JPH04121419A - Suction swirl control device of diesel engine - Google Patents

Suction swirl control device of diesel engine

Info

Publication number
JPH04121419A
JPH04121419A JP2239227A JP23922790A JPH04121419A JP H04121419 A JPH04121419 A JP H04121419A JP 2239227 A JP2239227 A JP 2239227A JP 23922790 A JP23922790 A JP 23922790A JP H04121419 A JPH04121419 A JP H04121419A
Authority
JP
Japan
Prior art keywords
air
swirl
intake
speed
suction
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
Application number
JP2239227A
Other languages
Japanese (ja)
Inventor
Nobuji Eguchi
江口 展司
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.)
Hino Motors Ltd
Original Assignee
Hino Motors Ltd
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 Hino Motors Ltd filed Critical Hino Motors Ltd
Priority to JP2239227A priority Critical patent/JPH04121419A/en
Publication of JPH04121419A publication Critical patent/JPH04121419A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition

Landscapes

  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

PURPOSE:To have a proper control through adjustment of the swirl speed over a wide range so that a proper value is obtained relative to the load, by setting the normal swirl speed to some higher level, and jetting pressurized air being directed opposite the flow of suction air into divergent paths of a suction manifold. CONSTITUTION:A suction port P is formed so that it can hold the swirl speed at a high level. In each divergent path 2 of a suction manifold 1 in connection to the suction port P, an air injection nozzle 18 is provided which has an opening in the direction of jetting air 17 opposite the suction flow 10 leading from the suction manifold 1 to suction port P. These air jetting nozzles 18 are connected with a pressurized air tank 20 through an air pipe 19. This air pipe 19 is fitted with a solenoid valve 21 for opening or shutting it, and a control device 25 is provided, which is fed with an engine revolving speed signal 22 and a load signal 23 and which emits a control signal 24 for controlling opening/ shutting operation of this solenoid valve 21.

Description

【発明の詳細な説明】 [産業上の利用分野コ 本発明はディーゼル機関の吸気スワール制御装置に関す
るものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to an intake swirl control device for a diesel engine.

[従来の技術] 近年、ディーゼルエンジンの排ガス対策(N Ox対策
)に対する燃焼改善の1手段であるスワール制御か益々
重要になって来ており、吸気ポートの形状等に種々の工
夫がなされている。
[Prior art] In recent years, swirl control, which is a means of improving combustion for diesel engine exhaust gas countermeasures (NOx countermeasures), has become increasingly important, and various improvements have been made to the shape of the intake port, etc. .

前記吸気ポートとして代表的なものにヘリカル型吸気ポ
ートかあり、これは第3図〜第5図に示されるように、
吸気マニホールドlの分岐流路2に接続される入口部8
からほぼ直線状に延びる入口流路4と、該入口流路4か
ら連続して延び吸気バルブ5のバルブステム6軸線周り
に巻き回し燃焼室7への開口部8へ通じる渦巻状流路9
とから構成されている。Pは吸気ポートを示す。
A typical example of the intake port is a helical intake port, as shown in FIGS. 3 to 5.
Inlet portion 8 connected to branch flow path 2 of intake manifold l
an inlet passage 4 extending substantially linearly from the inlet passage 4; a spiral passage 9 extending continuously from the inlet passage 4 and winding around the axis of the valve stem 6 of the intake valve 5 and leading to an opening 8 into the combustion chamber 7;
It is composed of. P indicates an intake port.

これにより、吸気パルプ5の開動作によって吸気マニホ
ールドlから吸入される吸気流lOは、入口流路4から
渦巻状流路9を通過する間に旋回流となり、開口部8か
ら燃焼室7内に流入し、強いスワール11か形成され、
図示しない噴射ノズルから噴射される燃料と前記吸気流
10との混合が効率良く行われるようになっている。
As a result, the intake flow lO taken in from the intake manifold l by the opening operation of the intake pulp 5 becomes a swirling flow while passing from the inlet flow path 4 through the spiral flow path 9, and flows into the combustion chamber 7 from the opening 8. Inflow, a strong swirl 11 is formed,
The fuel injected from an injection nozzle (not shown) and the intake air flow 10 are mixed efficiently.

尚、第3図〜第5図中、12は排気ポート、13は排気
バルブ、14は排気ポート12に接続された排気マニホ
ールド、15はピストン、16はエアクリーナを表わし
ている。
3 to 5, 12 is an exhaust port, 13 is an exhaust valve, 14 is an exhaust manifold connected to the exhaust port 12, 15 is a piston, and 16 is an air cleaner.

一方、最近、前記吸気ポートPの入口流路4に、吸気流
10の流れ方向に加圧空気を噴射してスワール速度を調
整する技術か提案されている。
On the other hand, recently, a technique has been proposed in which pressurized air is injected into the inlet flow path 4 of the intake port P in the flow direction of the intake air flow 10 to adjust the swirl speed.

通常、負荷(燃料の噴射量)に対してスヮル速度が高す
ぎると燃焼室内の燃料の噴霧が重なってしまう現象(オ
ーバペネトレーション)が生じて燃料か微粒化せず、黒
煙の発生を抑制できなくなる問題を有し、又負荷に対し
てスワール速度か低すぎると、吸気流の乱れのエネルギ
か低下して燃焼改善に支障を来す問題を有するため、前
記スワール速度は負荷に応じた最適値に設定できること
か好ましい。
Normally, if the swell speed is too high relative to the load (fuel injection amount), a phenomenon occurs in which the fuel sprays in the combustion chamber overlap (overpenetration), which prevents the fuel from becoming atomized and prevents the generation of black smoke. In addition, if the swirl speed is too low relative to the load, the energy of turbulence in the intake air flow will decrease, which will hinder combustion improvement. It is preferable that it can be set to

[発明か解決しようとする課題] しかし、前記吸気ポートPの形状によってスワール速度
を制御する方式は、一般に吸気抵抗を与える方式である
ため、ポンピングロス増加により燃費か悪化する問題を
有しており、又スワール速度の制御範囲も狭い問題を有
していた。
[Problem to be solved by the invention] However, since the method of controlling the swirl speed by the shape of the intake port P is generally a method of providing intake resistance, there is a problem that fuel efficiency deteriorates due to an increase in pumping loss. Also, there was a problem that the control range of the swirl speed was narrow.

又、前記吸気ポートPに加圧空気を噴射する方式におい
ては、高負荷時の高回転数のときにスワール速度か最適
になるように設定しておき、低回転数時に加圧空気を噴
射してやってスワール速度の不足分を補ってやることに
より良好なスワール速度を保持させるようにした方式で
あるため、部分負荷時の燃料噴霧速度か弱まったときに
エンジン回転数によって高く保持されているスワール速
度を低下させる手段かなく、よって燃料の噴霧の重なり
か生じて黒煙の発生を抑制できなくなり、やはりこの場
合もスワール速度の制御範囲か狭くなる問題を有してい
た。
In addition, in the method of injecting pressurized air into the intake port P, the swirl speed is set to be optimal at high rotation speeds under high load, and pressurized air is injected at low rotation speeds. This method maintains a good swirl speed by compensating for the lack of swirl speed, so when the fuel spray speed at partial load is weakened, the swirl speed is maintained high by the engine speed. Since there is no means to reduce the swirl speed, the fuel spray only overlaps, making it impossible to suppress the generation of black smoke, and this case also has the problem of narrowing the control range of the swirl speed.

上記従来方式におけるスワール速度の制御範囲は、スワ
ールレシオ(ピストンの中に備えられた羽根車の回転数
をエンジン回転数で割った無次元値)でせいぜい6〜1
.4程度であった。
The control range of the swirl speed in the above conventional method is at most 6 to 1 based on the swirl ratio (a dimensionless value obtained by dividing the rotation speed of the impeller installed in the piston by the engine rotation speed).
.. It was about 4.

本発明は、上記従来の問題点に着目してなしたもので、
吸気流量を低減させることなく、高負荷時及び部分負荷
時の燃料に応じた最適なスワール速度を広範囲に選定し
得るディーゼル機関の吸気スワール制御装置を提供する
ことを目的とする。
The present invention was made by focusing on the above-mentioned conventional problems.
It is an object of the present invention to provide an intake swirl control device for a diesel engine that can select an optimal swirl speed according to fuel at high load and partial load over a wide range without reducing the intake flow rate.

[課題を解決するための手段] 本発明は各燃焼室に吸気する吸気ポートを高いスワール
速度を保持する形状とし、該吸気ポートに接続される吸
気マニホールドの各分岐流路内に、前記吸気マニホール
ドから前記吸気ポートに向かう吸気流に対して逆方向に
空気を噴射するための空気噴射ノズルを配設し、且っ該
各空気噴射ノズルを空気管を介して加圧空気タンクに接
続し、前記空気管に該空気管の開閉を行う電磁弁を設け
ると共に、エンジンの回転数信号及び負荷信号を入力し
て前記電磁弁の開閉を制御する制御装置を設けたことを
特徴とするディーゼル機関の吸気スワール制御装置にか
かるものである。
[Means for Solving the Problems] The present invention has an intake port that takes air into each combustion chamber into a shape that maintains a high swirl velocity, and in each branch flow path of the intake manifold connected to the intake port, the intake manifold is connected to the intake manifold. air injection nozzles are disposed for injecting air in a direction opposite to the intake air flow toward the intake port, and each air injection nozzle is connected to a pressurized air tank via an air pipe; An air intake for a diesel engine, characterized in that an air pipe is provided with a solenoid valve that opens and closes the air pipe, and a control device that inputs an engine rotation speed signal and a load signal to control the opening and closing of the solenoid valve. This is related to the swirl control device.

[作   用] スワール速度を高目に設定しておくと、高負荷時におけ
るエンジン低回転数のときに、スワール速度を向上させ
て燃料との混合を良好にすることができる。更にエンジ
ン高回転数のときには、回転数信号と負荷信号を入力し
ている制御装置により電磁弁を開き、加圧空気タンクの
加圧空気を空気噴射ノズルから吸気の方向を逆方向に噴
射させる。すると、スワール速度か低減され、よってス
ワール速度か過剰に高くなって燃料の噴霧の重なりか生
じることか防止される。
[Function] By setting the swirl speed to a high value, it is possible to improve the swirl speed and improve the mixing with the fuel when the engine speed is low under high load. Furthermore, when the engine speed is high, a control device inputting a speed signal and a load signal opens a solenoid valve, and pressurized air from a pressurized air tank is injected from an air injection nozzle in a direction opposite to the direction of intake air. The swirl rate is then reduced, thereby preventing the swirl rate from becoming too high, resulting in overlapping fuel sprays.

又、部分負荷時には燃料の噴射速度が低減されるので、
このときも、回転数信号と負荷信号か人力されている制
御装置によって前記電磁弁を開き、空気噴射ノズルから
吸気の方向と逆方向に空気を噴射してスワール速度を低
下させることにより、燃料の噴霧の重なりを防止する。
Also, since the fuel injection speed is reduced during partial load,
At this time as well, the solenoid valve is opened by a control device manually controlled by the rotation speed signal and the load signal, and air is injected from the air injection nozzle in the opposite direction to the intake direction to reduce the swirl speed of the fuel. Prevent overlapping sprays.

[実 施 例コ 以下、本発明の実施例を図面を参照しつつ説明する。[Implementation example] Embodiments of the present invention will be described below with reference to the drawings.

第1図は本発明の一実施例であり、図中第3図と同一の
符号を付した部分は同一物を表わしている。
FIG. 1 shows one embodiment of the present invention, and the parts in the figure with the same reference numerals as in FIG. 3 represent the same parts.

第1図に示す吸気ポートPの形状を高いスワル速度を保
持し得るように形成し、又前記吸気ポートPに接続され
る吸気マニホールド1の各分岐流路2内に、吸気マニホ
ールド1から吸気ポートPに向かう吸気流lOに対して
逆方向に空気17を噴射する方向に開口した空気噴射ノ
ズル18を夫々配設する。
The shape of the intake port P shown in FIG. 1 is formed so as to maintain a high swirl speed, and the intake port Air injection nozzles 18 are respectively provided which are opened in a direction to inject air 17 in a direction opposite to the intake air flow lO directed toward P.

又、上記各空気噴射ノズル18を、空気管19を介して
加圧空気タンク20に接続する。
Further, each of the air injection nozzles 18 is connected to a pressurized air tank 20 via an air pipe 19.

又、前記空気管19に該空気管19を流れる空気の開閉
を行う電磁弁21を設け、更にエンジンの回転数信号2
2と負荷信号23を入力して、前記電磁弁21の開閉作
動を制御する制御信号24を出力する制御装置25を設
ける。
Further, the air pipe 19 is provided with a solenoid valve 21 for opening and closing the air flowing through the air pipe 19, and further includes an engine rotation speed signal 2.
2 and a load signal 23, and outputs a control signal 24 for controlling the opening/closing operation of the electromagnetic valve 21.

上記実施例において、第2図に示す如く、本発明による
スワール速度か従来のスワール速度より全体に高目にな
るように吸気ポートPの形状等を選定していることによ
り、吸気ポートPによる吸気のポンピングロスか低減さ
れる。
In the above embodiment, as shown in FIG. 2, the shape of the intake port P is selected so that the swirl speed according to the present invention is higher overall than the conventional swirl speed. pumping losses are reduced.

く高負荷時〉 上記したように、通常のスワール速度を高目に設定して
おくことにより、エンジン回転数か低速時のスワール速
度か上昇し、燃料に対する空気の混合か良好となって燃
焼性が向上される。
At high loads> As mentioned above, by setting the normal swirl speed to a high value, the engine speed and the swirl speed at low speeds will increase, improving the mixing of air with fuel and improving combustibility. is improved.

又、エンジン回転数か中速乃至高速時は、前記エンジン
の回転数信号22及び負荷信号23か人力されている制
御装置25からの制御信号24により電磁弁21か開作
動される。
When the engine speed is medium to high, the solenoid valve 21 is opened by a control signal 24 from a control device 25 which is manually operated by the engine speed signal 22 and load signal 23.

これにより、加圧空気タンク20の加圧された空気17
か空気管19を介して空気噴射ノスル18から、吸気マ
ニホールド1の分岐流路2内を流れる吸気流lOに対し
て逆方向に噴射される。
As a result, the pressurized air 17 in the pressurized air tank 20
The air is injected from the air injection nostle 18 through the air pipe 19 in a direction opposite to the intake air flow lO flowing in the branch flow path 2 of the intake manifold 1.

従って、第2図に示すように高速側のスワール速度が押
えられ、よって燃料の噴霧の重なりが防止される。
Therefore, as shown in FIG. 2, the swirl speed on the high-speed side is suppressed, thereby preventing fuel sprays from overlapping.

く部分負荷時〉 下り坂走行時などのような部分負荷時には燃料の噴射速
度が弱まるため、このときにエンジン回転隊によってス
ワール速度か高くなると、燃料の噴霧の重なりが生じる
At partial load> At partial load, such as when driving downhill, the fuel injection speed is weakened, so if the swirl speed increases due to the engine rotation at this time, fuel sprays overlap.

従って、この場合も、回転数信号22及び負荷信号23
か入力されている制御装置25によって電磁弁21を開
けることにより空気噴射ノズル18から加圧空気を噴射
してスワール速度を低下させ、燃料の噴霧の重なりを防
止する。
Therefore, also in this case, the rotation speed signal 22 and the load signal 23
By opening the electromagnetic valve 21 by the control device 25 to which the control device 25 is input, pressurized air is injected from the air injection nozzle 18 to reduce the swirl speed and prevent fuel sprays from overlapping.

上記本発明の吸気スワール制御装置によれば、従来6〜
1.4程度であったスワールレシオを、6〜0まで広げ
ることができ、よって今後の燃料の高圧噴射(ノズル圧
〜3000kg/cj)に対しても制御可能となる。
According to the above-mentioned intake swirl control device of the present invention, conventional six to
The swirl ratio, which was about 1.4, can be increased to 6 to 0, making it possible to control future high-pressure fuel injection (nozzle pressure ~3000 kg/cj).

尚、本発明のディーゼル機関の吸気スワール制御装置は
、上述の実施例にのみ限定されるものではなく、空気噴
射ノズルを吸気ポート内に設けるようにすることもでき
ること、加圧空気の噴射時期、噴射量は任意に選定し得
ること、その他、本発明の要旨を逸脱しない範囲内にお
いて種々変更を加え得ることは勿論である。
It should be noted that the intake swirl control device for a diesel engine according to the present invention is not limited to the above-described embodiments, but may also include an air injection nozzle provided in the intake port, injection timing of pressurized air, It goes without saying that the injection amount can be arbitrarily selected and that various other changes can be made without departing from the gist of the present invention.

[発明の効果] 以上説明したように本発明のディーゼル機関の吸気スワ
ール制御装置によれは、通常のスワール速度が高目に設
定されており、且つ吸気マニホールドの分岐流路内に、
吸気流の流れと逆方向に加圧空気を噴射してスワール速
度を調整できるようにしているので、高負荷時と部分負
荷時において負荷に対して適正な値となるようにスワー
ル速度を広範囲に調節して適正に制御することができ、
更に吸気ポートのポンピングロスも低減できる等の優れ
た効果を奏し得る。
[Effects of the Invention] As explained above, the intake swirl control device for a diesel engine of the present invention has a normal swirl speed set to a high value, and a branch flow path of the intake manifold.
Since the swirl speed can be adjusted by injecting pressurized air in the opposite direction to the intake flow, the swirl speed can be adjusted over a wide range to maintain an appropriate value for the load at high loads and partial loads. can be adjusted and controlled properly,
Furthermore, excellent effects such as reducing pumping loss at the intake port can be achieved.

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

第1図は本発明の一実施例の平面図、第2図は本発明の
一実施例と従来方式の場合のエンジン回転数とスワール
速度との関係を比較して示した線図、第3図は従来装置
の一例を示す平面図、第4図は従来の吸気ポートの一例
を示す斜視図、第5図は第4図の切断側面図である。 Pは吸気ポート、■は吸気マニホールド、2は分岐流路
、7は燃焼室、10は吸気流、17は空気、18は空気
噴射ノズル、19は空気管、20は加圧空気タンク、2
1は電磁弁、22は回転数信号、23は負荷信号、25
は制御装置を示す。 特 許出願人 日野自動車工業株式会社
Fig. 1 is a plan view of an embodiment of the present invention, Fig. 2 is a diagram comparing the relationship between engine rotation speed and swirl speed in the case of an embodiment of the present invention and a conventional method; FIG. 4 is a plan view showing an example of a conventional device, FIG. 4 is a perspective view showing an example of a conventional intake port, and FIG. 5 is a cutaway side view of FIG. 4. P is an intake port, ■ is an intake manifold, 2 is a branch flow path, 7 is a combustion chamber, 10 is an intake flow, 17 is air, 18 is an air injection nozzle, 19 is an air pipe, 20 is a pressurized air tank, 2
1 is a solenoid valve, 22 is a rotation speed signal, 23 is a load signal, 25
indicates a control device. Patent applicant Hino Motors Co., Ltd.

Claims (1)

【特許請求の範囲】[Claims] 1)各燃焼室に吸気する吸気ポートを高いスワール速度
を保持する形状とし、該吸気ポートに接続される吸気マ
ニホールドの各分岐流路内に、前記吸気マニホールドか
ら前記吸気ポートに向かう吸気流に対して逆方向に空気
を噴射するための空気噴射ノズルを配設し、且つ該各空
気噴射ノズルを空気管を介して加圧空気タンクに接続し
、前記空気管に該空気管の開閉を行う電磁弁を設けると
共に、エンジンの回転数信号及び負荷信号を入力して前
記電磁弁の開閉を制御する制御装置を設けたことを特徴
とするディーゼル機関の吸気スワール制御装置。
1) The intake port that takes air into each combustion chamber is shaped to maintain a high swirl velocity, and in each branch flow path of the intake manifold connected to the intake port, there is a air injection nozzles for injecting air in opposite directions, each air injection nozzle is connected to a pressurized air tank via an air pipe, and an electromagnetic device is connected to the air pipe for opening and closing the air pipe. An intake swirl control device for a diesel engine, comprising a valve and a control device that inputs an engine rotation speed signal and a load signal to control opening and closing of the electromagnetic valve.
JP2239227A 1990-09-10 1990-09-10 Suction swirl control device of diesel engine Pending JPH04121419A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2239227A JPH04121419A (en) 1990-09-10 1990-09-10 Suction swirl control device of diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2239227A JPH04121419A (en) 1990-09-10 1990-09-10 Suction swirl control device of diesel engine

Publications (1)

Publication Number Publication Date
JPH04121419A true JPH04121419A (en) 1992-04-22

Family

ID=17041641

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2239227A Pending JPH04121419A (en) 1990-09-10 1990-09-10 Suction swirl control device of diesel engine

Country Status (1)

Country Link
JP (1) JPH04121419A (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5921030B2 (en) * 1976-02-13 1984-05-17 キヤノン株式会社 Sheet front/back conversion conveyance device
JPS59158324A (en) * 1983-02-28 1984-09-07 Hino Motors Ltd Intake auxiliary device for engine provided with turbocharger

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5921030B2 (en) * 1976-02-13 1984-05-17 キヤノン株式会社 Sheet front/back conversion conveyance device
JPS59158324A (en) * 1983-02-28 1984-09-07 Hino Motors Ltd Intake auxiliary device for engine provided with turbocharger

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