DE2628918A1 - Hydrodynamic bush bearing with axial oil pockets - has cylindrical end portions to limit axial escape of oil - Google Patents

Hydrodynamic bush bearing with axial oil pockets - has cylindrical end portions to limit axial escape of oil

Info

Publication number
DE2628918A1
DE2628918A1 DE19762628918 DE2628918A DE2628918A1 DE 2628918 A1 DE2628918 A1 DE 2628918A1 DE 19762628918 DE19762628918 DE 19762628918 DE 2628918 A DE2628918 A DE 2628918A DE 2628918 A1 DE2628918 A1 DE 2628918A1
Authority
DE
Germany
Prior art keywords
oil
bearing
pockets
bush
axial
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.)
Withdrawn
Application number
DE19762628918
Other languages
German (de)
Inventor
Erich Pessel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kraftwerk Union AG
Original Assignee
Kraftwerk Union AG
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 by Kraftwerk Union AG filed Critical Kraftwerk Union AG
Priority to DE19762628918 priority Critical patent/DE2628918A1/en
Priority to JP7645777A priority patent/JPS531744A/en
Publication of DE2628918A1 publication Critical patent/DE2628918A1/en
Withdrawn legal-status Critical Current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
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/10Construction relative to lubrication
    • F16C33/1025Construction relative to lubrication with liquid, e.g. oil, as lubricant
    • F16C33/106Details of distribution or circulation inside the bearings, e.g. details of the bearing surfaces to affect flow or pressure of the liquid
    • F16C33/108Details of distribution or circulation inside the bearings, e.g. details of the bearing surfaces to affect flow or pressure of the liquid with a plurality of elements forming the bearing surfaces, e.g. bearing pads
    • 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
    • F16C17/02Sliding-contact bearings for exclusively rotary movement for radial load only
    • F16C17/022Sliding-contact bearings for exclusively rotary movement for radial load only with a pair of essentially semicircular bearing sleeves
    • 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
    • F16C17/02Sliding-contact bearings for exclusively rotary movement for radial load only
    • F16C17/028Sliding-contact bearings for exclusively rotary movement for radial load only with fixed wedges to generate hydrodynamic pressure, e.g. multi-lobe bearings
    • 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
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/10Construction relative to lubrication
    • F16C33/1025Construction relative to lubrication with liquid, e.g. oil, as lubricant
    • F16C33/106Details of distribution or circulation inside the bearings, e.g. details of the bearing surfaces to affect flow or pressure of the liquid
    • F16C33/1075Wedges, e.g. ramps or lobes, for generating pressure

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)

Abstract

The bearing bush has a bush whose bearing surface has lobe-shaped pockets (4-7) for the hydrodynamic formation of wedges of oil. The pockets extend circumferentially between arcuate portions (10-13) centred on the axis of the bearing. Axially, the recesses extend short of the ends of the bush and terminate at cylindrical end portions or weirs (9). The weirs limit or prevent the escape of oil from the axial ends of the pockets. The weirs may extend over the whole inner circumference of the bush or only at the lower half of the bush.

Description

XadialgleitlagerXadial plain bearings

Die Erfindung betrifft ein Radialgleitlager in Ausbildung als Mehrkeillager für Turbosätze, wobei über den inneren Umfang der Lagerfläche einer axial geteilten Lagerschale verteilt im Querschnitt sichelförmige Taschen zum Aufbau der Schmierölkeile eingelassen sind, die mit Ülzuleitkanälenin Verbindung stehen.The invention relates to a radial plain bearing designed as a multi-wedge bearing for turbo sets, with an axially split over the inner circumference of the bearing surface Bearing shell distributes sickle-shaped pockets in cross section to build up the lubricating oil wedges are admitted, which are connected to oil supply channels.

Ein derartiges Lager ist beispielsweise aus der DU-OS 2 103 239 bekannt. Obwohl derartige Mehrkeillager in der Praxis eine relativ gute Tragfähigkeit aufweisen, hat sich jedoch gezeigt, daß in bestimmten Umfangsbereichen hohe Lagertemperaturen auftreten können und daß beispielsweise ein Drehen der Welle bei Druckölanhebung nur bei relativ geringen Belastungen, jedoch großen erforderlichen Ölmengen ohne Verkanten des Lagers erreicht werden konnten. Ein wesentlicher Grund dafür dürfte darin zu sehen sein, daß das über die Taschen zugeführte Drucköl zu schnell seitlich abfließt und daß sich dadurch die erforderlichen Ölkeile nur unzureichend ausbilden.Such a bearing is known from DU-OS 2 103 239, for example. Although such multi-wedge bearings have a relatively good load-bearing capacity in practice, However, it has been shown that high storage temperatures in certain circumferential areas can occur and that, for example, a rotation of the shaft when the pressure oil is increased only with relatively low loads, but large amounts of oil required without Canting of the bearing could be achieved. A major reason for this is likely it can be seen that the pressure oil supplied via the pockets is too quickly sideways flows off and that the necessary oil wedges are only insufficiently formed as a result.

Der Erfindung liegt daher die Aufgabe zugrunde, ein Radialgleit-Lager zu schaffen, das bei geringerem Ölverbrauch erheblich höheren Belastuzigen gewachsen ist.The invention is therefore based on the object of a radial sliding bearing to create that with lower oil consumption can cope with considerably higher loads is.

Ausgehend von einem Radialgleitlager der eingangs genannten Art ist zur Lösung der Aufgabe erfindungsgemäß vorgesehen, daß zumindest die untere Hälfte der Lagerschale an beiden Stirnseiten der Lagerfläche jeweils einen zylindrisch ausgebildeten Staurand aufweist.Starting from a radial plain bearing of the type mentioned above to solve the problem provided according to the invention that at least the lower half the bearing shell on both end faces of the bearing surface each one cylindrical has formed storage edge.

Die radiale Höhe der Stauränder soll dabei mindestens so bemessen sein, daß sie die sichelförmigen Taschen und die Mehrkeilschalen seitlich überdecken. Darüber hinaus ist es auch möglich, daß sich die Stauränder über den gesamten Umfang der Lagerschale erstrecken.The radial height of the retaining rims should be measured at least in this way be, that they laterally cover the sickle-shaped pockets and the multi-wedge shells. In addition, it is also possible that the retaining edge extends over the entire circumference the bearing shell extend.

Durch diese seitlichen Stauränder wird ein vorzeitiges Abströmen des Lageröls verhindert, so daß das Lager eine bessere Tragfähigkeit aufweist.Due to this side dam, a premature outflow of the Bearing oil prevented, so that the bearing has a better load capacity.

Anhand einer schematischen Zeichnung sind Aufbau und Wirkungsweise eines Ausführungsbeispiels nach der rfindung näher erläutert. Dabei zeigen: Fig. 1 eine Aufsicht auf die untere Hälfte der Lagerschale und Fig. 2 einen Längsschnitt durch eine Lagerschale entsprechend der Schnittlinie 11-11 nach Fig. 1.A schematic drawing shows the structure and mode of operation an embodiment according to the invention explained in more detail. They show: Fig. 1 is a plan view of the lower half of the bearing shell and FIG. 2 is a longitudinal section by a bearing shell according to the section line 11-11 of FIG. 1.

Die eine Maschinenwelle an den Lagerstellen umschließende Lagerschale 1 besteht aus einer unteren Hälfte 2 und der oberen Hälfte 3 und weist auf ihrer inneren Lagerfläche beispielsweise vier angenähert sichelförmige Taschen 4, 5, 6 und 7 auf, die über nicht näher dargestellte Öl zuführungen mit Lageröl versorgt werden. Um nun zu verhindern, daß das Drucköl vorzeitig aus der Lagerschale 1 seitlich abströmt, sind auf beiden Stirnseiten der Lagerfläche zylindrische Stauränder 8 und 9 vorgesehen, deren radiale Höhe mindestens so bemessen ist, daß die sichelförmigen Taschen 4 bis 7 und die Mehrkeilschalen 10 bis 13, d. h. die tragenden Bereiche der Lagerschale zwischen den Taschen, seitlich überdeckt werden.The bearing shell enclosing a machine shaft at the bearing points 1 consists of a lower half 2 and the upper half 3 and points to their inner bearing surface, for example, four approximately sickle-shaped pockets 4, 5, 6 and 7, which supplies oil supplies, not shown, with bearing oil will. In order to prevent the pressure oil from prematurely escaping from the bearing shell 1 laterally outflows, there are cylindrical retaining edges 8 on both end faces of the bearing surface and 9 are provided, the radial height of which is at least such that the sickle-shaped Pockets 4 to 7 and the multi-wedge shells 10 to 13, d. H. the load-bearing areas the bearing shell between the pockets, are laterally covered.

Durch dieses Anbringen der zylindrisch ausgebildeten Stauränder 8 und 9 und der dadurch bedingten Stauwirkung gegen das seitlich abfließende Öl kaim - wie Versuche gezeigt haben - eine erheblich niedrigere Lagertemperatur erreicht werden.By attaching the cylindrically shaped retaining edges 8 and 9 and the resulting damming effect against the laterally draining oil kaim - as tests have shown - reached a considerably lower storage temperature will.

Ein weiterer wesentlicher Vorteil besteht darin, daß bei einer Druckölanhebung der Welle, wie sie beispielsweise bei der Inbetriebs etzunp; erforderlich ist, mit erhel)lichgeringeren Ölmengen ausgekommen werden kann, wobei darüber hinaus die Belastung gegen- über Lagerschalen ohne Stauränder erhöht werden kann. Gleichzeitig hat sich gezeigt, daß die Verlustleistung etwa 30 % unter der einer Ausführung ohne seitliche Stauränder liegt.Another important advantage is that when the pressure oil is increased the shaft, as it etzunp, for example, when commissioning; is required with Obviously lower amounts of oil can be managed, and in addition the Load against can be increased via bearing shells without retaining rims can. At the same time it has been shown that the power loss is about 30% below the a version without lateral retaining edges.

Bei dem dargestellten Ausführungsbeispiel ist von einem Vierkeillager ausgegangen worden. Es ist jedoch auch möglich, die erfindungsgemäße Lagerausbildung auch bei jeder anderen Zahl von Ölkeilen vorzusehen, wobei sich gleichfalls sehr gute Ergebnisse zeigen.In the illustrated embodiment is of a four-key bearing been assumed. However, it is also possible to use the bearing design according to the invention also to be provided for any other number of oil wedges, which is also very show good results.

Claims (3)

Patentansprüche 1. Radialgleitlager in Ausbildung als Mehrkeillager ftirTurbosätze, wobei über den inneren Umfang der Lagerfläche einer axial geteilten Lagerschale verteilt im Querschnitt sichelförmige Taschen zum Aufbau der Schmierkeile eingelassen sind, die mit Ölzuleitkanälen in Verbindung stehen, dadurch gekenrlzeichnet, daß zumindest die untere Hälfte (2) der Lagerschale (1) an beiden Stirnseiten der Lagerfläche jeweils einen zylindrisch ausgebildeten Staurand (8, 9) aufweist.Claims 1. Radial plain bearings in training as multi-key bearings ftir turbo sets, with an axially split over the inner circumference of the bearing surface Bearing shell distributed in cross section with sickle-shaped pockets for the construction of the lubricating wedges are embedded, which are in connection with oil supply channels, thereby marked, that at least the lower half (2) of the bearing shell (1) on both ends of the Each bearing surface has a cylindrical storage edge (8, 9). 2. Radialgleitlager nach Anspruch 1, dadurch gekennzeichnet , daß sich die Stauränder (8, C)) über den gesamter Umfang der Lagerschale (1 ) erstrecken. 2. Radial plain bearing according to claim 1, characterized in that the retaining rims (8, C)) extend over the entire circumference of the bearing shell (1). 3. Radialgleitlager nach Anspruch 1 oder 2, dadurch gekennzeichne daß die radiale Höhe der Stauränder (8, 9) mindestens so bemessen ist, daB sie die sichelförmigen Taschen (4, 5, 6, 7) und die Mehrkeilschalen (10 bis 13) seitlich iiberdeckt. 3. Radial plain bearing according to claim 1 or 2, characterized that the radial height of the retaining rims (8, 9) is at least dimensioned so that they the sickle-shaped pockets (4, 5, 6, 7) and the multi-wedge shells (10 to 13) on the side covered.
DE19762628918 1976-06-28 1976-06-28 Hydrodynamic bush bearing with axial oil pockets - has cylindrical end portions to limit axial escape of oil Withdrawn DE2628918A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
DE19762628918 DE2628918A1 (en) 1976-06-28 1976-06-28 Hydrodynamic bush bearing with axial oil pockets - has cylindrical end portions to limit axial escape of oil
JP7645777A JPS531744A (en) 1976-06-28 1977-06-27 Radial bearing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19762628918 DE2628918A1 (en) 1976-06-28 1976-06-28 Hydrodynamic bush bearing with axial oil pockets - has cylindrical end portions to limit axial escape of oil

Publications (1)

Publication Number Publication Date
DE2628918A1 true DE2628918A1 (en) 1978-01-05

Family

ID=5981610

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19762628918 Withdrawn DE2628918A1 (en) 1976-06-28 1976-06-28 Hydrodynamic bush bearing with axial oil pockets - has cylindrical end portions to limit axial escape of oil

Country Status (2)

Country Link
JP (1) JPS531744A (en)
DE (1) DE2628918A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4834559A (en) * 1983-09-08 1989-05-30 Klein, Schanzlin & Becker Aktiengesellschaft Multiple-face radial plain bearing
US5129738A (en) * 1990-01-23 1992-07-14 Sankyo Seiki Mfg. Co., Ltd. Bearing device
US20180355916A1 (en) * 2015-12-03 2018-12-13 Flender-Graffenstaden S.A.S. Hydrodynamic bearing

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4834559A (en) * 1983-09-08 1989-05-30 Klein, Schanzlin & Becker Aktiengesellschaft Multiple-face radial plain bearing
US5129738A (en) * 1990-01-23 1992-07-14 Sankyo Seiki Mfg. Co., Ltd. Bearing device
US20180355916A1 (en) * 2015-12-03 2018-12-13 Flender-Graffenstaden S.A.S. Hydrodynamic bearing
US10443651B2 (en) * 2015-12-03 2019-10-15 Flender-Graffenstaden S.A.S. Hydrodynamic bearing

Also Published As

Publication number Publication date
JPS531744A (en) 1978-01-10

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OB Request for examination as to novelty
OC Search report available
8139 Disposal/non-payment of the annual fee