6256561A (en) * | 1985-09-06 | 1987-03-12 | Honda Motor Co Ltd | Method for hardening surface of ti or ti alloy |
JPS62270277A (en) * | 1986-05-18 | 1987-11-24 | Daido Steel Co Ltd | Production of titanium base alloy-made wear resistant member |
JPS6393875A (en) * | 1986-10-07 | 1988-04-25 | Mitsubishi Heavy Ind Ltd | Production of ti alloy member having superior wear resistance |
-
1989
- 1989-08-11 JP JP1209454A patent/JP2797201B2/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6256561A (en) * | 1985-09-06 | 1987-03-12 | Honda Motor Co Ltd | Method for hardening surface of ti or ti alloy |
JPS62270277A (en) * | 1986-05-18 | 1987-11-24 | Daido Steel Co Ltd | Production of titanium base alloy-made wear resistant member |
JPS6393875A (en) * | 1986-10-07 | 1988-04-25 | Mitsubishi Heavy Ind Ltd | Production of ti alloy member having superior wear resistance |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101102486B1 (en) * | 2011-05-11 | 2012-01-05 | 강릉원주대학교산학협력단 | Assistant apparatus for measuring speed of current and measuring method for speed of current using it |
Also Published As
Publication number | Publication date |
---|---|
JP2797201B2 (en) | 1998-09-17 |
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