JPH0139896Y2 - - Google Patents

Info

Publication number
JPH0139896Y2
JPH0139896Y2 JP1984114608U JP11460884U JPH0139896Y2 JP H0139896 Y2 JPH0139896 Y2 JP H0139896Y2 JP 1984114608 U JP1984114608 U JP 1984114608U JP 11460884 U JP11460884 U JP 11460884U JP H0139896 Y2 JPH0139896 Y2 JP H0139896Y2
Authority
JP
Japan
Prior art keywords
intake
air
flow path
cross
curvature
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
Application number
JP1984114608U
Other languages
Japanese (ja)
Other versions
JPS6129056U (en
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 filed Critical
Priority to JP11460884U priority Critical patent/JPS6129056U/en
Publication of JPS6129056U publication Critical patent/JPS6129056U/en
Application granted granted Critical
Publication of JPH0139896Y2 publication Critical patent/JPH0139896Y2/ja
Granted legal-status Critical Current

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  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

【考案の詳細な説明】 A 考案の目的 産業上の利用分野: 自動車用直噴式多気筒デイーゼル機関に主とし
て利用される。
[Detailed description of the invention] A. Purpose of the invention: Industrial application field: Mainly used in direct injection multi-cylinder diesel engines for automobiles.

従来の技術: 直噴式多気筒デイーゼル機関においては、シリ
ンダ間に出力偏差(出力のバラツキ)が生じない
ようにするため、等量の空気が各シリンダに分配
されるようにする配慮が吸気マニホルドの側に払
われると共に、等強度のスワールが各シリンダに
生成されるようにする配慮がシリンダヘツドの側
に払われる。吸気マニホルドに対しての配慮因子
としては空気導入口より吸気ポートに至る距離と
流路の断面積とがあり、シリンダヘツドに対して
の配慮因子としては吸気ポートの形状と姿勢とが
ある。従来の機関は、吸気マニホルドおよびシリ
ンダヘツドが上記配慮の下に設計されているので
あるが、実際的には上記出力偏差が存在する。
Conventional technology: In direct-injection multi-cylinder diesel engines, the intake manifold is designed to ensure that an equal amount of air is distributed to each cylinder in order to prevent output deviation (variations in output) between cylinders. care is taken on the side of the cylinder head to ensure that a swirl of equal intensity is produced in each cylinder. Factors to consider for the intake manifold include the distance from the air inlet to the intake port and the cross-sectional area of the flow path, and factors to consider for the cylinder head include the shape and orientation of the intake port. In conventional engines, the intake manifold and cylinder head are designed with the above consideration in mind, but in reality, the above output deviation exists.

考案が解決しようとする問題点: 上記の出力偏差の発生には吸気マニホルドより
吸気ポートに流入する空気の速度分布が関係する
ため、吸気ポートの入口における空気の速度分布
が第2図に示すものであるとして設計された吸気
ポートは、速度分布が第3図に示すようになつて
いる場合には所期のスワールをシリンダに生成さ
せ難く、それが出力偏差発生の原因となる。第3
図のO−Oは吸気ポートの入口の中心線、Vは吸
気の流速、VnaxはVの最大値、DはVnaxの位置
の片寄り量である。片寄り量Dは吸気マニホルド
における空気の導入口よりの距離が大きい前端お
よび後端のシリンダの吸気ポートに特に顕著であ
る。本案は出力偏差の発生の一つの原因となつて
いる速度分布の片寄り量Dを極力小さくし、それ
により機関の性能を改善することを目的とする。
Problem to be solved by the invention: Since the occurrence of the above output deviation is related to the velocity distribution of the air flowing into the intake port from the intake manifold, the velocity distribution of the air at the entrance of the intake port is as shown in Figure 2. If the velocity distribution is as shown in FIG. 3, it is difficult for an intake port designed to generate the desired swirl in the cylinder, which causes an output deviation. Third
In the figure, O-O is the center line of the inlet of the intake port, V is the flow rate of intake air, V nax is the maximum value of V, and D is the amount of deviation of the position of V nax . The offset amount D is particularly noticeable at the intake ports of the front and rear end cylinders, which are located a large distance from the air inlet in the intake manifold. The purpose of this invention is to minimize the deviation amount D of the speed distribution, which is one of the causes of output deviation, and thereby improve the performance of the engine.

B 考案の構成 問題点を解決するための手段: 本案によるものは、空気導入口よりの距離が大
きい吸気ポートに空気を送り込む矩形状断面形の
流路部分に対し、該部分を流過する気流に旋回を
与える形状の隅角部を設けたことを特徴とする。
B. Means for solving the structural problems of the device: The device according to the present invention has a rectangular cross-sectional flow path section that sends air to the intake port which has a large distance from the air inlet. It is characterized by having a corner portion shaped to give a turning motion to the corner portion.

作 用: さきに“解決しようとする問題点”の欄におい
て第3図に関連して指摘した「片寄り量D」は、
上記の流路部分がそれを流過する気流に与える旋
回により減少させられる。第2図はD=0の理想
状態を示す。流路部分の隅角部の形状は、該部分
の長さを考慮に入れて決定され、以後の修正は出
力偏差の測定結果を検討しつつ行われる。
Effect: The "unbalanced amount D" that was pointed out in relation to Figure 3 in the "Problem to be solved" column is
The above-mentioned flow path section is reduced by the swirl it imparts to the airflow passing through it. FIG. 2 shows an ideal state where D=0. The shape of the corner of the flow path section is determined taking into consideration the length of the section, and subsequent modifications are made while considering the measurement results of the output deviation.

実施例: 第1図は本案による吸気マニホルドの一例を示
す。この図において、1は吸気マニホルドの空気
導入口2よりの距離が大きい吸気ポート、3は吸
気ポート1に空気を送り込む矩形状断面形の流路
部分である。流路部分3の断面形は徐々に変化さ
せられる。流路部分3の隅角部に与えられた大き
い曲率半径はRで示され、小さい曲率半径はrで
示される。の断面において大きな曲率半径Rを
与えられていた隅角部Aは、気流の進行方向にお
いて曲率半径を次第に減少させられての断面に
おいて小さな曲率半径rをもつようになり、の
断面において小さな曲率半径rを与えられていた
隅角部Bは気流の進行方向において曲率半径を次
第に増大させられての断面において大きな曲率
半径Rをもつようになる。また、およびの断
面において小さな曲率半径rを与えられていた隅
角部Cはの断面よりの断面に移行させられる
過程において曲率半径を次第に増大させられて大
きな曲率半径Rをもつようになる。隅角部の曲率
半径を上記の如く変えた流路部分は、流路抵抗が
角度位相を90゜ずつ変えた断面位置において変る
のでそれを流過する気流に対して旋回作用を及ぼ
す。旋回作用は曲率半径の差R−rが大きくなる
につれて大きくなる。
Embodiment: FIG. 1 shows an example of an intake manifold according to the present invention. In this figure, reference numeral 1 indicates an intake port having a large distance from an air introduction port 2 of the intake manifold, and reference numeral 3 indicates a flow path portion with a rectangular cross section that feeds air into the intake port 1. The cross-sectional shape of the channel portion 3 is gradually changed. The large radius of curvature given to the corners of the channel section 3 is designated by R, and the small radius of curvature is designated by r. Corner A, which had been given a large radius of curvature R in the cross section of , gradually decreases its radius of curvature in the direction of air flow, and now has a small radius of curvature r in the cross section of . Corner B, which had been given r, gradually increases its radius of curvature in the traveling direction of the airflow, and now has a large radius of curvature R in its cross section. Also, the corner C, which was given a small radius of curvature r in the cross section of and, gradually increases its radius of curvature and comes to have a large radius of curvature R in the process of being transferred to a cross section from that of. In the flow path portion in which the radius of curvature of the corner portion is changed as described above, the flow path resistance changes at the cross-sectional position where the angular phase is changed by 90 degrees, and therefore exerts a swirling effect on the air flow passing through it. The swirling effect increases as the difference R-r in the radius of curvature increases.

C 考案の効果 本案は、吸気ポートの入口の速度分布の片寄り
のために吸気ポートが所期の強度のスワールを発
生することができずそれがシリンダ間に出力偏差
を生じさせる原因となつていた事情を改善するも
のである。すなわち、本案による吸気マニホルド
は、各シリンダに等量の吸気分配を行うと云う吸
気マニホルド本来の機能のほかに吸気ポートに流
入する吸気の速度分布を改善すると云う機能をも
ち、それによりシリンダ間の出力偏差を減少させ
るものである。
C. Effect of the invention This invention solves the problem that the intake port is unable to generate a swirl of the desired strength due to the unevenness of the velocity distribution at the entrance of the intake port, which causes output deviation between the cylinders. This is to improve the situation. In other words, the intake manifold according to the present invention has the function of improving the velocity distribution of intake air flowing into the intake ports, in addition to its original function of distributing an equal amount of intake air to each cylinder. This reduces output deviation.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本案による吸気マニホルドを示す断面
図、第2図および第3図は吸気ポートの入口にお
ける吸気の流速分布に片寄りがない場合と片寄り
がある場合とを示す図面である。 1……吸気導入口2よりの距離が大きい吸気ポ
ート、3……流路部分。
FIG. 1 is a sectional view showing an intake manifold according to the present invention, and FIGS. 2 and 3 are drawings showing cases where the flow velocity distribution of intake air at the entrance of the intake port is not biased and when it is biased. 1...Intake port having a large distance from the intake inlet 2, 3...Flow path portion.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] シリンダヘツドに設けられた多数の吸気ポート
への空気の導入を断面形が矩形状の吸気流路を経
て行わす形式のものにおいて、空気導入口よりの
距離が大きい吸気ポートに空気を送り込む流路部
分の隅角部に、シリンダ間の出力偏差を減少させ
る旋回を与える断面形状を与えたことを特徴とす
る、直噴式デイーゼル機関の吸気マニホルド。
In a type in which air is introduced into a large number of intake ports provided in the cylinder head through an intake flow path with a rectangular cross section, the flow path that sends air to the intake ports that are located at a greater distance from the air introduction port. An intake manifold for a direct injection diesel engine, characterized in that the corners of the parts have a cross-sectional shape that gives a turning shape that reduces output deviation between cylinders.
JP11460884U 1984-07-27 1984-07-27 Intake manifold of direct injection diesel engine Granted JPS6129056U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11460884U JPS6129056U (en) 1984-07-27 1984-07-27 Intake manifold of direct injection diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11460884U JPS6129056U (en) 1984-07-27 1984-07-27 Intake manifold of direct injection diesel engine

Publications (2)

Publication Number Publication Date
JPS6129056U JPS6129056U (en) 1986-02-21
JPH0139896Y2 true JPH0139896Y2 (en) 1989-11-30

Family

ID=30673620

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11460884U Granted JPS6129056U (en) 1984-07-27 1984-07-27 Intake manifold of direct injection diesel engine

Country Status (1)

Country Link
JP (1) JPS6129056U (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5325719A (en) * 1976-08-24 1978-03-09 Toyota Motor Corp Intake manifold for internal combustion engine

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5890323U (en) * 1981-12-12 1983-06-18 三菱自動車工業株式会社 Engine intake port structure

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5325719A (en) * 1976-08-24 1978-03-09 Toyota Motor Corp Intake manifold for internal combustion engine

Also Published As

Publication number Publication date
JPS6129056U (en) 1986-02-21

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