JPS6255944B2 - - Google Patents
Info
- Publication number
- JPS6255944B2 JPS6255944B2 JP58062021A JP6202183A JPS6255944B2 JP S6255944 B2 JPS6255944 B2 JP S6255944B2 JP 58062021 A JP58062021 A JP 58062021A JP 6202183 A JP6202183 A JP 6202183A JP S6255944 B2 JPS6255944 B2 JP S6255944B2
- Authority
- JP
- Japan
- Prior art keywords
- heat insulating
- metal material
- ceramic
- metal
- forming body
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B77/00—Component parts, details or accessories, not otherwise provided for
- F02B77/11—Thermal or acoustic insulation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2251/00—Material properties
- F05C2251/04—Thermal properties
- F05C2251/042—Expansivity
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Description
【発明の詳細な説明】
本発明は内燃機関の燃焼室から排出される排気
ガスの保温構造に係わり、更に詳しくは保温の為
の断熱層形成体の構造に関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a heat insulating structure for exhaust gas discharged from a combustion chamber of an internal combustion engine, and more particularly to a structure of a heat insulating layer forming body for heat insulating.
内燃機関の燃焼室を保温することにより燃焼温
度が上昇して熱効率が向上するのに加え、排気ガ
ス中のHC濃度の低減に有効であることが知られ
ている。又、排気公害対策としてサーマルリアク
ターや触媒コンバーターを排気系統に配設するこ
とが行われるようになつて来たが、この種の装置
は排気が所定温度に達する迄は排気の充分な浄化
作用を得ることが出来ない。従つてこれ等の装置
を有効に作動させる為にも、燃焼室から排出され
る排気の温度を出来る限り低下させないように保
温することが望ましい。 It is known that insulating the combustion chamber of an internal combustion engine increases combustion temperature and improves thermal efficiency, and is also effective in reducing the HC concentration in exhaust gas. Additionally, as a measure against exhaust pollution, thermal reactors and catalytic converters have been installed in the exhaust system, but these types of devices do not provide sufficient exhaust purification until the exhaust reaches a predetermined temperature. I can't get it. Therefore, in order to operate these devices effectively, it is desirable to keep the temperature of the exhaust gas discharged from the combustion chamber as low as possible.
このような排気の保温を行う為に、断熱材であ
るセラミツクス自体を燃焼室内面、ピストン上面
及び排気ポート内面に直接に固定したり、溶射す
ることが行われていた。しかしながらこのような
方法でセラミツクスの断熱層を形成しても、セラ
ミツクスと機関構造金属との熱膨張率の相違や、
振動及び衝撃等の影響によりセラミツクスが割れ
て剥れ落ち、耐久性上問題があること、更に、燃
焼室の場合には、機関寿命を著しく短縮してしま
う欠点が避けられず、問題となつていた。即ち、
極めて過酷な使用条件にも充分耐えられるような
断熱層の形成、換言すればセラミツクスを金属材
料と如何に結合すれば過酷条件にも耐えられるか
が最大の課題となつていた。 In order to insulate the exhaust gas, ceramics itself, which serves as a heat insulating material, has been directly fixed or thermally sprayed on the inside of the combustion chamber, the top of the piston, and the inside of the exhaust port. However, even if a ceramic heat insulating layer is formed using this method, there may be a difference in thermal expansion coefficient between the ceramic and the engine structural metal,
The effects of vibration and impact can cause ceramics to crack and peel off, causing problems in terms of durability.Furthermore, in the case of combustion chambers, there are unavoidable shortcomings that significantly shorten the engine life, which is a problem. Ta. That is,
The biggest challenge has been how to form a heat insulating layer that can withstand extremely harsh usage conditions, or in other words, how to combine ceramics with metal materials to withstand even the harshest conditions.
本発明はこの点に鑑みてなされたものであり、
従来の欠点を解消して過酷な条件にも耐え得る内
燃機関の排気保温の為の断熱層形成体の構造を提
供することを目的とする。 The present invention has been made in view of this point,
It is an object of the present invention to provide a structure of a heat insulating layer forming body for heat insulating the exhaust gas of an internal combustion engine, which eliminates the conventional drawbacks and can withstand even severe conditions.
この構造とは、セラミツクスを熱膨張差を吸収
する空孔もしくは空隙の多い金属材料に含浸させ
て焼成された断熱材が機関構造部材の所定位置に
鋳ぐるまれて構成されていることを特徴とするも
のである。 This structure is characterized by a heat insulating material made by impregnating ceramics with pores or a metal material with a large number of voids to absorb differences in thermal expansion, and then casting the fired heat insulating material into predetermined positions of engine structural members. It is something to do.
即ちこの特徴により、本発明による断熱層形成
体はそれ自体が熱伝導率の小さなセラミツクスと
熱膨張差を吸収する空孔もしくは空隙の多い金属
材料との組合わせにより優れた断熱性を得られ、
しかもこの断熱材が機関構造部材に鋳ぐるまれて
いるので固定が確実となり、熱膨張率の相違等に
よる悪影響は空孔もしくは空隙の多い金属材料に
より吸収され、セラミツクス層に例えき裂が生じ
ても脱落する危険性は著しく低減されるのであ
る。 That is, due to this feature, the heat insulating layer forming body according to the present invention can obtain excellent heat insulating properties by combining ceramics, which itself has a small thermal conductivity, and a metal material with many pores or voids that absorb the difference in thermal expansion.
Moreover, since this heat insulating material is cast into the engine structural members, it is securely fixed, and the negative effects caused by differences in thermal expansion coefficients are absorbed by the metal material with many pores or voids, preventing cracks from occurring in the ceramic layer. The risk of them falling off is significantly reduced.
以下に本発明の実施例につき図面を参照して更
に詳しく説明する。 Embodiments of the present invention will be described in more detail below with reference to the drawings.
第1図に示した実施例に於いては、便宜的に〇
印を連らねて示した範囲Aが断熱材の芯材となる
熱膨張差を吸収する空孔もしくは空隙の多い金属
材料1である。この金属材料1には片側のある範
囲にわたり符点で示したセラミツクス2が金属材
料1内に含浸され且つ焼成されてセラミツクス層
Bを形成している。又金属材料1の他側は右斜線
で示した機関構造部材3内にある範囲にわたり埋
め込まれるように鋳ぐるまれている。即ちこの構
成に於いては、金属材料1がセラミツクスの芯材
として作用するためこのセラミツクス2の担持体
をなすとともに構造部材3との連結体をなし、か
つセラミツクス層Bが主たる断熱層形成体を構成
しているのである。 In the embodiment shown in FIG. 1, a range A indicated by a series of circles for convenience is a metal material 1 with many holes or voids that absorbs the difference in thermal expansion and becomes the core material of the heat insulating material. It is. A ceramic layer B is formed by impregnating the metal material 1 over a certain area on one side with a ceramic 2 indicated by a dot. The other side of the metal material 1 is cast so as to be embedded within a certain range of the engine structural member 3 shown by diagonal lines on the right. That is, in this configuration, the metal material 1 acts as a core material for the ceramics, and therefore serves as a support for the ceramics 2 as well as a connecting body with the structural member 3, and the ceramic layer B serves as the main heat insulating layer forming body. It is composed of
このような構成は例えば先ず多孔性金属材料1
に対して適当にセラミツクス2を含浸塗布させて
焼成することで断熱材を形成し、然る後これらの
断熱材を排気保温の為に取付けることが望まれる
機関構成部材の鋳造に際して所定位置に一緒に鋳
ぐるむことによつて達成出来る。 For example, such a configuration first includes a porous metal material 1.
A heat insulating material is formed by impregnating and applying ceramics 2 to the material and firing the material, and then these heat insulating materials are placed together in a predetermined position when casting an engine component to which it is desired to be installed for exhaust heat insulation. This can be achieved by immersing yourself in the
この実施例に於いては、金属材料1に含浸され
焼成されるセラミツクス層Bも若干の多孔性を有
することが出来、機関運転時に未燃HCがこのセ
ラミツクス層B内に捕捉されて燃焼され得るの
で、HC排出量を更に低減出来る効果が得られ
る。又構造部材3の鋳造時に金属材料1の空孔も
しくは空隙内に鋳造金属が浸透し、強固な固定即
ち鋳造金属と断熱材との接続固定を得られる。更
に又、機関運転時に生じる熱応力等によるセラミ
ツクス層Bの変形は、芯材である金属材料1が熱
膨張差を吸収するものであることから充分に吸収
され、又セラミツクス2が剥がれて燃焼室内等に
脱落する危険は強い結合により充分に低減出来る
のである。 In this embodiment, the ceramic layer B impregnated with the metal material 1 and fired can also have some porosity, and unburned HC can be trapped in this ceramic layer B and burned during engine operation. Therefore, the effect of further reducing HC emissions can be obtained. Furthermore, when the structural member 3 is cast, the cast metal penetrates into the pores or voids of the metal material 1, so that strong fixation, that is, the connection and fixation of the cast metal and the heat insulating material can be achieved. Furthermore, the deformation of the ceramic layer B due to thermal stress etc. that occurs during engine operation is sufficiently absorbed because the metal material 1, which is the core material, absorbs the difference in thermal expansion, and the ceramic layer 2 is peeled off, causing damage to the combustion chamber. The risk of the material falling off due to other factors can be sufficiently reduced by strong bonding.
第2図に示す実施例は前述の実施例に加えて更
に金属材料1による応力吸収性の向上を図つた構
成を示している。即ち、セラミツクス層Bと構成
部材3の界面4との間に金属材料1だけの層Cを
形成してある。このように構成すれば、層Cによ
り構成部材3とセラミツクス層Bとの間の応力は
ほとんど吸収されるので、セラミツクス層Bのき
裂発生等が更に低減される利点がある。 The embodiment shown in FIG. 2 shows a structure in which, in addition to the above-mentioned embodiment, the stress absorbability of the metal material 1 is further improved. That is, a layer C of only the metal material 1 is formed between the ceramic layer B and the interface 4 of the component 3. With this configuration, most of the stress between the component 3 and the ceramic layer B is absorbed by the layer C, so there is an advantage that the occurrence of cracks in the ceramic layer B is further reduced.
第3図に示す実施例は断熱材の成形時に更にセ
ラミツクス層Bの表面に金属溶射や金属デイツプ
等による表面処理を行つて被覆層Dを形成し、こ
れを構造部材3に鋳ぐるんだ構成を示している。
このように被覆層Dを形成することにより、たと
えセラミツクス層Bにき裂が生じても、割れたセ
ラミツクス2の小片が脱落する危険性が大巾に低
減される利点がある。 The embodiment shown in FIG. 3 has a structure in which, when forming the heat insulating material, the surface of the ceramic layer B is further subjected to surface treatment by metal spraying, metal dip, etc. to form a coating layer D, and this is cast into the structural member 3. It shows.
By forming the coating layer D in this manner, even if a crack occurs in the ceramic layer B, there is an advantage that the risk of small pieces of the broken ceramic 2 falling off is greatly reduced.
第4図〜第6図に示した各実施例は夫々第1図
〜第3図の実施例に於けるセラミツクス層Bの厚
さを増し、セラミツクス2だけの部分Eを形成す
るように構成したものである。このようにセラミ
ツクス2だけの部分Eが形成されることにより、
セラミツクス自体は熱伝導率が小さいので断熱効
果を更に向上することが出来、目的とする保温の
為に極めて有利となる。 In each of the embodiments shown in FIGS. 4 to 6, the thickness of the ceramic layer B in the embodiments shown in FIGS. 1 to 3 is increased to form a portion E consisting only of ceramics 2. It is something. By forming the portion E of only the ceramics 2 in this way,
Since ceramics itself has a low thermal conductivity, it is possible to further improve the heat insulation effect, which is extremely advantageous for achieving the desired heat retention.
ここで数値的に例をあげれば、例えば芯材とな
る熱膨張差を吸収する空孔もしくは空隙の多い金
属材料1の厚さ即ちAは大体6mm〜8mmとされ、
セラミツクス層Bの厚さは大体3mm〜4mmとさ
れ、鋳造金属3が前記金属材料1内に浸透する深
さは大体2mm〜3mmとされ、更に又前記金属材料
1自体の層Cの厚さは大体3mm〜4mmとされるこ
とによつて充分な結果を得られることが見出され
ている。 To give a numerical example here, for example, the thickness of the metal material 1 which is a core material and has many pores or voids that absorb the difference in thermal expansion, that is, A is approximately 6 mm to 8 mm,
The thickness of the ceramic layer B is approximately 3 mm to 4 mm, the depth at which the cast metal 3 penetrates into the metal material 1 is approximately 2 mm to 3 mm, and the thickness of the layer C of the metal material 1 itself is approximately 2 mm to 3 mm. It has been found that satisfactory results can be obtained with a thickness of approximately 3 mm to 4 mm.
熱膨張差としては、鋳造金属とセラミツクスの
材質によつて異なるが、AlとSicの組合せの場合
で約10〜50μ程度であり、空孔もしくは空隙の多
い金属材料で吸収する。 The difference in thermal expansion varies depending on the materials of the cast metal and ceramics, but in the case of a combination of Al and Sic, it is about 10 to 50μ, and is absorbed by a metal material with many pores or voids.
又、前述の説明では多孔性金属材料との総称で
述べたが、これには粉末焼結多孔体、繊維焼結多
孔体及び海綿状金属等の空孔率がある程度大きい
金属材料が使用出来、例えば海綿状金属としては
空孔率30〜70%程度の発泡金属が好ましく、又こ
れ以外に「グツドローパツキン」なる商品名で市
販されている耐熱金属で作つた金タワシ状の材料
も好ましく使用出来る。 In addition, in the above explanation, the general term "porous metal material" was used, but metal materials with a certain degree of porosity such as powder sintered porous bodies, fiber sintered porous bodies, and spongy metals can be used. For example, a foamed metal with a porosity of about 30 to 70% is preferable as the spongy metal, and a metal scrubber-like material made of a heat-resistant metal sold under the trade name "Gutsudoropatsukin" is also preferably used. I can do it.
空孔もしくは空隙の多い金属材料の組成として
は例えばニツケルクロム合金のようなNiをベー
スとした耐熱合金を使用でき、またNiをベース
として組成の例えばニツケルクロム合金は熱膨張
差を吸収する金属材料としても使用することがで
きる。また、このような空孔もしくは空隙の多い
金属材料の製造方法および製造条件を簡単に説明
すれば、例えばウレタン発泡樹脂に対し、液体を
加えられて泥状とされた金属粉を充填し、乾燥さ
せた後加熱してウレタンを焼く。然る後さらに温
度を高めて1300℃〜1400℃で焼結させる。これに
より前述した熱膨張差を吸収する空孔もしくは空
隙の多い金属材料として使用できる金属材料が得
られる。 For example, a Ni-based heat-resistant alloy such as a nickel-chromium alloy can be used as a metal material with many pores or voids, and a nickel-chromium alloy with a Ni-based composition that absorbs thermal expansion differences can be used. It can also be used as In addition, to briefly explain the manufacturing method and manufacturing conditions for metal materials with many pores or voids, for example, urethane foam resin is filled with metal powder that has been made into a slurry by adding a liquid, and then dried. After heating, the urethane is baked. After that, the temperature is further increased to 1300°C to 1400°C for sintering. As a result, a metal material that can be used as a metal material with many pores or voids that absorb the above-mentioned difference in thermal expansion can be obtained.
一方、使用できるセラミツクスの組成としては
例えば窒化珪素(Si3N4)がある。セラミツクスを
空孔もしくは空隙の多い金属材料に含浸させる方
法としては、例えば窒化珪素の粉をSiの粉と混合
し、粘土状にしたものを前記金属材料に押しつけ
て含浸させることができる。セラミツクスの含浸
厚さは例えば3〜4mmとされる。セラミツクスの
焼成は、例えば上記セラミツクスを前記金属材料
に含浸させたものを例えば窒素雰囲気中にて加熱
し、1300℃前後にて焼結させて行われる。 On the other hand, examples of the composition of ceramics that can be used include silicon nitride (Si 3 N 4 ). As a method for impregnating ceramic into a metal material with many pores or voids, for example, silicon nitride powder can be mixed with Si powder, and the clay-like mixture can be pressed onto the metal material to impregnate it. The impregnation thickness of the ceramic is, for example, 3 to 4 mm. Firing of ceramics is carried out, for example, by impregnating the above-mentioned ceramic into the above-mentioned metal material, heating it in, for example, a nitrogen atmosphere, and sintering it at around 1300°C.
空孔もしくは空隙の多い金属材料にセラミツク
スを焼成させて形成した断熱材を内燃機関の構成
部材の所定個所に鋳ぐるむ方法は、例えば特公昭
52−48602号公報等に記載されている方法で行わ
れる。このような方法は当業者にとつて良く知ら
れた方法であり、断熱材を鋳型内の所定位置に設
置する方法も通常の鋳ぐるみ鋳造方法で行われる
何れかの適当な方法を採用すれば良い。また、例
えばアルミニウム合金製の内燃機関構成部材に鋳
ぐるむ場合にはその鋳込み温度は670℃〜720℃程
度で行われるのであり、断熱材に何等の障害も生
じないことは勿論である。 For example, a method of casting a heat insulating material made by firing ceramics into a metal material with many pores or voids into predetermined locations of the structural members of an internal combustion engine is known as
This is carried out by the method described in Publication No. 52-48602, etc. Such methods are well known to those skilled in the art, and the method for placing the insulation material in a predetermined position within the mold can be any suitable method used in conventional cast casting methods. good. Furthermore, when casting into an internal combustion engine component made of aluminum alloy, for example, the casting temperature is about 670°C to 720°C, and it goes without saying that no damage will occur to the heat insulating material.
前述した如き本発明による断熱材すなわち芯材
となる多孔性金属材料1にセラミツクス2を含浸
焼成し、更に任意ではあるが被覆層Dを形成して
なる断熱材を実際に機関の適所に配設した状態を
第7図〜第9図に示す。第7図はシリンダーヘツ
ド6の燃焼室内面及びシリンダーボアーの上部側
壁全周に沿つて断熱材Sを配設した場合を示し、
第8図はピストン7の上面に断熱材Sを配設した
場合を示し、又第9図はシリンダーヘツド6の特
に排気ポート10の壁面に沿つて断熱材Sを配設
した場合を示している。このように断熱材Sを配
設し組合せることによつて、燃焼室及び排気ポー
ト10に於ける保温が充分に行い得て、燃焼室に
於いては熱効率が向上するとともに前述した如く
HC排出が低減され、排気ポート10に於いては
排気の酸化持続が行われるとともに保温によるサ
ーマルリアクターや触媒コンバーターの有効な作
動を確保出来る。 The heat insulating material according to the present invention as described above, that is, the porous metal material 1 serving as the core material is impregnated with ceramics 2 and fired, and further, optionally, a covering layer D is formed, and the heat insulating material is actually placed at a suitable location in the engine. This state is shown in FIGS. 7 to 9. FIG. 7 shows a case where a heat insulating material S is provided along the entire circumference of the inner surface of the combustion chamber of the cylinder head 6 and the upper side wall of the cylinder bore.
FIG. 8 shows a case in which a heat insulating material S is provided on the upper surface of the piston 7, and FIG. 9 shows a case in which a heat insulating material S is provided along the wall surface of the cylinder head 6, especially the exhaust port 10. . By arranging and combining the heat insulating materials S in this way, it is possible to sufficiently retain heat in the combustion chamber and the exhaust port 10, improving thermal efficiency in the combustion chamber and as described above.
HC emissions are reduced, the exhaust gas continues to be oxidized at the exhaust port 10, and effective operation of the thermal reactor and catalytic converter can be ensured by heat retention.
以上説明した通り本発明による断熱層形成体の
構造は、断熱性に優れ、セラミツクスの固定強度
が極めて大きく、しかもセラミツクスに対する応
力を吸収出来るので耐久力が大巾に向上されるの
に加え、断熱材を予め形成した後これに所定位置
に鋳ぐるむものであるから、例えば排気ポート内
にも容易に配設出来る利点があり、実用上極めて
有利である。 As explained above, the structure of the heat insulating layer forming body according to the present invention has excellent heat insulating properties, extremely high fixing strength of ceramics, and can absorb stress to ceramics, so durability is greatly improved. Since the material is formed in advance and then cast in a predetermined position, it has the advantage that it can be easily disposed within, for example, an exhaust port, which is extremely advantageous in practice.
第1図は本発明の第1の実施例とせる断熱層形
成体の構成を示す断面図。第2図は第1図の実施
例に芯材自体の層を形成した実施例の構成を示す
断面図。第3図は第2図の実施例に被覆層を形成
した実施例の構成を示す断面図。第4図〜第6図
は第1図〜第3図の実施例のセラミツクス層を厚
くし、セラミツクス自体の層を形成した夫々の実
施例の構成を示す断面図。第7図〜第9図は夫々
燃焼室内面及びシリンダーボア内面、ピストン上
面、及び排気ポート壁面に本発明による断熱層形
成体を形成した状態を示す断面図。
1……多孔性金属材料、2……セラミツクス、
3……機関構造部材、4……界面、6……シリン
ダーヘツド、7……ピストン、10……排気ポー
ト。
FIG. 1 is a sectional view showing the structure of a heat insulating layer forming body according to a first embodiment of the present invention. FIG. 2 is a sectional view showing the structure of an embodiment in which a layer of the core material itself is formed in the embodiment of FIG. 1. FIG. 3 is a sectional view showing the structure of an embodiment in which a covering layer is formed on the embodiment of FIG. 2. 4 to 6 are cross-sectional views showing the structure of each embodiment in which the ceramic layer of the embodiment shown in FIGS. 1 to 3 is thickened and a layer of ceramic itself is formed. 7 to 9 are cross-sectional views showing the state in which the heat insulating layer forming body according to the present invention is formed on the inner surface of the combustion chamber, the inner surface of the cylinder bore, the upper surface of the piston, and the wall surface of the exhaust port, respectively. 1... Porous metal material, 2... Ceramics,
3... Engine structural member, 4... Interface, 6... Cylinder head, 7... Piston, 10... Exhaust port.
Claims (1)
金属材料にセラミツクスが含浸されて断熱材が形
成され、この断熱材が機関構成部材の鋳造時に所
定位置に鋳ぐるまれて構成されたことを特徴とす
る内燃機関の断熱層形成体。 2 前記セラミツクスの含浸焼成されたセラミツ
クス層と構造部材の浸透鋳ぐるみ部分の界面との
間に前記金属材料だけの層が形成されていること
を特徴とする特許請求の範囲第1項記載の内燃機
関の断熱層形成体。 3 前記セラミツクス層が前記金属材料に含浸焼
成された部分とセラミツクス自体の部分とからな
ることを特徴とする特許請求の範囲第1項記載の
内燃機関の断熱層形成体。 4 前記セラミツクス層の表面に金属からなる被
覆層が形成されていることを特徴とする特許請求
の範囲第1項乃至第3項の何れか1項に記載の内
燃機関の断熱層形成体。[Claims] 1. A heat insulating material is formed by impregnating ceramics into a metal material with many pores or voids that absorb differences in thermal expansion, and this heat insulating material is cast into a predetermined position during casting of engine component parts. A heat insulating layer forming body for an internal combustion engine, characterized in that: 2. The internal combustion engine according to claim 1, wherein a layer made of only the metal material is formed between the impregnated and fired ceramic layer of the ceramic and the interface of the impregnated cast part of the structural member. Engine insulation layer forming body. 3. The heat insulating layer forming body for an internal combustion engine according to claim 1, wherein the ceramic layer is comprised of a portion impregnated with the metal material and fired and a portion of the ceramic itself. 4. The heat insulating layer forming body for an internal combustion engine according to any one of claims 1 to 3, wherein a coating layer made of metal is formed on the surface of the ceramic layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6202183A JPS5927194A (en) | 1983-04-08 | 1983-04-08 | Heat insulating layer for internal-combustion engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6202183A JPS5927194A (en) | 1983-04-08 | 1983-04-08 | Heat insulating layer for internal-combustion engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5927194A JPS5927194A (en) | 1984-02-13 |
| JPS6255944B2 true JPS6255944B2 (en) | 1987-11-24 |
Family
ID=13188093
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6202183A Granted JPS5927194A (en) | 1983-04-08 | 1983-04-08 | Heat insulating layer for internal-combustion engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5927194A (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS60184949A (en) * | 1984-03-05 | 1985-09-20 | Isuzu Motors Ltd | Exhaust port of internal-combustion engine having inner face applied with heat insulating material |
| JPH09327103A (en) * | 1996-06-06 | 1997-12-16 | Isuzu Ceramics Kenkyusho:Kk | Control device for hybrid vehicle |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS4930707A (en) * | 1972-07-24 | 1974-03-19 |
-
1983
- 1983-04-08 JP JP6202183A patent/JPS5927194A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5927194A (en) | 1984-02-13 |
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