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JPS6045739B2 - Boost pressure control device for supercharged engines - Google Patents
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JPS6045739B2 - Boost pressure control device for supercharged engines - Google Patents

Boost pressure control device for supercharged engines

Info

Publication number
JPS6045739B2
JPS6045739B2 JP54062499A JP6249979A JPS6045739B2 JP S6045739 B2 JPS6045739 B2 JP S6045739B2 JP 54062499 A JP54062499 A JP 54062499A JP 6249979 A JP6249979 A JP 6249979A JP S6045739 B2 JPS6045739 B2 JP S6045739B2
Authority
JP
Japan
Prior art keywords
chamber
air
pressure
boost
exhaust
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
JP54062499A
Other languages
Japanese (ja)
Other versions
JPS55153819A (en
Inventor
重昭 堀内
捷治 長屋
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.)
Isuzu Motors Ltd
Original Assignee
Isuzu 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 Isuzu Motors Ltd filed Critical Isuzu Motors Ltd
Priority to JP54062499A priority Critical patent/JPS6045739B2/en
Publication of JPS55153819A publication Critical patent/JPS55153819A/en
Publication of JPS6045739B2 publication Critical patent/JPS6045739B2/en
Expired legal-status Critical Current

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Description

【発明の詳細な説明】 本発明は過給圧力制御装置、殊に排気ターボ過給機のタ
ービンに流入する排気ガスをバイパスさせて過給圧力を
制御する装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a boost pressure control device, and particularly to a device for controlling boost pressure by bypassing exhaust gas flowing into a turbine of an exhaust turbo supercharger.

一般に、車両、殊に自動車は発進性あるいは加速性が良
くなると非常に使にやすくなる。
In general, vehicles, especially automobiles, become much easier to use if they have better starting or acceleration characteristics.

このために、その内燃機関の出力;トルクのピークを極
力低速に置く様に種々の仕様を決めている。このことは
内燃機関に排気ターボ過給機を備えても変わりがなく、
従つて前記過給機の仕様を低速にマッチングさせるのが
通例である。ところが、ターボ過給機は排気ガスのエネ
ルギーで作動するものであるから低速にマッチングされ
た上記内燃機関においては、機関回転が上昇するにつれ
て過給圧力が過剰になつてしまい、これによる最大爆発
圧力の上昇から種々の不具合を生ずるものとなつてしま
う。このため、余剰となつた排気ガスを前記過給機のタ
ービンに流入させることなくバイパスさせていた。
For this reason, various specifications are determined so that the output/torque peak of the internal combustion engine is located as low as possible. This does not change even if the internal combustion engine is equipped with an exhaust turbo supercharger.
Therefore, it is customary to match the specifications of the supercharger to low speed. However, since the turbocharger operates using the energy of exhaust gas, in the above-mentioned internal combustion engine matched to low speed, the supercharging pressure becomes excessive as the engine speed increases, resulting in the maximum explosion pressure. This rise in temperature leads to various problems. Therefore, the excess exhaust gas is bypassed without flowing into the turbine of the supercharger.

しかしながら、従来の過給装置においては余剰となつた
排気ガスを急激に排出するものであつたために、過給圧
力が急激に大巾に低下し、車両運行中のフィーリングの
悪化、排気温度の異常上昇、スモーク濃度の悪化等の不
具合を生じせしめるものとなつていた。
However, because conventional supercharging systems rapidly discharge excess exhaust gas, the supercharging pressure suddenly drops significantly, resulting in poor feeling during vehicle operation and a drop in exhaust temperature. This was causing problems such as abnormal increase in smoke density and deterioration of smoke density.

また、特公昭38−15256号公報及び特許第147
95冴には排気ターボ過給機における排気バイパス弁を
過給気によつて制御される油圧により開閉させるように
なした過給装置が記載されているが、いずれも一次的に
制御するものであり、上述の過給圧力の急激な変動を十
分に緩和できないおそれがある。
Also, Japanese Patent Publication No. 38-15256 and Patent No. 147
95 Sae describes a supercharging device in which an exhaust bypass valve in an exhaust turbo supercharger is opened and closed by hydraulic pressure controlled by supercharging air, but none of them are primarily controlled. Therefore, there is a possibility that the above-mentioned rapid fluctuations in supercharging pressure cannot be sufficiently alleviated.

本発明は上述の点に鑑みて発明したもので、過J給圧力
の急激な変動を防止し、車両運行中のフィーリングを良
好にするとともに、排気温度の異常上昇、スモーク濃度
の悪化をも防止し、理想的な出力性能を得ることを目的
としたもので、その要旨は第一、第二の溝を摺動方向に
位相を変えて設7け且つ過給圧力により作動するスライ
ダに第一、第二制御弁のスラムを係合せしめてなるブー
スト制御器を、高圧エア源よりタービンバイパス路の切
換弁作動用エアシリンダに至る経路中に設け、第一、第
二設定過給圧力到達時に前記第一、第二制御弁により該
両制御弁と前記経路のエアシリンタ側とを連結する2本
の通路を順次大気又は高圧エアに連通せしめるようにし
てなる過給機関の過給圧力制御装置にあり、以下第1図
に示す一実施例により本発明を説明する。
The present invention was devised in view of the above-mentioned points, and it prevents sudden fluctuations in the supercharger pressure, improves the feeling during vehicle operation, and also prevents abnormal increases in exhaust temperature and deterioration of smoke density. The purpose is to prevent this problem and obtain ideal output performance.The gist of this is that the first and second grooves are provided with different phases in the sliding direction, and the second groove is installed in a slider operated by supercharging pressure. 1. A boost controller that engages the slam of the second control valve is installed in the path from the high-pressure air source to the air cylinder for actuating the switching valve in the turbine bypass path, and when the first and second set boost pressures are reached, A supercharging pressure control device for a supercharged engine, wherein the first and second control valves sequentially connect the two passages connecting the control valves and the air cylinder side of the passage to the atmosphere or high-pressure air. The present invention will be explained below with reference to an embodiment shown in FIG.

1は排気管2及び吸気管3を備える内燃機関、4は内燃
機関1の排気ガスで作動するタービン5を有する排気タ
ーボ過給機で、前記タービン5と出力軸6を介して直結
する圧縮機7を有し、圧縮機7によつて圧縮された空気
を吸気管3に供給する。
Reference numeral 1 denotes an internal combustion engine having an exhaust pipe 2 and an intake pipe 3; 4 an exhaust turbo supercharger having a turbine 5 operated by the exhaust gas of the internal combustion engine 1; and a compressor directly connected to the turbine 5 via an output shaft 6. 7, and supplies air compressed by the compressor 7 to the intake pipe 3.

8は排気管2と排気ターボ過給機4のタービン5とを連
通する排気ダクトで、排気通路9と同排気通路9の途中
からタービン5の出口5aに連通するタービンバイパス
路10と更に、排気通路9とタービンバイパス路10と
の連通を断続する弁機溝、例えば切換弁11とを備えて
いる。
8 is an exhaust duct that communicates the exhaust pipe 2 and the turbine 5 of the exhaust turbo supercharger 4; A valve groove, for example, a switching valve 11, is provided to connect and disconnect communication between the passage 9 and the turbine bypass path 10.

切換弁11によつて上記両路が連通されると排気ガスの
一部がタービン5に流入することなくタービン出口側に
排出される。12は切換弁11を作動させるエアシリン
ダで、そのシリンダ13に高圧エアが流入するとば−ね
15に抗してピストン14が切換弁11を作動させて排
気通路9とタービンバイパス路10との連通を遮断する
When the two passages are communicated by the switching valve 11, a part of the exhaust gas is discharged to the turbine outlet side without flowing into the turbine 5. Reference numeral 12 denotes an air cylinder that operates the switching valve 11. When high-pressure air flows into the cylinder 13, the piston 14 operates the switching valve 11 against the force of the spring 15, thereby establishing communication between the exhaust passage 9 and the turbine bypass passage 10. cut off.

16は高圧エア源としてのエアタンクで、例えば機関1
のコンプレッサ17よりの高圧エアを貯町えるエアタン
ク、18はエアチャンバ19とソレノイド20により連
動する2つの開閉弁21及び22とから成るエア制御器
、23は機関のメインスイッチ、24は電源でメインス
イッチ23を閉じるとソレノイド20に通電し二つの開
閉弁231,22を図中上方に引き上げ流入口25を開
放してエアタンク16とエアチャンバ19を連通すると
ともに、排出口26を閉鎖してエアチャンバ19ど外気
とを遮断する。
16 is an air tank as a high pressure air source, for example engine 1
18 is an air controller consisting of an air chamber 19 and two on-off valves 21 and 22 interlocked by a solenoid 20, 23 is a main switch for the engine, and 24 is a main switch for the engine. When the switch 23 is closed, the solenoid 20 is energized, the two on-off valves 231 and 22 are pulled upward in the figure, and the inlet 25 is opened to communicate the air tank 16 and the air chamber 19, while the outlet 26 is closed and the air chamber is closed. 19. Separate from outside air.

27は吸気管3と圧縮機7との途中から分岐し4た過圧
空気を受け、ばね28に抗して変位するダイヤフラム2
9と連動するスライダ30と、スライダ30の摺動に対
して直角にばね31及びばね32の付勢によつてステム
33a及びステム34aが当接する第一制御弁33及び
第二制御弁34と、エアチャンバ19と絞り35を介し
て連通する第一の室36と、エアシリンダ12に2本の
通路37a,38aを介して連通する第二の室37及び
第三の室38と、外気に連通する第四の室39とから成
るブースト制御器である。
27 is a diaphragm 2 which branches off from the middle of the intake pipe 3 and the compressor 7 and receives the overpressure air and is displaced against the spring 28.
a first control valve 33 and a second control valve 34 whose stems 33a and 34a are in contact with each other by the urging of springs 31 and 32 at right angles to the sliding movement of the slider 30; A first chamber 36 communicates with the air chamber 19 via a throttle 35, a second chamber 37 and a third chamber 38 communicate with the air cylinder 12 via two passages 37a and 38a, and communicate with the outside air. This is a boost controller consisting of a fourth chamber 39.

そして、そのスライダ30は第一、第二制御弁33,3
4のステム33a,34aの当接する側面に各々第一の
溝40及び第二の溝41を変位せしめて設けてノおり、
過給圧力がか)らない状態では第一制御弁33のステム
33aを第一の溝40上部のスライダ側面40aに、第
二制御弁34のステム34aを第二の溝41に当接させ
ている。尚、この状態では第一の室36と第二の室37
.とが連通し、第三の室38と第四の室39とが遮断さ
れている。
The slider 30 is connected to the first and second control valves 33 and 3.
A first groove 40 and a second groove 41 are respectively disposed on the side surfaces of the stems 33a and 34a of No. 4 in contact with each other, and
When no supercharging pressure is applied, the stem 33a of the first control valve 33 is brought into contact with the slider side surface 40a above the first groove 40, and the stem 34a of the second control valve 34 is brought into contact with the second groove 41. There is. In addition, in this state, the first chamber 36 and the second chamber 37
.. The third chamber 38 and the fourth chamber 39 are in communication with each other, and the third chamber 38 and the fourth chamber 39 are cut off.

更に、過給圧力が上昇し第一般定過給圧力になると第一
制御弁33のステム33aが第一の溝40に落込み、第
一制御弁33が第一の室36と第二の室37とを遮断す
るとともに同第二の室37と大気とを絞り42を介して
連通する。
Furthermore, when the boost pressure increases and reaches the first general constant boost pressure, the stem 33a of the first control valve 33 falls into the first groove 40, and the first control valve 33 opens the first chamber 36 and the second chamber. 37, and the second chamber 37 and the atmosphere are communicated through the aperture 42.

従つてエアシリンダ12の高圧エアが絞り42を通して
徐々に排出されることになる。そして、前記過給圧力が
上昇し第二設定過給圧力になると第二制御弁34のステ
ム34aが第二の溝41からせり出しスライダ側面41
aに当接し、第二制御弁34が第三の室38と第四の室
39、即ち第三の室38と大気を連通する。
Therefore, the high pressure air in the air cylinder 12 is gradually discharged through the throttle 42. Then, when the supercharging pressure increases and reaches the second set supercharging pressure, the stem 34a of the second control valve 34 protrudes from the second groove 41 and the slider side surface 41
a, and the second control valve 34 communicates the third chamber 38 and the fourth chamber 39, that is, the third chamber 38 and the atmosphere.

従つて、エアシリンダ12と大気との連通は、前記第二
の室37と絞り42とを介して行なわれるほか第四の室
39をも介して行なわれることになる。本発明の過給機
関の過給圧力制御装置は以上の様に構成されており、以
下作用について述べる。メインスイッチ23を閉じると
ソレノイド24に通電し、連動する二つの開閉弁21,
22が図中二点鎖線の如く引き上げられ流入口25を開
くとともに排出口26を閉じる。するとエアタンク16
よりの高圧エアがエアチャンバ19から絞り35、第一
の室36、第二の室37、通路37aを通りエアシリン
ダ12に流入してピストン14をばね15に抗して作動
させる。従つて、ピストン14は切換弁11と連動して
いるので、切換弁11を移動させ排気通路9とタービン
バイパス路10とを遮断する。
Therefore, the air cylinder 12 communicates with the atmosphere not only through the second chamber 37 and the throttle 42 but also through the fourth chamber 39. The supercharging pressure control device for a supercharged engine according to the present invention is constructed as described above, and its operation will be described below. When the main switch 23 is closed, the solenoid 24 is energized, and the two interlocking on-off valves 21,
22 is pulled up as shown by the two-dot chain line in the figure to open the inlet 25 and close the outlet 26. Then air tank 16
The higher pressure air flows from the air chamber 19 through the throttle 35, the first chamber 36, the second chamber 37, and the passage 37a, and flows into the air cylinder 12 to actuate the piston 14 against the spring 15. Therefore, since the piston 14 is interlocked with the switching valve 11, the switching valve 11 is moved to shut off the exhaust passage 9 and the turbine bypass passage 10.

この状態から、回転あるいは負荷が上昇してくると排気
ガスのエネルギとともに過給圧力も上昇してくる。
From this state, as the rotation or load increases, the energy of the exhaust gas and the boost pressure also increase.

そして、過給圧力が第一般定圧力に達すると、スライダ
30の上昇により第一制御弁33のステム33aが第一
の溝40に落を込み、第一制御弁33が第一の室36と
第二の室37とを遮断してエアタンク16よりの高圧エ
アのエアシリンダ12への供給を遮断するとともに、通
路37aと第二の室37と大気とを絞り42を介して連
通する。すると、エアシリンダ12のピストン14がは
ね15の作用によつて作動し、シリンダ13内の高圧エ
アを緩やかに大気に放出するので、切換弁11が徐々に
排気通路9とタービンバイパス路10とを連通する。こ
れにより排気ガスの一部がタービンバイパス路10から
徐々に捨てられるのでタービン5に流入する排気ガスが
徐々に減少する。
When the boost pressure reaches the first general constant pressure, the stem 33a of the first control valve 33 falls into the first groove 40 due to the rise of the slider 30, and the first control valve 33 connects with the first chamber 36. The second chamber 37 is cut off to cut off the supply of high-pressure air from the air tank 16 to the air cylinder 12, and the passage 37a, the second chamber 37, and the atmosphere are communicated via the throttle 42. Then, the piston 14 of the air cylinder 12 is actuated by the action of the spring 15, and the high pressure air in the cylinder 13 is slowly discharged to the atmosphere, so that the switching valve 11 gradually connects the exhaust passage 9 and the turbine bypass passage 10. communicate. As a result, a portion of the exhaust gas is gradually discarded from the turbine bypass path 10, so that the amount of exhaust gas flowing into the turbine 5 is gradually reduced.

従つて圧縮機7の回動がおさえられるので適正な過給圧
力を保つことになる。また、上記絞り42を介してエア
シリンダ12の高圧エアが緩やかに排出され切換弁11
が移行する途中て加速等の急激な負荷あるいは機関回転
上昇により過給圧力が異常上昇し第二設定過給圧力に達
した場合には、第二制御弁34のステム34aが第二の
溝41からスライダ側面41aにせり出す。
Therefore, since the rotation of the compressor 7 is suppressed, an appropriate supercharging pressure can be maintained. Also, the high pressure air in the air cylinder 12 is slowly discharged through the throttle 42 and the switching valve 11
If the supercharging pressure abnormally increases due to a sudden load such as acceleration or an increase in engine speed during the transition and reaches the second set supercharging pressure, the stem 34a of the second control valve 34 will move into the second groove 41. It protrudes from the slider side surface 41a.

この時、第二制御弁34が第三の室38と第四の室39
とを連通、即ち第三の室38と大気とを連通するので、
エアシリンダ12の高圧エアが通路38a1第三の室3
8、第四の室39を介して排出され、前述の第二の室3
7から絞り42を介して排出されるものに加えられ両方
から排出されることになる。従つて、切換弁11が速や
かに排気通路9とタービンバイパス路10との連通を拡
大してタービン5に流入する排気ガスを減少せしめるの
で、過給圧力の異常上昇をも防止するものとなる。この
状態から再び回転(あるいは負荷)が低下して排気ガス
量が減少してくると、過給圧力も減少するので今度は上
述とは逆の過程をたどる。
At this time, the second control valve 34 opens the third chamber 38 and the fourth chamber 39.
, that is, the third chamber 38 and the atmosphere,
High-pressure air from the air cylinder 12 flows through the passage 38a1 to the third chamber 3.
8. Exhausted through the fourth chamber 39 and the aforementioned second chamber 3
It is added to what is discharged from 7 through the throttle 42 and is discharged from both. Therefore, the switching valve 11 quickly expands the communication between the exhaust passage 9 and the turbine bypass passage 10 to reduce the amount of exhaust gas flowing into the turbine 5, thereby preventing an abnormal increase in supercharging pressure. From this state, when the rotation (or load) decreases again and the amount of exhaust gas decreases, the supercharging pressure also decreases, so the process reverses to that described above.

即ち、過給圧力が低下して第二設定圧力になると第二制
御弁34のステム34aが第二の溝41に落込み、同第
二制御弁34が第三の室38と第四の室39とを遮断す
る。更に、前記圧力が低下し第一般定圧力になると第一
制御弁33のステム33aが第一の溝40からせり出し
てスライダ側面40aに当接し、同第一制御弁33が第
一の室36と第二の室37とを連通するとともに同第二
の室37と外気との連通を遮断する。
That is, when the supercharging pressure decreases to the second set pressure, the stem 34a of the second control valve 34 falls into the second groove 41, and the second control valve 34 opens the third chamber 38 and the fourth chamber. 39. Further, when the pressure decreases to a first general constant pressure, the stem 33a of the first control valve 33 protrudes from the first groove 40 and comes into contact with the slider side surface 40a, and the first control valve 33 is brought into contact with the first chamber 36. It communicates with the second chamber 37 and blocks communication between the second chamber 37 and the outside air.

これによつてエアタンク16よりの高圧エアが絞り35
を通して徐々に緩やかにエアシリンダ12に流入して切
換弁11を排気通路9とタービンバイパス路10との遮
断方向に徐々に移行させる。
As a result, the high pressure air from the air tank 16 is restricted to the 35
The air gradually flows into the cylinder 12 through the air cylinder 12, thereby gradually moving the switching valve 11 in the direction of blocking the exhaust passage 9 and the turbine bypass passage 10.

従つてタービン5への排気ガス量が徐々に増えてくるの
で変動を生ずることもなく過給圧力を高めるので前述と
同様滑らかなトルクを得るものとなる。尚、機関1を停
止させメインスイッチ23を開くと、エア制御器18の
開閉弁21,22が流入口25を閉鎖して高圧エアの流
入を遮断するとともに排出口26を開放するので、エア
シリンダ12内のエアが第二の室37、第一の室36及
びエアチャンバ19を通して排出されるものとなる。
Therefore, since the amount of exhaust gas to the turbine 5 gradually increases, the supercharging pressure is increased without any fluctuation, and smooth torque can be obtained as described above. Note that when the engine 1 is stopped and the main switch 23 is opened, the on-off valves 21 and 22 of the air controller 18 close the inlet 25 to cut off the inflow of high-pressure air and open the outlet 26, so that the air cylinder The air in the air chamber 12 is exhausted through the second chamber 37, the first chamber 36, and the air chamber 19.

本発明による過給機関の過給圧力制御装置は、第一、第
二の溝を摺動方向に位相を変えて設け且つ過給圧力によ
り作動するスライダに第一、第二制御弁のステムを係合
せしめてなるブースト制御器を、高圧エア源よりタービ
ンバイパス路の切換弁作動用エアシリンダに至る経路中
に設け、第一、第二設定過給圧力到達時に前記第一、第
二制御弁により該両制御弁と前記経路のエアシリンダ側
とを連結する2本の通路を順次大気又は高圧エアに連通
せしめるようにして、排気ガスの一部を徐々にバイパス
させタービン5に流入する排気ガス量を制御する様にし
たので、従来の如く急激にバイパスすることによる過給
圧力の大巾な変動が防止できるのて車両運行中のフィー
リングを良好にする外、殊に過給圧力の急激な低下を防
げるので排気温度の異常上昇、スモーク濃度の悪化もな
くなるので理想的な出力性能を得ることができる。その
上、本発明においては切換弁11が排気通路9とタービ
ンバイパス路10とを連通する過程において過給圧力が
異常に上昇せんとしても、1上記連通を速やかに完全に
行なわしめる構造となつているので上記圧力の異常上昇
に伴なう燃焼圧力の異常上昇も回避てきるものである。
また、前述の特公昭38−15256号公報及び特許第
14795鏝公報の過給機関のような潤滑油等の油圧を
利用することなく、圧縮空気を利用するようにしたので
、高度のシール性の必要もなく、装置が安価となる効果
がある。
The supercharging pressure control device for a supercharging engine according to the present invention has first and second grooves provided with different phases in the sliding direction, and stems of the first and second control valves are mounted on a slider operated by supercharging pressure. A boost controller is provided in the path leading from the high-pressure air source to the air cylinder for actuating the switching valve in the turbine bypass passage, and when the first and second set boost pressures are reached, the boost controller is engaged with the boost controller. The two passages connecting the two control valves and the air cylinder side of the passage are successively communicated with the atmosphere or high-pressure air, thereby gradually bypassing a portion of the exhaust gas and controlling the amount of exhaust gas flowing into the turbine 5. As a result, wide fluctuations in supercharging pressure caused by sudden bypass as in the past can be prevented, which not only improves the feeling during vehicle operation, but also prevents sudden changes in supercharging pressure. Since this prevents the temperature from decreasing, there is no abnormal rise in exhaust temperature and no deterioration in smoke concentration, making it possible to obtain ideal output performance. Furthermore, in the present invention, even if the boost pressure does not rise abnormally during the process in which the switching valve 11 communicates the exhaust passage 9 and the turbine bypass passage 10, the structure is such that the above-mentioned communication is quickly and completely established. Therefore, an abnormal increase in combustion pressure due to the above-mentioned abnormal increase in pressure can also be avoided.
In addition, compressed air is used instead of using hydraulic pressure such as lubricating oil as in the supercharged engines of the above-mentioned Japanese Patent Publication No. 38-15256 and Japanese Patent No. 14795, which provides a high degree of sealing performance. This is not necessary and has the effect of making the device cheaper.

また、排気通路9とタービンバイパス路10との連通を
断続する弁機構を第2図に示す如く、スライドすること
によつて断続するポペット弁12″であつても良い。
Further, the valve mechanism that connects and disconnects the communication between the exhaust passage 9 and the turbine bypass path 10 may be a poppet valve 12'' that connects and disconnects communication by sliding, as shown in FIG.

尚、上記実施例においてはエアシリンダ12に高圧エア
を流入せしめて排気通路9とタービンバイパス路10と
の連通を遮断する様にしたが、ブースト制御器27とエ
アシリンダ12とを第3図の如く構成し、エアシリンダ
12のばね15によつて切換弁11を付勢して排気通路
9及びタービンバイパス路10の連通を遮断し、設定過
給圧力において高圧エアをシリンダ12に流入せしめて
上記排気通路9、タービンバイパス路10を連通する様
にしても良い。
In the above embodiment, high pressure air is caused to flow into the air cylinder 12 to block communication between the exhaust passage 9 and the turbine bypass passage 10, but the boost controller 27 and the air cylinder 12 are connected as shown in FIG. The switching valve 11 is biased by the spring 15 of the air cylinder 12 to cut off communication between the exhaust passage 9 and the turbine bypass passage 10, and high pressure air is allowed to flow into the cylinder 12 at the set boost pressure. The exhaust passage 9 and the turbine bypass passage 10 may be communicated with each other.

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

第1図は本発明の一実施例を示す概略系統図、第2図、
第3図は本発明の他の実施例を示す一部概略系統図であ
る。 1:内燃機関、2:排気管、3:吸気管、4:排気ター
ボ過給機、5;タービン、7;圧縮機、8;排気ダクト
、9;排気通路、10;タービンバイパス路、11;切
換弁、12;エアシリンダ、14;ピストン、16;エ
アタンク、18;”エア制御器、21,22;開閉弁、
27;ブースト制御器、29:ダイヤフラム、30;ス
ライダ、33;第一制御弁、34;第二制御弁、35,
42:絞り、36;第一の室、37:第二の室、38;
第三の室、39:第四の室、40;第一の溝、41;第
二の溝、37a,38a;通路。
FIG. 1 is a schematic system diagram showing an embodiment of the present invention, FIG.
FIG. 3 is a partially schematic system diagram showing another embodiment of the present invention. 1: Internal combustion engine, 2: Exhaust pipe, 3: Intake pipe, 4: Exhaust turbo supercharger, 5; Turbine, 7; Compressor, 8; Exhaust duct, 9; Exhaust passage, 10; Turbine bypass path, 11; Switching valve, 12; Air cylinder, 14; Piston, 16; Air tank, 18; Air controller, 21, 22; Opening/closing valve,
27; boost controller, 29: diaphragm, 30; slider, 33; first control valve, 34; second control valve, 35,
42: Aperture, 36; First chamber, 37: Second chamber, 38;
Third chamber, 39: Fourth chamber, 40; First groove, 41; Second groove, 37a, 38a; Passage.

Claims (1)

【特許請求の範囲】[Claims] 1 第一、第二の溝を摺動方向に位相を変えて設け且つ
過給圧力により作動するスライダに第一、第二制御弁の
ステムを係合せしめてなるブースト制御器を、高圧エア
源よりタービンバイパス路の切換弁作動用エアシリンダ
に至る経路中に設け、第一、第二設定過給圧力到達時に
前記第一、第二制御弁により該両制御弁と前記経路のエ
アシリンダ側とを連結する2本の通路を順次大気又は高
圧エアに連通せしめるようにしてなる過給機関の過給圧
力制御装置。
1. A boost controller in which the first and second grooves are provided with different phases in the sliding direction and the stems of the first and second control valves are engaged with a slider operated by boost pressure is connected to a boost controller from a high-pressure air source. The turbine bypass path is provided in a path leading to the air cylinder for actuating the switching valve, and when the first and second set supercharging pressures are reached, the first and second control valves connect both control valves and the air cylinder side of the path. A boost pressure control device for a supercharged engine that sequentially connects two passages to the atmosphere or high pressure air.
JP54062499A 1979-05-21 1979-05-21 Boost pressure control device for supercharged engines Expired JPS6045739B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP54062499A JPS6045739B2 (en) 1979-05-21 1979-05-21 Boost pressure control device for supercharged engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP54062499A JPS6045739B2 (en) 1979-05-21 1979-05-21 Boost pressure control device for supercharged engines

Publications (2)

Publication Number Publication Date
JPS55153819A JPS55153819A (en) 1980-12-01
JPS6045739B2 true JPS6045739B2 (en) 1985-10-11

Family

ID=13201911

Family Applications (1)

Application Number Title Priority Date Filing Date
JP54062499A Expired JPS6045739B2 (en) 1979-05-21 1979-05-21 Boost pressure control device for supercharged engines

Country Status (1)

Country Link
JP (1) JPS6045739B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20030021458A (en) * 2001-09-06 2003-03-15 현대자동차주식회사 The fate valve of an automotive turbo charger

Also Published As

Publication number Publication date
JPS55153819A (en) 1980-12-01

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