JPS5932621A - Lubricator for engine with turbosupercharger - Google Patents

Lubricator for engine with turbosupercharger

Info

Publication number
JPS5932621A
JPS5932621A JP14131682A JP14131682A JPS5932621A JP S5932621 A JPS5932621 A JP S5932621A JP 14131682 A JP14131682 A JP 14131682A JP 14131682 A JP14131682 A JP 14131682A JP S5932621 A JPS5932621 A JP S5932621A
Authority
JP
Japan
Prior art keywords
oil
engine
pressure
expansion chamber
oil pan
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
JP14131682A
Other languages
Japanese (ja)
Other versions
JPS6157931B2 (en
Inventor
Noriyuki Kurio
憲之 栗尾
Tatsuya Kida
達也 喜田
Sanehiro Yamamoto
山本 修弘
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.)
Mazda Motor Corp
Original Assignee
Mazda Motor Corp
Toyo Kogyo 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 Mazda Motor Corp, Toyo Kogyo Co Ltd filed Critical Mazda Motor Corp
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

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】 不弁明は、エンジンのυ1気ガスによって駆動さft、
エンジン・(/C過給気を(4(給Tるターボ過給機金
ターピノ軸ケ潤潅(4す造の改良に閏する)のでるる。
DETAILED DESCRIPTION OF THE INVENTION The indefensible engine is powered by υ1 air gas,
Engine /C Supercharged air is supplied to the turbo supercharger (to improve the 4-wheel structure).

従来、上記ターボ過給機のターピン軸に潤l’+Q 7
141を供給する構造として、特開昭5l−14(JO
13号公報には、エンジンとは別個に攬り一/こ:A−
d /レタンク刀・ら、エンジンl/7:駆動さ7しる
オイルJミンフ。
Conventionally, the turpin shaft of the above turbocharger was l'+Q7
As a structure for supplying 141, JP-A-5L-14 (JO
Publication No. 13 states that the engine is separated from the engine.
d/Retank sword et al. Engine l/7: Driven by 7 oil J minf.

とは別個の電動オイルモータによってエンジンの始動時
等にターボ過給機に潤屑油ケ供給し、イへ給した潤滑油
r上記号イルタンクに回収する構造か開示さ扛ている。
A structure is disclosed in which a separate electric oil motor supplies lubricating oil to the turbo supercharger at engine startup, etc., and collects the lubricating oil supplied to the lubricating oil tank.

し77)しながら、上記の構造は、エンジンのl閏l骨
装置の多系統化ケ招来する9え、エンジンク−−シンク
の1゛力Vc設rJ7ζオイルパン円の/[V] i骨
l出を消yl 71iH↑が妃・要7i:全ての個Iツ
rに供給する型式のエンジンの@肩装置には個用し難い
問題があった。
77) However, the above structure leads to multisystemization of the engine laryngeal device. Eliminate output 71iH↑ is important 7i: There was a problem with the @shoulder device of the engine that supplies all the units.

ところで、上記のよf)に、エンシンケースノ1一方に
設り−たオイルパン円のl閏l骨油γり一ホ過・m索の
ターピン軸に広紺した後、オーイノトリター2曲路を弁
して潤l骨1t11葡オイルパン内に巳l又するl閏l
骨力式では、以下VC呪明するように、タ〜ヒン軸への
@19が不足する問題がりる。
By the way, as described in f) above, after spreading the laryl bone oil of the oil pan circle installed on one side of the engine case no. 1 t 11 1 t 1 1 1 1 1 1 1 1 1 1 1 1
In the bone strength type, there is a problem of insufficient @19 to the Tahin axis, as described below by VC.

即ち、A−イルリターン通路が連通するピストン7=方
のエンジンケーシングの内部は、燃焼W(fγ動V)か
ら洩出する10−バイガスや、ピストンのn−1゛動に
よる圧カ父勤が生じ、この圧カ斐wJばその−f !万
イルリターン利路にも1g用するため、タービン軸の潤
滑にイ史用さn−たl閏/骨油が円滑にオイル/(ン[
111K還流さ71なくなりタービン軸の潤mがイ・足
する問題かめる。
That is, inside the engine casing on the side of the piston 7 with which the A-il return passage communicates, there is 10-by gas leaking from the combustion W (fγ movement V) and pressure exertion due to the n-1 movement of the piston. This pressure wJ Baso-f! Since 1g is also used for every return route, it is used to lubricate the turbine shaft.
111K reflux is eliminated and the turbine shaft moisture is added to the problem.

本発明は、かかる141題を解消すべぐlさnたもので
あって、タービン軸の潤7′骨に使用さnた潤/骨油ケ
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円の辻カ変動に−jICil 
(糸に、万イルパン内に通流させることかでさるターボ
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 has been made to solve these 141 problems, and the lubricant/bone oil used in the lubricant 7' bone of the turbine shaft can be smoothly removed through the oil return passage, that is, by blow-by gas. Changes in the power of the crankcase circle - jICil
(The purpose is to provide a lubricating device for a turbocharged engine in which a thread is passed through a million oil pan.)

この1こめ、本発明におV)ては、エンジンケーシング
下方に設けたオイルパン内部に連通し、かつピストン下
刃のエンジンケーシング内の圧カ変動ケ父けないように
該エンジンケース内部とは実質的に隔離されたは91人
気圧の拡張室金膜け、この拡張¥にタービン軸に送給し
たt閏屑油のオイルリターン通路全連通させ、オイルリ
ターン通路ケピストン1゛一方の工/ジンケーシンク同
部の圧力に!IUJに対して天貿t+XJに隔離(−1
こことケ基本的な特徴としている。
In addition, in V) of the present invention, the piston lower blade communicates with the inside of the oil pan provided below the engine casing, and is connected to the inside of the engine case so as to prevent pressure fluctuations in the engine casing of the piston lower blade. The expansion chamber is practically isolated with a gold film at 91 atmospheric pressure, and the oil return passage for the scrap oil fed to the turbine shaft is fully connected to this expansion chamber, and the oil return passage is connected to the piston 1 on one side. Due to pressure from the department! Isolated by Tenmao t+XJ against IUJ (-1
These are the basic features.

以下、図示の実施例に基ついて不発明夜より1、俸的に
脱明する。
Hereinafter, based on the illustrated embodiment, the invention will be briefly explained.

図m]ニおいて、1はシリンダ本体2とシリンタヘッド
3と、シリンタネ俸2上部のシリンダポア4内を上下方
向に任1す連動するビス1−ン5と、ビ、l l−ン5
の任復連動忙コネクテインクロツト6’<弁L1回転出
力として取り吊子りランクシー\tノド7とを基本1苫
成υさ系とするエンジンで、このコーンジン1には、過
槍気を供給゛するためのターホノ1ω1附機8を設けて
いる。
In Fig. m], 1 is a cylinder main body 2, a cylinder head 3, a screw 1-5 which interlocks with the cylinder pore 4 in the upper part of the cylinder cylinder 2 in the vertical direction, and a screw 1-5 which moves in the vertical direction.
It is an engine that has a basic 1 tomariness system with the rotational output of the connecting connector 6'<valve L1 and the rotational output of the valve L1. A turret 1 ω 1 auxiliary machine 8 is provided for supplying the water.

このターホ過、胎磯8は、吸気連路9とリド気連路10
とが互いに接近して平?イする部分にそのケーシング1
1が取付けLっれ、t811:気迫路IC1i流1−す
る排気カスによって駆動きれるタービン12の1川転r
、一対の軸受13,13によって軸受1,7ζタービン
軸14を介して、吸気連路9に臨ませたプロア15に伝
達し、このプロア15で吸気ヲ昇圧し、過給気ケエンジ
ン1の燃焼室16に供給する。
This Taho passage, the uterus 8 is the intake passage 9 and the lid air passage 10.
Are they close to each other? the casing 1
1 is installed L, t811: 1 river rotation r of the turbine 12 that can be driven by the exhaust gas flowing through the pressure path IC1i flow 1-
, is transmitted by a pair of bearings 13, 13 through the bearings 1, 7ζ turbine shaft 14 to the proar 15 facing the intake air passage 9, and the proar 15 boosts the pressure of the intake air, causing combustion in the supercharged engine 1. Supply to chamber 16.

」二記吸、排気通路9.lOば、大役エンジン1の回転
に向J4J+ L 1 過当なタイミンクで作動さ汎る
吸。
”2 Suction and exhaust passages 9. If it is, J4J+ L1 will be activated at an unreasonable timing as the main engine 1 rotates.

υト気力47.18によって開閉される吸、排気ボー1
−19.20VC大々m 結−a 、t’t −r−イ
ル。
Suction and exhaust bows opened and closed by υto energy 47.18
-19.20VC large m-a, t't-r-yl.

一方、21はシリンダ本体2のスカー) m 2 a(
ピストン5下刃のエンジンケーシングl)下端フ・7ン
シ部21)に上縁フランン部211を固定したA”イル
パンで、内部には通ボの潤滑油を収容し、エンジノ1の
各囮18′1部に必’B: 7r A−’17□1″目
11の供給會行なう。この11♀1rit油の供給は1
,1−1一体向に図示しないが、j−ンシン1により駆
動芒11−るオイルポンプに」、1」−Cイー1ない、
ターボ過給機8のタービンl1lIll14の?閑l′
i′iの7fこめ(/i−ば、シリフタヘッド13円の
オイル1lfl路22に一端ケ連通し7こオイル送給通
路23を設け、このAイル進相通路23の1142端勿
、ターナji−4)楕磯8の一対の軸受13,13間に
形成されたオイルシA′ケット24に連通さ、+!:て
いる。
On the other hand, 21 is the scar of the cylinder body 2) m 2 a (
The engine casing of the lower blade of the piston 5 is an A" tile pan in which the upper edge flange part 211 is fixed to the lower end flange part 21). 1st part requires 'B: 7r A-'17□1'' 11th supply meeting. The supply of this 11♀1rit oil is 1
, 1-1 is not shown in the figure, but the oil pump driven by the engine 1 is connected to the oil pump 11-1.
Turbine l1lIll14 of turbocharger 8? quiet time
i'i's 7f (/i-), a 7 oil feed passage 23 is provided, one end of which communicates with the oil 11 fll passage 22 of the cylinder head 13, and the 1142nd end of this A oil phase advancement passage 23, of course, the turner ji- 4) Communicates with the oil seal A'ket 24 formed between the pair of bearings 13, 13 of the oval rock 8, +! :ing.

図面に示すように、上記オイルジャケット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
ン連路25によって」−、ir[:!yr’イルジャケ
ット24刀)ら万イル/(ン21狽りに還流させる。
As shown in the drawings, the lubricating oil used for lubrication of the turbine shaft 14 in the oil jacket 24 is transferred through the oil return passage 25. yr'iljacket 24 swords) and 10,000 il/(n 21 swords) to return to.

このオーイルリターン連路25の下端は、不光明テハ、
A−イルy<ン21の内部と連Juiする拡張’J 2
6の上部に部曲込ぜている。この拡張室26は、木実施
例では、万イルパン21の側壁の一部を倶j方壁 イルパン211jl!+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を仰j方に契出させ7
こ突出壁29とによって1つの閉空間として形成する。
The lower end of this oil return passage 25 is
A-Extension 'J 2 connected to the interior of y<n21
The upper part of 6 is bent. In the wooden embodiment, this expansion chamber 26 includes a part of the side wall of the multi-purpose pan 21. + and the lower end flange portion 2b of the cylinder body 2 are exposed upward in the direction 7
This projecting wall 29 forms one closed space.

上記仕切壁28は、拡張室26盆ピストン5下方のエン
ジンケーシングの円部イシ間A、:は実質的に隔部する
ように、スカー1− HB 2 aの13端ノフンシ部
2bの下面4で伸び、下端側には、拡張室26の、1底
部と万イルパン21の1氏部とr部分的に部」川する絞
り連通口30?設けている。
The partition wall 28 is arranged at the lower surface 4 of the 13th end notch part 2b of the scar 1-HB2a so that the expansion chamber 26 and the circular part A of the engine casing below the piston 5 are substantially separated. At the lower end side, there is an aperture communication port 30 that connects the bottom part of the expansion chamber 26, the part 1 part of the pan 21, and the r part. It is set up.

また、拡張室26は、hIJ記突出壁29の杷fzI穴
に基部業差し込んだ人気連通用パイプ:31によって人
気と連通させ、これによって拡張室2(50円圧を大気
圧に維持するようにしている。
In addition, the expansion chamber 26 is communicated with the expansion chamber 2 (50 yen pressure is maintained at atmospheric pressure) by means of a connecting pipe 31 inserted into the hole fzI of the protruding wall 29. ing.

1N己の構成では、し1こがって、拡張室26の内圧か
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f’lF用し、ターボ過給機8の
A゛イルシーVケツト24オイル圧ば、t’EI r’
!) 7出がオイルポンプより送給されて2シ、大気圧
よりは尚い1こめ潤滑油はスムーズに拡張室26円に還
流きれる。即ち、オイルリターン進路25は、ビス!・
ン5下方のエンジンゲージング17′]窄間八に2i−
いて生じつる圧力変動の影響?何んら受けることなしに
、l蘭h7油ケ還流することができ、オイルジャケット
24VCs、−いて潤/肯油の送給量と還流量とかバフ
ンヌして、タービン軸14金有効に?閑l骨することか
でさる。
In the 1N configuration, the internal pressure of the expansion chamber 26 is maintained at atmospheric pressure, so atmospheric pressure is always applied to the lower end of the oil return passage 25, and the turbo supercharger 8 A゛Il Sea V Butt 24 Oil Pressure, t'EI r'
! ) The lubricating oil is supplied from the oil pump and the lubricating oil is returned to the expansion chamber 26 yen smoothly. That is, the oil return path 25 is a screw!・
Engine gauging 17' below engine 5] 2i-
What is the effect of pressure fluctuations that occur? Is it possible to recirculate the llan h7 oil without any damage, and with the oil jacket 24VCs, the oil supply amount and recirculation amount can be adjusted to make the turbine shaft 14-karat gold effective? It's a monkey to be lazy.

11こ、拡張室26に還流された潤滑油は、紋り開1d
30’<1ii1シてオイルポンプ1に返される。この
場合、絞り開[、、] 30 (5通し−こ、ピストン
5下方のエンジンケーシング内部夕闇Aの圧力変動が、
tl’昭’A lt+]の流J出として伝達される可能
性かめるが、佼ジtj#J LT、’+ 30はその収
シ効果によって上記の圧力変動を大賀的に超動1−るこ
とかできるので問題にない。
11, the lubricating oil returned to the expansion chamber 26 is opened 1d
30'<1ii1 and is returned to the oil pump 1. In this case, the pressure fluctuation inside the engine casing A below the piston 5 is as follows:
Although there is a possibility that the above pressure fluctuation is transmitted as a flow J of tl'Sho'A lt+], the above-mentioned pressure fluctuation can be suppressed by the above pressure fluctuation due to its convergence effect. It's not a problem because it can be done.

木弁明は、以上読明した実施例の調造に限定されるもの
ではない。
Kibenmei is not limited to the preparation of the examples described above.

例えは、前把仕切壁28は、ピストン51・一方のエン
ジンケージジグ内部空間Aと拡張室26とケ完全に仕切
る必要はなく、上記絞り開口30はオイルパン1氏面か
ら潤l肯油の711j間の着干上方1で開口して、該油
面と炊9開口の上縁部との間に小114J隙かでさるよ
うにしてもよく、彼するに上記円ib空闇Aの圧力変w
Jヲ緩オ目して万イルリターンJ市路25に圧力変動の
悪′#曹r及ぼさないものでめ1%はよい。ぼた、人気
連通用バイグ31は、必らずしも必要でなく、拡張室2
6の内圧か人気圧より高い所定圧に達したとぎにのみ、
円圧孕リリーフするリリーフ機能オ備え1こ都F3を用
い、拡張室26の内圧會l閏/!を油の還流に支障を生
じない、1−1l′!度の圧力に維持するよりにすれは
よい。さらに、拡張¥26を形成する部位%) niJ
記実施例に限られるもので7i−い。
For example, the front partition wall 28 does not need to completely partition the piston 51/one engine cage jig internal space A from the expansion chamber 26, and the aperture opening 30 is used to draw water and oil from the surface of the oil pan 1. It may be opened at the upper part 1 of the drying area between 711j and a small 114J gap between the oil level and the upper edge of the cooking 9 opening. Weird lol
1% is good as long as it does not have any adverse effects on pressure fluctuations on Jichiro 25. However, the popular communication bike 31 is not necessarily necessary, and the expansion chamber 2
Only when a predetermined pressure higher than the internal pressure of 6 or the human pressure is reached,
Equipped with a relief function to relieve circular pressure, use the F3 to release the internal pressure of the expansion chamber 26. 1-1l' without causing any hindrance to oil reflux! It is better to maintain the pressure at a certain degree. In addition, the part that forms the expansion ¥26%) niJ
The invention is limited to the above embodiments.

Claims (1)

【特許請求の範囲】 (II  ターボ過給機會匍え、エンジンケーシングの
一1゛方に設けたオイルパン1同のl閏l骨l田をター
ボ過給機のタービン調に送給した後、オイルリターンJ
用路を介してオイルパンに還流するようにしたエンシ/
VCおいて、 オイルパン[7同部に連通し、かつピストン下方のエノ
シンケーシ/り内の圧力変動金受t−1ないように6!
2 ]−ンジノケース[η部とは実質的に隔離されたほ
ぼ人気圧の拡張¥を設け、この拡張堅と上記オイルリタ
ーン通路と?J−!4!曲(7たことt特徴とするター
ボッ青5)店す(浅付コニンジンのl閏l骨装置。
[Scope of Claims] (II. After the turbocharger is installed and the oil pan provided on one side of the engine casing is fed to the turbine of the turbocharger, oil return J
The engine is designed to flow back to the oil pan via a channel.
At the VC, the oil pan [7 is connected to the same part, and the pressure fluctuation receiver t-1 in the enoshin casing below the piston is 6!
2] - Engine case [provide an expansion unit with almost human pressure that is substantially isolated from the η section, and connect this expansion case with the above oil return passage? J-! 4! Songs (7 features of Turbo Blue 5) Stores (A shallow ginseng's laryngeal apparatus.
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 true JPS5932621A (en) 1984-02-22
JPS6157931B2 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)

Cited By (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
JPS63112107A (en) * 1986-10-28 1988-05-17 ブリティッシュ ニュークリア フュエルス ピーエルシー Method and device for mixing colloidal grout
US20120067306A1 (en) * 2010-05-04 2012-03-22 Ford Global Technologies, Llc Internal combustion engine with liquid-cooled turbine

Cited By (5)

* 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
JPH0212276Y2 (en) * 1984-08-06 1990-04-06
JPS63112107A (en) * 1986-10-28 1988-05-17 ブリティッシュ ニュークリア フュエルス ピーエルシー Method and device for mixing colloidal grout
US20120067306A1 (en) * 2010-05-04 2012-03-22 Ford Global Technologies, Llc Internal combustion engine with liquid-cooled turbine
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
JPS6157931B2 (en) 1986-12-09

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