JPS58204101A - Manufacture of composite sintered alloy member - Google Patents

Manufacture of composite sintered alloy member

Info

Publication number
JPS58204101A
JPS58204101A JP8548282A JP8548282A JPS58204101A JP S58204101 A JPS58204101 A JP S58204101A JP 8548282 A JP8548282 A JP 8548282A JP 8548282 A JP8548282 A JP 8548282A JP S58204101 A JPS58204101 A JP S58204101A
Authority
JP
Japan
Prior art keywords
green compact
sintered alloy
alloy member
sintered
members
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.)
Pending
Application number
JP8548282A
Other languages
Japanese (ja)
Inventor
Masayuki Iijima
正幸 飯島
Hidetoshi Akutsu
阿久津 英俊
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.)
Mitsubishi Metal Corp
Original Assignee
Mitsubishi Metal Corp
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 Mitsubishi Metal Corp filed Critical Mitsubishi Metal Corp
Priority to JP8548282A priority Critical patent/JPS58204101A/en
Publication of JPS58204101A publication Critical patent/JPS58204101A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/062Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00Supplementary information concerning processes or compositions relating to powder metallurgy

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Powder Metallurgy (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

PURPOSE:To enhance the bonding strength of a sintered Fe, Ni or Co alloy member contg. prescribed amounts of a component having a great affinity for O and B, P or Si to a green compact member by bringing the green compact member into contact with the surface of the alloy member to be bonded and heating the green compact member to a liq. phase. CONSTITUTION:A sintered Fe, Ni or Co alloy member contg. >=0.5wt% component having a great affinity for 0 and 0.1-5wt% one or more among B, P and Si as alloying components and a green compact member having a prescribed blended composition are prepared. The green compact member is brought into contact with the surface of the alloy member to be bonded, and the green compact member is heated to a liq. phase. By the heating the green compact member is sintered and both the members are united in a body. Thus, the bonding strength of both members is enhanced.

Description

【発明の詳細な説明】 この発明は複合焼結合金部材の製造法に関するものであ
る。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for manufacturing a composite sintered alloy member.

一般に、金属部材同士を冶金的に結合して複合金属部材
を製造する方法には種々の方法があるが、この中でもろ
う付は法は最も簡便な方法として知られている。しかし
、複合金属部材のうちの少なくとも1部材を焼結合金部
材で構成する必要がある場合、ろう付は時に液化したろ
う材が、焼結合金部材の内部空孔内に毛細管作用により
吸収されて満足な相互部材間の結合が得られない場合が
ある。そこで、前記の複合せんとする焼結合金部材には
、ろう付けに先だって空孔口つぶし処理や溶浸材による
空孔充填処理などの前処理を施す必要があり、この結果
コスト高の原因となるばかりでなく、目つぶし材や溶浸
材によっては焼結合金部材の特性を害なう場合もあるな
ど種々の問題があるものであった。
In general, there are various methods for manufacturing composite metal members by metallurgically bonding metal members together, and among these methods, brazing is known as the simplest method. However, when at least one of the composite metal parts needs to be composed of a sintered alloy member, brazing is sometimes performed in such a way that the liquefied filler metal is absorbed into the internal pores of the sintered alloy member by capillary action. In some cases, a satisfactory bond between the members cannot be obtained. Therefore, it is necessary to perform pre-treatments on the sintered alloy members used as the composite steel before brazing, such as pore-crushing treatment and pore-filling treatment with an infiltrant, which results in high costs. In addition, there are various problems, such as the fact that depending on the blinding material or infiltration material, the properties of the sintered alloy member may be impaired.

そこで、本発明者等は、上述のような観点から、従来複
合焼結合金部材の製造に際して前処理として行なわれて
いた目つぶし処理や空孔充填処理などを施すことなく、
かつろう材をも使用しないで複合焼結合金部材、特に複
合焼結合金部材のうちの1方がC′r、’Mn 、””
 V 、 ”mb:Ti 、 Ta 、  およびZr
””などの酸素との親和力がきわめて強い成分のうちの
1種以上を0.5%以上含有する焼結合金部材で構成さ
れた複合焼結合金部材を製造すべく研究を行なった結果
、まず合金成分として酸素との親和力がきわめて強い成
分を0.5重量%以上含有するFe基。
Therefore, from the above-mentioned viewpoint, the present inventors created a composite sintered alloy member without performing blinding treatment or pore filling treatment, which were conventionally performed as a pretreatment when manufacturing a composite sintered alloy member.
One of the composite sintered alloy members, especially one of the composite sintered alloy members, is C'r, 'Mn, "" without using any brazing material.
V, "mb: Ti, Ta, and Zr
As a result of conducting research to manufacture a composite sintered alloy member composed of a sintered alloy member containing 0.5% or more of one or more of the components with extremely strong affinity for oxygen, such as Fe-based alloy containing 0.5% by weight or more of a component with extremely strong affinity for oxygen.

N1基、またはCO基燃焼結合金部材7その少なくとも
接合面にB、P、およびSiのうちの1種または2種以
上を0.1〜5,0重量%含有させた状態で用意し、こ
の焼結合金部材の接合面(別途用意した所定配合組成を
有する圧粉体部材を当接保持し、この状態で液相加熱す
ると、前記圧粉体部材は焼結されると共に、液相となっ
たP、B、 および8iが両部材の接合面ですぐれた濡
れ性を発揮することから、これら両部材は強固に結合し
、この結果として接合強度のきわめて高い複合焼結部材
が得られるようになるという知見を得たのである。
The N1-based or CO-based combustion alloy member 7 is prepared in such a manner that at least its joint surface contains 0.1 to 5.0% by weight of one or more of B, P, and Si. When a joint surface of a sintered metal member (a green compact member having a predetermined blending composition prepared separately is held in contact and heated in a liquid phase in this state, the green compact member is sintered and turns into a liquid phase). Since P, B, and 8i exhibit excellent wettability on the bonding surfaces of both components, these two components are strongly bonded, resulting in a composite sintered component with extremely high bonding strength. We obtained the knowledge that this is true.

この発明は、上記知見にもとづいてなさ゛れたものであ
って、合金成分として酸素との親和力がきわめて強い成
分を055重量%上含有すると共に、少なくとも接合面
部に、B、P、およびslのうちの1種または2種以上
二0.1〜5.0重量%を含有するFe基、 Ni基、
またはCO基燃焼結合金部材、所定配合組成の圧粉体部
材とをそれぞれ箭途用意し、前記焼結合金部材の接合面
に前記圧粉体部材を当接保持した状態で液相加熱して、
前記圧粉体部材を焼結すると共に、これら両部材を一体
化結合する複合焼結合金部材の製造法に特徴を有するも
のである。
This invention was made based on the above knowledge, and contains 0.55% by weight of a component with extremely strong affinity for oxygen as an alloy component, and at least in the joint surface portion, among B, P, and sl. Fe group containing 0.1 to 5.0% by weight of one or more of the following:
Alternatively, a CO-based combustible alloy member and a green compact member having a predetermined composition are prepared, and liquid phase heating is performed with the green compact member being held in contact with the joint surface of the sintered alloy member. ,
The present invention is characterized by a method for manufacturing a composite sintered alloy member in which the compacted powder member is sintered and both members are integrally bonded.

なお、この発明の方法において、焼結合金部材における
P、B、およびslの含有量を0.1〜5.0重量%に
限定した理由は、その含有量が01%未満では所望の濡
れ性を接合面に確保することができず、したがって接合
強度の低い複合焼結合金部材しか得ることができず、一
方5.0%を越えて含有させると、液相となったこれら
の成分が両部材の接合面からはみ出て製品価値を低下さ
せるようになることから、その含有量を01〜5.0重
量%と定めた。
In addition, in the method of this invention, the reason why the content of P, B, and sl in the sintered alloy member is limited to 0.1 to 5.0% by weight is that if the content is less than 0.1%, the desired wettability cannot be secured at the joint surface, and therefore only a composite sintered alloy member with low joint strength can be obtained.On the other hand, if the content exceeds 5.0%, these components in the liquid phase will Since it protrudes from the joint surfaces of the members and reduces the product value, its content is set at 01 to 5.0% by weight.

また、この発明の方法における焼結合金部材は、高温度
できわめて酸化し易い1.Cr 、 Mn、 V 、 
Nb 。
Furthermore, the sintered alloy member used in the method of this invention is extremely susceptible to oxidation at high temperatures. Cr, Mn, V,
Nb.

Ti、 Ta、およびZrなどの1種以上を0.5%以
上含有するので、この焼結合金部材製造に際しての焼結
雰囲気は、真空あるいは高純度還元性ガスによる雰囲気
とするのが望ましい。
Since it contains 0.5% or more of one or more of Ti, Ta, and Zr, it is desirable that the sintering atmosphere in producing this sintered alloy member be a vacuum or an atmosphere using a high-purity reducing gas.

つぎに、この発明の方法を実施例により具体的に説明す
る。
Next, the method of the present invention will be specifically explained using examples.

実施例 それぞれ第1表に示される成分組成および密度比をもっ
た焼結合金部材、並びに同じく第1表に示される配合組
成をもった5圧粉体部材を、通常の粉末冶金法にしたが
、つて別途用意し、ついで、これら焼結合金部材の接合
面に、前記圧粉体部材を当接保持した状態!、アンモニ
ア分解ガス中、温度:1050〜1200℃の温度範囲
内の所定温度に加熱して、前記焼結合金部材中に含有す
るP。
In each of the examples, sintered alloy members having the component compositions and density ratios shown in Table 1, and 5 green compact members having the compounding compositions also shown in Table 1 were processed using the usual powder metallurgy method. , separately prepared, and then the compacted powder member is held in contact with the joint surfaces of these sintered metal members! , P contained in the sintered alloy member by heating to a predetermined temperature within the temperature range of 1050 to 1200°C in ammonia decomposition gas.

B、Siを液相となすと共に、前記圧粉体部材を焼結し
、かつ前記の両部材を液相となったP、B。
P, B in which B and Si are in a liquid phase, the compacted powder member is sintered, and both members are in a liquid phase.

5− 2− −7− 8iの作用により結合することによって本発明複合焼結
合金部材1〜15をそれぞれ製造した。
Composite sintered alloy members 1 to 15 of the present invention were manufactured by bonding by the action of 5-2-7-8i.

ついで、この結果得られた本発明複合焼結合金部材1〜
15の接合強度を測定すると共に、上記圧粉体部材の焼
結後の密度比を測定した。これらの測定結果を第2表に
示した。
Next, the resulting composite sintered alloy members 1 to 1 of the present invention
In addition to measuring the bonding strength of No. 15, the density ratio of the compacted powder member after sintering was also measured. The results of these measurements are shown in Table 2.

第2表に示される結果から、本発明複合焼結合金部材1
−15は、いずれもきわめて高い接合強度をもつことが
明らかである。なお、ろう付は結合によった場合には、
16kg/−程度の接合強度しか得られないものである
From the results shown in Table 2, the composite sintered alloy member 1 of the present invention
It is clear that -15 has extremely high bonding strength. In addition, if brazing is done by joining,
A bonding strength of only about 16 kg/- can be obtained.

上述のように、この発明の方法によれば、簡単な工程で
、コスト安く、かつ特性劣化を伴うことなく接合強度の
きわめて高い複合焼結合金部材を製造することができ、
しかもこの発明の方法は、例えばカムとの当シ面部に硬
質焼結合金部材を結合した内燃機関用ロッカーアームや
タペットの製造に適用することができ、この場合には長
期に亘ってすぐれた性能を発揮する製品が得られるなど
工業上有用な効果がもたらされるのである。
As described above, according to the method of the present invention, it is possible to manufacture a composite sintered alloy member with extremely high bonding strength through a simple process, at low cost, and without deterioration of characteristics.
Moreover, the method of the present invention can be applied, for example, to the manufacture of rocker arms and tappets for internal combustion engines in which a hard sintered metal member is bonded to the surface that contacts the cam, and in this case, excellent performance can be achieved over a long period of time. This brings about industrially useful effects such as the production of products that exhibit the following properties.

−日−-day-

Claims (1)

【特許請求の範囲】 合金成分として酸素との親和力がきわめて強い成分を0
.5重量%以上含有すると共に、少なくとも接合面部に
、B、P、およびSlのうちの1種または2種以上二0
1〜5.0重量%を含有するFe基。 N1基、またはCO基焼結合金部材と、所定配合組成の
圧粉体部材とをそれぞれ別途用意し、前記焼結合金部材
の接合面に前記圧粉体部材を当接保持した状態で液相加
熱することによって、前記圧粉体部材を焼結すると共に
、これら両部材を一体化結合することを特徴とする複合
焼結合金部材の製造法。
[Scope of Claims] As an alloy component, a component with an extremely strong affinity for oxygen is used as an alloy component.
.. Contains 5% by weight or more, and at least one or more of B, P, and Sl at the joint surface.
Fe groups containing 1 to 5.0% by weight. An N1-based or CO-based sintered alloy member and a green compact member having a predetermined composition are separately prepared, and the green compact member is held in contact with the bonding surface of the sintered alloy member, and the liquid phase is heated. A method for manufacturing a composite sintered alloy member, characterized in that the green compact member is sintered by heating, and the two members are integrally bonded.
JP8548282A 1982-05-20 1982-05-20 Manufacture of composite sintered alloy member Pending JPS58204101A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8548282A JPS58204101A (en) 1982-05-20 1982-05-20 Manufacture of composite sintered alloy member

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8548282A JPS58204101A (en) 1982-05-20 1982-05-20 Manufacture of composite sintered alloy member

Publications (1)

Publication Number Publication Date
JPS58204101A true JPS58204101A (en) 1983-11-28

Family

ID=13860126

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8548282A Pending JPS58204101A (en) 1982-05-20 1982-05-20 Manufacture of composite sintered alloy member

Country Status (1)

Country Link
JP (1) JPS58204101A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01283339A (en) * 1988-02-29 1989-11-14 General Motors Corp <Gm> Iron powder article

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55113805A (en) * 1979-02-26 1980-09-02 Nippon Piston Ring Co Ltd Abrasion resistant member for internal combustion engine and production thereof
JPS56116804A (en) * 1980-02-15 1981-09-12 Mitsubishi Metal Corp Method of bonding sintered body to metal member

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55113805A (en) * 1979-02-26 1980-09-02 Nippon Piston Ring Co Ltd Abrasion resistant member for internal combustion engine and production thereof
JPS56116804A (en) * 1980-02-15 1981-09-12 Mitsubishi Metal Corp Method of bonding sintered body to metal member

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01283339A (en) * 1988-02-29 1989-11-14 General Motors Corp <Gm> Iron powder article

Similar Documents

Publication Publication Date Title
JPS6235442B2 (en)
JPH03158445A (en) Valve seat made of fe-base sintered alloy excellent in wear resistance
KR20020005586A (en) Weakly-magnetic sintered composite -material and a method for production thereof
JPS58204101A (en) Manufacture of composite sintered alloy member
KR840007446A (en) Super heat-resistant sintered alloy and its manufacturing method
JP2654043B2 (en) Heat resistant parts and their manufacturing method
JPS6146521B2 (en)
JPH03158444A (en) Valve seat made of fe-base sintered alloy excellent in wear resistance
JP2643743B2 (en) High strength valve seat made of lead impregnated iron-based sintered alloy for internal combustion engine
JPS58224154A (en) Sintered fe alloy for valve seat of internal combustion engine
JP2600352B2 (en) Valve seat made of copper-impregnated Fe-based sintered alloy with low opponent aggressiveness
JP4223185B2 (en) Iron aluminide-based bond metal with small opponent attack and excellent machinability and method for producing the same
JPS58213859A (en) Corrosion-resistant sintered material
JP3331963B2 (en) Sintered valve seat and method for manufacturing the same
JPH1053832A (en) Wc-iron alloy, containing iron-carbon as binding material, and its production
JP4223184B2 (en) Iron aluminide-based bond metal with small opponent attack and excellent machinability and method for producing the same
JP3254976B2 (en) Internal-combustion engine tappet member having high joining strength with chip material
JP3077274B2 (en) Valve seat made of lead impregnated Fe-based sintered alloy with excellent wear resistance
JPH05263181A (en) Manufacture of fe base sintered alloy member having high strength and high toughness
JPS63154291A (en) Brazing filler metal for sintered parts
JP3230126B2 (en) Internal-combustion engine tappet member having high joining strength with chip material
JP2002115513A (en) Iron group sintered alloy two-layer valve seat and method of its manufacture
GB2088414A (en) Sintering Stainless Steel Powder
JP2636585B2 (en) Sintered alloy valve sheet for internal combustion engine
JPH0158242B2 (en)