JPS58106522U - Turbo supercharger bearing device - Google Patents
Turbo supercharger bearing deviceInfo
- Publication number
- JPS58106522U JPS58106522U JP1982002485U JP248582U JPS58106522U JP S58106522 U JPS58106522 U JP S58106522U JP 1982002485 U JP1982002485 U JP 1982002485U JP 248582 U JP248582 U JP 248582U JP S58106522 U JPS58106522 U JP S58106522U
- Authority
- JP
- Japan
- Prior art keywords
- shaft
- turbo supercharger
- metal
- bearing device
- thrust
- 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
- 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
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial 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
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/10—Sliding-contact bearings for exclusively rotary movement for both radial and axial load
-
- 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
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第1図i従来例をあられす断面図、第2図は本考案の実
施例をあられす一要部断面図、第3゛図Ag−4・、゛
本−案の実施例にお、ける第二→ルフローテイングメ゛
タルの断面図1.第3図Bは同じく第二フどレフローテ
ィングメタルの吸気コンプレッサ側の正面図、。Figure 1 is a cross-sectional view of a conventional example; Figure 2 is a cross-sectional view of a main part of an embodiment of the present invention; Figure 3 is a cross-sectional view of an embodiment of the present invention; Cross-sectional view of the second → flow floating metal 1. Figure 3B is also a front view of the second flap floating metal on the intake compressor side.
Claims (1)
ごの排気タービンとシキラトを介して同軸的に7回□
゛ 転する吸気コイプレクツ常備え1、ノ1ウジン
グおよ゛びシャラ十に対して回転自由になるようiこシ
、ヤフ5 トの周りに第一めラロニテイングメ
タルを介装し、“ この第一フローティングメ
タルの端面に接触スる・スラストメタルをハウジングに
画定ザる二方、このスラストメタルを挾んで第一フロー
ティングメタルの反対側にシャツ十に固定奎れる環状の
、スラ゛ ストカラーを′設けたタニボ過給機の軸受
装置において、前記ハウリングおよびシャフト]に対し
て回、 転自由になるようにス2ストカ゛ラニとズ
ー?ストメ・−タルの間に第二のフロ・六テイングンタ
ルを介装し゛たiとを特徴とする゛ターボ過給機−受装
置。Exhaust driven by engine exhaust gas, turbine,
7 times coaxially through the exhaust turbine and Sikirat
The rotating intake coil rectifier is always provided 1, 1, 1 and 5 so that it can rotate freely against the shaft 5 and the shaft 5. A ring-shaped thrust collar is attached to the end surface of the first floating metal and fixed to the shirt on the opposite side of the first floating metal by sandwiching the thrust metal on the two sides that define the thrust metal in the housing. 'In the bearing device of the turbo supercharger provided, a second flow six bearing is installed between the two-stroke cylinder and the zoometal so that it can rotate and rotate freely relative to the howling and shaft. A turbo supercharger-receiving device characterized by an interposed i.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1982002485U JPS58106522U (en) | 1982-01-12 | 1982-01-12 | Turbo supercharger bearing device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1982002485U JPS58106522U (en) | 1982-01-12 | 1982-01-12 | Turbo supercharger bearing device |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS58106522U true JPS58106522U (en) | 1983-07-20 |
Family
ID=30015469
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1982002485U Pending JPS58106522U (en) | 1982-01-12 | 1982-01-12 | Turbo supercharger bearing device |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS58106522U (en) |
-
1982
- 1982-01-12 JP JP1982002485U patent/JPS58106522U/en active Pending
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