JPH02132121U - - Google Patents
Info
- Publication number
- JPH02132121U JPH02132121U JP1989042165U JP4216589U JPH02132121U JP H02132121 U JPH02132121 U JP H02132121U JP 1989042165 U JP1989042165 U JP 1989042165U JP 4216589 U JP4216589 U JP 4216589U JP H02132121 U JPH02132121 U JP H02132121U
- Authority
- JP
- Japan
- Prior art keywords
- pad
- inner circumferential
- thrust bearing
- hole
- circumferential groove
- 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
- F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial load only
- F16C17/047—Sliding-contact bearings for exclusively rotary movement for axial load only with fixed wedges to generate hydrodynamic pressure
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- 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
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/10—Construction relative to lubrication
- F16C33/1025—Construction relative to lubrication with liquid, e.g. oil, as lubricant
- F16C33/106—Details of distribution or circulation inside the bearings, e.g. details of the bearing surfaces to affect flow or pressure of the liquid
- F16C33/1075—Wedges, e.g. ramps or lobes, for generating pressure
-
- 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)
- Chemical & Material Sciences (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Sliding-Contact Bearings (AREA)
- Supercharger (AREA)
Description
第1図は本考案の一実施例の正面図、第2図は
第1図の−方向矢視図、第3図は第1図の
−方向矢視図、第4図はターボチヤージヤの側
断面図、第5図は従来のスラスト軸受の正面図、
第6図は第5図の−方向矢視図である。
3は回転主軸、4はスラスト軸受、9は軸心孔
、10は給油孔、11はパツド溝、12はテーパ
パツド面、13はパツド当り面、14はパツド、
15はスラスト受パツド面、18は油の排出口、
19は内周溝、21は貫通孔を示す。
Fig. 1 is a front view of an embodiment of the present invention, Fig. 2 is a view taken in the - direction arrow of Fig. 1, Fig. 3 is a view taken in the - direction arrow of Fig. 1, and Fig. 4 is a side cross-section of the turbocharger. Figure 5 is a front view of a conventional thrust bearing.
FIG. 6 is a view taken along the - direction arrow in FIG. 3 is a rotating main shaft, 4 is a thrust bearing, 9 is a shaft center hole, 10 is an oil supply hole, 11 is a pad groove, 12 is a tapered pad surface, 13 is a pad contact surface, 14 is a pad,
15 is the thrust receiving pad surface, 18 is the oil discharge port,
Reference numeral 19 indicates an inner circumferential groove, and reference numeral 21 indicates a through hole.
Claims (1)
面に有したスラスト受パツド面により前記回転主
軸の軸方向の移動を規制することができ、且つ前
記パツド面が前記軸心孔に連通して放射状に延び
る複数のパツド溝と、パツド当り面と、該パツド
溝とパツド当り面との間に形成されたテーパパツ
ド面とを有しているスラスト軸受において、前記
軸心孔の内周面に沿つて内周溝を刻設し、且つ前
記スラスト軸受内部に半径方向に延びて前記内周
溝に連通する給油孔を穿設し、更に前記内周溝を
前記各テーパパツド面の始点近傍に連通する貫通
孔を形成したことを特徴とするスラスト軸受。 The thrust receiving pad is fitted onto the rotating main shaft through an axial hole, and can restrict movement of the rotating main shaft in the axial direction by thrust receiving pad surfaces provided on both sides in the axial direction, and the pad surface communicates with the axial hole. In a thrust bearing having a plurality of pad grooves extending radially, a pad contact surface, and a tapered pad surface formed between the pad grooves and the pad contact surface, the inner circumferential surface of the shaft center hole an inner circumferential groove is carved along the thrust bearing, an oil supply hole is bored inside the thrust bearing that extends in the radial direction and communicates with the inner circumferential groove, and the inner circumferential groove is formed near the starting point of each of the tapered pad surfaces. A thrust bearing characterized by forming a communicating through hole.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1989042165U JPH02132121U (en) | 1989-04-11 | 1989-04-11 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1989042165U JPH02132121U (en) | 1989-04-11 | 1989-04-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH02132121U true JPH02132121U (en) | 1990-11-02 |
Family
ID=31553465
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1989042165U Pending JPH02132121U (en) | 1989-04-11 | 1989-04-11 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH02132121U (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2008095703A (en) * | 2006-10-05 | 2008-04-24 | Hitachi Ltd | Thrust bearing device |
WO2009107819A1 (en) * | 2008-02-25 | 2009-09-03 | 三菱重工業株式会社 | Cooling device of thrust bearing in exhaust turbo- supercharger |
WO2014057758A1 (en) * | 2012-10-10 | 2014-04-17 | 大豊工業株式会社 | Thrust bearing |
JP2015516054A (en) * | 2012-05-08 | 2015-06-04 | ボーグワーナー インコーポレーテッド | Axial bearing device |
WO2019015753A1 (en) * | 2017-07-19 | 2019-01-24 | Konzelmann Gmbh | Hydrodynamic bearing |
-
1989
- 1989-04-11 JP JP1989042165U patent/JPH02132121U/ja active Pending
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2008095703A (en) * | 2006-10-05 | 2008-04-24 | Hitachi Ltd | Thrust bearing device |
JP4554583B2 (en) * | 2006-10-05 | 2010-09-29 | 株式会社日立製作所 | Thrust bearing device |
WO2009107819A1 (en) * | 2008-02-25 | 2009-09-03 | 三菱重工業株式会社 | Cooling device of thrust bearing in exhaust turbo- supercharger |
JP2015516054A (en) * | 2012-05-08 | 2015-06-04 | ボーグワーナー インコーポレーテッド | Axial bearing device |
WO2014057758A1 (en) * | 2012-10-10 | 2014-04-17 | 大豊工業株式会社 | Thrust bearing |
JP2014077491A (en) * | 2012-10-10 | 2014-05-01 | Taiho Kogyo Co Ltd | Thrust bearing |
WO2019015753A1 (en) * | 2017-07-19 | 2019-01-24 | Konzelmann Gmbh | Hydrodynamic bearing |
US11047420B2 (en) | 2017-07-19 | 2021-06-29 | Konzelmann Gmbh | Hydrodynamic bearing |