JPH01247743A - Cylinder block - Google Patents

Cylinder block

Info

Publication number
JPH01247743A
JPH01247743A JP7344488A JP7344488A JPH01247743A JP H01247743 A JPH01247743 A JP H01247743A JP 7344488 A JP7344488 A JP 7344488A JP 7344488 A JP7344488 A JP 7344488A JP H01247743 A JPH01247743 A JP H01247743A
Authority
JP
Japan
Prior art keywords
cylinder
lower deck
cylinder liner
deck
liner
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
JP7344488A
Other languages
Japanese (ja)
Inventor
Etsuo Ogami
悦夫 大上
Takashi Yanagisawa
隆 柳沢
Namimasu Oosawa
浪益 大沢
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co 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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP7344488A priority Critical patent/JPH01247743A/en
Publication of JPH01247743A publication Critical patent/JPH01247743A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00Cylinders; Cylinder heads 
    • F02F1/004Cylinder liners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F7/00Casings, e.g. crankcases or frames
    • F02F7/0002Cylinder arrangements
    • F02F7/0007Crankcases of engines with cylinders in line

Abstract

PURPOSE:To prevent local projection of a cylinder liner due to temperature difference by forming a part of thin thickness part in the circumferential direction of a lower deck which supports the lower end of a separated cylinder liner fitted in a cylinder bore. CONSTITUTION:A cylinder block is made from aluminum alloy and manufactured by casting, and a separated cylinder liner 5 made from iron is fitted, for example by press fitting, in the cylinder bore wall 30. In this case, on respective lower end surfaces 13, 14 of a lower deck 6 opposed to a main bearing housing 8 and in the direction meeting at right angles against a camshaft 35, respective grooves 15, 16 are arranged and provided, for example, so that their width T is less than 6mm and their depth H is less than half of the distance between a water jacket 2 and the lower end of lower deck and total sum of their respective central angles against the cylinder is less than 90degree. This thickness part 17, 18 in a part of the circumferential direction are thus formed due to the respective grooves 15, 16.

Description

【発明の詳細な説明】 〈産業上の利用分野〉 本発明は内燃機関のライチ型シリンダブロックに関する
DETAILED DESCRIPTION OF THE INVENTION <Industrial Application Field> The present invention relates to a lychee-type cylinder block for an internal combustion engine.

〈従来の技術〉 従来の内燃機関のシリンダブロックとして、例えば第3
図に示すようなものがある。
<Prior art> As a cylinder block of a conventional internal combustion engine, for example, the third
There is something like the one shown in the figure.

この図に示すシリンダブロックは、アルミニウム合金製
で、鋳造によって製造され、シリンダ壁30に鉄製シリ
ンダライナ5を圧入するか、または該鉄製シリンダライ
ナ5をシリンダ壁30で鋳ぐるむようにして装着したも
のである。尚、第3図に示すシリンダブロックは、ドラ
イライナ型式で、図示しない互いに連続するシリンダ壁
30をつなげたサイ、ヤミーズ型のもので、トップデツ
キ1とロアデツキ6との間にはウォータジャケット2が
形成されており、該鉄製シリンダライナ5を冷却してい
る。
The cylinder block shown in this figure is made of aluminum alloy, manufactured by casting, and has an iron cylinder liner 5 press-fitted into the cylinder wall 30, or the iron cylinder liner 5 is fitted by being cast around the cylinder wall 30. . The cylinder block shown in FIG. 3 is of the dry liner type, and is of the Yammies type in which mutually continuous cylinder walls 30 (not shown) are connected, and a water jacket 2 is formed between the top deck 1 and the lower deck 6. The iron cylinder liner 5 is cooled.

1亥シリンダフ゛ロツクのボア面4をコンプレッション
リング31等が設けられたピストン32が摺動するが、
該ピストン32のピストンスカート部33はバルクヘッ
ド7によりメインベアリングハウジング8と区分けされ
る燃焼室11の燃焼圧力により側圧を受け、またピスト
ン32の放熱を行っている(例えば実開昭60−108
48号公報参照)。
A piston 32 equipped with a compression ring 31 etc. slides on the bore surface 4 of the cylinder block.
The piston skirt portion 33 of the piston 32 receives side pressure from the combustion pressure of the combustion chamber 11, which is separated from the main bearing housing 8 by the bulkhead 7, and also radiates heat from the piston 32 (for example, in Japanese Utility Model Application No. 60-108).
(See Publication No. 48).

〈発明が解決しようとする課題〉 しかしながら、このような従来のシリンダブロックにあ
っては、鉄製シリンダライナ5の下端部12がロアデツ
キ6の下端部まで挿入され、咳ロアデツキ6により全周
に渡って支持されているため次のような問題点があった
<Problems to be Solved by the Invention> However, in such a conventional cylinder block, the lower end 12 of the iron cylinder liner 5 is inserted up to the lower end of the lower deck 6, and the lower end 12 of the iron cylinder liner 5 is inserted all the way around the entire circumference by the lower deck 6. Because of the support, there were the following problems.

即ち、ビス7トン32からの放熱によりシリンダ壁30
の温度が上昇するが、鉄製シリンダライナ5の下端部1
2を支持しているロアデツキ6は冷却が不十分となり、
鉄製シリンダライナ5に接しているロアデツキ6の内面
が他部より高温となる。よって、機関運転中の熱により
該シリンダブロックを鋳造した際、該シリンダブロック
に残留していた内応力による凝固収縮歪みが解放され、
機関が例えば−40°Cの冷機時等においては、鉄製シ
リンダライナ5に接しているロアデツキ6の内面は膨張
し、外面は膨張しないので、該ロアデツキ6がシリンダ
の内側に局所的に押し込まれる。よって、ボア面4が局
所的にシリンダボア内側に押し込まれることになり、冷
機始動時においては、該押し込まれたボア面4に相当す
る鉄製シリンダライナ5の下端部12内周面が、ピスト
ン32のピストンスカート部33を傷つけ、潤滑不良に
よりスカッフィング摩耗が生じるという課題がある。
That is, due to heat radiation from the 7-ton screw 32, the cylinder wall 30
Although the temperature of the lower end 1 of the iron cylinder liner 5 increases,
The lower deck 6 supporting 2 becomes insufficiently cooled,
The inner surface of the lower deck 6, which is in contact with the iron cylinder liner 5, becomes hotter than other parts. Therefore, when the cylinder block is cast due to the heat generated during engine operation, the solidification shrinkage strain due to the internal stress remaining in the cylinder block is released.
When the engine is cold at, for example, -40° C., the inner surface of the lower deck 6 in contact with the iron cylinder liner 5 expands, but the outer surface does not, so that the lower deck 6 is locally pushed into the inside of the cylinder. Therefore, the bore surface 4 is locally pushed inside the cylinder bore, and when starting a cold engine, the inner circumferential surface of the lower end 12 of the iron cylinder liner 5 corresponding to the pushed bore surface 4 is pressed against the piston 32. There is a problem that the piston skirt portion 33 is damaged and scuffing wear occurs due to poor lubrication.

本発明は、このような従来の実情に着目してなされたも
ので、温度差によりボア面、ひいては鉄製シリンダライ
ナが局所的に突出しこれがピストンに作用しスカッフィ
ング摩耗を招くのを防止できるようにすることを目的と
している。
The present invention has been made in view of these conventional circumstances, and aims to prevent the bore surface, and even the iron cylinder liner, from locally protruding due to temperature differences, which acts on the piston and causes scuffing wear. The purpose is to

〈課題を解決するための手段〉 このため、本発明は、シリンダボア部分に別体のシリン
ダライナを装着してなるアルミニウム合金製のシリンダ
ブロックにおいて、シリンダライナの下端部を支持する
ロアデツキの肉厚が、周方向に一部薄く形成される構成
としたものである。
<Means for Solving the Problems> For this reason, the present invention provides a cylinder block made of aluminum alloy in which a separate cylinder liner is attached to the cylinder bore portion, in which the wall thickness of the lower deck supporting the lower end of the cylinder liner is increased. , it has a structure in which a portion is formed thinly in the circumferential direction.

く作用〉 上記の構成においては、ロアデツキの肉厚の一部を鋳造
時に薄く形成した場合は、その部分の熱集中が減少する
ことにより凝固収縮歪みが減少し、また、鋳造後の加工
により薄く形成した場合はその時の応力の解放により、
凝固収縮歪みが解放される。従って、冷機時等における
機関運転中の熱による該凝固収縮歪みが解放されること
に伴うロアデツキの内面への膨張、及び該膨張による別
体のシリンダライナで形成されるボア面が局所的にシリ
ンダボア内側に押し込まれることが抑制される。
In the above configuration, if a part of the wall of the lower deck is made thinner during casting, the heat concentration in that part will be reduced, thereby reducing the solidification shrinkage strain, and the thickness will be made thinner by processing after casting. If formed, due to the release of stress at that time,
Solidification shrinkage strain is released. Therefore, the inner surface of the lower deck expands due to the release of the solidification and shrinkage strain due to heat during engine operation when the engine is cold, and the bore surface formed by the separate cylinder liner due to this expansion locally becomes the cylinder bore. It is suppressed from being pushed inward.

〈実施例〉 以下に本発明の実施例を図面に基づいて説明する。<Example> Embodiments of the present invention will be described below based on the drawings.

尚、以下に説明する図において、第3図と同一要素のも
のには同一符号を付して説明を簡単にする。
In the figures described below, the same elements as in FIG. 3 are given the same reference numerals to simplify the explanation.

第1図に第1実施例を示す。FIG. 1 shows a first embodiment.

シリンダブロックは、第3図に示す従来例と同様、アル
ミニウム合金製で、鋳造によって製造され、シリンダボ
ア壁30に別体の鉄製シリンダライナ5を圧入するか、
または該鉄製シリンダライナ5をシリンダ壁30で鋳ぐ
るむようにして装着したものである。また、ドライライ
ナ型式で、互いに隣接するシリンダ部分(図示せず)を
つなげたサイヤミーズ型シリンダである。
Like the conventional example shown in FIG. 3, the cylinder block is made of aluminum alloy and manufactured by casting, and a separate iron cylinder liner 5 is press-fitted into the cylinder bore wall 30, or
Alternatively, the iron cylinder liner 5 is mounted so as to be cast around the cylinder wall 30. It is also a dry liner type cylinder, which is a Saiyamize type cylinder in which adjacent cylinder parts (not shown) are connected.

そして、本発明に係わる構成として、ロアデツキ6のメ
インベアリングハウジング8に合い対する下端面13.
14のカムシャフト35に対して直角方向に夫々中Tが
6ma+以下で、且つ深さHがロアデツキ6のウォータ
ジャケット2と前記下端面13゜14との距離の2分の
1以下である溝15.16を該溝15、16の該シリン
ダに対する中心各α、βの合計が90°以下になるよう
に設ける。該溝15.16はシリンダブロック鋳造時に
鋳型により設けるか、または鋳造時には前記ロアデツキ
6の下端面13.14は平坦に鋳込み、その後機械加工
により設けてもよい。
As a configuration according to the present invention, a lower end surface 13 of the lower deck 6 that fits into the main bearing housing 8.
Grooves 15 each having a medium T of 6 ma+ or less in the direction perpendicular to the camshaft 35 of 14, and a depth H of not more than half the distance between the water jacket 2 of the lower deck 6 and the lower end surface 13° 14. .16 are provided so that the sum of the centers α and β of the grooves 15 and 16 with respect to the cylinder is 90° or less. The grooves 15, 16 may be provided by a mold when the cylinder block is cast, or the lower end surfaces 13, 14 of the lower deck 6 may be cast flat during casting, and then provided by machining.

該溝15.16を設けることによりロアデツキの肉厚が
周方向に一部薄く形成される。
By providing the grooves 15 and 16, the thickness of the lower deck is partially reduced in the circumferential direction.

次に作用を説明する。Next, the effect will be explained.

該溝15.16を鋳造時に形成する場合は、該溝15゜
16により形成されるロアデツキの薄肉部17.18の
熱集中が小さくなり、シリンダブロックに残留する内応
力による凝固収縮歪みが少な(なる。また、鋳造時には
前記ロアデツキ6の下端面13.14は平坦に鋳込み、
その後機械加工により該溝15.16を設けた場合は、
溝15.16の加工時に凝固収縮歪みが解放される。
When the grooves 15 and 16 are formed during casting, heat concentration in the thin wall portions 17 and 18 of the lower deck formed by the grooves 15 and 16 is reduced, and solidification shrinkage distortion due to internal stress remaining in the cylinder block is reduced ( In addition, during casting, the lower end surfaces 13 and 14 of the lower deck 6 are cast flat,
If the grooves 15 and 16 are subsequently provided by machining,
Solidification shrinkage strains are released during machining of grooves 15,16.

よって、ピストン32からの放熱により、鉄製シリンダ
ライナ5に接しているロアデツキ6の下端部内面が高温
となっても、凝固収縮歪みが少ないため、冷機時等にお
ける機関運転中の熱による該凝固収縮歪みの解放に伴う
ロアデツキ6の内面への膨張、ひいては別体の鉄製のシ
ンダライナ5により形成されるボア面4が局所的にシリ
ンダボア内側に押し込まれることが抑制される。
Therefore, even if the inner surface of the lower end of the lower deck 6 in contact with the iron cylinder liner 5 becomes high temperature due to heat radiation from the piston 32, the solidification shrinkage distortion due to the heat during engine operation when the engine is cold is small, so that the solidification shrinkage due to the heat during engine operation when the engine is cold or the like is small. Expansion toward the inner surface of the lower deck 6 due to the release of strain, and furthermore, the bore surface 4 formed by the separate iron cinder liner 5 is suppressed from being locally pushed inside the cylinder bore.

さらに、鋳造時には前記ロアデツキ6の下端面13、1
4は平坦に鋳込み、その後機械加工により液溝15.1
6を設けた場合には、鋳造に伴う冷却時の熱歪みが除去
され、ボア下端部の変形を溝15.16側へ逃がすこと
ができるので一層効果的である。
Furthermore, during casting, the lower end surfaces 13, 1 of the lower deck 6 are
4 is cast flat and then machined to form the liquid groove 15.1.
6 is more effective because it eliminates thermal strain during cooling associated with casting and allows deformation of the lower end of the bore to escape toward the grooves 15 and 16.

以上のようにボア面4が局所的にシリンダボア内側に押
し込まれることが抑制されるので、鉄製シリンダライナ
5の下端部12によって、ピストン32のピストンスカ
ート部33を傷つけることが無く、潤滑不良によるスカ
ッフィング摩耗の発生が抑制される。
As described above, since the bore surface 4 is prevented from being locally pushed into the cylinder bore, the piston skirt portion 33 of the piston 32 is not damaged by the lower end portion 12 of the iron cylinder liner 5, and scuffing due to poor lubrication is avoided. The occurrence of wear is suppressed.

また、液溝15.16を設けることにより形成されるロ
アデツキ6の薄肉部17.18により、該ロアデツキ6
の下端部13.14が全周に渡っては拘束されないこと
になり、鉄製シリンダライナ5が高温になって膨張して
も、液溝15.16に該膨張が逃げ、内面に突出するこ
とも無い。
Further, the thin wall portion 17.18 of the lower deck 6 formed by providing the liquid groove 15.16 allows the lower deck 6 to
The lower end portion 13.14 is not restrained around the entire circumference, and even if the iron cylinder liner 5 becomes hot and expands, the expansion escapes into the liquid groove 15.16 and does not protrude to the inner surface. None.

第2図に示す第2実施例は、液溝15.16の底面19
、20とウォータジャケット2の液溝に対する端部との
距離A、Bを従来例と同様にするために、ロアデツキ6
のウォータジャケット方向の長さを液溝15.16の分
だけ短くしたものである。
A second embodiment, shown in FIG.
, 20 and the end of the water jacket 2 with respect to the liquid groove, in order to make the distances A and B similar to the conventional example, the lower deck 6
The length in the water jacket direction is shortened by the length of the liquid grooves 15 and 16.

本実施例においても、冷機時等における機関運転中の熱
による該凝固収縮歪みの解放に伴うロアデツキ6の内面
への膨張、および別体の鉄製のシリンダライナ5により
形成されるボア面4が局所的にシリンダボア内側に押し
込まれることが抑制されるという作用については、第1
実施例と同様に奏する。
In this embodiment as well, the inner surface of the lower deck 6 expands due to the release of the solidification shrinkage strain due to heat during engine operation when the engine is cold, and the bore surface 4 formed by the separate iron cylinder liner 5 locally. Regarding the effect of preventing the cylinder from being pushed into the inside of the cylinder bore, the first
It will be played in the same way as the example.

尚、第2実施例においては、ボア面4が内側に突出した
ときに、ピストン32に接触する肉厚が大きい部分がト
ップデツキ1方向に移動しているので、該ピストン32
とシリンダライナ5との間の摺動抵抗が若干大きくなる
だけで、シリンダライナ5の下端部12がピストン32
のピストンスカート部33を傷つけることはない。
In the second embodiment, when the bore surface 4 protrudes inward, the thicker portion that contacts the piston 32 moves toward the top deck 1, so that the piston 32
If the sliding resistance between the cylinder liner 5 and the piston 32 increases slightly, the lower end 12 of the cylinder liner 5
This will not damage the piston skirt portion 33 of the piston.

また、ロアデツキ6の肉厚を十分確保することができる
ので、該ロアデツキ6部分の強度を確保でき、剛性も高
まり、機関の振動特性の面で有利となる。
Further, since the lower deck 6 can be sufficiently thick, the strength of the lower deck 6 portion can be ensured, and the rigidity is also increased, which is advantageous in terms of the vibration characteristics of the engine.

〈発明の効果〉 以上説明したように、本発明によれば、温度差によって
別体のシリンダライナにより形成されるボア面が局所的
に突出し、これがピストンに作用しスカッフィング摩耗
を招くのを防止でき、ピストンの運動が円滑に行え、機
関騒音が低減でき、よって機関の寿命延長が可能となる
。また、ピストンのシリンダライナとの接触が常に良好
に保たれるため、燃焼室の気密性が向上して、機関の高
出力化が図れ、オイル消費量も低減できる実用的効果大
なるものである。
<Effects of the Invention> As explained above, according to the present invention, it is possible to prevent the bore surface formed by a separate cylinder liner from protruding locally due to temperature differences, which acts on the piston and causes scuffing wear. , the piston can move smoothly, engine noise can be reduced, and the life of the engine can be extended. In addition, since the piston always maintains good contact with the cylinder liner, the airtightness of the combustion chamber is improved, increasing the engine's output and reducing oil consumption, which has great practical effects. .

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

第1図(A)は本発明の第1実施例を示すシリト・・ト
ップデツキ  2・・・ウォータジャケット4・・・ボ
ア面  5・・・シリンダライナ  6・・・ロアデツ
キ  15.16・・・溝  17.18・・・ロアデ
ツキ薄肉部  30・・・シリンダ壁 代理人 弁理士 笹 島  富二雄 4・・・ボア面 15.16・・・溝 17、18・・・ロアデツキ薄肉部 30・・・シリンダ壁 (B) 第1図
FIG. 1(A) shows the first embodiment of the present invention: Top deck 2 Water jacket 4 Bore surface 5 Cylinder liner 6 Lower deck 15.16 Groove 17.18...Lower deck thin wall part 30...Cylinder wall agent Patent attorney Fujio Sasashima 4...Bore surface 15.16...Groove 17, 18...Lower deck thin wall part 30...Cylinder wall (B) Figure 1

Claims (1)

【特許請求の範囲】[Claims] シリンダボア部分に別体のシリンダライナを装着してな
るアルミニウム合金製のシリンダブロックにおいて、シ
リンダライナの下端部を支持するロアデッキの肉厚が、
周方向に一部薄く形成されていることを特徴とするシリ
ンダブロック。
In an aluminum alloy cylinder block with a separate cylinder liner attached to the cylinder bore, the thickness of the lower deck that supports the lower end of the cylinder liner is
A cylinder block characterized by being partially thin in the circumferential direction.
JP7344488A 1988-03-29 1988-03-29 Cylinder block Pending JPH01247743A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7344488A JPH01247743A (en) 1988-03-29 1988-03-29 Cylinder block

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7344488A JPH01247743A (en) 1988-03-29 1988-03-29 Cylinder block

Publications (1)

Publication Number Publication Date
JPH01247743A true JPH01247743A (en) 1989-10-03

Family

ID=13518408

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7344488A Pending JPH01247743A (en) 1988-03-29 1988-03-29 Cylinder block

Country Status (1)

Country Link
JP (1) JPH01247743A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
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US8664421B2 (en) 2005-04-01 2014-03-04 Daikin Industries, Ltd. Surface modifier and its use
CN103867329A (en) * 2014-03-12 2014-06-18 无锡华源凯马发动机有限公司 Split type cylinder sleeve for aluminium alloy single-cylinder water-cooled diesel engines
CN105909416A (en) * 2016-06-03 2016-08-31 河南省中原华工激光工程有限公司 Anti-cavitation and environment-friendly cylinder sleeve

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8664421B2 (en) 2005-04-01 2014-03-04 Daikin Industries, Ltd. Surface modifier and its use
CN103867329A (en) * 2014-03-12 2014-06-18 无锡华源凯马发动机有限公司 Split type cylinder sleeve for aluminium alloy single-cylinder water-cooled diesel engines
CN103867329B (en) * 2014-03-12 2016-08-24 无锡华源凯马发动机有限公司 Aluminium alloy single-cylinder water cooled diesel engine stepped liner
CN105909416A (en) * 2016-06-03 2016-08-31 河南省中原华工激光工程有限公司 Anti-cavitation and environment-friendly cylinder sleeve

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