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JPS6157931B2 - - Google Patents
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JPS6157931B2 - - Google Patents

Info

Publication number
JPS6157931B2
JPS6157931B2 JP14131682A JP14131682A JPS6157931B2 JP S6157931 B2 JPS6157931 B2 JP S6157931B2 JP 14131682 A JP14131682 A JP 14131682A JP 14131682 A JP14131682 A JP 14131682A JP S6157931 B2 JPS6157931 B2 JP S6157931B2
Authority
JP
Japan
Prior art keywords
oil
engine
expansion chamber
oil pan
turbine shaft
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
JP14131682A
Other languages
Japanese (ja)
Other versions
JPS5932621A (en
Inventor
Noryuki Kurio
Tatsuya Kida
Sanehiro Yamamoto
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.)
Matsuda KK
Original Assignee
Matsuda KK
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 Matsuda KK filed Critical Matsuda KK
Priority to JP14131682A priority Critical patent/JPS5932621A/en
Publication of JPS5932621A publication Critical patent/JPS5932621A/en
Publication of JPS6157931B2 publication Critical patent/JPS6157931B2/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)

Abstract

PURPOSE:To securely lubricate a turbine shaft, by a method wherein an expansion chamber maintained substantially at the atmospheric pressure is provided which is substantially shielded from the interior space of an engine casing below a piston, and the expansion chamber is communicated with an oil return passage. CONSTITUTION:A turbosupercharger 8 is provided, a lubricating oil contained in an oil pan 21 provided at the lower part of an engine casing 11 is fed to a turbine shaft 14, and thereafter the oil is returned to the oil pan 21 through an oil return passage 25. In said engine, the expansion chamber 26 maintained at approximately atmospheric pressure is provided which is communicated to the interior of the oil pan 2 and substantially shielded from the interior space A of the engine casing 11 below the piston 5 so that it is not affected by variations of the pressure inside the space A, and the chamber 26 is communicated to the passage 25. Accordingly, the lubricating oil can be returned to the oil pan side irrespectively of the variations in the pressure of a blow-by gas, and the turbine shaft 14 can be securely lubricated.

Description

【発明の詳細な説明】 本発明は、エンジンの排気ガスによつて駆動さ
れ、エンジンに過給気を供給するターブ過給機を
備えたエンジンの潤滑装置、特にターボ過給機の
タービン軸を潤滑する潤滑構造の改良に関するも
のである。
DETAILED DESCRIPTION OF THE INVENTION The present invention provides a lubricating device for an engine equipped with a turbocharger that is driven by engine exhaust gas and supplies supercharging air to the engine, and in particular a lubricating device for a turbine shaft of a turbocharger. This invention relates to improvements in lubrication structures.

従来、上記ターボ過給機のタービン軸に潤滑油
を供給する構造として、特開昭51−140013号公報
には、エンジンに駆動されるオイルポンプとは別
個の電動オイルモータによつてエンジンの始動時
等にターボ過給機に潤滑油を供給し、供給した潤
滑油を上記オイルタンクに回収する構造が開示さ
れている。
Conventionally, as a structure for supplying lubricating oil to the turbine shaft of the above-mentioned turbocharger, Japanese Patent Laid-Open No. 140013/1983 discloses a structure in which the engine is started using an electric oil motor that is separate from the oil pump driven by the engine. A structure is disclosed in which lubricating oil is supplied to the turbocharger at certain times, and the supplied lubricating oil is collected into the oil tank.

しかしながら、上記の構造は、エンジンケース
の下方に設けたオイルパン内の潤滑油をターボ過
給機のタービン軸に送給した後、オイルリターン
通路を介して潤滑油をオイルパン内に回収する潤
滑方式ゆえに、以下に説明するように、タービン
軸への潤滑が不足する問題がある。
However, in the above structure, the lubricating oil in the oil pan provided below the engine case is sent to the turbine shaft of the turbocharger, and then the lubricating oil is recovered into the oil pan via the oil return passage. Because of this system, there is a problem of insufficient lubrication to the turbine shaft, as will be explained below.

即ち、オイルリターン通路が連通するピストン
下方のエンジンケーシングの内部は、燃焼室(作
動室)から洩出するブローバイガスや、ピストン
の上下動による圧力変動が生じ、この圧力変動は
そのままオイルリターン通路にも作用するため、
タービン軸の潤滑に使用された潤滑油が円滑にオ
イルパン側に還流されなくなりタービン軸の潤滑
が不足する問題がある。
In other words, inside the engine casing below the piston with which the oil return passage communicates, pressure fluctuations occur due to blow-by gas leaking from the combustion chamber (working chamber) and the vertical movement of the piston, and this pressure fluctuation is directly transferred to the oil return passage. also acts,
There is a problem in that the lubricating oil used to lubricate the turbine shaft is not smoothly returned to the oil pan side, resulting in insufficient lubrication of the turbine shaft.

本発明は、かかる問題を解消すべくなされたも
のであつて、タービン軸の潤滑に使用された潤滑
油をオイルリターン通路を介して円滑に、即ちブ
ローバイガスによるクランクケース内の圧力変動
に無関係に、オイルパン内に還流させることがで
きるターボ過給機付エンジンの潤滑装置を提供す
ることを目的としている。
The present invention was made in order to solve this problem, and it is an object of the present invention to smoothly distribute the lubricating oil used for lubrication of the turbine shaft through the oil return passage, that is, without regard to pressure fluctuations in the crankcase due to blow-by gas. The object of the present invention is to provide a lubricating device for a turbocharged engine that allows the oil to flow back into the oil pan.

このため、本発明においては、エンジンケーシ
ングの下方に設けたオイルパン内部に連通し、か
つピストン下方のエンジンケーシング内部空間の
圧力変動を受けないように該エンジンケーシング
内部空間とは油面上部が実質的に隔離されたほぼ
大気圧の拡張室を設け、この拡張室と上記オイル
リターン通路とを連通したことを特徴としてい
る。
Therefore, in the present invention, the oil pan is connected to the inside of the oil pan provided below the engine casing, and the upper part of the oil level is substantially different from the engine casing inner space so as to avoid pressure fluctuations in the engine casing inner space below the piston. The present invention is characterized in that an expansion chamber at approximately atmospheric pressure that is isolated from the outside is provided, and the expansion chamber and the oil return passage are communicated with each other.

以下、図示の実施例に基づいて本発明をより具
体的に説明する。
Hereinafter, the present invention will be described in more detail based on illustrated embodiments.

図面において、1はシリンダ本体2とシリンダ
ヘツド3と、シリンダ本体2上部のシリンダボア
4内を上下方向に往復運動するピストン5と、ピ
ストン5の往復運動をコネクテイングロツド6を
介して回転出力として取り出すクランクシヤフト
7とを基本構成要素とするエンジンで、このエン
ジン1には、過給気を供給するためのターボ過給
機8を設けている。
In the drawing, 1 indicates a cylinder body 2, a cylinder head 3, a piston 5 that reciprocates vertically within a cylinder bore 4 at the top of the cylinder body 2, and a system that converts the reciprocating motion of the piston 5 into rotational output via a connecting rod 6. The engine 1 has a crankshaft 7 as a basic component, and is equipped with a turbo supercharger 8 for supplying supercharging air.

このターボ過給機8は、吸気通路9と排気通路
10とが互いに接近して平行する部分にそのケー
シング11が取付けられ、排気通路10を流下す
る排気ガスによつて駆動されるタービン12の回
転を、一対の軸受13,13によつて軸受したタ
ービン軸14を介して、吸気通路9に臨ませたブ
ロア15に伝達し、このブロア15で吸気を昇圧
し、過給気をエンジン1の燃焼室16に供給す
る。上記吸、排気通路9,10は、夫々エンジン
1の回転に同期して適当なタイミングで作動され
る吸、排気弁17,18によつて開閉される吸、
排気ポート19,20に夫々連結されている。
This turbo supercharger 8 has a casing 11 attached to a portion where an intake passage 9 and an exhaust passage 10 are close to each other and parallel to each other, and a turbine 12 is rotated by exhaust gas flowing down the exhaust passage 10. is transmitted to a blower 15 facing the intake passage 9 via a turbine shaft 14 supported by a pair of bearings 13, 13. Supply to chamber 16. The intake and exhaust passages 9 and 10 are opened and closed by intake and exhaust valves 17 and 18, respectively, which are operated at appropriate timing in synchronization with the rotation of the engine 1.
They are connected to exhaust ports 19 and 20, respectively.

一方、21はシリンダ本体2のスカート部2a
(ピストン5下方のエンジンケーシング)の下端
フランジ部2bに上縁フランジ部21aを固定し
たオイルパンで、内部には適量の潤滑油を収容
し、エンジン1の各潤滑部に必要な潤滑油の供給
を行なう。この潤滑油の供給は、具体的に図示し
ないが、エンジン1により駆動されるオイルポン
プによつて行ない、ターボ過給機8のタービン軸
14の潤滑のためには、シリンダヘツド3内のオ
イル通路22に一端を連通したオイル供給通路2
3を設け、このオイル送給通路23の他端を、タ
ーボ過給機8の一対の軸受13,13間に形成さ
れたオイルジヤケツト24に連通させている。
On the other hand, 21 is a skirt portion 2a of the cylinder body 2.
The oil pan has an upper edge flange 21a fixed to the lower end flange 2b (of the engine casing below the piston 5), and stores an appropriate amount of lubricating oil inside, supplying the lubricating oil necessary for each lubricating part of the engine 1. Do this. Although not specifically shown, this lubricating oil is supplied by an oil pump driven by the engine 1, and in order to lubricate the turbine shaft 14 of the turbocharger 8, an oil passage in the cylinder head 3 is supplied. Oil supply passage 2 with one end communicating with 22
3, and the other end of this oil feed passage 23 is communicated with an oil jacket 24 formed between a pair of bearings 13, 13 of the turbo supercharger 8.

図面に示すように、上記オイルジヤケツト24
内のタービン軸14の潤滑に使用された潤滑油
は、オイルリターン通路25によつて上記オイル
ジヤケツト24からオイルパン21側に還流させ
る。
As shown in the drawing, the oil jacket 24
The lubricating oil used to lubricate the turbine shaft 14 inside is returned from the oil jacket 24 to the oil pan 21 side through the oil return passage 25.

このオイルリターン通路25の下端は、本発明
では、オイルパン21の内部と連通する拡張室2
6の上部に連通させている。この拡張室26は、
本実施例では、オイルパン21の側壁の一部を側
方に膨出した膨出壁部27と、この膨出壁部27
とオイルパン21側とを仕切る仕切壁28と、シ
リンダ本体2の下端フランジ部2bを側方に突出
させた突出壁29とによつて1つの閉空間として
形成する。上記仕切壁28は、拡張室26をピス
トン5下方のエンジンケーシングの内部空間Aと
は実質的に隔離するように、スカート部2aの下
端フランジ部2bの下面まで伸び、下端側には、
拡張室26の底部とオイルパン21の底部とを部
分的に連通する絞り連通口30を設けている。
In the present invention, the lower end of this oil return passage 25 is connected to an expansion chamber 2 communicating with the inside of the oil pan 21.
It communicates with the upper part of 6. This expansion chamber 26 is
In this embodiment, a part of the side wall of the oil pan 21 is provided with a bulged wall portion 27 that bulges out laterally, and this bulged wall portion 27.
A closed space is formed by a partition wall 28 that partitions the cylinder body 2 and the oil pan 21 side, and a protrusion wall 29 that protrudes the lower end flange portion 2b of the cylinder body 2 laterally. The partition wall 28 extends to the lower surface of the lower end flange portion 2b of the skirt portion 2a so as to substantially isolate the expansion chamber 26 from the internal space A of the engine casing below the piston 5.
A throttle communication port 30 is provided that partially communicates the bottom of the expansion chamber 26 and the bottom of the oil pan 21.

また、拡張室26は、前記突出壁29の取付穴
に基部を差し込んだ大気連通用パイプ31によつ
て大気と連通させ、これによつて拡張室26の内
圧を大気圧に維持するようにしている。
Further, the expansion chamber 26 is communicated with the atmosphere through an atmosphere communication pipe 31 whose base is inserted into a mounting hole of the protruding wall 29, thereby maintaining the internal pressure of the expansion chamber 26 at atmospheric pressure. There is.

上記の構成では、したがつて、拡張室26の内
圧が大気圧に維持されるため、オイルリターン通
路25の下端側には大気圧が常時作用し、ターボ
過給機8のオイルジヤケツト24のオイル圧は、
潤滑油がオイルポンプより送給されており、大気
圧よりは高いため潤滑油はスムーズに拡張室26
内に還流される。即ち、オイルリターン通路25
は、ピストン5下方のエンジンケーシング内空間
Aにおいて生じうる圧力変動の影響を何んら受け
ることなしに、潤滑油を還流することができ、オ
イルジヤケツト24において潤滑油の送給量と還
流量とがバランスして、タービン軸14を有効に
潤滑することができる。
In the above configuration, the internal pressure of the expansion chamber 26 is maintained at atmospheric pressure, so atmospheric pressure always acts on the lower end side of the oil return passage 25, and the oil jacket 24 of the turbocharger 8 The oil pressure is
The lubricating oil is supplied by an oil pump, and since the pressure is higher than atmospheric pressure, the lubricating oil flows smoothly into the expansion chamber 26.
It is refluxed into the interior. That is, the oil return passage 25
The lubricating oil can be recirculated without being affected by pressure fluctuations that may occur in the engine casing internal space A below the piston 5, and the lubricating oil supply amount and recirculation amount can be adjusted in the oil jacket 24. With this balance, the turbine shaft 14 can be effectively lubricated.

また、拡張室26に還流された潤滑油は、絞り
開口30を通してオイルパン21に返される。こ
の場合、絞り開口30を通して、ピストン5下方
のエンジンケーシング内部空間Aの圧力変動が、
潤滑油の流通として伝達される可能性があるが、
絞り開口30はその絞り効果によつて上記の圧力
変動を実質的に遮断することができるので問題は
ない。
Furthermore, the lubricating oil returned to the expansion chamber 26 is returned to the oil pan 21 through the throttle opening 30. In this case, the pressure fluctuation in the engine casing internal space A below the piston 5 is caused through the throttle opening 30.
Although it may be transmitted through the distribution of lubricating oil,
There is no problem because the diaphragm opening 30 can substantially block the above-mentioned pressure fluctuation due to its diaphragm effect.

本発明は、以上説明した実施例の構造に限定さ
れるものではない。
The present invention is not limited to the structure of the embodiment described above.

例えば、前記仕切壁28は、ピストン5下方の
エンジンケーシング内部空間Aと拡張室26とを
完全に仕切る必要はなく、上記絞り開口30はオ
イルパン底面から潤滑油の油面の若干上方まで開
口して、該油面と絞り開口の上縁部との間に小間
隙ができるようにしてもよく、要するに上記内部
空間Aの圧力変動を緩和してオイルリターン通路
25の圧力変動の悪影響を及ぼさないものであれ
ばよい。また、大気連通用パイプ31は、必らず
しも必要でなく、拡張室26の内圧が大気圧より
高い所定圧に達したときにのみ、内圧をリリーフ
するリリーフ機能を備えた部材を用い、拡張室2
6の内圧を潤滑油の還流に支障を生じない程度の
圧力に維持するようにすればよい。さらに、拡張
室26を形成する部位も前記実施例に限られるも
のでない。
For example, the partition wall 28 does not need to completely partition the engine casing internal space A below the piston 5 from the expansion chamber 26, and the throttle opening 30 may open from the bottom of the oil pan to slightly above the lubricating oil level. In other words, a small gap may be formed between the oil level and the upper edge of the throttle opening, in short, pressure fluctuations in the internal space A are alleviated and pressure fluctuations in the oil return passage 25 do not have an adverse effect. It is fine as long as it is something. In addition, the atmospheric communication pipe 31 is not necessarily necessary, and a member having a relief function that relieves the internal pressure only when the internal pressure of the expansion chamber 26 reaches a predetermined pressure higher than atmospheric pressure is used. Expansion room 2
6 may be maintained at a level that does not interfere with the recirculation of the lubricating oil. Furthermore, the portion where the expansion chamber 26 is formed is not limited to the above embodiment.

以上の説明から明らかなように、本発明によれ
ば、油圧上部がピストン下方のエンジンケーシン
グ内部空間と実質的に隔離されたほぼ大気圧の拡
張室を設けて、この拡張室にタービン軸の潤滑に
送給された潤滑油のオイルリターン通路を連通し
たから、潤滑油をブローバイガスによる圧力変動
に無関係にオイルパン側に還流されることがで
き、タービン軸の潤滑を確保することができる。
As is clear from the above description, according to the present invention, an expansion chamber at approximately atmospheric pressure is provided in which the hydraulic upper part is substantially isolated from the internal space of the engine casing below the piston, and the expansion chamber is used to lubricate the turbine shaft. Since the oil return passage for the lubricating oil supplied to the engine is communicated with the lubricating oil, the lubricating oil can be returned to the oil pan side regardless of pressure fluctuations caused by blow-by gas, and lubrication of the turbine shaft can be ensured.

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

図面は本発明にかかるターボ過給機付エンジン
の潤滑装置を示すエンジンの垂直断面説明図であ
る。 1……エンジン、2……シリンダ本体、8……
ターボ過給機、21……オイルパン、23……オ
イル送給通路、25……オイルリターン通路、2
6……拡張室、A……ピストン下方のエンジンケ
ーシング内部空間。
The drawing is an explanatory vertical cross-sectional view of an engine showing a lubricating device for a turbocharged engine according to the present invention. 1...Engine, 2...Cylinder body, 8...
Turbo supercharger, 21...Oil pan, 23...Oil feed passage, 25...Oil return passage, 2
6... Expansion chamber, A... Engine casing internal space below the piston.

Claims (1)

【特許請求の範囲】 1 ターボ過給機を備え、エンジンケーシングの
下方に設けたオイルパン内の潤滑油をターボ過給
機のタービン軸に送給した後、オイルリターン通
路を介してオイルパンに還流するようにしたエン
ジンにおいて、 オイルパン内部に連通し、かつピストン下方の
エンジンケーシング内部空間の圧力変動を受けな
いように該エンジンケーシング内部空間とは油面
上部が実質的に隔離されたほぼ大気圧の拡張室を
設け、この拡張室と上記オイルリターン通路とを
連通したことを特徴とするターボ過給機付エンジ
ンの潤滑装置。
[Claims] 1. A turbocharger is provided, and after lubricating oil in an oil pan provided below an engine casing is supplied to a turbine shaft of the turbocharger, the lubricating oil is sent to the oil pan via an oil return passage. In an engine designed for recirculation, there is an approximately large area that communicates with the inside of the oil pan and is substantially separated from the internal space of the engine casing below the piston so as to avoid pressure fluctuations in the internal space of the engine casing. A lubricating device for a turbocharged engine, characterized in that an air pressure expansion chamber is provided, and the expansion chamber communicates with the oil return passage.
JP14131682A 1982-08-14 1982-08-14 Lubricator for engine with turbosupercharger Granted JPS5932621A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14131682A JPS5932621A (en) 1982-08-14 1982-08-14 Lubricator for engine with turbosupercharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14131682A JPS5932621A (en) 1982-08-14 1982-08-14 Lubricator for engine with turbosupercharger

Publications (2)

Publication Number Publication Date
JPS5932621A JPS5932621A (en) 1984-02-22
JPS6157931B2 true JPS6157931B2 (en) 1986-12-09

Family

ID=15289068

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14131682A Granted JPS5932621A (en) 1982-08-14 1982-08-14 Lubricator for engine with turbosupercharger

Country Status (1)

Country Link
JP (1) JPS5932621A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6136135U (en) * 1984-08-06 1986-03-06 ダイハツ工業株式会社 Turbo charger piping equipment
GB8625715D0 (en) * 1986-10-28 1986-12-03 British Nuclear Fuels Plc Colloidal grout mixing apparatus
US8621865B2 (en) * 2010-05-04 2014-01-07 Ford Global Technologies, Llc Internal combustion engine with liquid-cooled turbine

Also Published As

Publication number Publication date
JPS5932621A (en) 1984-02-22

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