JPH0524400B2 - - Google Patents

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Publication number
JPH0524400B2
JPH0524400B2 JP59239384A JP23938484A JPH0524400B2 JP H0524400 B2 JPH0524400 B2 JP H0524400B2 JP 59239384 A JP59239384 A JP 59239384A JP 23938484 A JP23938484 A JP 23938484A JP H0524400 B2 JPH0524400 B2 JP H0524400B2
Authority
JP
Japan
Prior art keywords
heat
wall
insulating
metal structure
ceramic
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 - Lifetime
Application number
JP59239384A
Other languages
Japanese (ja)
Other versions
JPS61119893A (en
Inventor
Hideo Kawamura
Hiroshi Matsuoka
Keiichi Yamashita
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.)
Isuzu Motors Ltd
Original Assignee
Isuzu Motors Ltd
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 Isuzu Motors Ltd filed Critical Isuzu Motors Ltd
Priority to JP23938484A priority Critical patent/JPS61119893A/en
Publication of JPS61119893A publication Critical patent/JPS61119893A/en
Publication of JPH0524400B2 publication Critical patent/JPH0524400B2/ja
Granted legal-status Critical Current

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  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Thermal Insulation (AREA)

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明は内燃機関におけるセラミツクス断熱壁
と金属構造体との間の熱遮蔽を図る、内燃機関の
断熱構造に関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field] The present invention relates to a heat insulating structure for an internal combustion engine that provides heat shielding between a ceramic heat insulating wall and a metal structure in the engine.

[従来の技術] 従来から提案されているセラミツクスを利用し
た断熱内燃機関は、モノリスタイプのチツ化ケイ
素、炭化ケイ素などを主体としたセラミツクス断
熱壁を、ピストン本体、シリンダボデイ、シリン
ダヘツドなどの燃焼ガスに曝される金属構造体の
内壁に結合している。セラミツクス断熱壁からの
熱放散を抑えるために、セラミツクス断熱壁と金
属構造体との間に断熱空部を備えたり(特願昭58
−151885号)、爆発圧力に耐えるようにセラミツ
クス断熱壁と金属構造体との間に金属板からなる
ガスケツトを挾んだり(特開昭58−25552号公報)
しているが、上述のような手段ではセラミツクス
断熱壁から金属構造体へ放散される伝熱量を抑え
るには限界がある。燃焼室の壁部の熱伝導率はセ
ラミツクス断熱壁の採用により25分の1程度に減
少しても、燃焼室と金属構造体との熱落差が3倍
にも達するために、伝熱量は7分の1程度に減少
するにすぎない。
[Prior art] Adiabatic internal combustion engines using ceramics that have been proposed in the past have a monolith type ceramic insulating wall mainly made of silicon nitride, silicon carbide, etc., which is used for combustion in the piston body, cylinder body, cylinder head, etc. Bonded to the inner wall of a metal structure exposed to gas. In order to suppress heat dissipation from the ceramic insulation wall, a heat insulation cavity is provided between the ceramic insulation wall and the metal structure (Japanese Patent Application No. 1983).
-151885), a gasket made of a metal plate is interposed between the ceramic insulation wall and the metal structure to withstand the explosion pressure (Japanese Patent Laid-Open No. 58-25552).
However, with the above-mentioned means, there is a limit to suppressing the amount of heat dissipated from the ceramic insulation wall to the metal structure. Even though the thermal conductivity of the walls of the combustion chamber is reduced to about 1/25th due to the use of ceramic insulation walls, the heat drop between the combustion chamber and the metal structure is three times as large, so the amount of heat transfer is still 7 times as large. It will only decrease by about 1/2.

[発明が解決しようとする問題点] 本発明の目的は上述の問題に鑑み、燃焼室の断
熱化を図るために、セラミツクス断熱壁と金属構
造体との間に断熱空部における熱輻射を抑え、熱
効率を高める、内燃機関の断熱構造を提供するこ
とにある。
[Problems to be Solved by the Invention] In view of the above-mentioned problems, an object of the present invention is to suppress heat radiation in an insulated cavity between a ceramic insulating wall and a metal structure in order to insulate a combustion chamber. An object of the present invention is to provide a heat insulating structure for an internal combustion engine that increases thermal efficiency.

[問題点を解決するための手段] 上記目的を達成するために、本発明の構成は耐
熱性金属からなる中空リングの内部に低熱伝導率
の粉末を充填して断熱ガスケツトを形成し、金属
構造体とセラミツクス断熱壁との間に前記断熱ガ
スケツトを介装して断熱ガスケツトを貫通するボ
ルトにより結合し、断熱ガスケツトで囲まれた空
部において少くとも金属構造体の内壁にステンレ
ス鋼板からなる熱反射板を重ね合せたものであ
る。
[Means for Solving the Problems] In order to achieve the above object, the present invention has a configuration in which a hollow ring made of a heat-resistant metal is filled with a powder having low thermal conductivity to form an insulating gasket, and a metal structure is The insulating gasket is interposed between the body and the ceramic insulating wall, the insulating gasket is connected by a bolt passing through the insulating gasket, and at least the inner wall of the metal structure is provided with a heat reflector made of a stainless steel plate in the cavity surrounded by the insulating gasket. It is made of overlapping boards.

[作 用] セラミツクス断熱壁と金属構造体との間の断熱
空部の内壁に備えた、耐熱性を有するステンレス
鋼板からなる熱反射板は、燃焼ガスに曝されるセ
ラミツクス断熱壁から断熱空部を経て金属構造体
へ向う熱輻射を抑える。
[Function] A heat reflecting plate made of a heat-resistant stainless steel plate provided on the inner wall of the heat-insulating cavity between the ceramic heat-insulating wall and the metal structure is designed to protect the heat-insulating cavity from the ceramic heat-insulating wall exposed to combustion gas. suppresses heat radiation directed toward the metal structure.

[発明の実施例] 第1図は本発明の原理的な内燃機関の断熱構造
を示す。燃焼ガスに曝されるセラミツクス断熱壁
51は、金属構造体52との間に断熱ガスケツト
55を挾み、これらを貫通するボルト53にナツ
ト54を締め付けて結合される。断熱ガスケツト
55はセラミツクス断熱壁51と金属構造体52
との間に断熱空部Aを区画する。
[Embodiments of the Invention] FIG. 1 shows a basic thermal insulation structure of an internal combustion engine according to the present invention. A ceramic heat insulating wall 51 exposed to combustion gas is connected to a metal structure 52 by tightening a nut 54 to a bolt 53 passing through the heat insulating gasket 55. The heat insulating gasket 55 connects the ceramic heat insulating wall 51 and the metal structure 52.
A heat insulating space A is defined between the two.

本発明によれば、セラミツクス断熱壁51から
断熱空部Aを経て金属構造体52へ向う熱輻射を
阻止するために、セラミツクス断熱壁51と金属
構造体52との間の断熱空部Aを区画する内壁に
熱反射板を備えるものである。具体的には、金属
構造体52の内壁に、ステンレスなどの耐熱性を
有する熱反射板59aを重ね合せる。好ましくは
セラミツクス断熱壁51の内壁にも、熱反射板5
9を重ね合せる。
According to the present invention, in order to prevent heat radiation from the ceramic insulation wall 51 toward the metal structure 52 via the insulation cavity A, the insulation cavity A is defined between the ceramic insulation wall 51 and the metal structure 52. It is equipped with a heat reflecting plate on the inner wall. Specifically, a heat-reflecting plate 59a having heat resistance such as stainless steel is superimposed on the inner wall of the metal structure 52. Preferably, a heat reflecting plate 5 is also provided on the inner wall of the ceramic heat insulating wall 51.
Overlap 9.

第2図に示すように、断熱ガスケツト55はス
テンレスなどの耐熱性を有する金属板から形成し
た中空リング56の内部に、熱伝導率の小さいチ
タン酸カリウム、コージライトなどの粉末57を
充填して構成され、ボルト挿通穴は円筒体56a
を嵌合され、円筒体56aの両端は縁曲げして中
空リング56の上下両面へ結合される。特に、チ
タン酸カリウムの粉末を密実に充填することが好
ましく、ボルト53を締め付けても圧縮荷重に耐
え、金属構造体52とセラミツクス断熱壁51と
の間隔を保持する。
As shown in FIG. 2, the insulating gasket 55 is made by filling a hollow ring 56 made of a heat-resistant metal plate such as stainless steel with powder 57 of potassium titanate, cordierite, or the like having low thermal conductivity. The bolt insertion hole is a cylindrical body 56a.
are fitted, and both ends of the cylindrical body 56a are bent and connected to both upper and lower surfaces of the hollow ring 56. In particular, it is preferable to densely fill the powder of potassium titanate, so that even when the bolts 53 are tightened, the compressive load can be withstood and the distance between the metal structure 52 and the ceramic heat insulating wall 51 can be maintained.

本発明は上述のように、断熱空部Aを区画する
セラミツクス断熱壁51と金属構造体52との各
内壁に熱反射板59,59aを重ね合せたから、
高温の燃焼ガスに曝されるセラミツクス断熱壁5
1からの熱輻射が、熱反射板59により反射さ
れ、断熱空部Aへ到達する熱輻射量が低減され
る。金属構造体52の内壁にも熱反射板59aを
重ね合せたから、金属構造体52へ到達する熱輻
射量はさらに低減される。この結果、金属構造体
52とセラミツクス断熱壁51との間に断熱空部
Aを設けただけのものに比べて、セラミツクス断
熱壁51から金属構造体52への伝熱量は大幅に
低減される。
In the present invention, as described above, the heat reflecting plates 59 and 59a are superimposed on the inner walls of the ceramic heat insulating wall 51 and the metal structure 52 that partition the heat insulating cavity A.
Ceramic insulation wall 5 exposed to high temperature combustion gas
Thermal radiation from 1 is reflected by the heat reflecting plate 59, and the amount of thermal radiation reaching the heat insulating cavity A is reduced. Since the heat reflecting plate 59a is also superimposed on the inner wall of the metal structure 52, the amount of heat radiation reaching the metal structure 52 is further reduced. As a result, the amount of heat transferred from the ceramic heat insulating wall 51 to the metal structure 52 is significantly reduced compared to the case where the heat insulating cavity A is simply provided between the metal structure 52 and the ceramic heat insulating wall 51.

断熱ガスケツト55としての中空リング56
は、セラミツクス断熱壁51と金属構造体52に
重ね合された熱反射板59,59aに接し、中空
リング56は内部に熱伝導率の極めて小さいチタ
ン酸カリウムの粉末57を充填されるから、セラ
ミツクス断熱壁51から中空リング56とチタン
酸カリウムの粉末57を経て金属構造体52への
熱伝導による伝熱量は大幅に低減される。
Hollow ring 56 as insulating gasket 55
The hollow ring 56 is in contact with the heat reflecting plates 59, 59a superimposed on the ceramic heat insulating wall 51 and the metal structure 52, and the inside of the hollow ring 56 is filled with potassium titanate powder 57 having extremely low thermal conductivity. The amount of heat transferred from the heat insulating wall 51 to the metal structure 52 via the hollow ring 56 and the potassium titanate powder 57 is significantly reduced.

第3図はセラミツクスを用いた具体的な断熱内
燃機関の正面断面図である。通常の金属からなる
シリンダヘツド1の下部に円筒部1aが形成さ
れ、円筒部1aの内部にセラミツクスからなる逆
カツプ形のヘツドライナ3が上下1対の位置決め
リング9を介して嵌合される。シリンダヘツド1
の天壁面1bとヘツドライナ3の上面との間に、
リング26、燃料噴射ノズル5、吸・排気ポート
11をそれぞれ取り囲むリング10,16が介装
される。吸・排気ポート11はセラミツクスをコ
ーテイングされた吸・排気弁7により開閉され
る。燃焼室はセラミツクスからなる逆カツプ形の
ヘツドライナ3とセラミツクスからなるピストン
冠部8とにより区画される。ヘツドライナ3はセ
ラミツクスからなるシリンダライナ4と、燃焼室
の主要部から離れた部分で突き合される。
FIG. 3 is a front sectional view of a specific adiabatic internal combustion engine using ceramics. A cylindrical portion 1a is formed at the lower part of a cylinder head 1 made of ordinary metal, and an inverted cup-shaped head liner 3 made of ceramic is fitted inside the cylindrical portion 1a via a pair of upper and lower positioning rings 9. Cylinder head 1
between the ceiling wall surface 1b and the top surface of the head liner 3,
Rings 10 and 16 are interposed to surround the ring 26, the fuel injection nozzle 5, and the intake/exhaust ports 11, respectively. The intake/exhaust ports 11 are opened and closed by intake/exhaust valves 7 coated with ceramics. The combustion chamber is defined by an inverted cup-shaped head liner 3 made of ceramics and a piston crown 8 made of ceramics. The head liner 3 butts against a cylinder liner 4 made of ceramics at a portion away from the main part of the combustion chamber.

実際には、ヘツドライナ3とシリンダライナ4
との熱膨張差による応力を回避するために、両者
の間は極めて僅かな〓間を備えられ、断熱ガスケ
ツト55と同様のガスケツト22が、ヘツドライ
ナ3の下端面とシリンダボデイ2の上端面との間
に介装され、シリンダヘツド1から図示してない
ボルトをシリンダボデイ2へ螺合して締結され
る。シリンダライナ4はシリンダボデイ2の円筒
部20に嵌合される。
Actually, head liner 3 and cylinder liner 4
In order to avoid stress due to the difference in thermal expansion between the head liner 3 and the cylinder body 2, an extremely small gap is provided between the two, and a gasket 22 similar to the heat insulating gasket 55 connects the lower end surface of the head liner 3 and the upper end surface of the cylinder body 2. A bolt (not shown) is inserted from the cylinder head 1 into the cylinder body 2 and fastened. The cylinder liner 4 is fitted into the cylindrical portion 20 of the cylinder body 2.

ピストン19はセラミツクスからなるピストン
冠部8を普通の金属からなるスカート部6の上に
重ね合せ、上から挿通したボルト31にナツト3
3を螺合して締結される。ピストン冠部8は上面
に燃料と空気の混合を促す窪み39を、下面中央
に円筒部34を、下面周縁部に段部をそれぞれ設
けられる。スカート部6は外周面にピストンリン
グ41を装着され、上面周縁部に設けた突条24
に前述のピストン冠部8の段部を嵌合される。ス
カート部6は上面中央に形成した柱35に、ガス
ケツト27を介してピストン冠部8を重ね合さ
れ、柱35と円筒部34との間に断熱空部Dを形
成される。ピストン冠部8とスカート部6との外
周側の重合せ面は、シールリング28を介装され
る。
The piston 19 has a piston crown part 8 made of ceramics superimposed on a skirt part 6 made of ordinary metal, and a nut 3 attached to a bolt 31 inserted from above.
3 are screwed together. The piston crown portion 8 is provided with a recess 39 on the upper surface to promote mixing of fuel and air, a cylindrical portion 34 at the center of the lower surface, and a stepped portion on the peripheral edge of the lower surface. The skirt portion 6 has a piston ring 41 mounted on its outer circumferential surface, and a protrusion 24 provided on its upper circumferential edge.
The above-mentioned stepped portion of the piston crown portion 8 is fitted into the piston crown portion 8. The piston crown 8 is superimposed on a pillar 35 formed at the center of the upper surface of the skirt part 6 via a gasket 27, and a heat insulating cavity D is formed between the pillar 35 and the cylindrical part 34. A seal ring 28 is interposed between the overlapping surfaces of the piston crown portion 8 and the skirt portion 6 on the outer peripheral side.

上述のように、シリンダヘツド11の円筒部1
aの内周面とヘツドライナ3との間に、上下1対
のリング9により閉鎖された断熱空部Cが形成さ
れ、シリンダヘツド1の天壁面1bとヘツドライ
ナ3の上面との間に、リング10,16,26に
より閉鎖された断熱空部Bが形成される。ピスト
ン冠部8とスカート部6との間に、リング28に
より閉鎖された断熱空部Dが形成される。
As mentioned above, the cylindrical portion 1 of the cylinder head 11
A heat insulating cavity C closed by a pair of upper and lower rings 9 is formed between the inner peripheral surface of the cylinder head 1 and the head liner 3, and a ring 10 is formed between the top wall surface 1b of the cylinder head 1 and the upper surface of the head liner 3. , 16, 26 form a closed adiabatic cavity B. A heat insulating cavity D closed by a ring 28 is formed between the piston crown part 8 and the skirt part 6.

上述したシリンダヘツド1の断熱空部B,Cと
ピストン19の断熱空部Dは、第1図に示した断
熱空部Aと同様に、断熱空部の内壁に熱反射板を
備えられ、燃焼室からヘツドライナ3を経てシリ
ンダヘツド1へ向う熱輻射を抑え、ピストン冠部
8からスカート部6へ向う熱輻射を抑える。
The heat-insulating cavities B and C of the cylinder head 1 and the heat-insulating cavity D of the piston 19 described above are equipped with a heat reflecting plate on the inner wall of the heat-insulating cavity, similar to the heat-insulating cavity A shown in FIG. Heat radiation from the chamber to the cylinder head 1 via the head liner 3 is suppressed, and heat radiation from the piston crown part 8 to the skirt part 6 is suppressed.

断熱空部Bの場合は、燃焼噴射ノズル5の取付
穴と吸・排気ポート11の穴を備えた上下2枚の
ステンレス鋼板を、シリンダヘツド1の天壁面1
bとヘツドライナ3の上面とにそれぞれ重ね合
せ、両者の間にガスケツト10,16,26を挾
んで熱反射板を形成する。燃焼噴射ノズル5の取
付穴と吸・排気ポート11の穴の各周囲には、第
2図に示すような断熱ガスケツト55またはイン
コネルなどの耐熱性金属からなる断面円形の中空
リングを装着してヘツドボルトの締付荷重を支持
する。
In the case of the heat insulating space B, two stainless steel plates (upper and lower) with mounting holes for the combustion injection nozzle 5 and holes for the intake/exhaust ports 11 are attached to the top wall surface 1 of the cylinder head 1.
b and the upper surface of the head liner 3, respectively, and gaskets 10, 16, and 26 are sandwiched between them to form a heat reflecting plate. Around each of the mounting holes of the combustion injection nozzle 5 and the holes of the intake/exhaust port 11, an insulating gasket 55 as shown in FIG. 2 or a hollow ring with a circular cross section made of a heat-resistant metal such as Inconel is installed and the head bolts Supports the tightening load of

断熱空部Cの場合は、熱反射板としてステンレ
ス鋼板からなる内外2つの円筒体の上下端部の間
に、位置決めリング9を装着して備える。
In the case of the heat insulating space C, a positioning ring 9 is installed as a heat reflecting plate between the upper and lower ends of two inner and outer cylindrical bodies made of stainless steel plates.

ピストン19の断熱空部Dの場合は、断熱空部
Dの内壁にステンレス鋼板からなる熱反射板を貼
り付けるか、クロムメツキを施す。
In the case of the heat insulating cavity D of the piston 19, a heat reflecting plate made of a stainless steel plate is attached to the inner wall of the heat insulating cavity D, or chrome plating is applied.

[発明の効果] 本発明は上述のように、耐熱性金属からなる中
空リングの内部に低熱伝導率の粉末を充填して断
熱ガスケツトを形成し、金属構造体とセラミツク
ス断熱壁との間に前記断熱ガスケツトを介装して
断熱ガスケツトを貫通するボルトにより結合し、
断熱ガスケツトで囲まれた空部において少くとも
金属構造体の内壁にステンレス鋼板からなる熱反
射板を重ね合せたものであるから、次のような効
果が得られる。
[Effects of the Invention] As described above, the present invention includes filling a hollow ring made of a heat-resistant metal with a powder having low thermal conductivity to form a heat insulating gasket, and forming the heat insulating gasket between the metal structure and the ceramic heat insulating wall. Interpose an insulating gasket and connect with bolts that pass through the insulating gasket,
Since a heat reflecting plate made of a stainless steel plate is superimposed on at least the inner wall of a metal structure in a cavity surrounded by a heat insulating gasket, the following effects can be obtained.

金属製のシリンダヘツドの内部に耐熱性に優れ
たセラミツクス製のヘツドライナを断熱空部を存
して嵌挿したことにより、燃焼室の燃焼ガスの温
度を高温に保つことができる。
By inserting a ceramic head liner with excellent heat resistance inside the metal cylinder head with an insulating cavity, the temperature of the combustion gas in the combustion chamber can be maintained at a high temperature.

ヘツドライナの外側に断熱空部を設けたことに
より、ヘツドライナからシリンダヘツドへの伝熱
量を抑え、シリンダヘツドを高温から保護でき
る。
By providing a heat insulating cavity outside the head liner, the amount of heat transferred from the head liner to the cylinder head can be suppressed and the cylinder head can be protected from high temperatures.

断熱空部の外側、すなわちシリンダヘツドの円
筒部の内面に熱反射板を重ね合せたことにより、
ヘツドライナから断熱空部を経て外部へ向う輻射
による伝熱量を抑止できる。
By superimposing a heat reflecting plate on the outside of the heat-insulating cavity, that is, on the inner surface of the cylindrical part of the cylinder head,
It is possible to suppress the amount of heat transfer due to radiation from the heat liner to the outside through the heat insulating cavity.

ヘツドライナとシリンダヘツドとの間に断熱空
部を形成するための断熱ガスケツトは、ステンレ
スなどの耐熱性金属からなる中空リングの内部に
熱伝導率の小さい粉末を充填したので、シリンダ
ヘツドとヘツドライナを結合する締付ボルトの締
付荷重に対して十分な強度を有し、ヘツドライナ
から断熱ガスケツトを経てシリンダヘツドへ向う
伝熱量を抑止できる。
The insulating gasket for forming an insulating cavity between the head liner and the cylinder head is a hollow ring made of heat-resistant metal such as stainless steel, filled with powder with low thermal conductivity, which connects the cylinder head and the head liner. It has sufficient strength to withstand the tightening load of the tightening bolt, and can suppress the amount of heat transferred from the head liner to the cylinder head via the insulating gasket.

金属構造体とセラミツクス断熱壁との間の空部
に、熱反射板を配設することは、従来の断熱内燃
機関に何ら設計変更をもたらさないで容易に実施
でき、燃焼室からの熱放散を抑え、内燃機関の熱
効率を向上できる。
Placing a heat reflector in the space between the metal structure and the ceramic insulation wall can be easily implemented without any design changes to conventional insulated internal combustion engines, and can reduce heat dissipation from the combustion chamber. This can improve the thermal efficiency of internal combustion engines.

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

第1図は内燃機関の断熱構造の原理的構成を示
す断面図、第2図は同断熱構造における金属構造
体とセラミツクス断熱壁との間に断熱空部を形成
するための断熱ガスケツトの一例を示す正面断面
図、第3図は本発明に係る断熱構造が適用される
断熱内燃機関の正面断面図である。 51:セラミツクス断熱壁、52:金属構造
体、5:断熱ガスケツト、59,59a:熱反射
板。
Figure 1 is a sectional view showing the basic structure of a heat insulation structure for an internal combustion engine, and Figure 2 is an example of a heat insulation gasket for forming a heat insulation cavity between a metal structure and a ceramic heat insulation wall in the heat insulation structure. FIG. 3 is a front sectional view of an adiabatic internal combustion engine to which the heat insulating structure according to the present invention is applied. 51: Ceramic heat insulating wall, 52: Metal structure, 5: Heat insulating gasket, 59, 59a: Heat reflecting plate.

Claims (1)

【特許請求の範囲】[Claims] 1 耐熱性金属からなる中空リングの内部に低熱
伝導率の粉末を充填して断熱ガスケツトを形成
し、金属構造体とセラミツクス断熱壁との間に前
記断熱ガスケツトを介装して断熱ガスケツトを貫
通するボルトにより結合し、断熱ガスケツトで囲
まれた空部において少くとも金属構造体の内壁に
ステンレス鋼板からなる熱反射板を重ね合せたこ
とを特徴とする、内燃機関の断熱構造。
1 Filling the inside of a hollow ring made of heat-resistant metal with powder of low thermal conductivity to form an insulating gasket, interposing the insulating gasket between the metal structure and the ceramic insulating wall, and penetrating the insulating gasket. A heat insulating structure for an internal combustion engine, characterized in that a heat reflecting plate made of a stainless steel plate is superimposed on at least the inner wall of a metal structure in a space connected by bolts and surrounded by a heat insulating gasket.
JP23938484A 1984-11-15 1984-11-15 Heat-insulating structure of heat engine, etc. Granted JPS61119893A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP23938484A JPS61119893A (en) 1984-11-15 1984-11-15 Heat-insulating structure of heat engine, etc.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP23938484A JPS61119893A (en) 1984-11-15 1984-11-15 Heat-insulating structure of heat engine, etc.

Publications (2)

Publication Number Publication Date
JPS61119893A JPS61119893A (en) 1986-06-07
JPH0524400B2 true JPH0524400B2 (en) 1993-04-07

Family

ID=17043981

Family Applications (1)

Application Number Title Priority Date Filing Date
JP23938484A Granted JPS61119893A (en) 1984-11-15 1984-11-15 Heat-insulating structure of heat engine, etc.

Country Status (1)

Country Link
JP (1) JPS61119893A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6419151A (en) * 1987-07-11 1989-01-23 Isuzu Motors Ltd Cooling device for heat insulated engine
JP4702103B2 (en) * 2006-03-01 2011-06-15 日産自動車株式会社 Engine intake control method and intake control device
JP5807220B2 (en) * 2010-12-30 2015-11-10 株式会社ザイキューブ Interposer and semiconductor module using the same

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5821095A (en) * 1981-07-31 1983-02-07 株式会社日立製作所 Heat insulating piping unit
JPS59122765A (en) * 1982-12-29 1984-07-16 Isuzu Motors Ltd Adiabatic engine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5821095A (en) * 1981-07-31 1983-02-07 株式会社日立製作所 Heat insulating piping unit
JPS59122765A (en) * 1982-12-29 1984-07-16 Isuzu Motors Ltd Adiabatic engine

Also Published As

Publication number Publication date
JPS61119893A (en) 1986-06-07

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