JPS5999131U - turbo supercharger - Google Patents
turbo superchargerInfo
- Publication number
- JPS5999131U JPS5999131U JP1982194780U JP19478082U JPS5999131U JP S5999131 U JPS5999131 U JP S5999131U JP 1982194780 U JP1982194780 U JP 1982194780U JP 19478082 U JP19478082 U JP 19478082U JP S5999131 U JPS5999131 U JP S5999131U
- Authority
- JP
- Japan
- Prior art keywords
- shaft
- exhaust turbine
- metal
- large diameter
- diameter part
- 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
- F16C17/02—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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Supercharger (AREA)
- Sliding-Contact Bearings (AREA)
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図は従来例の断面図、第2図はこの考案の一実施例
の要部断面図である。
1・・・排気タービン(タービンロータ)、2・・・吸
気コンプレッサ、3・・・シャフト、3A・・・シャフ
ト大径部、8・・・ハウジング(センサ)、9・・・フ
ルフローティングメタル、3B、 9B−接触端面、1
0・・・スラストメタル、11・・・スラストカラー、
20・・・環状溝。FIG. 1 is a sectional view of a conventional example, and FIG. 2 is a sectional view of a main part of an embodiment of this invention. DESCRIPTION OF SYMBOLS 1... Exhaust turbine (turbine rotor), 2... Intake compressor, 3... Shaft, 3A... Shaft large diameter part, 8... Housing (sensor), 9... Full floating metal, 3B, 9B-contact end surface, 1
0... Thrust metal, 11... Thrust color,
20... Annular groove.
Claims (1)
、この排気タービンとシャフトを介して同軸的に回転す
る吸気コンプレッサを備え、吸気コンプレッサ近傍のシ
ャフトの周りに設けたスラストカラーに排気タービン側
から接触するようにハウジングに設けたスラストメタル
と、排気タービン側に形成したシャフト大径部との間に
筒状のフルフローティングメタルを保持口たターボ過給
機において、シャフト大径部の外周にフルフローティン
グメタルとの接触端面に近接して環状溝を形成したこと
を特徴とするターボ過給機。It is equipped with an exhaust turbine that is driven by the discharge force of engine exhaust gas, and an intake compressor that rotates coaxially through the exhaust turbine and the shaft.The thrust collar that is installed around the shaft near the intake compressor is contacted from the exhaust turbine side. In a turbocharger that has a cylindrical full floating metal holding hole between the thrust metal provided in the housing and the large diameter part of the shaft formed on the exhaust turbine side, there is a full floating metal on the outer periphery of the large diameter part of the shaft. A turbo supercharger characterized in that an annular groove is formed close to the end surface that contacts the metal.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1982194780U JPS5999131U (en) | 1982-12-22 | 1982-12-22 | turbo supercharger |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1982194780U JPS5999131U (en) | 1982-12-22 | 1982-12-22 | turbo supercharger |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5999131U true JPS5999131U (en) | 1984-07-04 |
Family
ID=30418558
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1982194780U Pending JPS5999131U (en) | 1982-12-22 | 1982-12-22 | turbo supercharger |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5999131U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20150023693A (en) * | 2012-06-25 | 2015-03-05 | 보르그워너 인코퍼레이티드 | Exhaust-gas turbocharger |
-
1982
- 1982-12-22 JP JP1982194780U patent/JPS5999131U/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20150023693A (en) * | 2012-06-25 | 2015-03-05 | 보르그워너 인코퍼레이티드 | Exhaust-gas turbocharger |
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