JP2737107B2 - Compression ring for internal combustion engine - Google Patents

Compression ring for internal combustion engine

Info

Publication number
JP2737107B2
JP2737107B2 JP7521722A JP52172295A JP2737107B2 JP 2737107 B2 JP2737107 B2 JP 2737107B2 JP 7521722 A JP7521722 A JP 7521722A JP 52172295 A JP52172295 A JP 52172295A JP 2737107 B2 JP2737107 B2 JP 2737107B2
Authority
JP
Japan
Prior art keywords
compression ring
ring
groove
internal combustion
combustion engine
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 - Fee Related
Application number
JP7521722A
Other languages
Japanese (ja)
Inventor
良昭 和田
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.)
Riken Corp
Original Assignee
Riken 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 Riken Corp filed Critical Riken Corp
Priority to JP7521722A priority Critical patent/JP2737107B2/en
Application granted granted Critical
Publication of JP2737107B2 publication Critical patent/JP2737107B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Pistons, Piston Rings, And Cylinders (AREA)

Description

【発明の詳細な説明】 技術分野 この発明は、内燃機関用圧縮リングに関する。Description: TECHNICAL FIELD The present invention relates to a compression ring for an internal combustion engine.

背景技術 内燃機械用ピストンリングの中の一つのタイプのリン
グとして使用される圧縮リングに関しては、ピストンが
燃焼ガスの圧力を受ける際にガス漏れ即ちブローバイガ
スを防ぐため、そのシール性の向上について種々の改善
がなされている。
BACKGROUND ART With respect to a compression ring used as one type of piston ring for an internal combustion machine, in order to prevent gas leakage or blow-by gas when the piston receives the pressure of the combustion gas, various measures have been taken to improve the sealing performance. Improvements have been made.

改良された圧縮リングの1つに、特殊合口を有する圧
縮リングがある。その構成の1例を図3に示す。この例
では、圧縮リング1の一方の合口端部の上方外周側端部
に周方向に突出した直角三角形断面の突出部2が形成さ
れており、他方の合口端部の上方外周端部に上記突出部
2を受入れることのできる直角三角形断面の凹入部3が
形成されている。この圧縮リング1をピストン5のリン
グ溝4に取付け、シリンダ6に装着した状態では、上記
の合口部同志2、3は互いに重なった状態になる(米国
特許5,253,878号明細書参照)。
One of the improved compression rings is a compression ring having a special abutment. FIG. 3 shows an example of the configuration. In this example, a protruding portion 2 having a right-angled triangular cross section that protrudes in the circumferential direction is formed at an upper outer peripheral end of one abutting end of the compression ring 1, and the above-described outer peripheral end of the other abutting end is formed at the upper outer peripheral end of the other abutting end. A recess 3 having a right-angled triangular cross section capable of receiving the protrusion 2 is formed. When the compression ring 1 is attached to the ring groove 4 of the piston 5 and attached to the cylinder 6, the abutment parts 2 and 3 overlap each other (see US Pat. No. 5,253,878).

最近のガソリン機関の高速、高負荷化に対応すべくピ
ストンリングの強じん化が図られる一方、ピストンリン
グの加工性を充足する材料の選択が図られる。云い換え
れば、高強度の材質と加工性のよい低材質との釣合いの
下にピストンリング材の選択が成される。一方、ピスト
ンリングを納めるピストンそのものの材質がピストンリ
ングの材質に比し、低質化することから、ピストンのリ
ング溝側面の摩耗が大となり、ピストンリングのリング
溝内での不安定な動きを作る。この結果、図3と図4に
示すダブルアングルタイプのピストンリング1の突出部
2の折損を発生させ、エンジン性能を極端に低下させ
る。この折損は、ピストンリングの上方内周隅角部に周
方向に延在するインナーカット7を設け、小さな断面積
の突出部2を使用したときに多くみられる。
In order to cope with recent high-speed and high-load gasoline engines, the toughness of the piston ring has been improved, while the selection of materials satisfying the workability of the piston ring has been attempted. In other words, the selection of the piston ring material is made based on a balance between a material having high strength and a material having low workability. On the other hand, since the material of the piston itself that contains the piston ring is lower in quality than the material of the piston ring, the wear on the side of the ring groove of the piston increases, causing unstable movement in the ring groove of the piston ring. . As a result, breakage of the protruding portion 2 of the double-angle type piston ring 1 shown in FIGS. 3 and 4 is caused, and the engine performance is extremely reduced. This breakage is more likely to occur when an inner cut 7 extending in the circumferential direction is provided at the upper inner corner of the piston ring and the projection 2 having a small cross-sectional area is used.

発明の開示 圧縮リングの側面シール性(リング側壁面とリング溝
壁面との接触による)を向上させるインナーカット(英
国特許出願公開第2164418A号明細書参照)と同作用をな
す他の手段を開発し、当該側面シール性を維持したま
ゝ、突出部2の断面積を大とさせることで、従来技術の
不具合を解消させることを解決すべき課題とする。
DISCLOSURE OF THE INVENTION Another means for achieving the same function as an inner cut (see GB2164418A) for improving the side seal of the compression ring (by contact between the ring side wall surface and the ring groove wall surface) has been developed. It is another object of the present invention to solve the problem of the related art by increasing the sectional area of the protruding portion 2 while maintaining the side sealing performance.

前述の課題を解決するために、本発明の圧縮リング
は、その内周面に周方向に延在する環状の溝を設ける。
溝の中心は、リング幅中心より上方に位置させる。
In order to solve the above-mentioned problem, the compression ring of the present invention is provided with an annular groove extending in a circumferential direction on an inner peripheral surface thereof.
The center of the groove is located above the center of the ring width.

より具体的には、本発明は、一方の合口端部の上方外
周隅角部に周方向に突出する突出部が形成され、他方の
合口端部の上方外周隅角部に上記突出部を受入れ可能な
凹入部が形成された合口を有する内燃機関用圧縮リング
において、該圧縮リングの内周面にその幅中心より上方
に中心を位置させる溝を展開したとき溝の中心線が直線
となるようかつ該溝が圧縮リングの上面をその構成要件
としないよう周方向に延在させたことを特徴とする内燃
機関用圧縮リング。を提供する。
More specifically, the present invention is configured such that a projecting portion projecting in the circumferential direction is formed at an upper outer corner of one of the abutting ends, and the projecting portion is received at an upper outer corner of the other abutting end. In a compression ring for an internal combustion engine having an abutment in which a possible recess is formed, a center line of the groove becomes straight when a groove located above the center of its width is developed on the inner peripheral surface of the compression ring. A compression ring for an internal combustion engine, wherein the groove extends in the circumferential direction so as not to make the upper surface of the compression ring a constituent element. I will provide a.

好ましくは、溝は複数個にして、断面を半円形とす
る。
Preferably, a plurality of grooves are provided and the cross section is semicircular.

圧縮リングの端部の圧入部の上方内周隅部をリング内
周側にもってこれるので、突出部の断面積を大きくし、
その折損を防止できる。リングのねじれによる側面シー
ル性は本発明の圧縮リングでは維持される。
Since the upper inner peripheral corner of the press-fit portion at the end of the compression ring is brought to the inner peripheral side of the ring, the cross-sectional area of the protrusion is increased,
The breakage can be prevented. Side sealing due to ring torsion is maintained with the compression ring of the present invention.

図面の簡単な説明 図1は、本発明の一例の圧縮リングの合口部近傍と溝
との構成を示す断面図である。
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a cross-sectional view showing the configuration of the vicinity of an abutment portion and a groove of a compression ring according to an example of the present invention.

図2は、本発明の別の例の圧縮リングの合口部近傍の
構成を示す断面図である。
FIG. 2 is a cross-sectional view showing a configuration near an abutment portion of a compression ring according to another example of the present invention.

図3は、従来の圧縮リングの部分の近傍の構成の斜視
図である。
FIG. 3 is a perspective view of a configuration near a portion of a conventional compression ring.

図4は、従来のピストンリングを備えたエンジンの一
部を示す断面図である。
FIG. 4 is a sectional view showing a part of an engine provided with a conventional piston ring.

発明を実施するための最良の形態 以下に、本発明の実施例を図面に基づいて詳細に説明
する。
BEST MODE FOR CARRYING OUT THE INVENTION Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings.

図1は、本発明の第1実施例としての圧縮リングの合
口部近傍の構成を示す図である。合口の構成は、ダブル
アングル形状の特殊合口であって、圧縮リング11の一方
の合口端部の上方外周隅角部には周方向に延びる直角三
角形断面の突出部12が設けられ、他方の合口端部には上
方外周隅角部に、上記突出部12を受入れ可能な形状の凹
入部13が設けられ、ピストンのリング溝に装着し、シリ
ンダ内に嵌装した状態では、図1に示す如く、突出部12
は凹入部13と重なった状態となる。
FIG. 1 is a diagram showing a configuration near an abutment portion of a compression ring as a first embodiment of the present invention. The configuration of the joint is a special joint of a double angle shape, and a projection 12 having a right-angled triangular cross section extending in the circumferential direction is provided at the upper outer corner of one end of the joint of the compression ring 11, and the other joint is provided. The end portion is provided with a concave portion 13 having a shape capable of receiving the protruding portion 12 at the upper outer corner, and is mounted in the ring groove of the piston and fitted in the cylinder as shown in FIG. , Protrusion 12
Is in a state of overlapping with the recess 13.

ピストンリング11の内周面16に円周方向に延在する断
面略半円形の溝14を設ける。溝14の中心は、ピストンリ
ング11の幅方向の中心よりやゝ上方に位置し、この溝14
によりピストンリング11にねじれを与え側面シールをイ
ンナーカットの場合と同様に確保する。即ち、圧縮リン
グ11を展開したとき、溝14の中心線は圧縮リング11の幅
中心と平行する直線となる。
An inner peripheral surface 16 of the piston ring 11 is provided with a groove 14 having a substantially semicircular cross section and extending in the circumferential direction. The center of the groove 14 is located slightly above the center of the piston ring 11 in the width direction,
Thus, the piston ring 11 is twisted to secure the side seal in the same manner as in the case of the inner cut. That is, when the compression ring 11 is expanded, the center line of the groove 14 becomes a straight line parallel to the width center of the compression ring 11.

インナーカットを設けないため、凹入面13の内側縁を
リング上方内周隅角部近くまでもってくるとともに、突
出部12の内側縁をリング上方内周隅角部近くまで延在さ
せ、突出部12の断面積を大とさせ得る。
Since the inner cut is not provided, the inner edge of the concave surface 13 is brought near the inner corner of the upper ring, and the inner edge of the protrusion 12 is extended to near the inner corner of the ring. Twelve cross-sectional areas can be large.

この事実を実例をもって説明する。76φシリンダー径
の圧縮リングは、厚みが3.3mm、幅が1.5mmである。この
圧縮リング内周面に深さ0.5mm、高さ0.5mmの溝を設ける
と、突出部の断面積を1.65mm2(厚み又は高さ3.0mm×幅
1.1mm×1/2)とることができる。同寸法の圧縮リングの
上方内周隅角部に0.5×0.5mmの三角形のインナーカット
を設けると、突出部の断面積は1.43mm2(厚み又は高さ
2.6mm×幅1.1mm×1/2)で、本件の場合より小さい。即
ち、本件は、従来より15%増の断面積を得ることができ
る。
This fact will be explained with an example. The compression ring having a diameter of 76φ cylinder has a thickness of 3.3 mm and a width of 1.5 mm. When a groove with a depth of 0.5 mm and a height of 0.5 mm is provided on the inner peripheral surface of this compression ring, the cross-sectional area of the protrusion is 1.65 mm 2 (thickness or height 3.0 mm × width
1.1 mm x 1/2). When a 0.5 x 0.5 mm triangular inner cut is provided at the upper inner corner of a compression ring of the same dimensions, the cross-sectional area of the protrusion is 1.43 mm 2 (thickness or height)
2.6mm x 1.1mm x 1/2), smaller than in this case. That is, in the present case, the cross-sectional area can be increased by 15% as compared with the conventional case.

図2に示す例は、ピストンリング11の内周面16に2個
の溝14、15を平行に周方向に延在させたものである。下
側の溝14の中心がピストンリング11の幅中心よりやゝ上
方に位置するが、他の構成は図1と同じである。即ち、
圧縮リング11を展開したとき、溝14の中心線は圧縮リン
グ11の幅中心と平行する直線となる。
In the example shown in FIG. 2, two grooves 14, 15 extend in the circumferential direction in parallel with the inner peripheral surface 16 of the piston ring 11. The center of the lower groove 14 is located slightly above the center of the width of the piston ring 11, but the other configuration is the same as that of FIG. That is,
When the compression ring 11 is deployed, the center line of the groove 14 is a straight line parallel to the width center of the compression ring 11.

ピストンリング11の内周面の溝14、15は、ピストンリ
ング11の素材を線材として引抜くとき、金型に予め溝相
当部を作っておき、素材引抜き作業と同時に溝14、15を
形成するとよい。
When the grooves 14 and 15 on the inner peripheral surface of the piston ring 11 are drawn out of the material of the piston ring 11 as a wire, a groove equivalent portion is formed in a mold in advance, and the grooves 14 and 15 are formed simultaneously with the material drawing operation. Good.

前述した76φシリンダー径の圧縮リング(各寸法は前
述の通り)の内周面に溝を設けた本例と、そのリング上
方内周隅角部にアンダーカットを設けた従来例とを100
本テスト(4/4負荷2400rpm、200時間連続運転)した結
果、突出部2の折損のない両リングの側面シール効果は
同程度で、オイル消費量に差はみられなかったが、本例
では突出部12の折損がないのに対し、従来例では数本の
折損がみられエンジン性能の劣化が顕著であった。
The above-mentioned example in which a groove is provided on the inner peripheral surface of the above-described compression ring having a 76φ cylinder diameter (each dimension is as described above) and the conventional example in which an undercut is provided in the inner peripheral corner above the ring are 100%.
As a result of this test (4/4 load 2400 rpm, continuous operation for 200 hours), the side seal effect of both rings without breakage of the protrusion 2 was almost the same, and there was no difference in oil consumption. While there was no breakage of the protruding part 12, several breakages were observed in the conventional example, and the engine performance was significantly deteriorated.

産業上の利用可能性 本発明によれば、ピストンリング合口部の突出部の断
面積を充分に大きくとることができ、しかも側面シール
特性をインナーカットした例と同じように維持できる。
INDUSTRIAL APPLICABILITY According to the present invention, the cross-sectional area of the protruding portion of the piston ring abutment can be made sufficiently large, and the side seal characteristics can be maintained in the same manner as in the case of the inner cut.

Claims (3)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】一方の合口端部の上方外周隅角部に周方向
に突出する突出部が形成され、他方の合口端部の上方外
周隅角部に上記突出部を受入れ可能な凹入部が形成され
た合口を有する内燃機関用圧縮リングにおいて、該圧縮
リングの内周面にその幅中心より上方に中心を位置させ
る溝を展開したとき溝の中心線が直線となるようかつ該
溝が圧縮リングの上面をその構成要件としないよう周方
向に延在させたことを特徴とする内燃機関用圧縮リン
グ。
A projection is formed at an upper outer corner of one of the abutment ends so as to protrude in the circumferential direction, and a concave portion capable of receiving the projection is formed at an upper outer corner of the other apex end. In a compression ring for an internal combustion engine having a formed abutment, the center line of the groove is straightened when a groove positioned above the center of its width is developed on the inner peripheral surface of the compression ring, and the groove is compressed. A compression ring for an internal combustion engine, wherein an upper surface of the ring is extended in a circumferential direction so as not to be a component.
【請求項2】溝を平行に複数形成させている請求項1記
載の圧縮リング。
2. The compression ring according to claim 1, wherein a plurality of grooves are formed in parallel.
【請求項3】溝の断面が半円形である請求項2記載の圧
縮リング。
3. The compression ring according to claim 2, wherein the cross section of the groove is semicircular.
JP7521722A 1994-02-24 1995-02-22 Compression ring for internal combustion engine Expired - Fee Related JP2737107B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7521722A JP2737107B2 (en) 1994-02-24 1995-02-22 Compression ring for internal combustion engine

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP6-49948 1994-02-24
JP4994894 1994-02-24
JP7521722A JP2737107B2 (en) 1994-02-24 1995-02-22 Compression ring for internal combustion engine

Publications (1)

Publication Number Publication Date
JP2737107B2 true JP2737107B2 (en) 1998-04-08

Family

ID=26390384

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7521722A Expired - Fee Related JP2737107B2 (en) 1994-02-24 1995-02-22 Compression ring for internal combustion engine

Country Status (1)

Country Link
JP (1) JP2737107B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2021152363A (en) * 2020-03-24 2021-09-30 シーメンス アクチエンゲゼルシヤフトSiemens Aktiengesellschaft Seal ring for rotor, and rotor with such seal ring

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2021152363A (en) * 2020-03-24 2021-09-30 シーメンス アクチエンゲゼルシヤフトSiemens Aktiengesellschaft Seal ring for rotor, and rotor with such seal ring
JP7214774B2 (en) 2020-03-24 2023-01-30 シーメンス エナジー グローバル ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト Sealing rings for rotors and rotors with such sealing rings

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