JPS5815642Y2 - Intake switching device for turbocharged engines - Google Patents

Intake switching device for turbocharged engines

Info

Publication number
JPS5815642Y2
JPS5815642Y2 JP1978060657U JP6065778U JPS5815642Y2 JP S5815642 Y2 JPS5815642 Y2 JP S5815642Y2 JP 1978060657 U JP1978060657 U JP 1978060657U JP 6065778 U JP6065778 U JP 6065778U JP S5815642 Y2 JPS5815642 Y2 JP S5815642Y2
Authority
JP
Japan
Prior art keywords
bypass
blower
valve
turbine
passage
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
JP1978060657U
Other languages
Japanese (ja)
Other versions
JPS54163210U (en
Inventor
森祥一
Original Assignee
ヤンマーディーゼル株式会社
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 ヤンマーディーゼル株式会社 filed Critical ヤンマーディーゼル株式会社
Priority to JP1978060657U priority Critical patent/JPS5815642Y2/en
Publication of JPS54163210U publication Critical patent/JPS54163210U/ja
Application granted granted Critical
Publication of JPS5815642Y2 publication Critical patent/JPS5815642Y2/en
Expired legal-status Critical Current

Links

Description

【考案の詳細な説明】 一般にターボチャージャはエンジン始動直後から高速回
転し、最高8000Orpmに達するのに対し、ポンプ
で加圧した潤滑油はフィルターを通過した後ターボチャ
ージャへ供給されるため、回転初期の潤滑油の供給が不
充分となり、焼付の原因となる問題があるため、その対
策として、エンジンの回転初期に潤滑油圧が規定値未満
の時タービン側へ排気ガスがいかないように、タービン
と並列のバイパスと、油圧と連動するバイパス開閉装置
を設けることが考えられる。
[Detailed explanation of the invention] In general, a turbocharger rotates at high speed immediately after the engine starts, reaching a maximum of 8000 rpm. However, since lubricating oil pressurized by a pump is supplied to the turbocharger after passing through a filter, There is a problem in which the supply of lubricating oil is insufficient, which can cause seizure.As a countermeasure, we have installed a valve parallel to the turbine to prevent exhaust gas from flowing to the turbine side when the lubricating oil pressure is less than the specified value at the beginning of engine rotation. It is conceivable to provide a bypass and a bypass opening/closing device linked to hydraulic pressure.

ところがその場合は潤滑油圧が規定値に達するまでター
ビン(及びブロワ−)が回転しないため、ブロワ−側を
吸気が通ると抵抗が大きくなり、前述の不具合が生ずる
However, in that case, the turbine (and the blower) does not rotate until the lubricating oil pressure reaches a specified value, so when the intake air passes through the blower side, resistance increases, causing the above-mentioned problem.

本考案は前述の如く始動直後のタービンの回転を抑止す
る対策を施した場合に、ブロワ−に対し吸気をバイパス
させようとするもので、図面に関連して説明すると次の
通りである。
The present invention attempts to bypass the intake air to the blower when measures are taken to suppress the rotation of the turbine immediately after startup as described above, and will be explained in conjunction with the drawings as follows.

図中、ターボチャージャ1はブロワ−2とタービン3を
備え、エンジンのシリンダヘッド上部に取付けである。
In the figure, a turbocharger 1 includes a blower 2 and a turbine 3, and is attached to the upper part of the cylinder head of the engine.

ブロワ−2の入口側吸気通路4は空気清浄器5に接続し
、出口側吸気通路6はエンジンの吸気マニホールド(図
示せず)に接続する。
An intake passage 4 on the inlet side of the blower 2 is connected to an air purifier 5, and an intake passage 6 on the outlet side is connected to an intake manifold (not shown) of the engine.

ブロワ−2と並列に、入口側吸気通路4と出口側吸気通
路6をつなぐバイパスTが設けてあり、、このバイパス
1は開閉弁8により閉塞されている。
A bypass T connecting the inlet side intake passage 4 and the outlet side intake passage 6 is provided in parallel with the blower 2, and this bypass 1 is closed by an on-off valve 8.

開閉弁8の固定している軸9は、通路4とバイパス1の
分岐部分の通路壁の軸受に支承され、通路壁から通路外
部へ突出した軸9の先端部にレバー10を固定している
The shaft 9 to which the on-off valve 8 is fixed is supported by a bearing on the passage wall at the branching portion of the passage 4 and the bypass 1, and a lever 10 is fixed to the tip of the shaft 9 that protrudes from the passage wall to the outside of the passage. .

図示の実施例に於てはレバー10はロンド11を介し、
排気バイパス12に設けた開閉弁13のレバー14に接
続している。
In the illustrated embodiment, the lever 10 is connected via the iron 11,
It is connected to a lever 14 of an on-off valve 13 provided in the exhaust bypass 12.

開閉弁13とレバー14は共に軸15に固定してあり、
軸15はタービン3の入口側排気通路16とバイパス1
2の分岐部の通路壁に設けた軸受に支持され、レバー1
4は通路壁から外方へ突出した軸15の先端部に固定し
である。
Both the on-off valve 13 and the lever 14 are fixed to a shaft 15,
The shaft 15 connects the inlet side exhaust passage 16 of the turbine 3 and the bypass 1.
The lever 1 is supported by a bearing provided on the passage wall of the branch part of the lever 1.
4 is fixed to the tip of a shaft 15 projecting outward from the passage wall.

バイパス12は通路16とタービン3の出口側排気通路
1γを接続する。
The bypass 12 connects the passage 16 and the outlet side exhaust passage 1γ of the turbine 3.

入口側排気通路16はエンジンの排気マニホールドに接
続し、出口側排気通路11はマフラー(共に図示せず)
に接続する。
The inlet side exhaust passage 16 is connected to the exhaust manifold of the engine, and the outlet side exhaust passage 11 is connected to a muffler (both not shown).
Connect to.

開閉弁13を制御するために潤滑油ポンプ19の吐出口
に接続した油圧シリンダー20が設けてあり、シリンダ
ー20内に嵌合したピストン21のロッド23の先端が
レバー14にピン接続し、レバー14の先端には引張ば
ね23の一端が接続している。
In order to control the on-off valve 13, a hydraulic cylinder 20 connected to the discharge port of the lubricating oil pump 19 is provided. One end of a tension spring 23 is connected to the tip.

24は調圧部、25はフィルター、26〜28は潤滑油
通路、29はターボチャージャ1に対する潤滑油入口で
ある。
24 is a pressure regulating section, 25 is a filter, 26 to 28 are lubricating oil passages, and 29 is a lubricating oil inlet to the turbocharger 1.

第1図は通常運転状態を示しており、ターボチャージャ
1の潤滑油人口29には規定値以上の潤滑油圧が供給さ
れ、又油圧シリンダー20内にもポンプ19の吐出油圧
が供給されてピストン21はばね23の弾力に抗して右
端の位置まで移動し、開閉弁13はバイパス12を閉塞
し、これにより排気ガスはすべて入口側排気通路・16
をへてタービン3に入り、タービン3を駆動している。
FIG. 1 shows a normal operating state, in which the lubricating oil pressure 29 of the turbocharger 1 is supplied with lubricating oil pressure higher than the specified value, and the hydraulic cylinder 20 is also supplied with the discharge oil pressure of the pump 19, so that the piston 21 The on-off valve 13 moves to the right end position against the elasticity of the spring 23, and the on-off valve 13 closes the bypass 12, so that all the exhaust gas is transferred to the inlet side exhaust passage 16.
It then enters the turbine 3 and drives the turbine 3.

矢印Aはこの時の排気ガスの流通方向を示す。Arrow A indicates the flow direction of exhaust gas at this time.

この時ブロワ−2側に於ては、開閉弁13に連動して開
閉弁8がバイパス7を閉塞し、従って吸気はすべて入口
側吸気通路4をへてブロワ−2に入り、そこで加圧され
、出口側吸気通路6をへてエンジンに供給され、過給作
用が行われる。
At this time, on the blower 2 side, the on-off valve 8 closes the bypass 7 in conjunction with the on-off valve 13, so that all intake air enters the blower 2 through the intake passage 4 on the inlet side, where it is pressurized. , is supplied to the engine through the outlet side intake passage 6, and a supercharging effect is performed.

矢印Bはこの時の吸気の流通方向を示す。Arrow B indicates the flow direction of the intake air at this time.

ポンプ19の故障等によりターボチャージャ1に所定の
油圧が供給できない場合とか、エンジン始動直後等には
、油圧シリンダー20内の油圧が低いか、又はその立上
りがゆるやかなため、ピストン21はばね23の弾力に
よりシリンダー20内の左端の位置を占め、開閉弁13
は13′の位置にありバイパス12が開く。
When the predetermined hydraulic pressure cannot be supplied to the turbocharger 1 due to a failure of the pump 19, etc., or immediately after the engine is started, the piston 21 is moved by the spring 23 because the hydraulic pressure in the hydraulic cylinder 20 is low or its rise is slow. Due to elasticity, it occupies the left end position in the cylinder 20, and the on-off valve 13
is at position 13' and bypass 12 is open.

矢印Cはその時の排気ガスの流通方向を示し、その間タ
ービン3は回転しない。
Arrow C indicates the flow direction of the exhaust gas at that time, during which the turbine 3 does not rotate.

同時に開閉弁13に連動した開閉弁8は8′の位置を占
め、バイパス7が開放シ、すべての吸気はバイパス7を
矢印り方向に流れ、ブロワ−2をバイパスする。
At the same time, the on-off valve 8 interlocked with the on-off valve 13 occupies the position 8', the bypass 7 is opened, and all the intake air flows through the bypass 7 in the direction of the arrow, bypassing the blower 2.

即ち吸気は停止中のブロワ−2を通過しない。That is, the intake air does not pass through the stopped blower 2.

以上説明したように本考案によると、タービン3と並列
に設けたバイパス12に開閉弁13(開閉機構)を設け
、潤滑油圧が低い間は開閉弁13によりバイパス12を
開き、排気がタービン3をバイパスするようにしたので
、エンジン始動初期の潤滑油不足の状態においでタービ
ン3が高速回転することを防止し、タービン3の焼付を
確実に防止できる。
As explained above, according to the present invention, an on-off valve 13 (on-off mechanism) is provided in the bypass 12 provided in parallel with the turbine 3, and when the lubricating oil pressure is low, the on-off valve 13 opens the bypass 12, and the exhaust gas flows through the turbine 3. By bypassing the engine, it is possible to prevent the turbine 3 from rotating at high speed in a state of insufficient lubricating oil at the initial stage of engine startup, thereby reliably preventing seizure of the turbine 3.

しかもブロワ−2にバイパスγを並列に設け。Moreover, a bypass γ is provided in parallel to the blower 2.

バイパス7に設けた開閉−弁8をワンド11等を介して
上記開閉弁13と連結し、両弁8,13のバイパス開閉
動作が互に同期するようにしたので、エンジン始動初期
のタービン非回転時には吸気をブロワ−用バイパス7へ
流すことができ(ブロワ−2への流入を防止でき)、吸
気抵抗の増加及びそれによるエンジン運転状態の悪化(
燃焼不良等)を抑止することができる。
The on-off valve 8 provided on the bypass 7 is connected to the on-off valve 13 via the wand 11, etc., so that the bypass opening and closing operations of both valves 8 and 13 are synchronized with each other, so that the turbine does not rotate at the initial stage of engine startup. Sometimes the intake air can flow to the blower bypass 7 (preventing it from flowing into the blower 2), increasing intake resistance and deteriorating the engine operating condition (
combustion defects, etc.) can be suppressed.

油圧が規定値以上になると、弁8,13はバイパス7.
12を閉じるので、所定の過給作用を確実に得ることが
でき、通常の運転状態を保つことができる。
When the oil pressure exceeds the specified value, the valves 8 and 13 are bypassed.
12 is closed, a predetermined supercharging effect can be reliably obtained and normal operating conditions can be maintained.

なお本考案を具体化する時、開閉弁8はバイパスγのみ
を開閉させる構造であっても差支えない。
Note that when embodying the present invention, the on-off valve 8 may be structured to open and close only the bypass γ.

その場合開閉弁がバイパス1を開くと、吸気は抵抗の少
ないバイパスT側を通過し、従って簡単な構造により吸
気抵抗の増加を防止し得る。
In this case, when the on-off valve opens the bypass 1, the intake air passes through the bypass T side, which has less resistance, so that an increase in intake resistance can be prevented with a simple structure.

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

図は本考案による装置の正面略図である。 1・・・・・・ターボチャージャ、2・・・・・・ブロ
ワ−3・・・・・・タービン 4・・・・・・入口側吸
気通路、6・・・・・・出口側吸気通路、1・・・・・
・バイパス、8・・・・・・開閉弁、12・・・−・・
バイパス、13・・・・・・開閉弁(開閉機構)、16
・・・・・・入口側排気通路、1T・・・・・・出口側
排気通路。
The figure is a schematic front view of the device according to the invention. 1...Turbocharger, 2...Blower 3...Turbine 4...Inlet side intake passage, 6...Outlet side intake passage , 1...
・Bypass, 8...Opening/closing valve, 12...-...
Bypass, 13... Opening/closing valve (opening/closing mechanism), 16
...Inlet side exhaust passage, 1T...Outlet side exhaust passage.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] ターボチャージャのタービンと並列に、タービン入口側
排気通路とタービン出口側排気通路をつなぐバイパスを
設けると共に、エンジン始動初期の潤滑油圧が規定値未
満の時バイパスを開き、油圧が規定値以上になった時バ
イパスを閉じてタービン側へ排気ガスを導くように、潤
滑油圧と連動する開閉機構を上記バイパスに設け、ター
ボチャージャのブロワ・−と並列に、ブロワ−の入口側
吸気通路と出口側吸気通路をつなぐブロワ−用バイパス
を設けると共に、上記ブロワ−用バイパスに開閉弁を設
け、上記開閉機構と開閉弁を連結して開閉機構と開閉弁
のバイパス開放動作が同期するようにしたことを特徴と
するターボチャージャ式エンジンの吸気切換装置。
A bypass is installed in parallel with the turbocharger turbine to connect the exhaust passage on the turbine inlet side and the exhaust passage on the turbine outlet side, and when the lubricating oil pressure at the beginning of engine startup is less than the specified value, the bypass is opened and the oil pressure exceeds the specified value. In order to close the bypass and guide the exhaust gas to the turbine side, an opening/closing mechanism linked to the lubricating oil pressure is installed in the bypass, and the opening and closing mechanism is connected to the intake passage on the inlet side and the intake passage on the outlet side of the blower in parallel with the blower of the turbocharger. A blower bypass is provided to connect the blower, and an on-off valve is provided on the blower bypass, and the on-off mechanism and the on-off valve are connected so that the bypass opening operation of the on-off mechanism and the on-off valve is synchronized. Air intake switching device for turbocharged engines.
JP1978060657U 1978-05-04 1978-05-04 Intake switching device for turbocharged engines Expired JPS5815642Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1978060657U JPS5815642Y2 (en) 1978-05-04 1978-05-04 Intake switching device for turbocharged engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1978060657U JPS5815642Y2 (en) 1978-05-04 1978-05-04 Intake switching device for turbocharged engines

Publications (2)

Publication Number Publication Date
JPS54163210U JPS54163210U (en) 1979-11-15
JPS5815642Y2 true JPS5815642Y2 (en) 1983-03-30

Family

ID=28961351

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1978060657U Expired JPS5815642Y2 (en) 1978-05-04 1978-05-04 Intake switching device for turbocharged engines

Country Status (1)

Country Link
JP (1) JPS5815642Y2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59145331A (en) * 1983-02-04 1984-08-20 Mazda Motor Corp Safety device for engine fitted with turbosupercharger

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4837830B2 (en) * 1971-05-15 1973-11-14

Also Published As

Publication number Publication date
JPS54163210U (en) 1979-11-15

Similar Documents

Publication Publication Date Title
US5996347A (en) Variable-nozzle type turbo charger
JP6059299B2 (en) Combustion engine forced introduction device, combustion engine, and operation method of combustion engine
JPS58167827A (en) Controller for supply of air to internal combustion engine
JPS60169630A (en) Supercharger for internal-combustion engine
JPS59113236A (en) Supercharger protecting apparatus for supercharged engine
JPH0478818B2 (en)
JPS6344936B2 (en)
JPS5815642Y2 (en) Intake switching device for turbocharged engines
JPH0417767Y2 (en)
JPS61291725A (en) S-step type superchaging device
JPS6120294Y2 (en)
JPS601224Y2 (en) Internal combustion engine supercharging device
JPS6316130A (en) Exhaust turbo supercharger for internal combustion engine
JPS5822978Y2 (en) turbocharged engine
JPH0416606B2 (en)
JPS6245057Y2 (en)
JPS61164041A (en) Internal-combustion engine with turbo charger
SU1192634A3 (en) Supercharged internal combustion engine
JPH053715Y2 (en)
JPS6042191Y2 (en) Bypass path control device for engine with exhaust turbocharger
JPH0326826A (en) Supercharger for engine and device therefor
JPS61190124A (en) Supercharger of engine
JPS5930179Y2 (en) supercharger
JPS591060Y2 (en) Turbocharger pressure control device
JPS5951651B2 (en) Exhaust turbocharged engine