JPH064025Y2 - Structure of vehicle swirl chamber - Google Patents

Structure of vehicle swirl chamber

Info

Publication number
JPH064025Y2
JPH064025Y2 JP9769986U JP9769986U JPH064025Y2 JP H064025 Y2 JPH064025 Y2 JP H064025Y2 JP 9769986 U JP9769986 U JP 9769986U JP 9769986 U JP9769986 U JP 9769986U JP H064025 Y2 JPH064025 Y2 JP H064025Y2
Authority
JP
Japan
Prior art keywords
swirl chamber
chamber wall
divided
ring
swirl
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
JP9769986U
Other languages
Japanese (ja)
Other versions
JPS634331U (en
Inventor
義彦 都築
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.)
Toyota Motor Corp
Original Assignee
Toyota Motor 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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP9769986U priority Critical patent/JPH064025Y2/en
Publication of JPS634331U publication Critical patent/JPS634331U/ja
Application granted granted Critical
Publication of JPH064025Y2 publication Critical patent/JPH064025Y2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

【考案の詳細な説明】 〔産業上の利用分野〕 本考案はセラミック材からなる車両用機関渦流壁を縦割
り分割構成片を組合せてリングで固定した渦流室の構造
に関する。
DETAILED DESCRIPTION OF THE INVENTION [Industrial field of application] The present invention relates to a structure of a swirl chamber in which a vehicle engine swirl wall made of a ceramic material is combined with vertically split component pieces and fixed by a ring.

〔従来の技術〕[Conventional technology]

機関の渦流室壁の全部または一部をセラミック材で構成
し、耐熱性、低燃費を達成させる技術は多数知られてい
る(たとえば特開昭47-21508号公報)。セラミック渦流
室壁は型成形で作製されるので、渦流室壁の下部のみを
セラック成形体で作製するときは、型が抜けるので問題
がないが、天井部も含み渦流室壁全体をセラミック材で
作製するときは、中子型抜きの問題から渦流室壁を分割
して形成する。
There are many known techniques for achieving heat resistance and low fuel consumption by constructing all or part of the wall of the swirl chamber of the engine with a ceramic material (for example, Japanese Patent Laid-Open No. 47-21508). Since the ceramic swirl chamber wall is made by molding, when making only the lower part of the swirl chamber wall with shellac molding, there is no problem because the mold will come off, but the entire swirl chamber wall including the ceiling part is made of ceramic material. At the time of manufacture, the wall of the swirl chamber is divided and formed due to the problem of die cutting.

従来、セラミック渦流室壁の分割形成においては、上記
特開昭47-21508号公報に示されているように、分割線は
水平、すなわち軸芯に対して直角な面とされ、横割りで
作製されるのが普通であった。これは、もし縦割りにす
ると、組合せが緩んだときに当接部に隙間ができ、噴孔
以外の場所において渦流室とピストン直上の燃焼室6が
連通して所望の燃焼が得られなくなるおそれがあるため
である。
Conventionally, in the divisional formation of the ceramic swirl chamber wall, the dividing line is horizontal, that is, a plane perpendicular to the axis, as shown in the above-mentioned JP-A-47-21508, and is produced by transverse division. It was usual to be done. This is because if it is split vertically, a gap is created in the abutting part when the combination is loosened, and the swirl chamber and the combustion chamber 6 immediately above the piston communicate with each other in a place other than the injection hole, and desired combustion may not be obtained. Because there is.

〔考案が解決しようとする問題点〕[Problems to be solved by the invention]

しかし、横割り製作においては、渦流室壁面が上部が半
球面、下部が下方に向って縮径されたほぼ円筒面である
場合、中子抜き上少なくとも3分割構成が望ましく、分
割の増加、それに伴う成形型、成形工数の増加、コスト
アップが問題となる。また、横方向に輪切りされた分割
片を型成形で作ることは一般的に難しく、量産に向かな
い等の問題もある。
However, in the case of horizontal production, if the vortex chamber wall surface is a hemispherical surface in the upper part and a substantially cylindrical surface in which the lower part is reduced in diameter downward, it is desirable to have at least three divisions on the core, and increase the division. As a result, there is a problem in that the number of molding dies, the number of molding steps, and the cost increase increase. Further, it is generally difficult to form a laterally sliced divided piece by molding, and there is a problem that it is not suitable for mass production.

本考案は、従来は渦流室壁体の成形でかえり見られなか
った縦割成形を適用して製作の容易化をはかり、縦割り
によって生じる問題の解決手段も与えて、縦割り成形の
実用化を可能ならしめることを目的とする。
In the present invention, the vertical split molding, which has not been seen in the past for forming the wall of the swirl chamber, is applied to facilitate the production, and also the solution for the problem caused by the vertical split is provided, and the vertical split molding is put into practical use. The purpose is to make possible.

〔問題点を解決するための手段〕[Means for solving problems]

上記目的を達成するための本考案の車両用機関渦流室の
構造は、機関の渦流室壁をセラミック材で構成した車両
用機関渦流室の構造において、渦流室壁体を縦割に2分
割形成し、分割渦流室壁体を周方向に互にシムを介して
組合せ、外周側から金属製のリングで焼ばめして組合せ
渦流室壁体を固定するとともに渦流室壁体に圧縮のプリ
ロードをかけたものから成る。
In order to achieve the above object, the structure of a vehicle engine swirl chamber of the present invention is a vehicle engine swirl chamber structure in which an engine swirl chamber wall is made of a ceramic material. Then, the divided vortex chamber wall bodies are assembled in the circumferential direction with shims, and the combined vortex chamber wall bodies are fixed by shrink-fitting with a metal ring from the outer peripheral side, and compression preload is applied to the vortex chamber wall bodies. It consists of

〔作用〕[Action]

上記本考案の機関渦流室の構造では、渦流室壁体を縦割
り成形とすることによって製作の容易化がはかられる。
この縦割りされた分割渦流室壁体の組立は外周に焼ばめ
されるリングによってなされる。リングは引張応力に弱
いセラミック材に圧縮のプリロードをかけて圧縮応力下
で使用するために従来からも用いられてきたものである
が、このプリロードの発生と同時に周方向に分割された
分割渦流室壁体を互に固定する機能も同時に果たすとい
う相剰効果を果たしている。また分割渦流室壁体はシム
を介して当接されているので、分割面に隙間が生じてガ
スが流通することによる燃焼の乱れは生じない。
In the structure of the engine swirl chamber according to the present invention, the manufacture of the swirl chamber wall can be facilitated by vertically dividing the wall of the swirl chamber.
This vertically divided split vortex chamber wall body is assembled by a ring that is shrink-fitted to the outer periphery. The ring has been used in the past to apply a compressive preload to a ceramic material that is weak against tensile stress and to use it under compressive stress.However, at the same time when this preload occurs, the divided vortex chamber is divided in the circumferential direction. It also has the effect of reciprocally fixing the walls to each other. Further, since the divided vortex chamber wall bodies are in contact with each other through the shims, the combustion surface is not disturbed due to the formation of gaps in the divided surfaces and the flow of gas.

〔実施例〕〔Example〕

以下に、本考案に係る機関渦流室の構造の望ましい実施
例を図面を参照して説明する。
Hereinafter, preferred embodiments of the structure of an engine swirl chamber according to the present invention will be described with reference to the drawings.

第1図において、1は機関のシリンダブロック、2はシ
リンダヘッドで、シリンダブロック1の上部にガスケッ
ト3を介して装着されている。シリンダブロック1には
ピストン4が往復動可能に挿入され、ピストン4の頂面
には凹部が形成され、ピストン上方燃焼室5の一部を形
成している。シリンダヘッド2には下方に向って開口し
た凹部6が形成され、そこに渦流室壁体7が挿入され
る。渦流室壁体7は内部に渦流室8を有し、渦流室8は
ピストン上方燃焼室5と、渦流室壁体7の底部に形成さ
れた、斜めに貫通して延びる噴孔9によって、連通され
ている。渦流室壁体7には孔10、11、12が貫通されてお
り、該孔10、11、12を貫通してそれぞれグロープラグ13、
インジェクションノズル14、着火時時センサ15が渦流室
8に臨んでいる。シリンダブロック1、シリンダヘッド
2には燃焼室まわりにウォータジャケット16、17が形成
され、そこにエンジン冷却水が循環される。以上までの
構成は、従来と同じである。
In FIG. 1, 1 is a cylinder block of an engine, 2 is a cylinder head, which is mounted on the top of the cylinder block 1 via a gasket 3. A piston 4 is reciprocally inserted in the cylinder block 1 and a recess is formed on the top surface of the piston 4 to form a part of the piston upper combustion chamber 5. The cylinder head 2 is formed with a recess 6 that opens downward, and the swirl chamber wall 7 is inserted therein. The swirl chamber wall 7 has a swirl chamber 8 therein, and the swirl chamber 8 communicates with the piston upper combustion chamber 5 and a nozzle hole 9 formed at the bottom of the swirl chamber wall 7 and extending obliquely therethrough. Has been done. The swirl chamber wall 7 has holes 10, 11 and 12 penetrating therethrough, and the glow plugs 13 and 12 respectively penetrating the holes 10, 11 and 12 respectively.
The injection nozzle 14 and the sensor 15 at the time of ignition face the swirl chamber 8. Water jackets 16 and 17 are formed around the combustion chamber in the cylinder block 1 and the cylinder head 2, and engine cooling water is circulated therein. The configuration up to this point is the same as the conventional one.

渦流室壁体7は、噴孔9が穿設された円板状の底部7a
と、底部7aから上方に立上る円筒外周面を有する筒状
の中間部7bと、中間部7bから上方につらなる半球状
の天井部7cとから成る。渦流室8はそれらの内部に形
成されていて、球体を底部7aの上面で切断した形状を
有している。
The swirl chamber wall 7 has a disk-shaped bottom portion 7a having a nozzle hole 9 formed therein.
And a cylindrical intermediate portion 7b having a cylindrical outer peripheral surface rising upward from the bottom portion 7a, and a hemispherical ceiling portion 7c extending upward from the intermediate portion 7b. The swirl chamber 8 is formed inside them and has a shape obtained by cutting a sphere at the upper surface of the bottom portion 7a.

渦流室壁体7はSi3N4等のセラミック材(ファインセラ
ミック材使用可)からなり、射出成形途上においてほぼ
中央で縦割りに2分割される。第1図中符号Aはその分
割面を示しており、中子抜きが容易である。第1図で
は、分割面Aは噴孔9を切断しているが、噴孔9は分割
面Aを含まない位置に設けられていてもよい。
The swirl chamber wall 7 is made of a ceramic material such as Si 3 N 4 (a fine ceramic material can be used), and is divided into two vertically in the middle of injection molding. Reference numeral A in FIG. 1 indicates the divided surface, and core removal is easy. In FIG. 1, the divided surface A cuts the injection hole 9, but the injection hole 9 may be provided at a position not including the divided surface A.

第2図および第3図はかくして成形された分割渦流室壁
体7−1、7−2を示している。
2 and 3 show the divided vortex chamber wall bodies 7-1 and 7-2 thus formed.

分割渦流室壁体7−1、7−2は、シム18を介して周方
向に当接される。シム18は第4図に示すような、当接面
と同じ平面形状を有する板状体からなる。シム18はクッ
ション性を有し、締め付けられたときにガスケットの機
能を果たしうる構造のものであり、たとえば無機繊維
体、金属箔膜板体、金属および無機材の板の重ね合せ体
等から成る。シム18の介装により、分割渦流室壁体7の
分割当接面の射出成形時の精度出しは不要であり、射出
成形のみで十分な精度が出るが、分割当接面に切削加工
を加えて一層高精度としてもよい。
The divided vortex chamber wall bodies 7-1 and 7-2 are circumferentially abutted via a shim 18. The shim 18 is made of a plate-like body having the same plane shape as the contact surface as shown in FIG. The shim 18 has a cushioning property and has a structure that can function as a gasket when tightened, and is made of, for example, an inorganic fiber body, a metal foil film plate body, a laminated body of metal and inorganic material plates, or the like. . The insertion of the shim 18 eliminates the need for precision in the injection molding of the divided contact surface of the divided vortex chamber wall body 7, and sufficient precision can be obtained only by injection molding. It may be more accurate.

分割渦流室壁体7−1、7−2はシム18を介して周方向
に当接された後、外周側からシリンダ19、20をかけら
れ、周方向に一体的に固定されるとともに、渦流室壁体
7に圧縮のプリロードがかけられる。これらのリング1
9、20のうち、リング19は第5図に示す如く周方向に連続
してのびるはちまき状の金属製(Fe素材がよい)リング
からなり、渦流室壁体7外周の高さ方向中央部近傍に焼
ばめされてプリロードを発生させる。リング19は薄肉故
オーバロードにならずかつ弾性変形量も大きい。もう一
つのリング20は、棒線形の金属製リングで、第6図に示
すように周状1ヶ所切れ目をもち、渦流室壁体7の底部
7aの外周に形成された周方向に全周に延びる溝21内に
嵌着されて切れ目部を突合せて溶接し周方向に切れ目の
ないリングに形成され、分割渦流室壁体7−1、7−2
を位置決め固定する。なお、リング20は予め閉リングと
して形成されたものを焼ばめしてもよい。リング20には
引張り力がかかるようにしてリング20と渦流室壁体7は
周方向に位置ずれを起さないように密着される。これ
は、たとえばリング20を高温下でロボットで掴んで切れ
目を溶接し、冷却時点でリング20に引張力が生じるよう
にすればよい。22はピンでリング20に一体化溶接され、
シリンダヘッド2の凹部6の出口に軸方向に延びるよう
に、ドリル加工等で形成された溝23に打ち込まれ、渦流
室壁体7のシリンダヘッド2に対する周方向位置を固定
する。
The divided vortex chamber wall bodies 7-1 and 7-2 are circumferentially abutted via the shim 18, and then cylinders 19 and 20 are hung from the outer peripheral side to be integrally fixed in the circumferential direction and swirled. A compression preload is applied to the chamber wall 7. These rings 1
Of 9 and 20, the ring 19 is made of a metal-like (Fe material is good) ring that extends continuously in the circumferential direction as shown in FIG. 5, and is located near the central portion in the height direction of the outer circumference of the swirl chamber wall body 7. Shrink fit to generate preload. Since the ring 19 is thin, it is not overloaded and has a large elastic deformation amount. The other ring 20, which is a rod-shaped metal ring, has one circumferential cut, as shown in FIG. 6, and is formed on the outer circumference of the bottom portion 7a of the swirl chamber wall 7 along the entire circumference in the circumferential direction. The split swirl chamber wall bodies 7-1 and 7-2 are fitted into the extending groove 21 and the cut portions are butted and welded to each other to form a ring having no break in the circumferential direction.
Position and fix. It should be noted that the ring 20 may be pre-formed as a closed ring and shrink-fitted. A tensile force is applied to the ring 20 so that the ring 20 and the vortex chamber wall 7 are in close contact with each other so as not to be displaced in the circumferential direction. This may be done by, for example, gripping the ring 20 with a robot at a high temperature and welding the cuts so that a tensile force is generated in the ring 20 at the time of cooling. 22 is a pin integrally welded to the ring 20,
The cylinder head 2 is driven into a groove 23 formed by drilling or the like so as to extend in the exit of the recess 6 of the cylinder head 2 in the axial direction to fix the circumferential position of the swirl chamber wall body 7 with respect to the cylinder head 2.

リング19、20の嵌着により、渦流室壁体7がシリンダヘ
ッド2の凹部6に挿入されたときに、渦流室壁体7の外
面と凹部6の表面との間には隙間24が形成される。該隙
間24は、渦流室壁体7とシリンダヘッド2との熱膨張差
を逃げるとともに、熱伝導による熱損失を最小におさえ
る。
When the vortex chamber wall body 7 is inserted into the recess 6 of the cylinder head 2 by the fitting of the rings 19 and 20, a gap 24 is formed between the outer surface of the vortex chamber wall body 7 and the surface of the recess 6. It The gap 24 escapes the difference in thermal expansion between the swirl chamber wall 7 and the cylinder head 2, and minimizes heat loss due to heat conduction.

上記構成を有する渦流室の構造では、渦流室壁体7が縦
割り分割のため、成形が容易で、中子の数も減少かつ単
純化でき、かつセラミック材料にSiC、Si3N4等の最高級
材を用いなくとも低コストのファインセラミック材を使
用し得る。
In the structure of the swirl chamber having the above configuration, since the swirl chamber wall body 7 is vertically divided, molding is easy, the number of cores can be reduced and simplified, and the ceramic material is made of SiC, Si 3 N 4, or the like. It is possible to use low-cost fine ceramic materials without using the highest grade materials.

固定の方法もリング19、20の嵌着で済み、これはプリロ
ードを発生させる上で従来からも必要な部材であったも
のを、そのまま分割渦流室壁7−1、7−2の周方向一
体的固定に利用できるので、相剰効果を発揮できる。
The ring 19 and 20 need only be fitted by the method of fixing, which is a member that has been necessary in the past for generating preload, but is directly integrated in the circumferential direction of the divided vortex chamber walls 7-1 and 7-2. Since it can be used for static fixation, it is possible to exert a summation effect.

縦割り分割において問題となる分割渦流室壁7−1、7
−2間の隙間はシム18によってシールされ側路がガスが
洩れることはない。
Dividing vortex chamber walls 7-1 and 7 which are problems in vertical division
The gap between the two is sealed by the shim 18 so that no gas leaks in the bypass.

プリロードを与えるリング19、20はその断面積が小さ
く、弾性変形可能で、渦流室壁7に大きすぎるプリロー
ドを与えない。
The rings 19 and 20 for providing the preload have a small cross-sectional area, are elastically deformable, and do not give an excessively large preload to the swirl chamber wall 7.

渦流室壁7の周方向固定はピン22によって容易になされ
得る。
The circumferential fixing of the swirl chamber wall 7 can be facilitated by the pin 22.

〔考案の効果〕 本考案に係る車両用機関渦流室の構造によるときは、セ
ラミック渦流室壁体を縦割り2分割としたので、成形の
容易化をはかることができる。
[Advantages of the Invention] In the structure of the vehicle engine swirl chamber according to the present invention, since the ceramic swirl chamber wall is divided into two vertically, the molding can be facilitated.

またリングによる周方向一体固定としたので、プリロー
ドを与えるためのリングがそのまま固定にも利用でき、
相剰効果が得られる。
In addition, since it is fixed integrally with the ring in the circumferential direction, the ring for giving the preload can be used as it is,
A reciprocal effect is obtained.

さらに、分割渦流室壁体をシムを介して突き合わせて組
合せたので、突合せ面のガス洩れを防止でき、安定した
燃焼を得ることができる。
Further, since the divided vortex chamber wall bodies are butted against each other via the shims and combined, it is possible to prevent gas leakage at the butted surfaces and to obtain stable combustion.

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

第1図は本考案の一実施例に係る機関渦流室の構造の断
面図、 第2図は一方の分割渦流室壁体の斜視図、 第3図は他方の分割渦流室壁体の斜視図、 第4図はシムの斜視図、 第5図はリング(はちまき状)の斜視図、 第6図はリング(棒線状)の斜視図、 である。 2……シリンダヘッド 7……渦流室壁体 7−1、7−2……分割渦流室壁体 8……渦流室 18……シム 19、20……リング 22……ピン
FIG. 1 is a sectional view of the structure of an engine swirl chamber according to an embodiment of the present invention, FIG. 2 is a perspective view of one divided swirl chamber wall, and FIG. 3 is a perspective view of the other divided swirl chamber wall. FIG. 4 is a perspective view of a shim, FIG. 5 is a perspective view of a ring (bill-shaped), and FIG. 6 is a perspective view of a ring (rod-shaped). 2 ... Cylinder head 7 ... Vortex chamber wall 7-1, 7-2 ... Split vortex chamber wall 8 ... Vortex chamber 18 ... Shim 19, 20 ...... Ring 22 ...... Pin

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 【請求項1】機関の渦流室壁体をセラミック材で構成し
た車両用機関渦流室の構造において、渦流室壁体を縦割
りに2分割形成し、分割渦流室壁体を周方向に互にシム
を介して組合せ、外周側から金属製のリングを焼ばめし
て組合せ渦流室壁体を固定するとともに渦流室壁体に圧
縮のプリロードをかけたことを特徴とする車両用機関渦
流室の構造。
1. In a structure of a vehicle engine swirl chamber in which the swirl chamber wall of the engine is made of a ceramic material, the swirl chamber wall is divided into two vertically divided parts, and the divided swirl chamber walls are mutually circumferentially arranged. Structure of vehicle engine swirl chamber characterized by combining through a shim, shrink-fitting a metal ring from the outer peripheral side to fix the combined swirl chamber wall body and applying compression preload to the swirl chamber wall body .
JP9769986U 1986-06-27 1986-06-27 Structure of vehicle swirl chamber Expired - Lifetime JPH064025Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9769986U JPH064025Y2 (en) 1986-06-27 1986-06-27 Structure of vehicle swirl chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9769986U JPH064025Y2 (en) 1986-06-27 1986-06-27 Structure of vehicle swirl chamber

Publications (2)

Publication Number Publication Date
JPS634331U JPS634331U (en) 1988-01-12
JPH064025Y2 true JPH064025Y2 (en) 1994-02-02

Family

ID=30964924

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9769986U Expired - Lifetime JPH064025Y2 (en) 1986-06-27 1986-06-27 Structure of vehicle swirl chamber

Country Status (1)

Country Link
JP (1) JPH064025Y2 (en)

Also Published As

Publication number Publication date
JPS634331U (en) 1988-01-12

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