JPS58133425A - Bearing protector of turbocharger - Google Patents

Bearing protector of turbocharger

Info

Publication number
JPS58133425A
JPS58133425A JP57014752A JP1475282A JPS58133425A JP S58133425 A JPS58133425 A JP S58133425A JP 57014752 A JP57014752 A JP 57014752A JP 1475282 A JP1475282 A JP 1475282A JP S58133425 A JPS58133425 A JP S58133425A
Authority
JP
Japan
Prior art keywords
turbocharger
engine
bearing
key switch
lubricating oil
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.)
Granted
Application number
JP57014752A
Other languages
Japanese (ja)
Other versions
JPH0335497B2 (en
Inventor
Masami Yamazaki
山崎 正己
Sueo Shibata
柴田 末男
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.)
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP57014752A priority Critical patent/JPS58133425A/en
Publication of JPS58133425A publication Critical patent/JPS58133425A/en
Publication of JPH0335497B2 publication Critical patent/JPH0335497B2/ja
Granted 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
    • F02B39/00Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F02B39/14Lubrication of pumps; Safety measures therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00Sliding-contact bearings for exclusively rotary movement
    • F16C17/12Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load
    • F16C17/18Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load with floating brasses or brushing, rotatable at a reduced speed
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/10Construction relative to lubrication
    • F16C33/1025Construction relative to lubrication with liquid, e.g. oil, as lubricant
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00Sliding-contact bearings for exclusively rotary movement
    • F16C17/02Sliding-contact bearings for exclusively rotary movement for radial load only
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00Engines or pumps
    • F16C2360/23Gas turbine engines
    • F16C2360/24Turbochargers

Abstract

PURPOSE:To prevent deterioration of lubricating oil in a bearing part, by introducing a jet stream of high pressure gas to a floating bearing part at stopping of an engine and blowing the lubricating oil accumulated in the bearing part with the jet stream to dry the bearing part. CONSTITUTION:During operation of an engine, a key switch 144 is placed in an ON position and a solenoid 132 is excited. This causes a shut off valve 134 to close. Intake air pressurized by a compressor of a turbocharger is partially accumulated in a surge tank 130 through a supercharge intake pipe 140. When the key switch is turned to an OFF position to stop the engine, an oil pump 108 is also stopped. Action of a delay timer 142 causes the solenoid 132 after opening of the key switch to open after elapsed a prescribed time, and high pressure air in the surge tank is injected toward an oil inlet pipe 112.

Description

【発明の詳細な説明】 本発明はターボチャージャ付き内燃機関に係り、より詳
しくは、ターボチャージャのホットシャットタウン時に
ターボチャージャ軸受部を保護するための装置に関する
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a turbocharged internal combustion engine, and more particularly to a device for protecting a turbocharger bearing during hot shutdown of the turbocharger.

車両用内燃機関のターボチャージャにおいてはコンプレ
ッサおよびタービンは最高的毎分10万回転もの^速度
で回転するため、シャフトの軸受としては第1図に示す
ようにフルフローティング軸受10.10が使用される
。エンジンのオイルポンプに接続されたオイルインレッ
トパイプ11はターボチャージャのメインハウジング1
2に設は九パイプ接続口13にねじ込まれており、潤滑
油は分配孔14を経て給油孔15に分配され各フル70
−テイ/グ軸受10.10に供給される。
In a turbocharger for a vehicle internal combustion engine, the compressor and turbine rotate at a maximum speed of 100,000 revolutions per minute, so a full floating bearing 10.10 is used as the shaft bearing, as shown in Figure 1. . The oil inlet pipe 11 connected to the engine oil pump is connected to the main housing 1 of the turbocharger.
2 is screwed into the nine pipe connection port 13, and the lubricating oil is distributed to the oil supply hole 15 through the distribution hole 14, and the lubricating oil is distributed to each full 70
- fed to the Tei/Ge bearing 10.10;

第2図に拡大して示し九ように、メインハウジングに形
成した内孔16とフルフローティング軸受10とターボ
チャージャシャフト17の間には微小なすきまが形成さ
れており、エンジン作動中にこの微小なすきまが形成さ
れており、エンジン作動中はこの微小すきまに潤滑油の
油膜が形成ハれてシャフトの回転振動を減衰し吸収する
機能を果している。潤滑油Fiまたエンジンの排気系か
ら波及伝播して来る熱により加熱された軸受部を冷却す
る作用も果している。
As shown in an enlarged view in Fig. 2, a minute gap is formed between the inner hole 16 formed in the main housing, the full floating bearing 10, and the turbocharger shaft 17, and this minute gap is formed during engine operation. A gap is formed, and during engine operation, a film of lubricating oil is formed in this minute gap and functions to dampen and absorb rotational vibrations of the shaft. The lubricating oil Fi also has the function of cooling the bearing section, which is heated by the heat propagated from the engine's exhaust system.

エンジンが停止し、これに伴いターlチャージャの回転
が停止すると共にオイルポンプからの潤滑油供給が停止
した時には、ターボチャージャ内の潤滑油は重力によ5
滴下してエンジンのオイルパンに戻るが、フル70−テ
ィング軸受部においては第38CIに示したように微小
す!壕には潤滑油が滞留する。高速走行後直ちに車両を
駐停車する場合の如く、エンジンの高速高負荷運転の直
後にエンジンを停止した場合KFi、排気系が高温に熱
せられている状態で突然にターボチャージャの回転およ
び潤滑油の供給が停止することKなる。この状5tFi
ターボチヤージヤのホットシャットダウンと称されてい
る。ホットシャットダウン時しては、フルフローティン
グ軸受部の微小すきまに滞留した潤滑油は、高温に熱せ
られた排気系から漸次伝播して来る熱により酸化し、ス
ラッジ化し、或いは極端な場合には炭化するに至る。こ
のような熱による潤滑油の変質を本明細書では広く劣化
というものとする。劣化した1llIlv油は軸受の微
小すきまに付着ないし固着して、エンジンの次の作動の
際に潤滑油の供給不足を招き、軸受部の墨常磨耗を引起
す。
When the engine stops, the rotation of the turbocharger stops, and the supply of lubricating oil from the oil pump stops, the lubricating oil inside the turbocharger is
It drips and returns to the engine's oil pan, but in the full 70-ring bearing part, it is very small as shown in No. 38 CI! Lubricating oil remains in the trench. KFi occurs when the engine is stopped immediately after high-speed, high-load operation, such as when parking a vehicle immediately after driving at high speed, and the exhaust system is heated to a high temperature and the turbocharger suddenly rotates and the lubricating oil drains. The supply will stop. This state 5tFi
This is called a turbocharger hot shutdown. During a hot shutdown, the lubricating oil that remains in the tiny gaps in the fully floating bearing becomes oxidized, turns into sludge, or in extreme cases becomes carbonized due to the heat that gradually propagates from the highly heated exhaust system. leading to. In this specification, such change in quality of lubricating oil due to heat is broadly referred to as deterioration. The deteriorated 1llllv oil adheres or sticks to minute gaps in the bearing, leading to insufficient supply of lubricating oil during the next operation of the engine and causing permanent wear of the bearing.

本発明の目的は、ターボチャージャのホットシャットダ
ウン時にもフルフローティング軸受部の潤滑油の劣化を
防止し得るような軸受部11i4!I!置を提供するこ
とである。
An object of the present invention is to provide a bearing portion 11i4 that can prevent deterioration of the lubricating oil in the full floating bearing portion even during hot shutdown of the turbocharger! I! The goal is to provide a

上記目的を達成するため、本発明は、エンジン停止時に
フルフローティング軸受部に高圧の気体噴流を導入して
軸受部に滞留するfR滑油を噴流により吹き飛ばして軸
受部をドライにし、これにより軸受部にシける潤滑油の
劣化を防止しようというものである。
In order to achieve the above object, the present invention introduces a high-pressure gas jet into the fully floating bearing when the engine is stopped, blows off the fR lubricant that remains in the bearing, and dries the bearing. The purpose is to prevent the deterioration of lubricating oil when it is exposed to water.

このため、本発明の軸受部Satは、圧力気体源と、−
熾がこの圧力気体源に接続されかつ他端がターボチャー
ジャのフルフローティング軸受部に連通されていて圧力
気体を圧力気体源から軸受mK導くように々っ九配管と
、前記配管中に設置されていて工/ジ/作動中は閉鎖さ
れていて圧力気体のfi通を遮断しているがエンジン停
止時には開放されて圧力気体を通過せしめて軸受部に噴
出せしめ得るようになった遮断弁とを具備して成ること
を要旨とするものである。
Therefore, the bearing part Sat of the present invention has a pressure gas source and -
A pipe is connected to the pressure gas source, and the other end is connected to the full floating bearing part of the turbocharger, and the pipe is installed in the pipe so that the pressure gas is guided from the pressure gas source to the bearing mK. It is equipped with a shutoff valve that is closed during operation and blocks the passage of pressurized gas, but is opened when the engine is stopped to allow pressurized gas to pass through and be ejected to the bearing section. The gist of this is to accomplish the following:

本発明の具体的実施態様においては、上記圧力気体源は
ターボチャージャのコンプレッサの吐出側に接続されタ
ーボチャージャの過給圧を蓄圧し得るようにな9たサー
ジタyりのような貯賊容器で構成することができる。過
給圧が低下した時に容器内の圧力空気がコンプレッサ吐
出側に逆流するのを阻止するため、貯蔵容器とコンプレ
ッサ吐出側との間には逆止弁を設けることができる。
In a specific embodiment of the invention, the source of pressurized gas is a storage container, such as a surge tank, connected to the discharge side of the compressor of the turbocharger and adapted to store the boost pressure of the turbocharger. Can be configured. A check valve can be provided between the storage container and the compressor discharge side to prevent the pressurized air in the container from flowing back to the compressor discharge side when the boost pressure decreases.

圧力気体用配管の上記他端は軸受部に直11KIl1口
させても良いが、好ましくはターボチャージャのオイル
インレットバイブに合流させる。圧力気体を噴出させた
時にその圧力気体がオイルポンプに向って逆流するのを
防止するため、オイルインレットパイプには合流点の上
流において逆止弁を設けるのが良い。
The other end of the pressure gas piping may be connected directly to the bearing, but is preferably connected to the oil inlet pipe of the turbocharger. In order to prevent the pressurized gas from flowing back toward the oil pump when the pressurized gas is ejected, the oil inlet pipe is preferably provided with a check valve upstream of the confluence point.

遮断弁はエンジンのキースイッチに連係されたソレノイ
ド式電磁弁で構成することができる。ターボチャージャ
のシャフトはエンジン停止後も僅かの間楕性回転するの
であるが、この楕性回転終了後にはじめて潤滑油を吹き
飛ばすようにする九め、キースイッチとソレノイドの間
に遅延回路を設けてもよい。
The shutoff valve may be a solenoid-type electromagnetic valve linked to the engine key switch. The turbocharger shaft rotates in an elliptical manner for a short time even after the engine has stopped, but in order to blow out the lubricant only after this elliptical rotation has ended, it is possible to install a delay circuit between the key switch and the solenoid. good.

以下、図面により本発明の詳細な説明し、本発明の作用
効果も併せて記す。
Hereinafter, the present invention will be explained in detail with reference to the drawings, and the effects of the present invention will also be described.

第4図は本発明の軸受保護装置の一実施例を取り付けた
ターボチャージャおよび潤滑系の立rM図で、ターボチ
ャージャ100のフルフローティング軸受は点線の円1
02により略示しである。エンジン本体およびターボチ
ャージャの潤滑系は周知のもので、オイルパン104内
の潤滑油は吸込み管106を介してオイルポンプ10B
に吸い込tttてフィルタ110を通ってターボチャー
ジャ用のオイルインレットパイプ112およびエンシフ
本体17&油管114に向つて圧送される。インレット
バイブ112中には逆止弁116が設置しである。館1
図を参照して既K16!明したように、このオイルイン
レットパイプ112はターボチャージャ1000メイン
ハウジ/グ118に形成され九インレットパ、イブ接続
口にねじ込まれている。
FIG. 4 is an elevation view of a turbocharger and a lubrication system equipped with an embodiment of the bearing protection device of the present invention.
It is abbreviated as 02. The lubrication system for the engine body and the turbocharger is well known, and the lubricating oil in the oil pan 104 is supplied to the oil pump 10B through the suction pipe 106.
The oil is sucked in, passes through a filter 110, and is sent under pressure to an oil inlet pipe 112 for the turbocharger and an enshiff main body 17 & oil pipe 114. A check valve 116 is installed in the inlet vibe 112. Hall 1
Refer to the figure and it's already K16! As explained above, this oil inlet pipe 112 is formed in the main housing/guage 118 of the turbocharger 1000 and is screwed into the nine inlet pipe connection ports.

潤滑油はメインハウジング内の分配孔および給油孔(第
1図参照)を経て軸受部102に供給される。軸受部を
潤滑した油は戻り管120によりオイルパンに帰還され
る。他方、給油管114を経てエンジン本体の軸受部1
22を潤滑した潤滑油は適当に形成された戻り管124
を通ってオイルパンに帰還する。
Lubricating oil is supplied to the bearing portion 102 through a distribution hole and an oil supply hole (see FIG. 1) in the main housing. The oil that has lubricated the bearing portion is returned to the oil pan through a return pipe 120. On the other hand, the bearing part 1 of the engine body is connected through the oil supply pipe 114.
The lubricating oil used to lubricate 22 is passed through the appropriately formed return pipe 124.
It passes through and returns to the oil pan.

ターボチャージャ100のコンプレッサの吐出口126
には過給気ダクト128が取り付けてあり、この過給気
ダクトはエンジンの吸気マニホールド(図示せず)Kl
l!続されている。
Compressor discharge port 126 of turbocharger 100
A supercharging air duct 128 is attached to the engine, and this supercharging duct connects to the engine's intake manifold (not shown) Kl.
l! It is continued.

エンジンの適宜部位には専用サージタンク130が設置
しである。このサージタンク130t:tソレノイド1
32をもった電磁式遮断弁134を備えた圧力空気配管
136によpオイルインレットパイプ112に接続され
ている。圧力空気配管136と過給気ダクト128の間
には逆上弁138を備えた過給気取入れ管140が接続
されている。
A dedicated surge tank 130 is installed at an appropriate location on the engine. This surge tank 130t:t solenoid 1
It is connected to the p-oil inlet pipe 112 by a pressurized air line 136 with an electromagnetic shutoff valve 134 having a diameter of 32. A supercharging air intake pipe 140 equipped with a reverse valve 138 is connected between the pressurized air pipe 136 and the supercharging air duct 128 .

電磁式遮断弁134のソレノイド132は遅延タイマー
142およびエンジンのキースイッチ144を介して電
源146に接続されている。
The solenoid 132 of the electromagnetic shutoff valve 134 is connected to a power source 146 via a delay timer 142 and an engine key switch 144.

次に1本発明の装置の作動について述べるに、エンジン
動作中はキースイッチ144はONの位置にあり、ソレ
ノイド132it励磁されている。
Next, the operation of the device of the present invention will be described. When the engine is operating, the key switch 144 is in the ON position and the solenoid 132 is energized.

このため、遮断弁134は閉鎖している。ターボチャー
ジャのコンプレッサにより加圧された吸気の一部は過給
気取入れ管140を介してサージタンク130に蓄積さ
れる。過給気取入れ管140には逆止弁138が設けで
あるので、サージタンクにはターボチャージャ運転時に
到達する最高過給圧が蓄積される。また、エンジンが高
速運転されればそれだけ高い過給圧が発生せられるので
、ホットシャットダウン時に軸受部が受ける熱が多い時
程、高い圧力の空気がサージタンクに貯えられるのであ
る。
Therefore, the shutoff valve 134 is closed. A portion of the intake air pressurized by the turbocharger compressor is stored in the surge tank 130 via the supercharging air intake pipe 140. Since the supercharging air intake pipe 140 is provided with a check valve 138, the maximum supercharging pressure reached during turbocharger operation is accumulated in the surge tank. Additionally, the higher the engine speed, the higher the boost pressure generated, so the more heat the bearing receives during hot shutdown, the more high pressure air is stored in the surge tank.

キースイッチをOFFの位置に回動させてエンジンを停
止させた時には、オイルポンプ108も停止し、潤滑系
内の潤滑油圧力は消失する。また、ターボチャージャの
コンプレッサならびにタービンはエンジン停止後短時間
慣性回転した後やがて停止する。遅延タイマー142の
作用によりソレノイド132i;tキースイッチ開放後
衛定時間経過後に開放され、サージタンク内の高圧空気
をオイルインレットパイプ112に向って噴出させる。
When the key switch is turned to the OFF position to stop the engine, the oil pump 108 also stops, and the lubricating oil pressure in the lubrication system disappears. Further, the compressor and turbine of the turbocharger rotate inertia for a short time after the engine is stopped, and then eventually stop. Due to the action of the delay timer 142, the solenoid 132i; t is opened after a predetermined period of time has elapsed after the key switch is opened, and the high pressure air in the surge tank is blown out toward the oil inlet pipe 112.

オイルインレットパイプの上流側KVi逆止弁116が
設けであるので、空気の噴流はオイルポンプ側に逆流す
ることなくインレットバイブ接続口、分配孔、および給
油孔を経て、フルフローティング軸受部に吹き付けられ
る。その結果、軸受部のすきまに付着している潤滑油は
鯖5図に示したように吹き飛ばされる。したがって、ホ
ットシャットダウン時に排気系から軸受部に熱が波及伝
達しても、軸受部に潤滑油が滞留していないので、潤滑
油の膠着、スラッジ化、または炭化の問題を引起すこと
が々い。なお、軸受部における受熱量の大きい時機、潤
滑油の粘度が低下しているので、空気噴流による潤滑油
の吹き飛ばし効果が大きい。
Since the KVi check valve 116 is provided on the upstream side of the oil inlet pipe, the jet of air is blown onto the full floating bearing through the inlet vibe connection port, distribution hole, and oil supply hole without flowing back to the oil pump side. . As a result, the lubricating oil adhering to the gap in the bearing portion is blown away as shown in Fig. 5. Therefore, even if heat is transferred from the exhaust system to the bearing during a hot shutdown, the lubricating oil does not remain in the bearing, which often causes problems such as sticking, sludge, or carbonization of the lubricating oil. . Note that when the amount of heat received in the bearing portion is large, the viscosity of the lubricating oil is reduced, so that the effect of blowing off the lubricating oil by the air jet is large.

また、軸受部に空気を吹き付けることによりg!冷効果
も期待することができるO 以上のように、本発明のi&鎧によればホットシャット
ダウン時にフルフローティング軸受部に劣化したfi4
渭油がflIa城するのが防止され、軸受の肌荒れや異
’l’l醋耗が回避される。また、この装置はエンジン
停止時に自動的に作動する75為ら、「高速高負荷運転
後は暫くアイドル運転した抜工/ジンを停止すること」
との煩しい運転上の注意を実行する必要がない、
Also, by blowing air onto the bearing part, g! A cooling effect can also be expected.O As described above, according to the i & armor of the present invention, the fi4 which deteriorated to a full floating bearing part during hot shutdown
This prevents oil from building up and prevents roughening of the bearing surface and abnormal wear and tear. In addition, since this device automatically operates when the engine is stopped75, it is recommended that after high-speed, high-load operation, stop the extractor/gin that has been running idly for a while.
There is no need to perform cumbersome driving precautions,

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

餌1図はターボチャージャの垂直断面を示す参考図、第
2図はエンジン作動時の潤滑状態を示す軸受部の断面図
、鯖3図はエンジン停止時の軸受部の断面図、第4図は
本発明の装置の立面図、第5図は軸受部の潤滑油を吹き
飛ばす状態を図解1〜た軸受部の断面図である。 100−・・ターボチャージャ、102・・フルフロー
ティング軸受、112・・オイルインレットパイプ、1
16・・逆止弁、126・・コンプレッサの吐出口、1
28・・過給気夕′クト、130・・・サージタンク、
132・・電磁式遮断弁のソレノイド、134・・電研
式遮断弁、136 ・圧力空気配管、138・・逆上弁
、140・・・過給気取入れ管、142・・・遅延タイ
マー、144・・・エンジンのキースイッチ。 第1図 第5図 第2図     第3図 第4図
Figure 1 is a reference diagram showing a vertical cross section of the turbocharger, Figure 2 is a cross-sectional view of the bearing showing the lubrication state when the engine is running, Figure 3 is a cross-sectional view of the bearing when the engine is stopped, and Figure 4 is a cross-sectional view of the bearing when the engine is stopped. FIG. 5 is an elevational view of the apparatus of the present invention, and is a cross-sectional view of the bearing section illustrating the state in which lubricating oil is blown away from the bearing section. 100--turbocharger, 102--full floating bearing, 112--oil inlet pipe, 1
16...Check valve, 126...Compressor discharge port, 1
28...Supercharging air tank, 130...Surge tank,
132... Solenoid of electromagnetic shutoff valve, 134... Denken type cutoff valve, 136 - Pressure air piping, 138... Reverse valve, 140... Supercharge air intake pipe, 142... Delay timer, 144 ...Engine key switch. Figure 1 Figure 5 Figure 2 Figure 3 Figure 4

Claims (1)

【特許請求の範囲】 1、圧力気体源と、一端が上記圧力気体源に接続されか
つ他端がターボチャージャのフルフローティング軸受部
に連通されていて圧力気体を圧力気体源からフルフロー
ティング軸受部に導くようになった配管と、前記配管中
に介在されていてエンジン作動中は閉鎖されていて圧力
気体の流通を遮断しているがエンジン停止時には開放さ
れて圧力気体を通過せしめてフルフローティング軸受部
に噴出せしめるようになった遮断弁とを具備して成り、
エンジン停止時にフルフローティング軸受部Kfi留す
る潤滑油を圧力気体の噴流により吹き飛ばし、もって、
ターボチャージャのホットシャットダウン時のフルフロ
ーティング軸受部における潤滑油の劣化を防止し得るよ
うにしたことを特徴とするターボチャージャのフルフロ
ーティング軸受保護装置。 2、上記圧力気体源はターボチャージャのコンプレッサ
の吐出側に接続されターボチャージャの過給圧を蓄圧し
得るようになった貯蔵容器から成り、上記貯蔵容器とコ
ンプレッサ吐出側との間には過給圧が低下した時に該容
器内に蓄圧された圧力空気がコンプレッサ吐出側に逆流
するのを阻止するための逆止弁が設けであることを特徴
とする特許請求の範囲第1項記載の軸受像S装置。 3、上記配管の上記他端はターボチャージャのオイルイ
ンレットパイプに接続してあり、このオイルインレット
バイブには上記配管との合流点より上流において逆止弁
を設けて圧力空気の噴出時に圧力空気が上流に向って逆
流するのを阻止し得るようになっていることを特徴とす
る特許請求の範囲1i2項記載の軸受保護装置。 4、上記遮断弁はソレノイドを有する電磁式連断弁であ
り、該ソレノイドはエンジンのキースイッチがONの時
に励磁されて遮断弁を閉鎖するとともにキースイッチが
OFFの時に消磁されて遮断弁を開放し得るようになっ
ていることを特徴とする特許請求の範囲第3項記載の軸
受保II装置。 5. エンジンのキースイッチと上記ソレノイドの間に
は遅延回路が挿入されており、もって、エンジン停止後
所定時間経過後K11断弁が開放して圧力空気を噴出さ
せ得るよう罠なっていることを特徴とする特許請求の範
囲!4項記載の軸受保−装置。
[Claims] 1. A pressure gas source, one end of which is connected to the pressure gas source and the other end communicated with the full floating bearing of the turbocharger, and the pressure gas is supplied from the pressure gas source to the full floating bearing. A fully floating bearing section that is interposed in the piping and is closed during engine operation to block the flow of pressurized gas, but is opened when the engine is stopped to allow pressurized gas to pass through. It is equipped with a shutoff valve that allows the water to flow out,
When the engine is stopped, the lubricating oil remaining in the fully floating bearing part Kfi is blown away by a jet of pressurized gas.
A full-floating bearing protection device for a turbocharger, characterized in that it is capable of preventing deterioration of lubricating oil in a full-floating bearing during hot shutdown of a turbocharger. 2. The pressure gas source consists of a storage container connected to the discharge side of the compressor of the turbocharger and capable of accumulating the supercharging pressure of the turbocharger, and between the storage container and the compressor discharge side, the supercharging The bearing image according to claim 1, characterized in that a check valve is provided to prevent the pressurized air accumulated in the container from flowing back to the compressor discharge side when the pressure decreases. S device. 3. The other end of the piping is connected to the oil inlet pipe of the turbocharger, and this oil inlet vibe is equipped with a check valve upstream of the confluence with the piping to prevent the pressure air from flowing when it is jetted out. The bearing protection device according to claim 1i2, characterized in that it is capable of preventing backflow toward the upstream side. 4. The above-mentioned shutoff valve is an electromagnetic connection valve having a solenoid, and the solenoid is energized to close the shutoff valve when the engine key switch is ON, and demagnetized to open the shutoff valve when the key switch is OFF. The bearing maintenance II device according to claim 3, characterized in that the bearing maintenance II device is capable of 5. A delay circuit is inserted between the engine key switch and the solenoid, so that the K11 cutoff valve opens after a predetermined period of time after the engine stops, and the pressure air is spouted out. The scope of patent claims! Bearing maintenance device according to item 4.
JP57014752A 1982-02-03 1982-02-03 Bearing protector of turbocharger Granted JPS58133425A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57014752A JPS58133425A (en) 1982-02-03 1982-02-03 Bearing protector of turbocharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57014752A JPS58133425A (en) 1982-02-03 1982-02-03 Bearing protector of turbocharger

Publications (2)

Publication Number Publication Date
JPS58133425A true JPS58133425A (en) 1983-08-09
JPH0335497B2 JPH0335497B2 (en) 1991-05-28

Family

ID=11869832

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57014752A Granted JPS58133425A (en) 1982-02-03 1982-02-03 Bearing protector of turbocharger

Country Status (1)

Country Link
JP (1) JPS58133425A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6045723A (en) * 1983-08-22 1985-03-12 Hitachi Ltd Exhaust turbine system supercharger
KR20030020115A (en) * 2001-09-03 2003-03-08 현대자동차주식회사 Device for turbo charger protect of engine in vehicle
KR100399177B1 (en) * 2000-11-29 2003-09-22 기아자동차주식회사 Sticking Prevention System of Turbo Charger Bearing by Time Control for Engine Output Increane
KR100402174B1 (en) * 2000-12-19 2003-10-17 기아자동차주식회사 lubricating system for turbo chager of a deisel vehicle

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6045723A (en) * 1983-08-22 1985-03-12 Hitachi Ltd Exhaust turbine system supercharger
JPH0515900B2 (en) * 1983-08-22 1993-03-02 Hitachi Ltd
KR100399177B1 (en) * 2000-11-29 2003-09-22 기아자동차주식회사 Sticking Prevention System of Turbo Charger Bearing by Time Control for Engine Output Increane
KR100402174B1 (en) * 2000-12-19 2003-10-17 기아자동차주식회사 lubricating system for turbo chager of a deisel vehicle
KR20030020115A (en) * 2001-09-03 2003-03-08 현대자동차주식회사 Device for turbo charger protect of engine in vehicle

Also Published As

Publication number Publication date
JPH0335497B2 (en) 1991-05-28

Similar Documents

Publication Publication Date Title
US4884406A (en) Turbocharger
US9447753B2 (en) Blow-by gas ventilation device
US4422295A (en) Lubricating system for turbo-chargers
JP2012215155A (en) Blowby gas returning apparatus for engine with supercharger
JP4057522B2 (en) Turbocharger for 2-stroke diesel engine
US4679992A (en) Turbo-compound compressor system
JPS58133425A (en) Bearing protector of turbocharger
JPS58135325A (en) Lubricating mechanism for supercharger
JPS59113236A (en) Supercharger protecting apparatus for supercharged engine
JP2005009434A (en) Oil leakage preventing device for turbo supercharger
JPH06212939A (en) Blow-by gas cooler
JP2009287513A (en) Supercharger
JPH0893490A (en) Lubricating device of turbocharger
JP6211367B2 (en) Supercharger cleaning device, supercharger provided with the same, internal combustion engine provided therewith, and supercharger cleaning method
JPH0882220A (en) Turbo charger
KR0121376Y1 (en) Prevention device of positive pressure in an engine
KR950008312Y1 (en) Lubricating maintaining device for super charger
KR960005060Y1 (en) Protection apparatus of turbo-charger
KR100388200B1 (en) Apparatus for controlling an idling of exhaust gas turbo-charger using air pressure circuit
KR20030039470A (en) Icing prevention apparatus of PCV hose
KR100208757B1 (en) Apparatus for preventing of overheating in a turbo-charger engine
JPS60216092A (en) Starting load reducer for screw compressor
KR101848564B1 (en) Breathing-system of engine for vehicle
KR100412615B1 (en) Lubricant apparatus for turbo charger when engine start
JPS6045723A (en) Exhaust turbine system supercharger