JPS60138228A - Supercharger - Google Patents
SuperchargerInfo
- Publication number
- JPS60138228A JPS60138228A JP58244039A JP24403983A JPS60138228A JP S60138228 A JPS60138228 A JP S60138228A JP 58244039 A JP58244039 A JP 58244039A JP 24403983 A JP24403983 A JP 24403983A JP S60138228 A JPS60138228 A JP S60138228A
- Authority
- JP
- Japan
- Prior art keywords
- metal
- radial
- radial metal
- circlip
- supercharger
- 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.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/166—Sliding contact bearing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/12—Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load
- F16C17/18—Sliding-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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
- F16C35/02—Rigid support of bearing units; Housings, e.g. caps, covers in the case of sliding-contact bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/02—Sliding-contact bearings for exclusively rotary movement for radial load only
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2360/00—Engines or pumps
- F16C2360/23—Gas turbine engines
- F16C2360/24—Turbochargers
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Supercharger (AREA)
Abstract
Description
【発明の詳細な説明】
〔発明の利用分野〕
本発明は超高速回転のタービン及びコンプレッサを有す
る過給機に関するものである。DETAILED DESCRIPTION OF THE INVENTION [Field of Application of the Invention] The present invention relates to a supercharger having an extremely high-speed rotating turbine and compressor.
実開昭50−149710号公報にあるような過給機の
耐久性能は、ラジアルメタルの内径及び外径の摩耗量に
大きく影響される。摩耗を促進させる要因の一つに、ラ
ジアルメタルの黒化腐食があり、この対策として、耐黒
化腐食性の優れた銅合金が採用されつつある。しかし、
この銅合金は模様的な切削に弱く、タービン及び、コン
プレッサの微小アンバランスによるタービンロータ組立
体のふれ捷わりにより、スラスト方向の推力をうけると
、安易に端面が摩耗してし貰う不具合いが発生する。The durability of a supercharger as disclosed in Japanese Utility Model Application Publication No. 50-149710 is greatly influenced by the amount of wear on the inner diameter and outer diameter of the radial metal. One of the factors that accelerates wear is blackening corrosion of radial metal, and as a countermeasure to this problem, copper alloys with excellent blackening corrosion resistance are being adopted. but,
This copper alloy is susceptible to pattern cutting, and when subjected to thrust in the thrust direction due to fluctuations in the turbine rotor assembly caused by minute imbalances in the turbine and compressor, the end face easily wears out. Occur.
この摩耗は、ラジアルメタル端面が、メタルを支えるサ
ークリップ表面におしあてられ、サークリップが、構造
的に潤滑油膜を保持できないために発生するものである
。This wear occurs because the radial metal end face is pressed against the circlip surface that supports the metal, and the circlip is structurally unable to retain a lubricating oil film.
本発明の目的は耐黒化腐食性能に優れた銅合金メタルを
過給機に採用する場合、ラジアルメタル端面摩耗を防止
し、耐久性能を向上させるために必妥なラジアルメタル
軸受構造を提供することにある。The purpose of the present invention is to provide a radial metal bearing structure that is essential for preventing radial metal end face wear and improving durability when a copper alloy metal with excellent blackening corrosion resistance is used in a turbocharger. There is a particular thing.
本発明の%徴は超高速回転形過給機のラジアル方向の回
転を安定させる、フルフロートタイプのラジアルメタル
において、ラジアルメタル端面摩耗を、該メタルと、サ
ークリップの間に板状ワッシャを挿入し、メタル端面の
潤滑油膜きれを無く17、端面摩耗を防止した過給機に
ある。The % characteristic of the present invention is that in a full float type radial metal that stabilizes the radial rotation of an ultra-high-speed rotating supercharger, a plate washer is inserted between the radial metal end face wear and the circlip. However, there is no lubricating oil film on the metal end face17, which prevents wear on the end face.
図面において機関から排出された排気カス17が過給機
のタービンケース2に導かれ、タービン1を駆動して、
排出18される。タービン1と一体になったコンプレッ
サ11と、コンプレッサケース12により、空気が吸入
19され、機関に過給空気20を供給する。タービンの
高速回転のラジアル方向の動きを支えるため、2個のラ
ジアルメタル6が、サークリップ7によりlpHl受箱
5に収納されている。址だ、スラスト方向の動きを支え
るために、スラストメタル8がバックプレート9に挿入
されているスラストスプリング1oにより、軸受箱5に
押しつけられている。In the drawing, exhaust gas 17 discharged from the engine is led to the turbine case 2 of the supercharger, drives the turbine 1,
It is discharged 18. Air is taken in 19 by a compressor 11 integrated with the turbine 1 and a compressor case 12, and supercharged air 20 is supplied to the engine. In order to support the radial movement of the turbine at high speed, two radial metals 6 are housed in the lpHl receiving box 5 by a circlip 7. In order to support movement in the thrust direction, the thrust metal 8 is pressed against the bearing box 5 by a thrust spring 1o inserted into a back plate 9.
ぼた、機関の潤滑油は、入口21から軸受箱6に供給さ
れ、ラジアルメタル6、スラストメタル8を潤滑し、排
油22される。潤滑油の過給機外部への洩れについては
、タービン側は、ピストンリング4.コンプレッサ側は
、シートリング16と、メカニカルシール15によって
、シールを計っている。タービンが高速回転をするため
、微小なアンバランス量が発生すると、タービン1側筐
たはコンプレッサ11側がふれまわり、ラジアルメタル
6が、ある判定のスラスト方向に押しあてられ、サーク
リップ7の表面でこすられ、ラジアルメタルの端面が摩
耗してしまう不具合いが発生した。実開昭50−149
710号公報にあるようなラジアルメタル部の詳細につ
いて第2図および第3図に示す。サークリップ7は第2
図および第3図に示めす形状をしており、機関から供給
される潤滑油は、サークリップの断続部で排油されてし
まい、ラジアルメタル6とサークリップ7の間に油膜を
富に確保できなくなってしまう。Lubricant oil for the engine is supplied to the bearing box 6 from an inlet 21, lubricates the radial metal 6 and thrust metal 8, and is drained 22. Regarding leakage of lubricating oil to the outside of the supercharger, on the turbine side, piston ring 4. The compressor side is sealed by a seat ring 16 and a mechanical seal 15. Since the turbine rotates at high speed, when a slight unbalance occurs, the turbine 1 side casing or the compressor 11 side swings around, and the radial metal 6 is pushed in a determined thrust direction, causing the surface of the circlip 7 to A problem occurred where the end face of the radial metal was rubbed and worn. Jitsukai 50-149
Details of the radial metal part as disclosed in Japanese Patent No. 710 are shown in FIGS. 2 and 3. Circlip 7 is the second
The lubricating oil supplied from the engine is drained at the interrupted parts of the circlip, ensuring a rich oil film between the radial metal 6 and the circlip 7. I won't be able to do it.
そこで本発明では第4図および第5図に示すようにラジ
アルメタル6と板状ワッシャ30の間に潤滑油膜が確保
され、ラジアルメタルがある特定のスラスト方向に押し
あてられてもこの油膜により端面の摩耗は発生しない。Therefore, in the present invention, as shown in FIGS. 4 and 5, a lubricating oil film is secured between the radial metal 6 and the plate washer 30, and even when the radial metal is pressed in a certain thrust direction, this oil film prevents No wear occurs.
タービンインペラ1.コンプレッサインペラ11の重量
及び過給機の使用最高回転数により、タービンロータ組
立体の振動モードが決まってくる。これによって、ラジ
アルメタル6の端面摩耗がきまった位置に発生すること
もおる。例えば、2個のラジアルメタルの外部側端面に
のみ摩耗が発生する様な場合は、その部分にのみつまり
、外部側2カ所に板状ワッシャ30を挿入することも考
えられる。Turbine impeller 1. The vibration mode of the turbine rotor assembly is determined by the weight of the compressor impeller 11 and the maximum operating speed of the supercharger. As a result, end face wear of the radial metal 6 may occur at specific positions. For example, if wear occurs only on the outer end surfaces of the two radial metals, it may be possible to insert plate washers 30 at two locations on the outer side to block only those parts.
本発明によれば切削性の良い銅合金メタル材をラジアル
メタルとして使用する場合、本発明の板状ワッシャをラ
ジアルメタルとサークリップ間に挿入することにより、
メタル摩耗を防止することができ、過給機の耐久性能を
向上させることができる。According to the present invention, when a copper alloy metal material with good machinability is used as a radial metal, by inserting the plate-shaped washer of the present invention between the radial metal and the circlip,
It is possible to prevent metal wear and improve the durability of the supercharger.
第1図は、過給機の断面図、第2図は、ラジアルメタル
部の詳細を示す断面図、第3図はサークリップの斜視図
、第4図は、本発明による過給機のラジアルメタル部詳
細を示す断面図、第5図は板状ワッシャの斜視図である
。
5・・・軸受箱、6・・・ラジアルメタル、7・・・サ
ークリップ、30・・・ワッシャ
代理人 弁理士 高橋明夫
槽2図
も4−図
0 30
0FIG. 1 is a sectional view of the turbocharger, FIG. 2 is a sectional view showing details of the radial metal part, FIG. 3 is a perspective view of the circlip, and FIG. 4 is a radial view of the turbocharger according to the present invention. FIG. 5 is a cross-sectional view showing details of the metal part, and FIG. 5 is a perspective view of the plate washer. 5...Bearing box, 6...Radial metal, 7...Circlip, 30...Washer agent Patent attorney Akio Takahashi Tank 2 diagram also 4-Figure 0 30 0
Claims (1)
ンと一体に回転するコンプレッサにより、該機関に過給
を行なう過給機の、軸受箱、該軸受箱に収納されたラジ
アルメタル、該ラジアルメタルを支えるサークリップに
より構成した過給機において、該ラジアルメタルと、該
サークリップの間に、板状ワッシャを挿入したことを特
許とする過給機。1. The bearing box of the supercharger that supercharges the engine by the compressor that rotates together with the turbine driven by the exhaust gas emitted by the engine, the radial metal housed in the bearing box, and the radial metal. This patented supercharger includes a circlip that supports the radial metal and a plate washer inserted between the radial metal and the circlip.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58244039A JPS60138228A (en) | 1983-12-26 | 1983-12-26 | Supercharger |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58244039A JPS60138228A (en) | 1983-12-26 | 1983-12-26 | Supercharger |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS60138228A true JPS60138228A (en) | 1985-07-22 |
Family
ID=17112798
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP58244039A Pending JPS60138228A (en) | 1983-12-26 | 1983-12-26 | Supercharger |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS60138228A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0339921A (en) * | 1988-10-15 | 1991-02-20 | Asahi Optical Co Ltd | Control method for zoom lens for camera and zoom lens barrel |
US5528427A (en) * | 1991-10-30 | 1996-06-18 | Canon Kabushiki Kaisha | Zoom lens |
US6793468B2 (en) * | 2001-07-31 | 2004-09-21 | Hitachi, Ltd. | Turbo-charger for internal-combustion engine |
US20180238383A1 (en) * | 2015-02-09 | 2018-08-23 | Mitsubishi Heavy Industries, Ltd. | Turbocharger |
-
1983
- 1983-12-26 JP JP58244039A patent/JPS60138228A/en active Pending
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0339921A (en) * | 1988-10-15 | 1991-02-20 | Asahi Optical Co Ltd | Control method for zoom lens for camera and zoom lens barrel |
US5528427A (en) * | 1991-10-30 | 1996-06-18 | Canon Kabushiki Kaisha | Zoom lens |
US6793468B2 (en) * | 2001-07-31 | 2004-09-21 | Hitachi, Ltd. | Turbo-charger for internal-combustion engine |
US20180238383A1 (en) * | 2015-02-09 | 2018-08-23 | Mitsubishi Heavy Industries, Ltd. | Turbocharger |
US10844902B2 (en) * | 2015-02-09 | 2020-11-24 | Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. | Turbocharger |
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