JPH068621B2 - Sealed structure of adiabatic engine - Google Patents

Sealed structure of adiabatic engine

Info

Publication number
JPH068621B2
JPH068621B2 JP59239382A JP23938284A JPH068621B2 JP H068621 B2 JPH068621 B2 JP H068621B2 JP 59239382 A JP59239382 A JP 59239382A JP 23938284 A JP23938284 A JP 23938284A JP H068621 B2 JPH068621 B2 JP H068621B2
Authority
JP
Japan
Prior art keywords
cylinder
ring
cylinder liner
metal
soft carbon
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
JP59239382A
Other languages
Japanese (ja)
Other versions
JPS61118550A (en
Inventor
英男 河村
寛 松岡
恵一 山下
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 JP59239382A priority Critical patent/JPH068621B2/en
Publication of JPS61118550A publication Critical patent/JPS61118550A/en
Publication of JPH068621B2 publication Critical patent/JPH068621B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/02Sealings between relatively-stationary surfaces
    • F16J15/021Sealings between relatively-stationary surfaces with elastic packing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B77/00Component parts, details or accessories, not otherwise provided for
    • F02B77/11Thermal or acoustic insulation

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明はセラミツクスを利用した断熱エンジンのシール
構造に関するものである。
TECHNICAL FIELD The present invention relates to a seal structure of a heat insulating engine using ceramics.

[従来の技術] 高温に耐えしかも断熱効果の優れたセラミツクスをエン
ジンの燃焼室の壁部に使用することにより、熱サイクル
効率の向上を図るとともに、高温の排気を排気タービン
へ送るなどしてエネルギを回収し、全体としての熱効率
を向上する断熱エンジンは、例えば特開昭58-72652号公
報などに開示されているが、いまだ種々の問問題で実用
の段階に達していない。
[Prior Art] By using ceramics that withstands high temperatures and has an excellent heat insulation effect on the wall of the combustion chamber of the engine, the thermal cycle efficiency is improved and the high temperature exhaust is sent to an exhaust turbine to save energy. An adiabatic engine that recovers heat and improves the overall thermal efficiency is disclosed in, for example, Japanese Patent Laid-Open No. 58-72652, but it has not reached the stage of practical use due to various problems.

特に、セラミツクス製のヘツドライナとセラミツクス製
のシリンダライナとが直接合しないようにし、金属製の
シリンダヘツドと金属製のシリンダ本体とがガスケツト
を挟んで結合される構造では、燃焼室の燃焼ガスがシリ
ンダライナの上端部から洩れると、シリンダ本体の円筒
部とシリンダライナとの隙間を経てクランク室へ吹き抜
ける恐れがある。つまり、シリンダ本体とシリンダライ
ナとの熱膨張率の相違から両者の嵌合部に僅かな隙間が
生じると、燃焼ガスがヘツドライナの下端部とシリンダ
ライナの上端部との隙間から、シリンダ本体の円筒部と
シリンダライナとの嵌合部の隙間を経てクランク室へ吹
き抜ける。
In particular, in a structure in which the ceramic headliner and the ceramic cylinder liner do not come into direct contact with each other, and the metal cylinder head and the metal cylinder body are connected with a gasket in between, the combustion gas in the combustion chamber If it leaks from the upper end of the liner, it may blow through the gap between the cylinder portion of the cylinder body and the cylinder liner into the crank chamber. In other words, if there is a slight gap in the fitting part between the cylinder body and the cylinder liner due to the difference in the coefficient of thermal expansion, the combustion gas will flow from the gap between the lower end of the headliner and the upper end of the cylinder liner into the cylinder of the cylinder body. Blows into the crank chamber through the gap between the fitting part and the cylinder liner.

そこで、特開昭58-30454号公報に開示されるように、シ
リンダ本体の円筒部の上端部に内径を拡開して段部を形
成する一方、鋳鉄製のシリンダライナの上端部にフラン
ジを一体に形成し、予め円筒部の段部へシールリングを
当て、シリンダライナを上側からシリンダ本体の円筒部
へ嵌合するか螺合すれば、シリンダライナの上端部に隙
間が生じないから、燃焼ガスがシリンダ本体の円筒部と
シリンダライナとの嵌合部へもれ、クランク室へ吹き抜
けることはない。
Therefore, as disclosed in Japanese Patent Laid-Open No. 58-30454, a step is formed by expanding the inner diameter at the upper end of the cylindrical portion of the cylinder body, while a flange is formed at the upper end of the cast iron cylinder liner. If it is formed integrally and a seal ring is applied to the step of the cylinder in advance and the cylinder liner is fitted or screwed into the cylinder of the cylinder body from the upper side, there will be no gap at the upper end of the cylinder liner. The gas does not leak to the fitting portion between the cylinder portion of the cylinder body and the cylinder liner and blows into the crank chamber.

しかし、上述の構造では鋳鉄製のシリンダライナならば
問題ないが、セラミツクス製のシリンダライナでは、シ
リンダライナと一体にフランジを設けることはシリンダ
ライナの熱分布が複雑になり、またフランジがシリンダ
本体の円筒部の段部へ押し付けられると、フランジが押
圧力と熱変形により割れる恐れがある。
However, the cast iron cylinder liner has no problem in the above-mentioned structure, but in the ceramic cylinder liner, providing the flange integrally with the cylinder liner makes the heat distribution of the cylinder liner complicated, and the flange of the cylinder body If the flange is pressed against the stepped portion of the cylindrical portion, the flange may crack due to the pressing force and thermal deformation.

[発明が解決しようとする問題点] 本発明の目的は従来の構成に変更を加えることなく、簡
単な構造で燃焼室から燃焼ガスがシリンダ本体の円筒部
とシリンダライナとの嵌合部へ洩れ、クランク室へ吹き
抜けるのを抑えることができる、断熱エンジンのシール
構造を提供することにある。
[Problems to be Solved by the Invention] An object of the present invention is to allow a combustion gas to leak from a combustion chamber to a fitting portion between a cylindrical portion of a cylinder body and a cylinder liner with a simple structure without changing the conventional configuration. Another object of the present invention is to provide a seal structure for an adiabatic engine capable of suppressing blow-through to the crank chamber.

[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、本発明の構成は金属製のシ
リンダ本体の円筒部の上端部に内径を拡大して段部を形
成し、セラミツクス製シリンダライナを前記円筒部へ嵌
合し、シリンダライナの上端部に熱膨張率がセラミツク
スと同等の金属リングを外嵌し、金属リングの下半部内
周壁に形成した円錐部に軟質カーボンリングを係合し、
シリンダヘツドの下面と金属リングの上端面の間に挟ん
だ弾性金属リングにより、金属リングを前記段部へ押し
付け、軟質カーボンリングの下端部を前記段部へ、軟質
カーボンリングの内周壁をシリンダライナの外周壁へ密
接させたものである。
[Means for Solving the Problems] In order to achieve the above object, according to the configuration of the present invention, a cylinder liner made of ceramics is formed by enlarging the inner diameter to form a step at the upper end of the cylindrical portion of the metal cylinder body. Is fitted to the cylindrical portion, a metal ring having a coefficient of thermal expansion equivalent to that of ceramics is externally fitted to the upper end of the cylinder liner, and a soft carbon ring is engaged with the conical portion formed on the inner peripheral wall of the lower half of the metal ring. ,
With the elastic metal ring sandwiched between the lower surface of the cylinder head and the upper end surface of the metal ring, the metal ring is pressed against the step portion, the lower end portion of the soft carbon ring is moved to the step portion, and the inner peripheral wall of the soft carbon ring is attached to the cylinder liner. It is closely attached to the outer peripheral wall of.

[作用] シリンダライナと熱膨張率がほぼ同じ金属の金属リング
がシリンダライナの上端部へ外嵌され、金属リングはシ
リンダ本体の円筒部の上端部の段部へ嵌挿され、金属リ
ングの下端面が円筒部の段部へ押し付けられる。金属リ
ングの内周面に形成した円錐部に、軟質カーボンリング
が係合される。軟質カーボンリングはシリンダライナの
外周壁とシリンダ本体の円筒部の段部とに弾性的に密接
されるので、燃焼室の燃焼ガスがヘツドライナとシリン
ダライナとの突合せ部の隙間へ洩れても、シリンダライ
ナの外周壁と段部に密接する軟質カーボンリングによ
り、シリンダライナとシリンダ本体の円筒部との隙間を
経てクランク室へ吹き抜けるのを阻止される。
[Operation] A metal ring made of a metal having substantially the same coefficient of thermal expansion as that of the cylinder liner is externally fitted to the upper end of the cylinder liner, and the metal ring is fitted and inserted into the stepped part of the upper end of the cylindrical portion of the cylinder body. The end face is pressed against the step of the cylindrical portion. The soft carbon ring is engaged with the conical portion formed on the inner peripheral surface of the metal ring. Since the soft carbon ring is elastically brought into close contact with the outer peripheral wall of the cylinder liner and the stepped portion of the cylinder portion of the cylinder body, even if the combustion gas in the combustion chamber leaks into the gap between the head liner and the cylinder liner, The soft carbon ring that is in close contact with the outer peripheral wall of the liner and the step portion prevents the soft carbon ring from blowing through the gap between the cylinder liner and the cylinder portion of the cylinder body into the crank chamber.

[発明の実施例] 第2図に示すように、通常の金属製のシリンダヘツド1
の下面に円筒部37が形成され、円筒部37の内部に逆
カツプ形のセラミツクス製のヘツドライナ15が上下1
対のリング6を介して嵌合され、かつシリンダヘツド1
の下面1aとヘツドライナ15との間にリング23と、
燃料噴射ノズル5、吸・排気ポート(図示せず)をそれ
ぞれ取り囲むリング22とが介装される。燃焼室はセラ
ミツクス製のヘツドライナ15とセラミツクス製のピス
トン冠部3とにより区画され、燃焼室の主要部から離れ
た部分でヘツドライナ15がセラミツクス製のシリンダ
ライナ10と突き合される。
[Embodiment of the Invention] As shown in FIG. 2, an ordinary metal cylinder head 1 is used.
A cylindrical portion 37 is formed on the lower surface of the head, and an inverted cup-shaped ceramic hedliner 15 is formed inside the cylindrical portion 37.
Cylinder head 1 fitted through a pair of rings 6
A ring 23 between the lower surface 1a of the
A fuel injection nozzle 5 and a ring 22 surrounding the intake / exhaust ports (not shown) are interposed. The combustion chamber is partitioned by a ceramics liner 15 and a ceramics piston crown 3, and the headliner 15 is abutted against the ceramics cylinder liner 10 at a portion apart from the main part of the combustion chamber.

実際には、ヘツドライナ15とシリンダライナ10との
熱膨張差による応力を回避するために、両者の間には極
めて僅かな隙間が備えられ、金属製のシリンダヘツド1
の下端面と金属製のシリンダ本体9の上端面との間にガ
スケツト8が介装され、シリンダヘツド1から図示して
ないヘツドボルトをシリンダ本体9へ螺合して締結され
る。シリンダライナ10はシリンダ本体9の円筒部20
に嵌合される。
In reality, in order to avoid stress due to the difference in thermal expansion between the head liner 15 and the cylinder liner 10, a very small gap is provided between the two, and the metal cylinder head 1
A gasket 8 is interposed between the lower end surface of the cylinder and the upper end surface of the metal cylinder body 9, and a head bolt (not shown) is screwed from the cylinder head 1 to the cylinder body 9 for fastening. The cylinder liner 10 has a cylindrical portion 20 of the cylinder body 9.
Is fitted to.

ピストン13はセラミツクス製のピストン冠部3を普通
の金属製のスカート部7に重ね合せ、上から挿通したボ
ルト18に皿ばね17を介しナツト16を締め付けて結
合される。ピストン冠部3は上面に燃料と空気の混合を
促す窪み2を設けられ、下面中央に円筒部34を、下面
外周部に段部をそれぞれ設けられる。スカート部7は外
周面にピストンリング39を装着される一方、上面外周
部に設けた突条4を前述したピストン冠部3の段部へ嵌
合される。また、スカート部7は上面中央に柱35を形
成され、柱35にガスケツト19を介してピストン冠部
3を重ね合せ、柱35と円筒部34との間に空部12を
形成される。ピストン冠部3とスカート部7との外周側
の重合せ面にシールリング31が介装される。
In the piston 13, the ceramic crown portion 3 made of ceramics is superposed on the ordinary skirt portion 7 made of metal, and the nut 16 is fastened and coupled to the bolt 18 inserted from above through the disc spring 17. The piston crown portion 3 is provided with a recess 2 for promoting mixing of fuel and air on the upper surface, a cylindrical portion 34 at the center of the lower surface, and a step portion at the outer peripheral portion of the lower surface. A piston ring 39 is mounted on the outer peripheral surface of the skirt portion 7, while the protrusion 4 provided on the outer peripheral surface of the upper surface is fitted to the step portion of the piston crown portion 3 described above. Further, the skirt portion 7 has a pillar 35 formed in the center of the upper surface, and the piston crown portion 3 is superposed on the pillar 35 via the gasket 19, so that an empty portion 12 is formed between the pillar 35 and the cylindrical portion 34. A seal ring 31 is provided on the overlapping surface of the piston crown portion 3 and the skirt portion 7 on the outer peripheral side.

かくして、シリンダヘツド1の円筒部37の内周面とヘ
ツドライナ15との間に上下1対のリング6により空部
21が区画され、シリンダヘツド1の下面1aとヘツド
ライナ15との間にリング23,22により空部30が
区画される。また、ピストン冠部3とスカート部7との
間にシールリング31により空部12が区画される。こ
れらの空部21,30,12は断熱層として働く。
Thus, an empty portion 21 is defined between the inner peripheral surface of the cylindrical portion 37 of the cylinder head 1 and the headliner 15 by a pair of upper and lower rings 6, and a ring 23 is formed between the lower surface 1a of the cylinder head 1 and the headliner 15. An empty portion 30 is defined by 22. Further, the space 12 is defined by the seal ring 31 between the piston crown portion 3 and the skirt portion 7. These voids 21, 30, 12 act as a heat insulating layer.

上述の断熱エンジンでは燃料の燃焼期間の大半がヘツド
ライナ15とピストン冠部3とにより囲まれる空間で行
われ、ヘツドライナ15とシリンダライナ10との突合
せ部は燃焼ガスが最高温度から幾分低下する部分に配置
され、ガスケツト8の熱負荷を軽減する。
In the adiabatic engine described above, most of the combustion period of fuel is performed in the space surrounded by the headliner 15 and the piston crown portion 3, and the abutting portion between the headliner 15 and the cylinder liner 10 is a portion where the combustion gas is somewhat lowered from the maximum temperature. Are placed in the space to reduce the heat load on the gasket 8.

第1図に示すように、本発明によれば、セラミツクス製
のシリンダライナ10の上端部に、セラミツクスと同等
の熱伝導率を有する例えばコバールと称する合金などの
金属リング42を外嵌する。金属リング42の下半部内
周壁に形成した円錐部53に、耐熱性を有する軟質カー
ボンリング52を挾んで、シリンダ本体9の円筒部20
と円筒部20の上端部に形成した大径円筒部20aとの
間の段部47へ押し付ける。軟質カーボンリング52は
段部47へ弾性的に密接されるとともに、シリンダライ
ナ10の外周壁にも密接される。
As shown in FIG. 1, according to the present invention, a metal ring 42, such as an alloy called Kovar, having a thermal conductivity equivalent to that of ceramics is externally fitted to the upper end of a cylinder liner 10 made of ceramics. The soft carbon ring 52 having heat resistance is sandwiched between the conical portion 53 formed on the inner peripheral wall of the lower half portion of the metal ring 42 to form the cylindrical portion 20 of the cylinder body 9.
And the large-diameter cylindrical portion 20a formed at the upper end of the cylindrical portion 20 are pressed against the stepped portion 47. The soft carbon ring 52 is elastically brought into close contact with the step portion 47, and is also brought into close contact with the outer peripheral wall of the cylinder liner 10.

金属リング42の上端面42aとヘツドライナ15の下
端面15aとの間に、耐熱性を有するインコネルなどの
中空の弾性金属リング42を弾性的に挾み、シリンダヘ
ツド1をシリンダ本体9に結合するヘツドボルトにより
締め付ける。
A head bolt for connecting the cylinder head 1 to the cylinder body 9 by elastically sandwiching a hollow elastic metal ring 42 such as Inconel having heat resistance between the upper end surface 42a of the metal ring 42 and the lower end surface 15a of the headliner 15. Tighten with.

本発明は上述のように、金属リング42がシリンダライ
ナ10を構成するセラミツクスと熱伝導率がほぼ同等の
金属製のものであるから、両者の嵌合部において熱破壊
が生じる恐れはない。
As described above, in the present invention, since the metal ring 42 is made of a metal whose thermal conductivity is almost the same as that of the ceramics forming the cylinder liner 10, there is no risk of thermal breakage in the fitting portion of both.

金属リング42の円錐部53に、断面楔形をなし円錐部
53よりも軸方向に長く、かつ内径がシリンダライナ1
0の外径よりも小さい軟質カーボンリング52を挾み、
金属リング42の下端面42bを段部47へヘツドボル
トの締付け力により押し付ければ、軟質カーボンリング
52がヘツドライナ10の外周壁と段部47とに密接さ
れる。したがつて、熱膨張によりシリンダ本体9の円筒
部20とセラミツクス製のシリンダライナ10との嵌合
部に隙間が生じても、燃焼ガスがヘツドライナ15の下
端面15aとシリンダライナ10の上端面10aとの隙
間57から、円筒部20とシリンダライナ10との嵌合
部の隙間へ流れるのを阻止できる。
The conical portion 53 of the metal ring 42 has a wedge-shaped cross section, is longer in the axial direction than the conical portion 53, and has an inner diameter of the cylinder liner 1.
Sandwiching a soft carbon ring 52 smaller than the outer diameter of 0,
When the lower end surface 42b of the metal ring 42 is pressed against the step portion 47 by the tightening force of the head bolt, the soft carbon ring 52 is brought into close contact with the outer peripheral wall of the headliner 10 and the step portion 47. Therefore, even if a gap is generated in the fitting portion between the cylindrical portion 20 of the cylinder body 9 and the cylinder liner 10 made of ceramics due to thermal expansion, the combustion gas causes the lower end surface 15a of the headliner 15 and the upper end surface 10a of the cylinder liner 10. It is possible to prevent the flow from the gap 57 between the cylindrical portion 20 and the cylinder liner 10 into the gap between the fitting portions.

また、弾性金属リング42の部分的接触不良により燃焼
ガスが隙間57から大径円筒部20aと金属リング42
の外周壁との隙間へ回り込んでも、軟質カーボンリング
52が段部47へ密接されているので、この部分からの
燃焼ガスの吹抜けも阻止できる。なお、シリンダヘツド
1の下端面とシリンダ本体9の上端面との間は、第2図
に示したガスケツト8により密封される。
Further, due to the partial contact failure of the elastic metal ring 42, the combustion gas is forced from the gap 57 to the large-diameter cylindrical portion 20a and the metal ring 42.
Even if the soft carbon ring 52 goes into the gap with the outer peripheral wall of the above, since the soft carbon ring 52 is in close contact with the step portion 47, the blow-off of the combustion gas from this portion can be prevented. The lower end surface of the cylinder head 1 and the upper end surface of the cylinder body 9 are sealed by a gasket 8 shown in FIG.

第3図は他の形式の断熱エンジンの正面断面図を示す。
この実施例では、シリンダ本体9の上端面にセラミツク
ス製のシリンダヘツド1Aの下面1aがガスケツト8を
介して重ね合され、図示してないヘツドボルトにより結
合される。他の構成については第2図に示すものと同様
であり、同様の構成部材に共通の符号をつけて説明を省
略する。
FIG. 3 shows a front sectional view of another type of adiabatic engine.
In this embodiment, a lower surface 1a of a cylinder head 1A made of ceramics is superposed on the upper end surface of the cylinder body 9 via a gasket 8 and is joined by a head bolt (not shown). The other structure is the same as that shown in FIG. 2, and the same components are designated by the common reference numerals and the description thereof will be omitted.

この実施例でも、セラミツクス製のシリンダライナ10
の上端部外周壁にシール構造40が備えられ、シール構
造40によりシリンダ本体9の円筒部20とシリンダラ
イナ10との隙間からの燃焼ガスの吹抜けを阻止でき
る。
Also in this embodiment, the cylinder liner 10 made of ceramics is used.
A seal structure 40 is provided on the outer peripheral wall of the upper end portion of the cylinder, and the seal structure 40 can prevent the combustion gas from passing through the gap between the cylinder portion 20 of the cylinder body 9 and the cylinder liner 10.

[発明の効果] 本発明は上述のように、金属製のシリンダ本体の円筒部
の上端部に内径を拡大して段部を形成し、セラミツクス
製シリンダライナを前記円筒部へ嵌合し、シリンダライ
ナの上端部に熱膨張率がセラミツクスと同等の金属リン
グを外嵌し、金属リングの下半部内周壁に形成した円錐
部に軟質カーボンリングを係合し、シリンダヘツドの下
面と金属リングの上端面の間に挟んだ弾性金属リングに
より、金属リングを前記段部へ押し付け、軟質カーボン
リングの下端部を前記段部へ、軟質カーボンリングの内
周壁をシリンダライナの外周壁へ密接させたから、次の
ような効果を奏する。
EFFECTS OF THE INVENTION As described above, the present invention forms a step by enlarging the inner diameter at the upper end of the cylindrical portion of the metal cylinder body, and fits the ceramic cylinder liner to the cylindrical portion, A metal ring with a coefficient of thermal expansion equal to that of ceramics is fitted on the upper end of the liner, and a soft carbon ring is engaged with the conical part formed on the inner peripheral wall of the lower half of the metal ring. With the elastic metal ring sandwiched between the end faces, the metal ring was pressed against the step, and the lower end of the soft carbon ring was brought into close contact with the step, and the inner peripheral wall of the soft carbon ring was brought into close contact with the outer peripheral wall of the cylinder liner. It produces the effect like.

セラミツクス製シリンダライナの上端部に金属リングを
外嵌し、金属リングの内壁下半部の円錐部へ軟質カーボ
ンリングを装着したうえ、ヘツドボルトの締付力により
金属リングをシリンダ本体の段部へ押し付けたから、軟
質カーボンリングの下端面が段部へ弾性的に密接し、同
時に軟質カーボンリングの内周壁がセラミツクス製シリ
ンダライナの外周壁へ弾性的に密接する。
A metal ring is externally fitted to the upper end of the ceramic cylinder liner, a soft carbon ring is attached to the conical part of the lower half of the inner wall of the metal ring, and the metal ring is pressed against the stepped part of the cylinder body by the tightening force of the head bolt. Therefore, the lower end surface of the soft carbon ring elastically comes into close contact with the step portion, and at the same time, the inner peripheral wall of the soft carbon ring comes into elastic close contact with the outer peripheral wall of the ceramic cylinder liner.

燃焼ガスがヘツドライナとシリンダライナとの隙間から
洩れても、シリンダライナと金属リングとの隙間は軟質
カーボンリングの内周壁で、金属リングと段部との隙間
は軟質カーボンリングの下端壁で密封されるので、燃焼
ガスがシリンダライナとシリンダ本体との隙間を経てク
ランク室へ吹き抜けることはない。
Even if the combustion gas leaks through the gap between the headliner and the cylinder liner, the gap between the cylinder liner and the metal ring is sealed by the inner wall of the soft carbon ring, and the gap between the metal ring and the step is sealed by the lower end wall of the soft carbon ring. Therefore, the combustion gas does not blow into the crank chamber through the gap between the cylinder liner and the cylinder body.

シリンダライナはフランジがなく単純な形状のものであ
り、ヘツドボルトの締付力や複雑な熱変形力を受けない
ので、割れるなどの損傷をうけない。
The cylinder liner has no flange and has a simple shape. Since it does not receive the tightening force of the head bolt or the complicated thermal deformation force, it does not suffer damage such as cracking.

各部品の構成が簡単であり、従来の主要部を何ら変更す
ることなく構成することができ、量産が容易であり、組
付も簡単である。
The structure of each part is simple, the conventional main parts can be formed without any modification, mass production is easy, and assembly is also easy.

【図面の簡単な説明】[Brief description of drawings]

第1図は本発明に係る断熱エンジンのシール構造の要部
を示す正面断面図、第2図は本発明が適用される断熱エ
ンジンの正面断面図、第3図は同じく他の形式の断熱エ
ンジンの正面断面図である。 1:シリンダヘツド 9:シリンダ本体 10:シリン
ダライナ 13:ピストン 15:ヘツドライナ 2
0:円筒部 40:シール構造 42:金属リング 4
7:段部 52:軟質カーボンリング 53:円錐部
FIG. 1 is a front sectional view showing a main part of a sealing structure of a heat insulating engine according to the present invention, FIG. 2 is a front sectional view of a heat insulating engine to which the present invention is applied, and FIG. 3 is another heat insulating engine of the same type. FIG. 1: Cylinder head 9: Cylinder body 10: Cylinder liner 13: Piston 15: Headliner 2
0: Cylindrical part 40: Seal structure 42: Metal ring 4
7: Step portion 52: Soft carbon ring 53: Conical portion

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】金属製のシリンダ本体の円筒部の上端部に
内径を拡大して段部を形成し、セラミツクス製シリンダ
ライナを前記円筒部へ嵌合し、シリンダライナの上端部
に熱膨張率がセラミツクスと同等の金属リングを外嵌
し、金属リングの下半部内周壁に形成した円錐部に軟質
カーボンリングを係合し、シリンダヘツドの下面と金属
リングの上端面の間に挟んだ弾性金属リングにより、金
属リングを前記段部へ押し付け、軟質カーボンリングの
下端部を前記段部へ、軟質カーボンリングの内周壁をシ
リンダライナの外周壁へ密接させたことを特徴とする、
断熱エンジンのシール構造。
Claim: What is claimed is: 1. A cylinder body made of metal has a stepped portion formed by enlarging an inner diameter at an upper end portion of the cylinder body. A ceramic cylinder liner is fitted to the cylinder portion, and a coefficient of thermal expansion is provided at an upper end portion of the cylinder liner. Is fitted with a metal ring equivalent to the ceramics, the soft carbon ring is engaged with the conical portion formed on the inner peripheral wall of the lower half of the metal ring, and the elastic metal sandwiched between the lower surface of the cylinder head and the upper end surface of the metal ring. By the ring, the metal ring is pressed against the step, the lower end of the soft carbon ring to the step, the inner peripheral wall of the soft carbon ring is in close contact with the outer peripheral wall of the cylinder liner,
Seal structure for adiabatic engine.
JP59239382A 1984-11-15 1984-11-15 Sealed structure of adiabatic engine Expired - Lifetime JPH068621B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59239382A JPH068621B2 (en) 1984-11-15 1984-11-15 Sealed structure of adiabatic engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59239382A JPH068621B2 (en) 1984-11-15 1984-11-15 Sealed structure of adiabatic engine

Publications (2)

Publication Number Publication Date
JPS61118550A JPS61118550A (en) 1986-06-05
JPH068621B2 true JPH068621B2 (en) 1994-02-02

Family

ID=17043949

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59239382A Expired - Lifetime JPH068621B2 (en) 1984-11-15 1984-11-15 Sealed structure of adiabatic engine

Country Status (1)

Country Link
JP (1) JPH068621B2 (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5830454A (en) * 1981-08-14 1983-02-22 Yamaha Motor Co Ltd Cylinder body for internal combustion engine

Also Published As

Publication number Publication date
JPS61118550A (en) 1986-06-05

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