JPS6247469A - Heat insulating member - Google Patents

Heat insulating member

Info

Publication number
JPS6247469A
JPS6247469A JP18784885A JP18784885A JPS6247469A JP S6247469 A JPS6247469 A JP S6247469A JP 18784885 A JP18784885 A JP 18784885A JP 18784885 A JP18784885 A JP 18784885A JP S6247469 A JPS6247469 A JP S6247469A
Authority
JP
Japan
Prior art keywords
base material
undercoat
heat insulating
insulating member
layer
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
JP18784885A
Other languages
Japanese (ja)
Inventor
Takashi Tomota
隆司 友田
Noritaka Miyamoto
典孝 宮本
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.)
Toyota Motor Corp
Original Assignee
Toyota Motor 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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP18784885A priority Critical patent/JPS6247469A/en
Publication of JPS6247469A publication Critical patent/JPS6247469A/en
Pending legal-status Critical Current

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  • Coating By Spraying Or Casting (AREA)

Abstract

PURPOSE:To improve the durability of a heat insulating member obtd. by forming a ceramic layer on a base material with an undercoat in-between, by forming a buffer layer on the boundary between the base material and the undercost so as to improve the adhesion of the ceramic layer to the base material. CONSTITUTION:An undercoat (b) is formed on the roughened surface of a base material (a) by thermal spraying and a ceramic layer (c) is formed on the undercoat (b) by thermal spraying. At this time, a buffer layer (p) having pores is formed in the base material (a) and near the boundary between the base material (a) and the undercoat (b) or a buffer layer (q) having voids (s) is formed on the boundary between the base material (a) and the undercoat (b). The buffer layer absorbs large thermal expansion of the base material (a) and relieves thermal stress produced by the difference in thermal expansion between the base material (a) and the ceramic layer (c), so the adhesion of the ceramic layer (c) to the base material (a) can be improved.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は、断熱部材にかかり、特に、例えば自動車の
エンジン部品等のように高温にざらされる部材の断熱性
を高めるために、母材上にセラミック層を溶射により形
成する断熱部材の改良に関するものである。
[Detailed Description of the Invention] [Field of Industrial Application] The present invention relates to heat insulating members, and in particular, to improve the heat insulating properties of members exposed to high temperatures, such as engine parts of automobiles, the present invention is directed to heat insulating members. This invention relates to an improvement in a heat insulating member on which a ceramic layer is formed by thermal spraying.

〔従来の技1ネテ〕 従来から、溶射によりセラミック層を形成するときには
、あらかじめ母材上にNi系合金のアンダーコートを行
っている。
[Conventional Technique 1] Conventionally, when forming a ceramic layer by thermal spraying, a base material is undercoated with a Ni-based alloy in advance.

これは、例えばAβ等の母材の熱膨張率がセラミックの
熱膨張率よりも大きく、またセラミックは元来金属との
密着性が悪いため、アンダーコートにより熱膨張差を吸
収しまた密着性を向上するようにしたものである。
This is because the coefficient of thermal expansion of the base material, such as Aβ, is higher than that of ceramic, and since ceramics inherently have poor adhesion to metals, the undercoat absorbs the difference in thermal expansion and improves the adhesion. It is designed to improve.

しかしながら、この方法により製造した断熱部材の試験
片や燃焼、排気系部品を熱サイクルをかけて試験してみ
ると、セラミック層内部、セラミック層とアンダーコー
トの境界部およびアンダーコートと母材の境界部にクラ
ックが生じるという問題があった。また、これにより、
ひいては溶射層の剥離を生じるという問題があった。
However, when test specimens of heat insulating materials and combustion and exhaust system parts manufactured using this method were subjected to thermal cycles, it was found that There was a problem that cracks formed in the parts. Also, this allows
As a result, there was a problem in that the sprayed layer peeled off.

このような問題が生じる原因は、母材と溶射層との熱膨
張差、およびエロージョン熱応力による亀裂作用である
The causes of such problems are the difference in thermal expansion between the base material and the sprayed layer, and cracking caused by erosion thermal stress.

この剥離を防止するため、従来、公知文献であるRAN
GASWAMY&H,HERMAN、THERMAL 
 EXPANSION  5TADYOF  PLAS
MASPRA’1.D  0XIDE  C0ATIN
GS、Th1n  SoIlidFifm、73 (1
980)43〜52等に記載されているように、溶射層
の気孔率を大きくすることにより熱膨張差を緩和する試
みがなされてきた。
In order to prevent this peeling, conventionally known literature RAN
GASWAMY&H,HERMAN,THERMAL
EXPANSION 5TADYOF PLAS
MASPRA'1. D 0XIDE C0ATIN
GS, Th1n SoIlidFifm, 73 (1
980) 43-52, attempts have been made to alleviate the difference in thermal expansion by increasing the porosity of the sprayed layer.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

しかしながら、この場合セラミック層とアンダーコート
の密着性が低下する問題があり、またアンダーコートと
母材との熱膨張差から耐久性が十分でないという問題が
あった。
However, in this case, there was a problem in that the adhesion between the ceramic layer and the undercoat decreased, and there was also a problem in that durability was insufficient due to the difference in thermal expansion between the undercoat and the base material.

さらに、ショツトブラスト法におけるショツトブラスト
粒を大きくしたり、目立て加工等により、母材表面の凹
凸を増してその投錨効果によって密着性を向上させる方
法も検討されたが、やはりこの場合も母材の熱膨張率が
大きいため十分な耐久性を確保できないという問題があ
った。
Furthermore, methods of increasing the roughness of the base material surface by increasing the size of the shot blast particles in the shot blasting method, or by sharpening, etc., and improving adhesion through the anchoring effect have also been considered, but in this case as well, the There was a problem in that sufficient durability could not be ensured due to the large coefficient of thermal expansion.

そして、上記のような問題は、例えばピストンのように
厳しい熱的条件に加えて機械的条件にさらされる摺動部
品においては、一段と重大な問題であった。
The above problems are even more serious in sliding parts such as pistons, which are exposed to severe mechanical conditions in addition to thermal conditions.

従って、本発明の目的は、アンダーコートと母材との密
着性を向上させて、断熱部材の耐久性を向上することに
ある。
Therefore, an object of the present invention is to improve the adhesion between the undercoat and the base material, thereby improving the durability of the heat insulating member.

〔問題点を解決するための手段〕[Means for solving problems]

このため、本発明にかかる断熱部材は、溶射層と母材と
の間に、これらの熱膨張差を吸収する緩衝層を設けたこ
とを特徴とするものである。
Therefore, the heat insulating member according to the present invention is characterized in that a buffer layer is provided between the sprayed layer and the base material to absorb the difference in thermal expansion between them.

具体的には、断熱部材の母材上にアンダーコートを施し
た後この上にセラミック層を形成する断熱部材において
、この母材とアンダーコートとの境界部に熱膨張差を吸
収する緩衝層を形成したものである。
Specifically, in a heat insulating member in which an undercoat is applied on a base material of the heat insulating member and a ceramic layer is formed on the undercoat, a buffer layer is provided at the boundary between the base material and the undercoat to absorb the difference in thermal expansion. It was formed.

本発明の好ましい態様では、あらかじめ表面に凹凸加工
を施した母材a上にアンダーコートbを溶射した後セラ
ミック層Cを溶射する。そして第1図に示すように母材
a内であって母材aとアンダーコートbの境界部近傍に
気孔を有する緩衝層pを設けるか、または第2図に示す
ように境界部に空隙Sを有する緩衝Mqを設ける。
In a preferred embodiment of the present invention, the ceramic layer C is sprayed after the undercoat b is sprayed onto the base material a whose surface has been textured in advance. Then, as shown in FIG. 1, a buffer layer p having pores is provided in the base material a near the boundary between the base material a and the undercoat b, or as shown in FIG. A buffer Mq is provided.

〔作用〕[Effect]

上記の構成にかかる本発明の詳細な説明すると、緩衝層
が母材の大きな熱膨張を吸収し、溶射層との熱膨張差に
起因する熱応力を緩和して、母材と溶射層との密着性を
向上させる作用をする。
To explain in detail the present invention having the above configuration, the buffer layer absorbs the large thermal expansion of the base material and relieves thermal stress caused by the difference in thermal expansion between the base material and the sprayed layer. It works to improve adhesion.

〔実施例〕〔Example〕

以下、本発明の実施例を図面に基づいて詳細に説明する
Embodiments of the present invention will be described in detail below with reference to the drawings.

(本発明品) 下記に示す実施例の断熱部材を用い、直径8鰭、長さ5
0mmの円柱試験片を作成した。
(Product of the present invention) Using the heat insulating member of the example shown below, a fin with a diameter of 8 and a length of 5
A 0 mm cylindrical test piece was prepared.

(第1実施例) 第1図は本発明にかかる断熱部材の第1実施例を示す断
面図である。
(First Example) FIG. 1 is a sectional view showing a first example of a heat insulating member according to the present invention.

まず、A1母材(JIS  ACBA相当)aを鋳造す
るときに、A1表面の凝固速度を調整することにより、
その表面直下にブローホールを形成する。次に、これに
ショツトブラストまたは表面凹凸加工を施す。
First, when casting A1 base material (JIS ACBA equivalent) a, by adjusting the solidification rate of the A1 surface,
A blowhole is formed just below the surface. Next, this is subjected to shot blasting or surface roughening.

このようにして得られた母材aの表面にアンダーコート
bとして、75Ni−19Cr−6A#合金を9.1m
mの厚さにプラズマ溶射して形成した。
As an undercoat b, 9.1 m of 75Ni-19Cr-6A# alloy was applied to the surface of the base material a thus obtained.
It was formed by plasma spraying to a thickness of m.

そして、さらにこの上にセラミック層Cとして、ZrO
2・5CaOを0.5Hの厚さにプラズマ溶射して形成
した。゛ このようにして、第1図に示すような層構成を有する断
熱部材2を得た。
Then, on top of this, ZrO is added as a ceramic layer C.
It was formed by plasma spraying 2.5CaO to a thickness of 0.5H. In this way, a heat insulating member 2 having a layered structure as shown in FIG. 1 was obtained.

上記の構成にかかる第1実施例の作用を説明すると、母
材aとアンダーコートbの境界部に形成された緩衝層p
が、その層内の空隙により母材aの熱膨張を吸収し、ア
ンダーコートbとの熱膨張差に起因する境界面の剪断応
力を緩和して母材aとアンダーコートbとの密着性を向
上させる作用をする。
To explain the operation of the first embodiment according to the above structure, the buffer layer p formed at the boundary between the base material a and the undercoat b
However, the voids in the layer absorb the thermal expansion of base material a, relieve the shear stress at the interface caused by the difference in thermal expansion with undercoat b, and improve the adhesion between base material a and undercoat B. It acts to improve.

(第2実施例) 第2図は本発明にかかる断熱部材の第2実施例を示す断
面図である。
(Second Embodiment) FIG. 2 is a sectional view showing a second embodiment of the heat insulating member according to the present invention.

まず、AI!母材aの表面にあらかじめ第3図に示すよ
うに、断面の溝深さHが0.5鶴、溝と溝のピッチTが
0.4m、溝の頂部の角度θが300の、断面が2等辺
三角形の連続的な溝32を形成する。
First, AI! As shown in Fig. 3, a cross-section was prepared on the surface of the base material a with a groove depth H of 0.5 m, a groove pitch T of 0.4 m, and an angle θ at the top of the grooves of 300. A continuous isosceles triangular groove 32 is formed.

次に、このようにして得られた母材aの表面に第1実施
例と同様にしてアンダーコートbおよびセラミック層C
を形成した。
Next, an undercoat b and a ceramic layer C are applied to the surface of the base material a thus obtained in the same manner as in the first embodiment.
was formed.

このようにして、第2図に示すような層構成を有する断
熱部材3を得た。
In this way, a heat insulating member 3 having a layered structure as shown in FIG. 2 was obtained.

このようにして得られた断熱部材は、第3図に示すよう
に母材aの表面が鋸歯状になっており、しかもその溝3
2の頂部が鋭角なため、アンダーコートbが溝32の最
奥部までは入り込めず空隙Sを残していた。
The heat insulating member thus obtained has a sawtooth surface on the base material a, as shown in FIG.
Since the top of groove 2 had an acute angle, undercoat b could not penetrate to the deepest part of groove 32, leaving a gap S.

上記の構成にかかる第2実施例の作用を説明すると、母
材a内であってアンダーコートbとの境界部近傍に形成
された空隙Sを有する緩衝Jlqが、母材aが熱膨張す
る際弾性または塑性変形し、アンダーコートbとの熱膨
張差に起因する境界面の剪断応力を緩和して、母材aと
アンダーコートbとの密着性を向上させる作用をする。
To explain the operation of the second embodiment according to the above configuration, when the base material a thermally expands, the buffer Jlq having the void S formed in the base material a and near the boundary with the undercoat b It deforms elastically or plastically, relieves the shear stress at the interface caused by the difference in thermal expansion with the undercoat b, and acts to improve the adhesion between the base material a and the undercoat b.

以上の実施例で作成した断熱部材の性能を評価するため
に、400℃の高温と室温を繰り返す冷熱サイクル試験
を行った。
In order to evaluate the performance of the heat insulating member produced in the above examples, a cold/heat cycle test was conducted in which the heat insulating member was repeatedly tested at a high temperature of 400° C. and at room temperature.

(比較品) 比較のために、本発明の実施例と同じ組成で、表面直下
にブローホールを形成しないAl母材を用い、他は実施
例と同じ溶射材料および溶射層厚さに形成した断熱部材
を用い、本発明品と同様な円柱試験片を作成した。
(Comparative product) For comparison, a heat insulating material was used that had the same composition as the example of the present invention and did not form a blowhole directly under the surface, and was formed using the same thermal spraying material and the same thermal spray layer thickness as the example. A cylindrical test piece similar to the product of the present invention was created using the member.

この試験の結果、比較品は冷熱サイクル50〜100回
で溶射層の剥離が生じたが、本発明品は2000回後も
溶射層に亀裂、剥離は生じなかった。
As a result of this test, the thermal sprayed layer of the comparative product peeled off after 50 to 100 cycles of heating and cooling, but the thermal sprayed layer of the product of the present invention showed no cracks or peeling even after 2000 cycles.

また、第4図に示すように、本発明品および比較品の断
熱部材44を外径83鶴の噴孔部42を有するアルミニ
ウム合金製(JISACBA相当)のピストン本体41
の噴孔部内面に形成したピストン4を作成し、これを各
別のエンジンに組み込み冷熱サイクルのかかる実機評価
に供した。
In addition, as shown in FIG. 4, the heat insulating members 44 of the products of the present invention and comparative products were attached to a piston body 41 made of aluminum alloy (equivalent to JISACBA) and having a nozzle hole 42 with an outer diameter of 83 mm.
A piston 4 formed on the inner surface of the nozzle hole was created, and the piston 4 was installed in each different engine and subjected to an evaluation of an actual machine subjected to a cooling/heating cycle.

実機評価の条件は、エンジン回転数4500rpm、圧
縮比18で行った。
The conditions for the actual machine evaluation were an engine speed of 4500 rpm and a compression ratio of 18.

この結果、比較品は5〜10時間で評価に供したピスト
ンのほぼ全数に溶射層の剥離、脱落が発生したが、本発
明品のピストンには500時間後も全く異常が認められ
なかった。
As a result, peeling and falling off of the sprayed layer occurred in almost all of the comparative pistons subjected to the evaluation after 5 to 10 hours, but no abnormalities were observed in the pistons of the present invention even after 500 hours.

以上、本発明を特定の実施例に基づいて説明したがこれ
に限定されるものではなく、特許請求の範囲に記載した
範囲内で当業者が実施可能な種々の別な態様が考えられ
る。例えば、溶射方法については、密着性から考えてプ
ラズマ溶射が最も良いと考えられるが、他のガス溶射ま
たはアーク溶射で行っても良い。
Although the present invention has been described above based on specific embodiments, it is not limited thereto, and various other embodiments can be considered by those skilled in the art within the scope of the claims. For example, plasma spraying is considered to be the best thermal spraying method in terms of adhesion, but other gas spraying or arc spraying may also be used.

〔発明の効果〕〔Effect of the invention〕

以上説明したように、本発明は、断熱部材の母材上にア
ンダーコートを施した後この上にセラミック層を形成す
る断熱部材において、この母材とアンダーコートとの境
界部に熱膨張差を吸収する緩衝層を形成したため、溶射
層と母材との密着性を向上させて、断熱部材の耐久性を
向上することができる。
As explained above, the present invention provides a heat insulating member in which an undercoat is applied on a base material of the heat insulating member and then a ceramic layer is formed thereon, in which a difference in thermal expansion is created at the boundary between the base material and the undercoat. Since the absorbing buffer layer is formed, the adhesion between the sprayed layer and the base material can be improved, and the durability of the heat insulating member can be improved.

また、特にピストンのように、母材の外周が冷却されて
いたり、ボア等により膨張を抑制されていることにより
、外部から相対的に圧縮応力を受ける場合には、母材の
熱膨張による溶射層界面への影響を減らすことができる
というすぐれた効果を奏する。
In addition, especially when the outer periphery of the base material is cooled or the expansion is suppressed by a bore etc., such as a piston, which receives relative compressive stress from the outside, thermal spraying due to thermal expansion of the base material This has the excellent effect of reducing the influence on layer interfaces.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明にかかる断熱部材の第1実施例を示す断
面図、第2図は同じ(第2実施例を示す断面図、第3図
は第2図の母材とアンダーコートとの境界部を拡大して
示す断面図、第4図は本発明にかかる断熱部材をピスト
ンの噴孔部に組み込んだ状態を示す断面図である。 2.3−・−・断熱部材 a −−−−−−一母材 b−−−−−−−アンダルコート c−−−−−−−セラミック層 p、q−−−−〜・−緩衝層 出願人  トヨタ自動車株式会社 第1図 第2図    第3図
FIG. 1 is a sectional view showing the first embodiment of the heat insulating member according to the present invention, FIG. 2 is the same (a sectional view showing the second embodiment), and FIG. FIG. 4 is a cross-sectional view showing an enlarged boundary portion, and FIG. 4 is a cross-sectional view showing a state in which the heat insulating member according to the present invention is incorporated into the nozzle hole portion of the piston. 2.3 - Heat insulating member a --- --- Base material b ---------- Andal coat c --- Ceramic layer p, q --- Buffer layer Applicant: Toyota Motor Corporation Figure 1 Figure 2 Figure 3

Claims (1)

【特許請求の範囲】[Claims] 断熱部材の母材上にアンダーコートを施した後該アンダ
ーコート上にセラミック層を形成する断熱部材において
、前記母材と前記アンダーコートとの境界部に熱膨張差
を吸収する緩衝層を形成したことを特徴とする断熱部材
In a heat insulating member in which an undercoat is applied on a base material of the heat insulating member and a ceramic layer is formed on the undercoat, a buffer layer is formed at the boundary between the base material and the undercoat to absorb a difference in thermal expansion. A heat insulating member characterized by:
JP18784885A 1985-08-26 1985-08-26 Heat insulating member Pending JPS6247469A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18784885A JPS6247469A (en) 1985-08-26 1985-08-26 Heat insulating member

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18784885A JPS6247469A (en) 1985-08-26 1985-08-26 Heat insulating member

Publications (1)

Publication Number Publication Date
JPS6247469A true JPS6247469A (en) 1987-03-02

Family

ID=16213275

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18784885A Pending JPS6247469A (en) 1985-08-26 1985-08-26 Heat insulating member

Country Status (1)

Country Link
JP (1) JPS6247469A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6411910A (en) * 1987-07-06 1989-01-17 Nippon Dia Clevite Co Carbon container for sintering
KR101231666B1 (en) * 2010-12-21 2013-02-08 재단법인 포항산업과학연구원 Method for coating adiabatic layer

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6411910A (en) * 1987-07-06 1989-01-17 Nippon Dia Clevite Co Carbon container for sintering
KR101231666B1 (en) * 2010-12-21 2013-02-08 재단법인 포항산업과학연구원 Method for coating adiabatic layer

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