JPH0578645B2 - - Google Patents
Info
- Publication number
- JPH0578645B2 JPH0578645B2 JP59215395A JP21539584A JPH0578645B2 JP H0578645 B2 JPH0578645 B2 JP H0578645B2 JP 59215395 A JP59215395 A JP 59215395A JP 21539584 A JP21539584 A JP 21539584A JP H0578645 B2 JPH0578645 B2 JP H0578645B2
- Authority
- JP
- Japan
- Prior art keywords
- outer cylinder
- inner cylinder
- cylinder
- chamber
- coupling ring
- 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
Links
- 230000008878 coupling Effects 0.000 claims description 13
- 238000010168 coupling process Methods 0.000 claims description 13
- 238000005859 coupling reaction Methods 0.000 claims description 13
- 238000004519 manufacturing process Methods 0.000 claims description 10
- 239000000919 ceramic Substances 0.000 claims description 9
- 238000005245 sintering Methods 0.000 claims description 9
- 239000000463 material Substances 0.000 claims description 8
- 229910052751 metal Inorganic materials 0.000 claims description 6
- 239000002184 metal Substances 0.000 claims description 6
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 239000002657 fibrous material Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 229910010293 ceramic material Inorganic materials 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 239000000446 fuel Substances 0.000 description 3
- 239000007769 metal material Substances 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 229910052581 Si3N4 Inorganic materials 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 2
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 229910001928 zirconium oxide Inorganic materials 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/16—Chamber shapes or constructions not specific to sub-groups F02B19/02 - F02B19/10
- F02B19/165—The shape or construction of the pre-combustion chambers is specially adapted to be formed, at least in part, of ceramic material
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Ceramic Products (AREA)
- Devices For Post-Treatments, Processing, Supply, Discharge, And Other Processes (AREA)
Description
(産業上の利用分野)
この発明はエンジンにおける予熱焼室の技術分
野で利用されるもので、主として副室の製造技術
に関するものである。
(従来の技術)
デイーゼルエンジンの予熱焼室としての副室構
造体は従来から周知である。またこの副室の構造
において副室内の耐熱性を高めるためにセラミツ
クス材で成型する考案もある。例えば実開昭54−
77802号公報に開示されている副室は、セラミツ
クス材で製作した内筒の外周を鋳鉄で鋳ぐるみし
て一体化したものである。
しかしながら前記考案の構造による鋳造設備を
必要とし、作業性に問題がある。
(発明の目的)
この発明の完成に先立つて、前記副室を形成す
る部材(内筒)をセラミツクス製とし、この部材
の外周に断熱材を環状に設けるとともに、副室を
形成する部材(外筒)を焼結金属材によつて覆つ
た構造のものを試作したところ、該焼結金属材は
内外筒の接触の強い部位を中心に軸方向およぴ直
径方向において不均一な収縮をし、焼結金属材
(外筒)と副室部材(内筒)との間でずれが生じ、
エンジンへの組付時に問題となる外形の寸法精度
が保持できなくなることが判明した。例えばこの
発明の製造工程を示す第1図において、焼結金属
製外筒2の肩面2dとセラミツクス製内筒1の底
面との平面度がくずれて、組付時に燃焼室精度を
確保できない等の不具合を生じるのである。
この発明においては、充分な断熱効果を有する
と共に副室を形成する部材(内筒)と該部材を覆
う焼結金属製部材(外筒)とがずれることなく緊
密に接合された構造のエンジンの副室の製造法を
提供することを目的とする。
(発明の構成)
この発明における製造法は、焼結材によつて予
備形成した外筒の開口部からセラミツクス製の内
筒を嵌装し、前記開口部における外筒と内筒との
隙間にこの外筒の焼結温度においてこれと一体化
される金属製の断面くさび状の結合リングを圧入
し内外筒の間を固定してから加熱焼結するように
した副室の製造法である。
この発明の作用は、上記製法によつて、内筒と
外筒が該外筒の開口部において拘束した状態で加
熱し焼結するから、焼結材の特性として外筒が部
分的に不均等な収縮をするとしても、前記拘束部
分が固定した状態で収縮することによつて内筒と
外筒の寸法的関係、例えば内筒の底面と外筒の肩
面との平行度が良好な精度で仕上げられるもので
ある。
(実施例)
以下、図面を参照しつつこの発明の実施例を詳
述する。
副室構成部材である内筒1はセラミツクス(例
えば窒化珪素)で形成され、その下半部1aと上
半部1bとに分割したものになつている。下半部
1aはほぼ有底円筒状に上半部1bはほぼ半球状
に形成される。そして下半部1aの底部には噴口
1cが開口され、上半部1bには燃料噴出口1d
が開口されている。副室構成部材である外筒2は
第1図に示すように鉄系の焼結材によつて上端が
ドーム状の壁面を有し、下端が開口した内筒状に
予備形成されている。この予備形成は常温で圧粉
成形したものでもよいが、さらに仮焼結して強度
を高めておけば、加工工程において取扱いが容易
となり望ましい。外筒2は下端に開口端2aが形
成され、前記の予備形成後において内筒1を嵌装
しうるようになつている。外筒2の上壁部にはグ
ローブラグ開口2bおよび燃料噴射弁開口2cが
開口されている。内筒1を外筒2に嵌装したとき
に、内筒1の外筒に断熱部形成部位3としての環
状の空間が形成されるように、内筒1および外筒
2それぞれに段部が形成されている。外筒2の開
口部2aの内縁と、この部分に対応する内筒1の
下半部1aの外縁部位1eとの間の隙間Cには、
第2図に示す如く、断面がくさび状で環状の一部
を切断した結合リング4が圧入される。結合リン
グ4の切断部4aは圧入時の締代のためのもので
ある。また結合リング4は焼結の際に外筒2の焼
結温度においてこの外筒2と一体化される金属、
この場合は鉄またはニツケル系の金属で製作され
る。
前記のように製作した内筒1を外筒2に嵌装す
るに際し、断熱部形成部位3にセラミツクフアイ
バー材5、例えばアルミナシリケートフアイバー
材を適当量充填する。
前記開口部2aと内筒の下半部1aの外縁部位
1eとの隙間に挿入した結合リング4を更に強く
圧入して内筒1と外筒2とを固定する。このとき
外筒2の肩面2dと内筒1の下半部1aの底面1
fとの平行を正確にするためと内筒1の下半部1
aと上半部1bとの相互の接合面1gが左右に喰
い違いのないよう正確に合せる。
上記のように組み立てための(第1図参照)の
内筒1の底面1fを台6上に載せて焼結工程の準
備を終える。
この状態で加熱(約1000℃)して外筒2を焼結
すると、外筒2と結合リング4とは結合して一体
化すると共に、外筒2は収縮して、断熱部形成部
位3以外の、すなわちセラミツクフアイバー材5
のない部位において、外筒2の内側が内筒1の外
側を締め付けて一体化される(第2図参照)。
このとき、内筒1の下半部1aと上半部1bは
特に接合されていなくとも、結合リング4の圧入
により内筒1は外筒2と一体化された状態で、か
つ、内筒1の底面1fが台6上に載置され、外筒
2は自由な状態で焼結されて収縮する。
一方焼結材を焼結するときの収縮現象はその形
状によつて不均等になると共に、強固に固着され
ている部位を中心に収縮する特性を有している。
従つてこの実施例の場合、底面1fを基準に外
筒2が収縮し、内筒1の下半部1aと上半部1b
間の接合面1gもずれることなく、内筒1の底面
1fと外筒2の肩面2dとの平行度はくるいが少
く一定の精度で焼結が完了する。
最後に外筒2および結合リング4の下部の不要
部分2e、4bを除去することにより完成する。
このようにして製作した副室7は第5図に示す
ようにシリンダヘツド8に一体的に嵌装される。
その他9はグロープラグ、10は燃料噴射弁、1
1はシリンダブロツク、12はピストンである。
(試験結果)
次にでき上つた副室(構造体)7の精度を測定
した結果を説明する。(下表参照)
精度は肩面2dを基準として、底面1fの傾き
寸法を平行度S(mm)であらわしてその値が小さ
い程精度が良好であると判断する(3図、第6図
参照)。
本発明の実施例の副室7についての精度は試料
No.1〜15に示し、比較例として第6図に示す構造
の結合リング4を使用しなかつた場合の副室17
についての精度は従来品試料No.1〜8に示す。
(Industrial Application Field) The present invention is used in the technical field of preheating combustion chambers in engines, and mainly relates to the manufacturing technology of pre-chambers. (Prior Art) A pre-chamber structure serving as a preheating chamber for a diesel engine has been well known. In addition, in order to improve the heat resistance of the sub-chamber structure, there is also an idea of molding the sub-chamber with ceramic material. For example, Utsukai Showa 54-
The auxiliary chamber disclosed in Publication No. 77802 is made by integrating an inner cylinder made of ceramic material and surrounding the outer periphery with cast iron. However, it requires casting equipment having the structure of the above-mentioned invention, and there is a problem in workability. (Object of the Invention) Prior to the completion of this invention, the member (inner cylinder) forming the sub-chamber was made of ceramics, a heat insulating material was provided annularly around the outer periphery of this member, and the member (outer cylinder) forming the sub-chamber was provided with a ring shape around the outer periphery of the member. When we prototyped a structure in which a cylinder was covered with a sintered metal material, we found that the sintered metal material contracted unevenly in the axial and diametrical directions, centering on areas where the inner and outer cylinders were in strong contact. , a misalignment occurs between the sintered metal material (outer cylinder) and the sub-chamber member (inner cylinder),
It was found that the dimensional accuracy of the external shape could not be maintained, which was a problem when assembling it into the engine. For example, in FIG. 1 showing the manufacturing process of the present invention, the flatness of the shoulder surface 2d of the sintered metal outer cylinder 2 and the bottom surface of the ceramic inner cylinder 1 is distorted, making it impossible to ensure the accuracy of the combustion chamber during assembly. This causes problems. In this invention, an engine having a structure that has a sufficient heat insulation effect and a member (inner cylinder) that forms the auxiliary chamber and a sintered metal member (outer cylinder) that covers this member are tightly joined without shifting. The purpose of the present invention is to provide a method for manufacturing an antechamber. (Structure of the Invention) The manufacturing method of the present invention is to fit an inner cylinder made of ceramics into an opening of an outer cylinder preformed with a sintered material, and fill the gap between the outer cylinder and the inner cylinder in the opening. In this method, a sub-chamber is manufactured by press-fitting a metal coupling ring with a wedge-shaped cross section to be integrated with the outer cylinder at the sintering temperature of the outer cylinder, fixing the space between the inner and outer cylinders, and then heating and sintering. The effect of this invention is that the inner cylinder and the outer cylinder are heated and sintered while being restrained at the opening of the outer cylinder by the above manufacturing method, so that the outer cylinder is partially uneven due to the characteristics of the sintered material. Even if the constraint part contracts in a fixed state, the dimensional relationship between the inner cylinder and the outer cylinder, for example, the parallelism between the bottom surface of the inner cylinder and the shoulder surface of the outer cylinder, can be maintained with good accuracy. It can be finished with. (Example) Hereinafter, an example of the present invention will be described in detail with reference to the drawings. The inner cylinder 1, which is a component of the subchamber, is made of ceramics (for example, silicon nitride), and is divided into a lower half 1a and an upper half 1b. The lower half portion 1a is formed into a substantially cylindrical shape with a bottom, and the upper half portion 1b is formed into a substantially hemispherical shape. A nozzle 1c is opened at the bottom of the lower half 1a, and a fuel nozzle 1d is opened at the upper half 1b.
is opened. As shown in FIG. 1, the outer cylinder 2, which is a component of the sub-chamber, is pre-formed from iron-based sintered material into an inner cylinder shape with a dome-shaped upper end and an open lower end. This preliminary formation may be performed by powder compaction at room temperature, but it is desirable to further increase the strength by pre-sintering, as this will facilitate handling during the processing process. An open end 2a is formed at the lower end of the outer cylinder 2, and the inner cylinder 1 can be fitted therein after the above-mentioned preliminary formation. A globe lug opening 2b and a fuel injection valve opening 2c are opened in the upper wall portion of the outer cylinder 2. Each of the inner cylinder 1 and the outer cylinder 2 has a stepped portion so that when the inner cylinder 1 is fitted into the outer cylinder 2, an annular space is formed in the outer cylinder of the inner cylinder 1 as a heat insulating part forming part 3. It is formed. In the gap C between the inner edge of the opening 2a of the outer cylinder 2 and the outer edge part 1e of the lower half 1a of the inner cylinder 1 corresponding to this part,
As shown in FIG. 2, a coupling ring 4 having a wedge-shaped cross section and a partially cut annular ring is press-fitted. The cut portion 4a of the coupling ring 4 is for interference during press-fitting. The coupling ring 4 is made of a metal that is integrated with the outer cylinder 2 at the sintering temperature of the outer cylinder 2 during sintering.
In this case, it is made of iron or nickel metal. When the inner cylinder 1 manufactured as described above is fitted into the outer cylinder 2, an appropriate amount of ceramic fiber material 5, such as alumina silicate fiber material, is filled into the heat insulating portion forming region 3. The coupling ring 4 inserted into the gap between the opening 2a and the outer edge portion 1e of the lower half 1a of the inner cylinder is further press-fitted to fix the inner cylinder 1 and the outer cylinder 2. At this time, the shoulder surface 2d of the outer cylinder 2 and the bottom surface 1 of the lower half part 1a of the inner cylinder 1
In order to ensure accurate parallelism with f, the lower half 1 of the inner cylinder 1
A and the upper half part 1b are accurately aligned so that the joint surfaces 1g of the upper half part 1b are not misaligned left and right. The bottom surface 1f of the inner cylinder 1 (see FIG. 1) for assembly as described above is placed on the stand 6 to complete the preparation for the sintering process. When the outer cylinder 2 is heated (approximately 1000°C) to sinter the outer cylinder 2 in this state, the outer cylinder 2 and the coupling ring 4 are combined and integrated, and the outer cylinder 2 is shrunk, except for the area where the heat insulating part 3 is formed. That is, ceramic fiber material 5
The inner side of the outer cylinder 2 tightens the outer side of the inner cylinder 1 and is integrated with the outside of the inner cylinder 1 at a portion where there is no . At this time, even if the lower half 1a and the upper half 1b of the inner cylinder 1 are not particularly joined, the inner cylinder 1 is integrated with the outer cylinder 2 by the press-fitting of the coupling ring 4, and the inner cylinder 1 is integrated with the outer cylinder 2. The bottom surface 1f of is placed on the stand 6, and the outer cylinder 2 is sintered and contracted in a free state. On the other hand, when a sintered material is sintered, the shrinkage phenomenon is uneven depending on its shape, and the material has the characteristic of shrinking mainly in the strongly fixed parts. Therefore, in the case of this embodiment, the outer cylinder 2 contracts with respect to the bottom surface 1f, and the lower half part 1a and the upper half part 1b of the inner cylinder 1
The joint surface 1g between them does not shift, and the parallelism between the bottom surface 1f of the inner cylinder 1 and the shoulder surface 2d of the outer cylinder 2 is slightly distorted, and sintering is completed with a constant accuracy. Finally, the unnecessary parts 2e and 4b of the lower part of the outer cylinder 2 and the coupling ring 4 are removed to complete the assembly. The auxiliary chamber 7 manufactured in this manner is integrally fitted into the cylinder head 8 as shown in FIG.
Others 9 are glow plugs, 10 are fuel injection valves, 1
1 is a cylinder block, and 12 is a piston. (Test Results) Next, the results of measuring the accuracy of the completed auxiliary chamber (structure) 7 will be explained. (See the table below) Accuracy is determined by expressing the inclination dimension of the bottom surface 1f as parallelism S (mm) with the shoulder surface 2d as the reference, and the smaller the value, the better the accuracy is (see Figures 3 and 6). ). The accuracy of the subchamber 7 in the embodiment of the present invention is
Sub-chamber 17 shown in Nos. 1 to 15 and when the coupling ring 4 having the structure shown in FIG. 6 as a comparative example is not used.
The accuracy is shown in conventional product samples No. 1 to 8.
【表】
上記試験結果を対比すれば本発明実施例の副室
7の平行度Sは、0.02〜0.05mm、比較例の副室1
7の平行度Sは、0.07〜0.46mmで本発明の製法に
よるものが格段に良好である。
またこの発明の製法による副室7は内筒1の外
周にセラミツクフアイバー材5を充填したから、
その断熱特性も良好である。
この発明は前記実施例以外に下記の変更も可能
である。
(1) 内筒1と外筒2との相互の回り止めのため、
相互に係合する凹凸を設けてもよい。
(2) 断熱部形成部位3は、内筒1、外筒2共に段
を付して形成したが、これを内筒1の外周面に
環状の凹部を設けるか、または外筒2の内周面
に環状の凹部を設けるかして形成してもよい。
(3) 内筒1のセラミツクス材として窒化珪素を使
用すれば比較的熱衝撃に強い利点があるが、こ
の他、酸化ジルコニウム、炭化硅素などであつ
てもよい。
(発明の効果)
この発明は前記のごとく、焼結材を予備形成し
て製作した外筒にセラミツクス製の内筒を嵌装し
その開口部隙間に断面くさび状の結合リングを圧
入し、内外筒を位置ずれしないように固定してか
ら、加熱焼結して一体化する副室の製造法である
から、副室の平坦面のずれや、傾きが防止され、
エンジンのシリンダヘツドに副室を取り付けたと
きの精度が向上する。[Table] Comparing the above test results, the parallelism S of the subchamber 7 of the example of the present invention is 0.02 to 0.05 mm, and the parallelism S of the subchamber 1 of the comparative example
The parallelism S of No. 7 is 0.07 to 0.46 mm, and the one produced by the manufacturing method of the present invention is much better. Furthermore, since the sub-chamber 7 according to the manufacturing method of the present invention is made by filling the outer periphery of the inner cylinder 1 with ceramic fiber material 5,
Its insulation properties are also good. In addition to the embodiments described above, the present invention can also be modified as described below. (1) To prevent mutual rotation between inner cylinder 1 and outer cylinder 2,
It is also possible to provide recesses and recesses that engage with each other. (2) The heat insulating portion forming part 3 is formed by adding steps to both the inner cylinder 1 and the outer cylinder 2, but this can be done by providing an annular recess on the outer circumferential surface of the inner cylinder 1 or by forming a step on the inner circumference of the outer cylinder 2. It may also be formed by providing an annular recess in the surface. (3) If silicon nitride is used as the ceramic material for the inner cylinder 1, it has the advantage of being relatively resistant to thermal shock, but other materials such as zirconium oxide and silicon carbide may also be used. (Effects of the Invention) As described above, the present invention includes fitting an inner cylinder made of ceramics into an outer cylinder manufactured by preforming sintered material, and press-fitting a coupling ring with a wedge-shaped cross section into the opening gap of the outer cylinder. The sub-chamber is manufactured by fixing the cylinder so that it does not shift and then heating and sintering it to integrate it, which prevents the flat surface of the sub-chamber from shifting or tilting.
Improves accuracy when attaching a pre-chamber to the cylinder head of an engine.
第1図ないし第5図はこの発明の実施例を示
し、第1図ないし第3図はこの実施例の副室の製
造法を工程毎に説明する副室(構造体)の中央縦
断側面図、第4図は結合リングの斜視図、第5図
はこの発明の実施例の製造法によつて製造された
副室の中央縦断側面図、第6図はこの発明の実施
例に対する比較例の副室を示す中央縦断側面図で
ある。
1……内筒、2……外筒、2a……開口部、4
……結合リング、7……副室(構造体)。
Figures 1 to 5 show an embodiment of the present invention, and Figures 1 to 3 are central longitudinal cross-sectional side views of the subchamber (structure) for explaining each step of the manufacturing method of the subchamber of this embodiment. , FIG. 4 is a perspective view of a coupling ring, FIG. 5 is a central longitudinal cross-sectional side view of a subchamber manufactured by the manufacturing method of an embodiment of the present invention, and FIG. 6 is a comparative example of the embodiment of this invention. FIG. 3 is a central vertical sectional side view showing the subchamber. 1... Inner cylinder, 2... Outer cylinder, 2a... Opening, 4
...Coupling ring, 7...Subchamber (structure).
Claims (1)
ら予め成型したセラミツクス製の内筒を嵌装して
前記開口部における外筒と内筒との間に、前記外
筒の焼結温度においてこの外筒と一体化される金
属製の断面くさび状の結合リングを圧入し、前記
内筒と外筒とを位置ずれしないように固定した後
に、加熱焼結することを特徴とするエンジンの副
室の製造法。1. A preformed ceramic inner cylinder is inserted into the opening of an outer cylinder preformed with a sintered material, and the sintering temperature of the outer cylinder is adjusted between the outer cylinder and the inner cylinder at the opening. A metal coupling ring having a wedge-shaped cross section that is integrated with the outer cylinder is press-fitted in the engine, and after the inner cylinder and the outer cylinder are fixed so as not to be displaced, the engine is heated and sintered. Method of manufacturing antechamber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59215395A JPS6196121A (en) | 1984-10-15 | 1984-10-15 | Method of producing auxiliary chamber of engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59215395A JPS6196121A (en) | 1984-10-15 | 1984-10-15 | Method of producing auxiliary chamber of engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6196121A JPS6196121A (en) | 1986-05-14 |
| JPH0578645B2 true JPH0578645B2 (en) | 1993-10-29 |
Family
ID=16671605
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP59215395A Granted JPS6196121A (en) | 1984-10-15 | 1984-10-15 | Method of producing auxiliary chamber of engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6196121A (en) |
-
1984
- 1984-10-15 JP JP59215395A patent/JPS6196121A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6196121A (en) | 1986-05-14 |
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