JPH0294917U - - Google Patents

Info

Publication number
JPH0294917U
JPH0294917U JP1989003765U JP376589U JPH0294917U JP H0294917 U JPH0294917 U JP H0294917U JP 1989003765 U JP1989003765 U JP 1989003765U JP 376589 U JP376589 U JP 376589U JP H0294917 U JPH0294917 U JP H0294917U
Authority
JP
Japan
Prior art keywords
pad
axial
hole
oil supply
main shaft
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
Application number
JP1989003765U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP1989003765U priority Critical patent/JPH0294917U/ja
Publication of JPH0294917U publication Critical patent/JPH0294917U/ja
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00Sliding-contact bearings for exclusively rotary movement
    • F16C17/04Sliding-contact bearings for exclusively rotary movement for axial load only
    • F16C17/047Sliding-contact bearings for exclusively rotary movement for axial load only with fixed wedges to generate hydrodynamic pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00Engines or pumps
    • F16C2360/23Gas turbine engines
    • F16C2360/24Turbochargers

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Supercharger (AREA)
  • Sliding-Contact Bearings (AREA)

Description

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本考案の第1の実施例の正面図、第2
図は第1図の―矢視断面図、第3図は第1図
の―矢視断面図、第4図は第1図の―矢
視断面図、第5図は本考案の第2の実施例の正面
図、第6図は第5図の―矢視断面図、第7図
は従来のターボチヤージヤの側断面図、第8図は
従来のスラスト軸受の正面図、第9図は第8図の
―矢視断面図である。 4はスラスト軸受、9は軸心孔、10は給油孔
、13はパツド溝、14はパツドテーパ面、15
はパツド当り面、17はスラスト受パツド面を示
す。
Figure 1 is a front view of the first embodiment of the present invention;
The figure is a cross-sectional view taken in the direction of the arrow in FIG. 1, FIG. 3 is a cross-sectional view taken in the direction shown in the arrow in FIG. A front view of the embodiment, FIG. 6 is a sectional view taken along the - arrow in FIG. 5, FIG. 7 is a side sectional view of a conventional turbocharger, FIG. 8 is a front view of a conventional thrust bearing, and FIG. FIG. 4 is a thrust bearing, 9 is a shaft center hole, 10 is an oil supply hole, 13 is a pad groove, 14 is a pad tapered surface, 15
17 indicates the pad contact surface, and 17 indicates the thrust receiving pad surface.

Claims (1)

【実用新案登録請求の範囲】 (1) 回転主軸に軸心孔を介して嵌合され、軸方
向両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、前
記軸心孔から半径方向に延びる給油孔を内部に有
し、更に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
パツドテーパ面とを有しているスラスト軸受にお
いて、前記給油孔と軸心孔との連通部に近い位置
のパツド溝の流路断面積を小さく、前記連通部か
ら遠い位置のパツド溝の流路断面積を大きく形成
したことを特徴とするスラスト軸受。 (2) 回転主軸に軸心孔を介して嵌合され、軸方
向両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
つ前記軸心孔から半径方向に延びる給油孔を内部
に有し、更に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
れたパツドテーパ面とを有しているスラスト軸受
において、スラスト軸受の軸中心に対し、軸心孔
を前記給油孔側に偏心して形成したことを特徴と
するスラスト軸受。
[Claims for Utility Model Registration] (1) A thrust receiving pad that is fitted onto the rotating main shaft through an axial hole and has thrust receiving pad surfaces on both sides in the axial direction can restrict the movement of the rotating main shaft in the axial direction; The pad has an oil supply hole extending in the radial direction from the axial hole, and further includes a plurality of pad grooves in which the pad surface communicates with the axial hole and extends radially, a pad contacting surface, and the pad groove and the pad contacting surface. In a thrust bearing having a pad groove formed between the oil supply hole and the shaft center hole, the passage cross-sectional area of the pad groove at a position close to the communication portion between the oil supply hole and the shaft center hole is made small, and the flow path area far from the communication portion is reduced. A thrust bearing characterized by a large passage cross-sectional area of the pad groove at the position. (2) A thrust receiving pad that is fitted to the rotating main shaft through an axial hole, is capable of restricting axial movement of the rotating main shaft by thrust receiving pad surfaces provided on both axial surfaces, and has a radial direction from the axial center hole. The pad surface has a plurality of pad grooves extending radially in communication with the shaft center hole, a pad contact surface, and a pad contact surface formed between the pad groove and the pad contact surface. 1. A thrust bearing having a pad and a tapered surface, characterized in that an axial hole is formed eccentrically toward the oil supply hole side with respect to the axial center of the thrust bearing.
JP1989003765U 1989-01-17 1989-01-17 Pending JPH0294917U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1989003765U JPH0294917U (en) 1989-01-17 1989-01-17

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1989003765U JPH0294917U (en) 1989-01-17 1989-01-17

Publications (1)

Publication Number Publication Date
JPH0294917U true JPH0294917U (en) 1990-07-27

Family

ID=31205694

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1989003765U Pending JPH0294917U (en) 1989-01-17 1989-01-17

Country Status (1)

Country Link
JP (1) JPH0294917U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
KR100973540B1 (en) * 2002-04-12 2010-08-02 에이비비 터보 시스템즈 아게 Turbo charger with means on the shaft for axially securing of said shaft if the compressor wheel bursts
JPWO2015190364A1 (en) * 2014-06-12 2017-04-20 株式会社Ihi Bearing structure and turbocharger
WO2019015753A1 (en) * 2017-07-19 2019-01-24 Konzelmann Gmbh Hydrodynamic bearing

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100973540B1 (en) * 2002-04-12 2010-08-02 에이비비 터보 시스템즈 아게 Turbo charger with means on the shaft for axially securing of said shaft if the compressor wheel bursts
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
JPWO2015190364A1 (en) * 2014-06-12 2017-04-20 株式会社Ihi Bearing structure and turbocharger
WO2019015753A1 (en) * 2017-07-19 2019-01-24 Konzelmann Gmbh Hydrodynamic bearing
US11047420B2 (en) 2017-07-19 2021-06-29 Konzelmann Gmbh Hydrodynamic bearing

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