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JPS595765B2 - Secondary air supply device for exhaust turbocharged engine - Google Patents
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JPS595765B2 - Secondary air supply device for exhaust turbocharged engine - Google Patents

Secondary air supply device for exhaust turbocharged engine

Info

Publication number
JPS595765B2
JPS595765B2 JP16236578A JP16236578A JPS595765B2 JP S595765 B2 JPS595765 B2 JP S595765B2 JP 16236578 A JP16236578 A JP 16236578A JP 16236578 A JP16236578 A JP 16236578A JP S595765 B2 JPS595765 B2 JP S595765B2
Authority
JP
Japan
Prior art keywords
exhaust
engine
secondary air
passage
exhaust gas
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
JP16236578A
Other languages
Japanese (ja)
Other versions
JPS5591717A (en
Inventor
「あきら」 高松
紀男 森本
安貞 正本
弘志 宗時
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.)
Daihatsu Motor Co Ltd
Original Assignee
Daihatsu Motor Co 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 Daihatsu Motor Co Ltd filed Critical Daihatsu Motor Co Ltd
Priority to JP16236578A priority Critical patent/JPS595765B2/en
Publication of JPS5591717A publication Critical patent/JPS5591717A/en
Publication of JPS595765B2 publication Critical patent/JPS595765B2/en
Expired legal-status Critical Current

Links

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  • Supercharger (AREA)
  • Exhaust Gas After Treatment (AREA)

Description

【発明の詳細な説明】 本発明は、排気ガスタービンで駆動される過給機、つま
り排気ターボ過給機を備えたエンジンにおいて、その排
気系に、HC7CO等の未燃成分を浄化する目的で2次
空気を供給するための装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention aims to purify unburned components such as HC7CO in the exhaust system of an engine equipped with a supercharger driven by an exhaust gas turbine, that is, an exhaust turbo supercharger. The present invention relates to a device for supplying secondary air.

一般にエンジンの排気系に2次空気を供給する手段とし
ては、排気系における排気ガスの脈動を利用して2次空
気を自然吸入させるものと、排気系にエアポンプにて2
次空気を圧力供給するものとがあるが、排気ターボ過給
式エンジンにおいては、排気系での排気脈動は排気系に
設けた排気タービンによって低減されるから、排気脈動
によっては十分な量の2次空気を供給できず、2次空気
はエアポンプで圧力供給するようにしなければならず、
エアポンプの駆動分だけエンジン出力が低下すると共に
燃費が悪ろくなるのである。
Generally speaking, there are two ways to supply secondary air to the engine exhaust system: one is to use the pulsation of exhaust gas in the exhaust system to naturally suck in the secondary air, and the other is to use an air pump in the exhaust system to supply secondary air.
However, in exhaust turbocharged engines, the exhaust pulsation in the exhaust system is reduced by the exhaust turbine installed in the exhaust system, so depending on the exhaust pulsation, a sufficient amount of Secondary air cannot be supplied, and secondary air must be supplied under pressure using an air pump.
Engine output decreases by the amount of air pump drive, and fuel efficiency worsens.

また、排気系の途中にベンチュリー、管オリフィス又は
管ノズル等の絞り部を設は流れ罠よって圧力が低くなる
部位を形成して2次空気を吸引することも考えられるが
、エンジンの排気ガス量はエンジンの負荷に応じて大き
く変化するため、前記絞り部の口径を高負荷域の排気ガ
ス量に合せて設定すれば、低負荷域において所定の量の
2次空気が確保できず、絞り部の口径を低負荷域の排気
ガス量に合せて設定すれば、高負荷域において排気ガス
の流れ抵抗が著しく増大し、エンジンからの排気ガス圧
力が高くなって出力ダウンになるばかりか、排気タービ
ンの効率が低下することになる。
It is also conceivable to install a constriction part such as a venturi, pipe orifice, or pipe nozzle in the middle of the exhaust system to create a flow trap where the pressure is low and to suck in secondary air, but the amount of exhaust gas from the engine changes greatly depending on the engine load, so if the aperture of the throttle part is set to match the amount of exhaust gas in the high load range, the specified amount of secondary air cannot be secured in the low load range, and the throttle part If the diameter of the engine is set to match the amount of exhaust gas in the low load range, the flow resistance of the exhaust gas will increase significantly in the high load range, which will not only increase the exhaust gas pressure from the engine and reduce the output, but also reduce the exhaust gas turbine output. efficiency will decrease.

本発明は、エンジンから排気タービンに至る排気通路中
に、2次空気を吸引するための絞り部と、エンジンの負
荷に連動する調節弁とを並列状に設け、低負荷域では主
として絞り部を流れる排気ガスによって所定の量の2次
空気を吸引せしめ、高負荷域では排気ガスの一部を絞り
部を迂回させることにより所定の2次空気量を確保した
状態の下で排気ガスの流れ抵抗の低減を図ったものであ
る。
The present invention provides a throttle section for sucking secondary air and a control valve that is linked to the engine load in parallel in the exhaust passage leading from the engine to the exhaust turbine. A predetermined amount of secondary air is sucked in by the flowing exhaust gas, and in high load ranges, part of the exhaust gas is bypassed through the throttle section to ensure a predetermined amount of secondary air, and the flow resistance of the exhaust gas is reduced. The aim is to reduce the

次に本発明の一例を図面について説明するに、図におい
て1は吸気マニホールド2及び排気マニホールド3を有
するエンジン、3は排気タービン5とブロワ−圧縮機6
とを直結した排気ターボ過給機、7は排気ガスを大気に
放出するマフラー又は触媒コンバータを各々示し、前記
吸気マニホールド2にはエンジン1における各気筒ごと
に燃料噴射装置8を備えている。
Next, an example of the present invention will be explained with reference to the drawings, in which 1 is an engine having an intake manifold 2 and an exhaust manifold 3, 3 is an exhaust turbine 5 and a blower-compressor 6.
7 indicates a muffler or a catalytic converter for discharging exhaust gas into the atmosphere, and the intake manifold 2 is provided with a fuel injection device 8 for each cylinder in the engine 1.

また、吸気マニホールド2における集合部9には、エン
ジン1への空気量を増減するためのスロットル弁10を
備え(この場合、他の実施例にあっては燃料噴射装置に
代えて集合部又はプロワ−圧縮機の吸入側に気化器を設
けても良い)、且つ集合部は過給通路11を介して前記
ブロワ−圧縮機6の吐出側に接続され、プロワ−圧縮機
6の吸入側はエアフローメータ14付き空気吸入通路1
2を介してエアクリーナ13に接続されている。
Further, the collecting part 9 of the intake manifold 2 is provided with a throttle valve 10 for increasing or decreasing the amount of air to the engine 1 (in this case, in other embodiments, a collecting part or a processor is installed instead of the fuel injection device). - A vaporizer may be provided on the suction side of the compressor), and the collecting section is connected to the discharge side of the blower-compressor 6 via the supercharging passage 11, and the suction side of the blower-compressor 6 is connected to the air flow. Air intake passage 1 with meter 14
It is connected to the air cleaner 13 via 2.

また、排気タービン5の排気側は排気管15を介してマ
フラー7に、排気タービン5の入口側は排気通路16を
介して排気マニホールド3に各々接続されている。
Further, the exhaust side of the exhaust turbine 5 is connected to the muffler 7 via an exhaust pipe 15, and the inlet side of the exhaust turbine 5 is connected to the exhaust manifold 3 via an exhaust passage 16.

そして、前記排気通路16の途中(好ましくは排気ター
ビン5の入口側に近い所)にハ管ノズル17を設け、該
管ノズル17の下流側で且つこれに近接した位置にはポ
ート18を設け、このポート18に先端が大気吸入用フ
ィルター19又は前記エアクリーナ13に接続された逆
止弁21付き2次空気供給通路20を接続する一方、排
気通路16には前記管ノズル17に対するバイパス通路
22を設け、該バイパス通路22中に前記スロットル弁
10と連動しこれと略同様に開閉する調節弁23を設け
て成るものである。
A pipe nozzle 17 is provided in the middle of the exhaust passage 16 (preferably near the inlet side of the exhaust turbine 5), and a port 18 is provided at a position downstream of and close to the pipe nozzle 17, This port 18 is connected to a secondary air supply passage 20 with a check valve 21 whose tip is connected to an air suction filter 19 or the air cleaner 13, while a bypass passage 22 for the pipe nozzle 17 is provided in the exhaust passage 16. A control valve 23 is provided in the bypass passage 22, and is interlocked with the throttle valve 10 and opens and closes in substantially the same manner as the throttle valve 10.

この場合、管ノズル17に代えて管オリフィスを用いて
も良く、管ノズル17に代えてベチュリーを用いそのの
ど部に2次空気供給通路20を接続しても良く、また、
調節弁23Fi排気ガスの圧力に関連させたり、他の手
段(スロットル開度、エンジン回転数、吸気管負圧又は
これらの組み合せ等)によってエンジンの負荷に関連し
て開閉するようにしても良い。
In this case, a pipe orifice may be used in place of the pipe nozzle 17, a veturi may be used in place of the pipe nozzle 17, and the secondary air supply passage 20 may be connected to its throat;
The control valve 23Fi may be opened and closed in relation to the pressure of exhaust gas, or in relation to the engine load by other means (throttle opening, engine speed, intake pipe negative pressure, or a combination thereof).

なお、図中符号24は過給通路11と吸入通路12とを
プロワ−圧縮機6を迂回して接続した吸気迂回通路で、
該通路24には、スロットル弁10を急閉しての減速時
に開くプローオフ弁25が設けられ、また符号26は排
気通路16とマフラー7又は排気管15とを排気タービ
ン5を迂回して接続した排気迂回−路で、該通路26に
は、過給がエンジンの危険回転を越えて過過給になった
とき開くウェストゲート弁27が設けられている。
In addition, the reference numeral 24 in the figure is an intake bypass passage that connects the supercharging passage 11 and the intake passage 12 by bypassing the blower compressor 6.
The passage 24 is provided with a plow-off valve 25 that opens during deceleration by rapidly closing the throttle valve 10, and reference numeral 26 connects the exhaust passage 16 and the muffler 7 or the exhaust pipe 15 by bypassing the exhaust turbine 5. In the exhaust detour, the passage 26 is provided with a wastegate valve 27 that opens when the supercharging exceeds the engine's critical speed and becomes supercharging.

この構成において、エンジンの運転中にエンジンから排
出された排気ガスは、排気通路16から排気タービン5
に入り、排気タービン5を回転してこれに直結したブロ
ワ−圧縮機6を回転駆動する。
In this configuration, exhaust gas discharged from the engine during operation of the engine is transferred from the exhaust passage 16 to the exhaust turbine 5.
The engine enters the engine, rotates the exhaust turbine 5, and rotationally drives the blower-compressor 6 directly connected thereto.

この場合、スロットル弁10の開度が少ない低負荷域で
は、吸入空気量が少なく従って排気ガス量が少なく、タ
ーボ過給機14の回転が遅くていわゆるターボ過給を行
ない得ない状態で、この状態ではバイパス通路22中の
調節弁23が閉じているので、エンジン1からの排気ガ
スは総て管ノズル17を通り、その下流部位のポート1
8に圧力の低い場を形成するから、当該箇所には2次空
気が2次空気供給通路20を介して吸引され、排気ガス
に混合されることになり、この低負荷域における排気ガ
ス量に合せて管ノズル17の口径を設定しておくことに
より、低負荷域において所定の2次空気量を確保できる
のである。
In this case, in a low load range where the opening degree of the throttle valve 10 is small, the amount of intake air is small, and therefore the amount of exhaust gas is small, and the rotation of the turbocharger 14 is slow, so that so-called turbocharging cannot be performed. In this state, the control valve 23 in the bypass passage 22 is closed, so all the exhaust gas from the engine 1 passes through the pipe nozzle 17 and enters the port 1 downstream of it.
Since a low pressure field is formed at 8, secondary air is sucked into the area through the secondary air supply passage 20 and mixed with the exhaust gas, and the amount of exhaust gas in this low load area is reduced. By setting the diameter of the pipe nozzle 17 in advance, a predetermined amount of secondary air can be secured in the low load range.

そして、スロットル弁10を大きく開らいての高負荷域
では、吸入空気量の増大に伴って排気ガス量が増加し、
ターボ過給機4の回転が早くなりいわゆるターボ過給状
態となる。
In a high load range with the throttle valve 10 wide open, the amount of exhaust gas increases as the amount of intake air increases.
The rotation of the turbo supercharger 4 becomes faster, resulting in a so-called turbo supercharging state.

この状態では負荷の増大に関連してバイパス通路22中
の調節弁23が開らくから、エンジン1からの排気ガス
は管ノズル17及びバイパス通路22の両方を流れ、管
ノズル17を流れる一部の排気ガスによって2次空気が
2次空気供給通路20から吸引される一方、エンジンか
らの排気ガスのうち一部の排気ガスはバイパス通路22
を通り、圧力損失を殆んど受けない状態で、管ノズル1
7の下流側に流れて、管ノズル17からの排気ガスと合
流して、その合流後における圧力は、管ノズル17前後
の平均圧力と略等しくなる。
In this state, the control valve 23 in the bypass passage 22 does not open due to the increase in load, so the exhaust gas from the engine 1 flows through both the pipe nozzle 17 and the bypass passage 22, and some of the exhaust gas flowing through the pipe nozzle 17 flows through the pipe nozzle 17 and the bypass passage 22. While secondary air is sucked from the secondary air supply passage 20 by the exhaust gas, some of the exhaust gas from the engine is sucked into the bypass passage 22.
through the pipe nozzle 1 with almost no pressure loss.
7 and merges with the exhaust gas from the tube nozzle 17, and the pressure after the merge becomes approximately equal to the average pressure before and after the tube nozzle 17.

従って、管ノズル17前後間における圧力損失は、排気
ガスの全量が低負荷域の排気ガス量に合せた管ノズル1
7を通る場合とは比較にならない程低減できるのである
Therefore, the pressure loss between the front and back of the pipe nozzle 17 is such that the total amount of exhaust gas is adjusted to the amount of exhaust gas in the low load range.
This can be reduced to an incomparable extent compared to the case where it passes through 7.

従って本発明によれば、排気通路中に設けた管ノズル等
の絞り部により、ターボ過給式エンジンの全負荷域につ
いて、所定量の2次空気を確実に供給できて、HC2C
O等の未燃成分を的確に浄化できる一方、前記絞り部に
対して設けた調節弁付きバイパス通路により、高負荷域
におけるエンジンの排気圧力の上昇及び排気タービン効
率の低下を防止できてエンジンの出力を向上できる効果
を有する。
Therefore, according to the present invention, it is possible to reliably supply a predetermined amount of secondary air over the entire load range of a turbocharged engine by means of a constriction section such as a pipe nozzle provided in the exhaust passage, and the HC2C
While it is possible to accurately purify unburned components such as O, the bypass passage with a control valve provided for the throttle section prevents an increase in engine exhaust pressure and a decrease in exhaust turbine efficiency in a high load range, thereby improving engine efficiency. It has the effect of improving output.

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

図面は本発明実施例装置の図である。 1・・・・・・エンジン、4・・・・・・排気ターボ過
給機、5・・・・・・排気タービン、6・・・・・・プ
ロワ−圧縮機、16・・・・・・排気通路、1T・・・
・・・管ノズル、20・・・・・・2次空気供給通路、
22・・・・・・バイパス通路、23・・・・・・調節
弁。
The drawing is a diagram of an apparatus according to an embodiment of the present invention. 1... Engine, 4... Exhaust turbo supercharger, 5... Exhaust turbine, 6... Prower compressor, 16...・Exhaust passage, 1T...
... Pipe nozzle, 20 ... Secondary air supply passage,
22...Bypass passage, 23...Control valve.

Claims (1)

【特許請求の範囲】[Claims] 1 排気ターボ過給機を備えたエンジンにおいて、エン
ジンから排気ターボ過給機@排気タービンに至る排気通
路中に、絞り部を設けると共に、該絞り部に対するバイ
パス通路を設け、このバイパス通路にはエンジンの負荷
に連動する調節弁を設ける一方、前記絞り部に2次空気
供給通路を接続したことを特徴とする排気ターボ過給式
エンジンにおける2次空気供給装置。
1. In an engine equipped with an exhaust turbo supercharger, a constriction part is provided in the exhaust passage leading from the engine to the exhaust turbo supercharger@exhaust turbine, and a bypass passage for the constriction part is provided, and the engine 1. A secondary air supply device for an exhaust turbocharged engine, characterized in that a control valve is provided that is linked to a load, and a secondary air supply passage is connected to the throttle portion.
JP16236578A 1978-12-28 1978-12-28 Secondary air supply device for exhaust turbocharged engine Expired JPS595765B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16236578A JPS595765B2 (en) 1978-12-28 1978-12-28 Secondary air supply device for exhaust turbocharged engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16236578A JPS595765B2 (en) 1978-12-28 1978-12-28 Secondary air supply device for exhaust turbocharged engine

Publications (2)

Publication Number Publication Date
JPS5591717A JPS5591717A (en) 1980-07-11
JPS595765B2 true JPS595765B2 (en) 1984-02-07

Family

ID=15753171

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16236578A Expired JPS595765B2 (en) 1978-12-28 1978-12-28 Secondary air supply device for exhaust turbocharged engine

Country Status (1)

Country Link
JP (1) JPS595765B2 (en)

Also Published As

Publication number Publication date
JPS5591717A (en) 1980-07-11

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