JPH041453A - Cylinder liner - Google Patents
Cylinder linerInfo
- Publication number
- JPH041453A JPH041453A JP9977490A JP9977490A JPH041453A JP H041453 A JPH041453 A JP H041453A JP 9977490 A JP9977490 A JP 9977490A JP 9977490 A JP9977490 A JP 9977490A JP H041453 A JPH041453 A JP H041453A
- Authority
- JP
- Japan
- Prior art keywords
- cylinder
- cylinder liner
- cooling
- annular groove
- arrow
- 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
Links
- 238000001816 cooling Methods 0.000 claims abstract description 16
- 239000000498 cooling water Substances 0.000 claims abstract description 9
- 230000013011 mating Effects 0.000 abstract 2
- 230000002349 favourable effect Effects 0.000 abstract 1
- 239000002131 composite material Substances 0.000 description 3
- 238000005192 partition Methods 0.000 description 2
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- 229910001208 Crucible steel Inorganic materials 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明はディーゼル機関の高冷却、高強度の複合シリン
ダライナに関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a high-cooling, high-strength composite cylinder liner for a diesel engine.
第4図は従来形高強度複合シリンダライナの縦断面図で
、潤滑性に優れた鋳鉄製の内筒O1と、高強度鋳鋼製の
外筒02とが、その接合面03においてHIP接合され
ていた。Figure 4 is a longitudinal cross-sectional view of a conventional high-strength composite cylinder liner, in which an inner cylinder O1 made of cast iron with excellent lubricity and an outer cylinder O2 made of high-strength cast steel are HIP-jointed at their joint surface 03. Ta.
前記シリンダライナの内面04と図示しないピストンリ
ングとの間は、油潤滑による摺動面となっている為、ス
カッフィング防止のため該摺動面の過熱を避ける必要が
ある。ところが前記従来形のシリンダライナのように外
面05からの水冷で且、高出力機関のシリンダライナに
於ては内面04の冷却が不充分となる欠点があった。Since the inner surface 04 of the cylinder liner and the piston ring (not shown) are oil-lubricated sliding surfaces, it is necessary to avoid overheating the sliding surfaces to prevent scuffing. However, like the conventional cylinder liner, water cooling is performed from the outer surface 05, and in cylinder liners for high-output engines, the inner surface 04 is not sufficiently cooled.
本発明の目的は前記従来装置の問題点を解消し、特に内
面を効率よく冷却できる高出力機関用シリンダライナを
提供するにある。SUMMARY OF THE INVENTION An object of the present invention is to provide a cylinder liner for a high-output engine that can solve the problems of the conventional apparatus, and in particular can efficiently cool the inner surface.
本発明の高出力機関用シリンダライナは内筒と外筒とよ
り、形成されると共に両接合面03に冷却溝を設は一該
冷却溝に冷却水を通して特にシリンダライナの内面を冷
却するようにしたものである。The cylinder liner for high-output engines of the present invention is formed of an inner cylinder and an outer cylinder, and cooling grooves are provided on both joint surfaces 03. Cooling water is passed through the cooling grooves so as to particularly cool the inner surface of the cylinder liner. This is what I did.
接合面03は外面05よりも内面04に近く又冷却水の
通路面積がせまくて流速も速いため内面04の冷却が十
分に行われる。The joint surface 03 is closer to the inner surface 04 than the outer surface 05, and the passage area of the cooling water is small and the flow rate is high, so that the inner surface 04 is sufficiently cooled.
以下第1図を参照し本発明の第1実施例について説明す
る。A first embodiment of the present invention will be described below with reference to FIG.
第1図は高強度複合シリンダライナの縦断面図である。FIG. 1 is a longitudinal sectional view of a high-strength composite cylinder liner.
内筒1と外筒2からなるシリンダライナで外筒2の接合
面3の上部26に螺旋状の冷却溝6が設けられ、冷却水
は矢印7のようL二流入し矢印8のように流出するよう
になっている。冷却溝6は外面5よりも内面に近く、且
流速もはやいので内面4の冷却は良好となる。The cylinder liner consists of an inner cylinder 1 and an outer cylinder 2, and a spiral cooling groove 6 is provided in the upper part 26 of the joint surface 3 of the outer cylinder 2, and the cooling water flows into L2 as shown by arrow 7 and flows out as shown by arrow 8. It is supposed to be done. Since the cooling grooves 6 are closer to the inner surface than the outer surface 5 and the flow velocity is faster, the inner surface 4 can be cooled well.
なお、らせん状の冷却溝6を外筒に設けたが、内筒1側
に設けることもできる。Although the spiral cooling grooves 6 are provided on the outer cylinder, they may also be provided on the inner cylinder 1 side.
又内筒1と外筒2の接合はHIPによるほか焼ばめ接合
としてもよい。In addition to HIP, the inner tube 1 and outer tube 2 may be joined by shrink fit.
第2〜3図は第2実施例を示すもので、第2図はシリン
ダライナ上部付近(第3図の■−■矢視)の縦断面であ
り、第3図は外筒側接合面に対するP矢視展間図である
。なお第図の上部はシリンダヘッド11である。Figures 2 and 3 show the second embodiment. Figure 2 is a vertical cross section of the cylinder liner near the top (as seen from This is a view from P arrow. Note that the upper part of the figure is the cylinder head 11.
シリンダライナの接合面3の外筒側2の上部は連通して
いる。なお上部円環溝9は仕切金物14で螺旋溝16が
2個ずつ4個の室に仕切られ、冷却水の反転室13を形
成している。一方下部円環10は仕切金物15で螺旋溝
16のすべてが仕切られており、入口室18と出口室1
7を交互に形成している。又入口室18は入口孔23と
連通し、出口室17は連絡溝24をへて出口孔25と連
通している。冷却水は矢印7から流入し矢印19、矢印
20、矢印21、矢印22をへて矢印8から流出する。The upper part of the outer cylinder side 2 of the joint surface 3 of the cylinder liner is in communication. The upper annular groove 9 is partitioned into four chambers each having two spiral grooves 16 by a partition metal fitting 14 to form a cooling water reversal chamber 13. On the other hand, in the lower ring 10, all of the spiral grooves 16 are partitioned by partition hardware 15, and an inlet chamber 18 and an outlet chamber 1 are separated.
7 are formed alternately. Further, the inlet chamber 18 communicates with the inlet hole 23, and the outlet chamber 17 communicates with the outlet hole 25 through the communication groove 24. Cooling water flows in from arrow 7, passes through arrow 19, arrow 20, arrow 21, and arrow 22, and flows out from arrow 8.
上記構成によりシリンダライナの内面の螺旋溝6、上部
円環溝9、下部円環溝10を通る冷却水により、所定の
温度まで容易に冷却させることができる。With the above configuration, the cylinder liner can be easily cooled to a predetermined temperature by the cooling water passing through the spiral groove 6, upper annular groove 9, and lower annular groove 10 on the inner surface of the cylinder liner.
なお、この第2実施例で螺旋溝16、上部円環溝9、下
部円環溝10、連絡溝24等を接合面の外筒2側に設け
たが内筒1側に設けてもよい。In this second embodiment, the spiral groove 16, the upper annular groove 9, the lower annular groove 10, the communication groove 24, etc. are provided on the outer cylinder 2 side of the joint surface, but they may be provided on the inner cylinder 1 side.
本発明のシリンダライナは内筒と外筒との接合面に冷却
溝を配設したため、その内面が特に効率よく冷却可能と
なり、高出力機関に最も適したシリンダライナを提供で
きる。Since the cylinder liner of the present invention has cooling grooves disposed on the joint surface between the inner cylinder and the outer cylinder, the inner surface can be cooled particularly efficiently, and a cylinder liner most suitable for high-output engines can be provided.
第1〜3図は本発明に係わるもので、第1図は第1実施
例の縦断面図、第3図は第2実施例の外筒側接合面の展
開図、第2図は第3図の■−■矢視縦断面図、第4図は
従来例の縦断面図である。
1・・・内筒、2・・・外筒、3・・・接合面、6・・
・冷却溝、9・・・上部円環溝、10・・・下部円環溝
、16・・・螺旋溝、17・・・出口室、18・・・入
口室。
第1図
第2
図
O4内面
第4
図1 to 3 are related to the present invention. FIG. 1 is a longitudinal sectional view of the first embodiment, FIG. 3 is a developed view of the outer cylinder side joint surface of the second embodiment, and FIG. 2 is a third embodiment. FIG. 4 is a vertical cross-sectional view of the conventional example. 1...Inner cylinder, 2...Outer cylinder, 3...Joint surface, 6...
- Cooling groove, 9... Upper annular groove, 10... Lower annular groove, 16... Spiral groove, 17... Outlet chamber, 18... Inlet chamber. Fig. 1 Fig. 2 Fig. O4 inner surface Fig. 4
Claims (2)
ライナにおいて、両者の接合面に冷却溝を有してなるシ
リンダライナ。(1) A cylinder liner constituted by a double cylinder consisting of an inner cylinder and an outer cylinder, which has cooling grooves on the joining surface of the two.
(10)を複数個の螺旋溝(16)でつなぎ、上部円環
溝(9)(又は下部円環溝(10))を円周上に仕切っ
て冷却水の反転室(13)を形成し、下部円環溝(10
)(又は上部円環溝(9))を円周上に仕切って冷却水
の入口室(18)および出口室(17)を構成したこと
を特徴とするシリンダライナ。(2) The cooling groove of claim 1 connects the upper annular groove (9) and the lower annular groove (10) with a plurality of spiral grooves (16), and the upper annular groove (9) (or the lower annular groove ( 10)) on the circumference to form a cooling water reversal chamber (13), and a lower annular groove (10).
) (or the upper annular groove (9)) is circumferentially partitioned to form a cooling water inlet chamber (18) and an outlet chamber (17).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9977490A JPH041453A (en) | 1990-04-16 | 1990-04-16 | Cylinder liner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9977490A JPH041453A (en) | 1990-04-16 | 1990-04-16 | Cylinder liner |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH041453A true JPH041453A (en) | 1992-01-06 |
Family
ID=14256309
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP9977490A Pending JPH041453A (en) | 1990-04-16 | 1990-04-16 | Cylinder liner |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH041453A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5553585A (en) * | 1994-05-27 | 1996-09-10 | Wartsila Diesel International Ltd Oy | Anti-polishing ring |
US8602356B2 (en) | 2005-08-17 | 2013-12-10 | Airbus Operations Gmbh | Framework wing box for a wing |
JP2014521866A (en) * | 2011-07-29 | 2014-08-28 | アカーテース パワー,インク. | Cylinder collision cooling in opposed piston engines. |
JP2014206174A (en) * | 2006-04-18 | 2014-10-30 | ピナクル エンジンズ インコーポレイテッド | Internal combustion engine |
US9650951B2 (en) | 2010-10-08 | 2017-05-16 | Pinnacle Engines, Inc. | Single piston sleeve valve with optional variable compression ratio capability |
CN106930853A (en) * | 2015-12-31 | 2017-07-07 | 沪东重机有限公司 | A kind of cooling jacket with spiral inlet channel |
WO2017128510A1 (en) * | 2016-01-28 | 2017-08-03 | 江苏科技大学 | Combined cylinder liner |
-
1990
- 1990-04-16 JP JP9977490A patent/JPH041453A/en active Pending
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5553585A (en) * | 1994-05-27 | 1996-09-10 | Wartsila Diesel International Ltd Oy | Anti-polishing ring |
US8602356B2 (en) | 2005-08-17 | 2013-12-10 | Airbus Operations Gmbh | Framework wing box for a wing |
JP2014206174A (en) * | 2006-04-18 | 2014-10-30 | ピナクル エンジンズ インコーポレイテッド | Internal combustion engine |
US9650951B2 (en) | 2010-10-08 | 2017-05-16 | Pinnacle Engines, Inc. | Single piston sleeve valve with optional variable compression ratio capability |
JP2014521866A (en) * | 2011-07-29 | 2014-08-28 | アカーテース パワー,インク. | Cylinder collision cooling in opposed piston engines. |
CN106930853A (en) * | 2015-12-31 | 2017-07-07 | 沪东重机有限公司 | A kind of cooling jacket with spiral inlet channel |
WO2017128510A1 (en) * | 2016-01-28 | 2017-08-03 | 江苏科技大学 | Combined cylinder liner |
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