JPH02241659A - Manufacture of article - Google Patents
Manufacture of articleInfo
- Publication number
- JPH02241659A JPH02241659A JP5925189A JP5925189A JPH02241659A JP H02241659 A JPH02241659 A JP H02241659A JP 5925189 A JP5925189 A JP 5925189A JP 5925189 A JP5925189 A JP 5925189A JP H02241659 A JPH02241659 A JP H02241659A
- Authority
- JP
- Japan
- Prior art keywords
- composite
- base
- forming
- piston
- preforming
- 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
- 238000004519 manufacturing process Methods 0.000 title claims description 9
- 239000002131 composite material Substances 0.000 claims abstract description 31
- 239000000463 material Substances 0.000 claims abstract description 17
- 239000012779 reinforcing material Substances 0.000 claims abstract description 9
- 238000000034 method Methods 0.000 claims description 9
- 229910000838 Al alloy Inorganic materials 0.000 abstract description 15
- 238000005336 cracking Methods 0.000 abstract 1
- 238000010438 heat treatment Methods 0.000 description 8
- 230000008646 thermal stress Effects 0.000 description 4
- 238000005520 cutting process Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000002344 surface layer Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、金属やプラスティック等の基材がら成る基部
材と、この基材および強化材の複合材から成る複合部材
とが一体に成形された物品の製造方法に関する。[Detailed Description of the Invention] [Industrial Application Field] The present invention is a method in which a base member made of a base material such as metal or plastic, and a composite member made of a composite material of this base material and a reinforcing material are integrally molded. The present invention relates to a method for manufacturing an article.
昨今、部分的に特別な機械的特性が要求される物品には
、その部分にF、R,M <an強化金属)等の複合材
から成る複合部材が適用されているものがある。BACKGROUND ART Nowadays, some articles that require special mechanical properties in some parts have composite members made of composite materials such as F, R, M <an reinforcing metal).
たとえば、自動車や自動二輪車等のエンジンに採用され
るアルミニウム合金製のピストンでは、その頂部表層に
SiCウィスカー等の41維強化材が複合化されており
、耐摩耗性の向上や耐熱性の向上等が図られている。For example, aluminum alloy pistons used in the engines of automobiles and motorcycles have composite 41-fiber reinforcements such as SiC whiskers on the top surface layer, which improves wear resistance and heat resistance. is planned.
ところで、上記のように複合材を含む物品では、溶体化
処理等のために熱処理を行う必要がある。By the way, as mentioned above, articles containing composite materials need to be subjected to heat treatment for solution treatment or the like.
一方、上記ピストンを構成する2つの材質、すなわち、
アルミニウム合金のみの基材と、このアルミニウム合金
およびSiCウィスカーから成る複合材とでは、それぞ
れの熱膨張率が異なっている。On the other hand, the two materials that make up the piston are:
A base material made of only an aluminum alloy and a composite material made of this aluminum alloy and SiC whiskers have different coefficients of thermal expansion.
したがって、上記ピストンに、加熱後急速冷却するよう
な熱処理を施した場合には、熱膨張率の相違から上記基
材から成る基部材と、複合材から成る複合部材との境界
域に熱応力が発生し、これらの間に亀裂を眉来する虞れ
がある。Therefore, when the above-mentioned piston is subjected to heat treatment such as rapid cooling after heating, thermal stress is generated in the boundary area between the base member made of the above-mentioned base material and the composite member made of the composite material due to the difference in coefficient of thermal expansion. There is a risk that this will occur and cause a rift between them.
本発明の目的は、上記実情に鑑みて、溶体化処理等の熱
処理を施した場合にも、基部材と複合部材との境界域で
の亀裂の発生を防止することのできる物品の製造方法を
提供することにある。In view of the above-mentioned circumstances, an object of the present invention is to provide a method for manufacturing an article that can prevent the occurrence of cracks in the boundary area between a base member and a composite member even when heat treatment such as solution treatment is performed. It is about providing.
本発明に係る物品の製造方法では、基材から成る基部材
と、該基材および強化材の複合材から成る複合部材とが
一体に成形されてなる物品の製造方法において、上記強
化材によって予め予成形部材を成形し、かつこの予成形
部材における上記基部材との境界に対応する部位に凹凸
を形成し、上記予成形部材に溶融した基材を添加するこ
とによって上記基材と上記強化材とを複合化させるよう
にしている。In the method of manufacturing an article according to the present invention, a base member made of a base material and a composite member made of a composite material of the base material and a reinforcing material are integrally molded. The base material and the reinforcing material are formed by molding a preformed member, forming irregularities in a portion of the preformed member corresponding to the boundary with the base member, and adding a molten base material to the preformed member. I am trying to combine these.
〔作用)
上記構成によれば、熱膨張率の相違により基部材と複合
部材との境界域に発生する熱応力を、予成形部材に形成
した凹凸によって緩和することができる。[Function] According to the above configuration, the thermal stress generated in the boundary area between the base member and the composite member due to the difference in coefficient of thermal expansion can be alleviated by the unevenness formed on the preformed member.
〔実施例]
以下、実施例を示す図面に基づいて本発明の詳細な説明
する。[Example] Hereinafter, the present invention will be described in detail based on drawings showing examples.
第1図は、本発明に係る製造方法によって成形された物
品を概念的に示したもので、自動車や自動二輪車の2サ
イクルエンジンに採用されるピストン10を例示してい
る。FIG. 1 conceptually shows an article molded by the manufacturing method according to the present invention, and illustrates a piston 10 employed in a two-stroke engine for an automobile or a motorcycle.
このピストン10は、耐摩耗性や耐熱性等の向上を図る
目的から、AC8A等のアルミニウム合金(基材)から
成る基部材11の頂部表層に、上記アルミニウム合金お
よびSiCウィスカー(強化材)の複合材から成る複合
部材12を備えたもので、以下に示す手順によって製造
される。This piston 10 has a base member 11 made of an aluminum alloy (base material) such as AC8A, and a composite of the aluminum alloy and SiC whiskers (reinforcing material) on the top surface layer of the base member 11 for the purpose of improving wear resistance, heat resistance, etc. The composite member 12 is manufactured by the following procedure.
まず、第2図に示すように、NSiCウィスカーによっ
て、上記ピストン10の頂部表層形状、すなわち、ピス
トン1oとほぼ同一の直径を有する円柱状部材(予成形
部材)20を成形し、さらにこの円柱状部材20の一端
面21に、同一の深さを有する複数の環状溝(凹凸)2
1a、21b。First, as shown in FIG. 2, a cylindrical member (preformed member) 20 having approximately the same diameter as the top surface shape of the piston 10, that is, the piston 1o, is formed using NSiC whiskers. A plurality of annular grooves (irregularities) 2 having the same depth are formed on one end surface 21 of the member 20.
1a, 21b.
20c、20d・・・を同一のピッチ、たとえば、上記
円柱状部材20の直径が60rI11の場合、深さ1#
の溝を1.5Mのピッチで同心上に切削加工する。20c, 20d... with the same pitch, for example, if the diameter of the cylindrical member 20 is 60rI11, the depth is 1#
Concentrically cut the grooves at a pitch of 1.5M.
その際、同図に示すように、回転軸30の先端に鋸歯状
の刃を有する工具31を備えた加工闘を用いれば、上記
切削加工を容易に行うことができる。At this time, as shown in the figure, the above-mentioned cutting process can be easily performed by using a machining machine equipped with a tool 31 having a sawtooth blade at the tip of a rotary shaft 30.
次に、上記円柱状部材20を700℃に予熱し、これを
第3図(a)に示すように、鋳型40内に収容させる。Next, the cylindrical member 20 is preheated to 700° C. and placed in a mold 40 as shown in FIG. 3(a).
このとき、円柱状部材20は、その切削加工を施さない
面22がピストン10の頂面に対応するように配置する
。At this time, the cylindrical member 20 is arranged so that its uncut surface 22 corresponds to the top surface of the piston 10.
この状態から、第3図(b)に示すように、上記鋳型4
0にアルミニウム合金を700℃、500気圧の状態で
注湯すると、このアルミニウム合金と上記円柱状部材2
0を構成するSiCウィスカーとが複合化した後に凝固
され、アルミニウム合金から成る基部材11と、アルミ
ニウム合金およびSiCウィスカーの複合材から成る複
合部材12とが一体に成形されたピストン10が製造さ
れる。From this state, as shown in FIG. 3(b), the mold 4
When aluminum alloy is poured into the cylindrical member 2 at 700°C and 500 atm, the aluminum alloy and the cylindrical member 2
A piston 10 is produced in which a base member 11 made of an aluminum alloy and a composite member 12 made of a composite material of an aluminum alloy and SiC whiskers are integrally molded. .
第1図からも明らかなように、上記基部材11と複合部
材12との接合部Aは、上記円柱状部材20に形成した
環状溝20b、20C。As is clear from FIG. 1, the joint A between the base member 11 and the composite member 12 is an annular groove 20b, 20C formed in the columnar member 20.
20d・・・によって鋸歯状に構成されている。20d... has a sawtooth shape.
このピストン10に、溶体化処理等のための熱処理、た
とえば、510℃で4時間加熱した後急冷し、さらに1
70℃で10時間の加熱を行った場合、アルミニウム合
金の熱膨張率と、このアルミニウム合金およびSiCウ
ィスカーの複合材の熱膨張率との相違から基部材11と
複合部材12との境界域に熱応力が発生する。This piston 10 is subjected to heat treatment such as solution treatment, for example, heating at 510° C. for 4 hours, followed by rapid cooling.
When heating is performed at 70° C. for 10 hours, heat is generated in the boundary area between the base member 11 and the composite member 12 due to the difference in thermal expansion coefficient of the aluminum alloy and that of the composite material of this aluminum alloy and SiC whiskers. Stress occurs.
しかしながら、上記のような方法によって製造されたピ
ストン10では、基部材11と複合部材12との接合部
が鋸歯状に構成されているため、この熱応力の水平方向
(ピストン10の径方向)成分が漸減緩和されることと
なり、上記2つの部材11.12の境界域での亀裂の発
生が防止される。However, in the piston 10 manufactured by the above method, since the joint between the base member 11 and the composite member 12 is configured in a sawtooth shape, the horizontal direction (radial direction of the piston 10) component of this thermal stress is is gradually reduced, and cracks are prevented from forming in the boundary area between the two members 11 and 12.
なお、上記実施例では、エンジンに採用されるピストン
10について例示しているが、本発明はもちろんその他
の物品にも適用できる。また、この物品は、アルミニウ
ム合金から成る基部材11と、アルミニウム合金および
SiCウィスカーの複合材から成る複合部材12とが一
体に成形されているが、本発明ではこれらの組み合わせ
に限定されない。In the above embodiment, the piston 10 employed in an engine is exemplified, but the present invention can of course be applied to other articles. Further, in this article, a base member 11 made of an aluminum alloy and a composite member 12 made of a composite material of an aluminum alloy and SiC whiskers are integrally molded, but the present invention is not limited to these combinations.
さらに、上記実施例では、複数の環状溝21a、21b
、21c、21d−・・を切削加工することによって凹
凸を構成するようにしているが、凹凸は必ずしも溝によ
って構成する必要はないし、また切削加工によって構成
する必要もない。Furthermore, in the above embodiment, the plurality of annular grooves 21a, 21b
, 21c, 21d, etc., the unevenness is formed by cutting, but the unevenness does not necessarily have to be formed by grooves, nor does it need to be formed by cutting.
上記したように、本発明に係る物品の製造方法によれば
、熱膨張率の相違により基部材と複合部材との境界域に
発生する熱応力を、予成形部材に形成した凹凸によって
緩和することができるので、溶体化処理等の熱処理を施
した場合にも、上記境界域での亀裂の発生を防止するこ
とができる。As described above, according to the method for manufacturing an article according to the present invention, the thermal stress generated in the boundary area between the base member and the composite member due to the difference in coefficient of thermal expansion can be alleviated by the unevenness formed on the preformed member. Therefore, even when heat treatment such as solution treatment is performed, cracks can be prevented from occurring in the boundary area.
第1図は、本発明に係る方法によって製造された物品を
概念的に示した断面斜視図、第2図および第3図(a)
、(b)は、本発明に係る方法によって物品を製造する
際の工程を順に示したもので、第2図は概念的斜視図、
第3図(a)。
(b)は概念的断面図である。
10・・・物品、
11・・・基部材、
12・・・複合部材、
20・・・予成形部材、
21a、21b、21c、21d−・・凹凸。
(a)
(b)
第2図
第3図FIG. 1 is a cross-sectional perspective view conceptually showing an article manufactured by the method according to the present invention, FIG. 2 and FIG. 3(a).
, (b) sequentially show the steps of manufacturing an article by the method according to the present invention, and FIG. 2 is a conceptual perspective view;
Figure 3(a). (b) is a conceptual cross-sectional view. DESCRIPTION OF SYMBOLS 10... Article, 11... Base member, 12... Composite member, 20... Preformed member, 21a, 21b, 21c, 21d-... Irregularities. (a) (b) Figure 2 Figure 3
Claims (1)
ら成る複合部材とが一体に成形されてなる物品の製造方
法において、上記強化材によつて予め予成形部材を成形
し、かつこの予成形部材における上記基部材との境界に
対応する部位に凹凸を形成し、上記予成形部材に溶融し
た基材を添加することによって上記基材と上記強化材と
を複合化させるようにしたことを特徴とする物品の製造
方法。A method for manufacturing an article in which a base member made of a base material and a composite member made of a composite material of the base material and a reinforcing material are integrally molded, comprising forming a preformed member in advance with the reinforcing material, and The base material and the reinforcing material are composited by forming irregularities in a portion of the preformed member corresponding to the boundary with the base member and adding a molten base material to the preformed member. A method of manufacturing an article characterized by:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5925189A JP2897243B2 (en) | 1989-03-10 | 1989-03-10 | Article manufacturing method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5925189A JP2897243B2 (en) | 1989-03-10 | 1989-03-10 | Article manufacturing method |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH02241659A true JPH02241659A (en) | 1990-09-26 |
JP2897243B2 JP2897243B2 (en) | 1999-05-31 |
Family
ID=13107975
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP5925189A Expired - Fee Related JP2897243B2 (en) | 1989-03-10 | 1989-03-10 | Article manufacturing method |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2897243B2 (en) |
-
1989
- 1989-03-10 JP JP5925189A patent/JP2897243B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
JP2897243B2 (en) | 1999-05-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
S531 | Written request for registration of change of domicile |
Free format text: JAPANESE INTERMEDIATE CODE: R313532 |
|
R350 | Written notification of registration of transfer |
Free format text: JAPANESE INTERMEDIATE CODE: R350 |
|
LAPS | Cancellation because of no payment of annual fees |