JPH068273Y2 - Secondary combustion chamber of internal combustion engine - Google Patents
Secondary combustion chamber of internal combustion engineInfo
- Publication number
- JPH068273Y2 JPH068273Y2 JP9151987U JP9151987U JPH068273Y2 JP H068273 Y2 JPH068273 Y2 JP H068273Y2 JP 9151987 U JP9151987 U JP 9151987U JP 9151987 U JP9151987 U JP 9151987U JP H068273 Y2 JPH068273 Y2 JP H068273Y2
- Authority
- JP
- Japan
- Prior art keywords
- combustion chamber
- hole
- chamber
- glow
- central axis
- 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
Landscapes
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
【考案の詳細な説明】 「産業上の利用分野」 本考案は、セラミック製の副燃焼室に好適に利用され
る。DETAILED DESCRIPTION OF THE INVENTION "Industrial field of application" The present invention is preferably used for a secondary combustion chamber made of ceramics.
「従来の技術」 近年、熱効率の向上、耐熱性向上、パティキュレート対
策等の目的でディーゼルエンジンの副燃焼室をセラミッ
クで形成することが実用化されている。この場合、第2
図に示すように副燃焼室下部(口金部)22は噴口23
を有し、熱負荷が大きいため、Si3N4等の耐熱性セラミ
ックを用い、上部(チャンバ部)24はZrO2、Al2TiO5
等の断熱性セラミックを用いるのが望ましい。“Prior Art” In recent years, it has been put into practical use to form a secondary combustion chamber of a diesel engine with ceramics for the purpose of improving thermal efficiency, heat resistance, and measures against particulates. In this case, the second
As shown in the figure, the lower part of the sub-combustion chamber (base part) 22 is a nozzle 23
Since it has a large heat load, a heat-resistant ceramic such as Si 3 N 4 is used, and the upper part (chamber part) 24 is ZrO 2 , Al 2 TiO 5
It is desirable to use a heat insulating ceramic such as.
「考案が解決しようとする問題点」 しかし、チャンバ部24にはフロー孔25及び燃料噴射
ノズル孔(以下「ノズル孔」という)26が近設されて
おり、しかもグロー孔25はグロー孔25とノズル孔2
6との間の内壁面に対して鋭角αに切り立っているた
め、ZrO2やAl2TiO5では加工時のカケや熱負荷、ホット
スポットに基づく溶損を生じるおそれがあった。また、
一般的に断熱性セラミックは熱伝導率が低いから、熱応
力の発生を抑えるため鋳ぐるみ等の圧縮場で用いられる
ことが多いが、その圧縮応力が上記鋭角部に集中するこ
とによってもカケが生じうる。[Problems to be Solved by the Invention] However, a flow hole 25 and a fuel injection nozzle hole (hereinafter referred to as “nozzle hole”) 26 are provided in the chamber portion 24 in the vicinity thereof, and the glow hole 25 is different from the glow hole 25. Nozzle hole 2
Since the inner wall surface between 6 and 6 is steep at an acute angle α, ZrO 2 and Al 2 TiO 5 may cause chipping during processing, heat load, and melting loss due to hot spots. Also,
In general, adiabatic ceramics have low thermal conductivity, so they are often used in compression fields such as castings to suppress the generation of thermal stress, but chipping also occurs when the compressive stress concentrates on the sharp corners. It can happen.
本考案はかかる問題点を解決することを目的とする。The present invention aims to solve such problems.
「問題点を解決するための手段」 その手段は、第1図(A)及び第1図(B)に示すようにチャ
ンバ部内壁のうちグロー孔15の開口端縁15aとノズ
ル孔16の開口端縁16aとによって挾まれる面を副燃
焼室の中心軸に対して垂直な平面17とするところにあ
る。並面17の形状は、中心軸と開口端縁15aとの最
短距離をp、中心軸と開口端縁16aとの最長距離をq
とするとき、中心軸と同心であって半径rがp≦r≦q
の範囲にある円周17aと開口端縁15aと開口端縁1
6aとによって囲まれる三ケ月形とするのが望ましい。"Means for Solving Problems" The means is, as shown in FIGS. 1 (A) and 1 (B), the opening end edge 15a of the glow hole 15 and the opening of the nozzle hole 16 in the inner wall of the chamber portion. The plane sandwiched by the edge 16a is a plane 17 perpendicular to the central axis of the auxiliary combustion chamber. As for the shape of the parallel surface 17, the shortest distance between the central axis and the opening edge 15a is p, and the longest distance between the central axis and the opening edge 16a is q.
Where r is concentric with the central axis and the radius r is p ≦ r ≦ q
17a, opening edge 15a and opening edge 1 in the range of
It is desirable to have a crescent shape surrounded by 6a.
「作用」 平面17とグロー孔15とのなす角βは従来の角αより
広いため、応力集中や溶損が避けられるうえ、肉厚も厚
くなるので強度的に有利になる。"Action" Since the angle β formed by the flat surface 17 and the glow hole 15 is wider than the conventional angle α, stress concentration and melting loss can be avoided, and the wall thickness becomes thicker, which is advantageous in strength.
なお、上記手段により燃焼室の容積が減少するが、実際
にはノズル孔が大きな面積を占めているので平面17は
わずかな面積にすぎず、容積変化は無視できる程度であ
る。Although the volume of the combustion chamber is reduced by the above means, since the nozzle hole occupies a large area in practice, the plane 17 is only a small area and the volume change is negligible.
また、中心軸に対して平面17が垂直であるから、刃先
をフラットにしたボールエンドミルを用いれば内壁の加
工は容易である。Further, since the plane 17 is perpendicular to the central axis, the inner wall can be easily processed by using a ball end mill with a flat blade edge.
「実施例」 チタン酸アルミニウム焼結体よりなり、外径30mm、肉
厚5mmのドームの外周をAC−4Bで鋳ぐるみ、T−6
処理後、機械加工によりドーム底に平面17を形成し、
平面17の部分以外の肉厚を3mmとし、グロー孔15及
びノズル孔16を穿設した。この際、平面17はグロー
孔15及びノズル孔16は穿設されていなければ円形を
なすもので、グロー孔15の開口端縁15aを1mmかぶ
るように形成した。次いでSUH−3製の口金12を圧
入して第1図に示す4気筒2000ccのディーゼルエンジン
の副燃焼室11を製造した。製造個数は各気筒10個と
した。[Example] A dome made of an aluminum titanate sintered body and having an outer diameter of 30 mm and a wall thickness of 5 mm was cast with AC-4B, and T-6 was used.
After the treatment, a flat surface 17 is formed on the dome bottom by machining,
The wall thickness other than the flat surface 17 was set to 3 mm, and the glow hole 15 and the nozzle hole 16 were formed. At this time, the flat surface 17 has a circular shape if the glow hole 15 and the nozzle hole 16 are not formed, and is formed so as to cover the opening edge 15a of the glow hole 15 by 1 mm. Then, a SUH-3 base 12 was press-fitted to manufacture the auxiliary combustion chamber 11 of the 4-cylinder 2000cc diesel engine shown in FIG. The number of manufactured cylinders was 10 for each cylinder.
上記エンジンを用いて4500rpm全負荷、500時間の耐
久テストを行った(n=10)ところ異常はなかった。Using the above engine, a durability test was carried out at a full load of 4500 rpm for 500 hours (n = 10), but no abnormality was found.
比較のためにドームの内壁全体が球面状であることを除
くほか上記副燃焼室11と同一条件で第2図の副燃焼室
21を製造したところ、40個のうちグロー孔25穿設
時に3個においてカケが生じていた。また、カケの生じ
ていないものについて上記耐久テストを行ったところ4
気筒のうち2気筒においてe点でカケ、他2気筒におい
てe点で溶損がみられた。For the purpose of comparison, except that the entire inner wall of the dome is spherical, the auxiliary combustion chamber 21 of FIG. 2 was manufactured under the same conditions as the auxiliary combustion chamber 11. There was chipping in the individual. In addition, when the above durability test was conducted on the ones without chipping, 4
Two of the cylinders suffered chipping at point e, and the other two cylinders had melting damage at point e.
「考案の効果」 信頼性、生産性に優れたセラミック製副燃焼室となる。"Effect of the idea" It becomes a ceramic auxiliary combustion chamber with excellent reliability and productivity.
第1図(A)は本考案の一実施例に係る副燃焼室の軸方向
断面図、第1図(B)は第1図(A)のA−A′線断面を下か
ら眺めた図、第2図(A)は従来の副燃焼室の軸方向断面
図、第2図(B)は第2図(A)のA−A′線断面を下から眺
めた図である。 14,24……チャンバ部、15,25……グロー孔、
16,26……燃料噴射ノズル孔、17……平面FIG. 1 (A) is an axial sectional view of a sub-combustion chamber according to an embodiment of the present invention, and FIG. 1 (B) is a sectional view taken along the line AA 'of FIG. 1 (A) as seen from below. FIG. 2 (A) is an axial sectional view of a conventional auxiliary combustion chamber, and FIG. 2 (B) is a view of a section taken along the line AA ′ of FIG. 14, 24 ... Chamber part, 15, 25 ... Glow hole,
16, 26 ... Fuel injection nozzle hole, 17 ... Plane
Claims (1)
ャンバ部がセラミックで形成され、グロー孔が中心軸側
に傾斜している副燃焼室において、チャンバ部内壁のう
ちグロー孔の開口端縁と燃料噴射ノズル孔の開口端縁と
によって挾まれる面を副燃焼室の中心軸に対して垂直な
平面としたことを特徴とする内燃機関の副燃焼室。1. In a sub-combustion chamber in which a chamber portion having a glow hole and a fuel injection nozzle hole is formed of ceramic, and the glow hole is inclined toward the central axis side, an inner edge of the chamber portion and an opening edge of the glow hole are formed. An auxiliary combustion chamber for an internal combustion engine, wherein a surface sandwiched by the opening edge of the fuel injection nozzle hole is a plane perpendicular to the central axis of the auxiliary combustion chamber.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9151987U JPH068273Y2 (en) | 1987-06-15 | 1987-06-15 | Secondary combustion chamber of internal combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9151987U JPH068273Y2 (en) | 1987-06-15 | 1987-06-15 | Secondary combustion chamber of internal combustion engine |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS63200626U JPS63200626U (en) | 1988-12-23 |
JPH068273Y2 true JPH068273Y2 (en) | 1994-03-02 |
Family
ID=30952378
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP9151987U Expired - Lifetime JPH068273Y2 (en) | 1987-06-15 | 1987-06-15 | Secondary combustion chamber of internal combustion engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH068273Y2 (en) |
-
1987
- 1987-06-15 JP JP9151987U patent/JPH068273Y2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JPS63200626U (en) | 1988-12-23 |
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