EP0346677A1 - Liquid-displacement machine - Google Patents

Liquid-displacement machine Download PDF

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Publication number
EP0346677A1
EP0346677A1 EP89109759A EP89109759A EP0346677A1 EP 0346677 A1 EP0346677 A1 EP 0346677A1 EP 89109759 A EP89109759 A EP 89109759A EP 89109759 A EP89109759 A EP 89109759A EP 0346677 A1 EP0346677 A1 EP 0346677A1
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EP
European Patent Office
Prior art keywords
ring element
shaft
impeller
face
turbomachine according
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.)
Granted
Application number
EP89109759A
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German (de)
French (fr)
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EP0346677B1 (en
Inventor
Karlheinz Becker
Karl-Heinz Bayer
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.)
KSB AG
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KSB AG
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Filing date
Publication date
Application filed by KSB AG filed Critical KSB AG
Priority to AT89109759T priority Critical patent/ATE75818T1/en
Publication of EP0346677A1 publication Critical patent/EP0346677A1/en
Application granted granted Critical
Publication of EP0346677B1 publication Critical patent/EP0346677B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/426—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for liquid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/08—Sealings
    • F04D29/10—Shaft sealings
    • F04D29/12—Shaft sealings using sealing-rings
    • F04D29/126—Shaft sealings using sealing-rings especially adapted for liquid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D7/00—Pumps adapted for handling specific fluids, e.g. by selection of specific materials for pumps or pump parts
    • F04D7/02—Pumps adapted for handling specific fluids, e.g. by selection of specific materials for pumps or pump parts of centrifugal type
    • F04D7/04—Pumps adapted for handling specific fluids, e.g. by selection of specific materials for pumps or pump parts of centrifugal type the fluids being viscous or non-homogenous

Definitions

  • the invention relates to a turbomachine according to the preamble of the main claim.
  • the invention has for its object to provide a measure for a turbomachine which is supplied with a conveying medium containing solids of the aforementioned magnitude, by means of which a space surrounding the shaft seal and the shaft seal itself can be protected against erosion wear. This object is achieved in accordance with the characterizing part of the main claim.
  • Embodiments of the invention described in claims 4 to 8 have the effect that dangerous wear marks were not detectable either on the shaft seal or in the space surrounding the shaft seal.
  • the split ring seal was damaged within a very short time without the ring element. If an annular element according to the invention was instead arranged in the space receiving the shaft seal, no signs of wear were detectable even on the split ring seal after a long test period.
  • the configurations of claims 9 to 11 describe the different possibilities for producing the ring element.
  • FIG. 1 shows a housing (1) of a turbomachine, which is designed here as a centrifugal pump, and an impeller (2) arranged inside the housing (1).
  • the impeller is equipped with split ring seals (3, 4) on the suction and pressure side.
  • the impeller (2) is attached to a shaft (5) on which a shaft protection sleeve (6) and a shaft seal (7) designed as a mechanical seal are also attached.
  • the impeller (2) has axial thrust compensation bores (9) in the area of the impeller hub (8) in the impeller cover disc on the pressure side.
  • the housing (1) Inside the space (10) surrounding the shaft seal (7), the housing (1), here a pressure-side housing cover (11), has an attached ring element (12). It extends in the area between the split ring (13) attached to the impeller and the impeller hub (8) and the shaft seal (7).
  • the free end face of the ring element (11) has a surface (14) running radially to the shaft, on the smallest diameter of which a nozzle (15) pointing in the axial direction to the shaft seal (7) is attached.
  • the ring element (12) formed here as a sheet metal part can also be designed as a solid part which would have a backward rotation on the side facing the shaft seal. Furthermore, it can be formed in one piece with the split ring (16) fixed to the housing.
  • FIG. 2 largely corresponds to that of FIG. 1. A difference is that the ring element (12) is provided on its free end face only with a surface (14) extending in the radial direction to the shaft.
  • Fig. 3 shows a frustoconical ring element (12) which extends diagonally to the shaft axis, its free end face (17) facing the shaft (5).
  • a frustoconical design of the ring element (12) there is one on its free end face (17), as well as on the smallest diameters of the surface (14) or a nozzle (15) attached to it shown in FIGS. 1 and 2 Tear-off edge, with the help of which erosion wear can be prevented within the space (10).

Abstract

PCT No. PCT/EP89/00604 Sec. 371 Date Dec. 13, 1990 Sec. 102(e) Date Dec. 13, 1990 PCT Filed May 30, 1989 PCT Pub. No. WO89/12755 PCT Pub. Date Dec. 28, 1989.A centrifugal pump has a housing which defines an annular chamber disposed downstream of the impeller and surrounding the shaft seal. The chamber receives a hollow cylindrical or frustoconical shroud which surrounds the shaft seal with spacing and protects it from solid particles in the conveyed fluid. A non-contact type annular seal between the impeller and the housing surrounds the shroud.

Description

Die Erfindung betrifft eine Strömungsmaschine gemäß dem Oberbegriff des Hauptanspruches.The invention relates to a turbomachine according to the preamble of the main claim.

Bei Strömungsmaschinen, die mit einem Feststoffe enthaltenden Fördermedium beaufschlagt sind, besteht die Gefahr eines Erosionsverschleisses innerhalb der Strömungsmaschine. Dem kann zwar durch eine entsprechende Auskleidung des Gehäuses entgegengewirkt werden, jedoch existiert eine besonders gefährdete Stelle im Bereich der Wellenabdichtung. Im Fördermedium enthaltene Feststoffe, welche eine Körnung von bis zu 1 mm aufweisen können, sind in der Lage, die Wellenabdichtung selbst oder die Wellenabdichtung haltende Gehäuseteile zu zerstören. Eine vorzeitiger Ausfall der Strömungsmaschine wäre dadurch gegeben.In turbomachines which are supplied with a conveying medium containing solids, there is a risk of erosion wear within the turbomachine. This can be counteracted by appropriate lining of the housing, but there is a particularly vulnerable area in the area of the shaft seal. Solids contained in the pumped medium, which can have a grain size of up to 1 mm, are capable of destroying the shaft seal itself or housing parts holding the shaft seal. This would result in premature failure of the turbomachine.

Der Erfindung liegt die Aufgabe zugrunde, für eine Strömungs­maschine, die mit einem Feststoffe der vorgenannten Größen­ordnung enthaltenden Fördermedium beaufschlagt ist, eine Maßnahme vorzusehen, mit deren Hilfe ein die Wellenabdichtung umgebender Raum und die Wellenabdichtung selbst vor Erosions­verschleiß geschützt werden kann. Die Lösung dieser Aufgabe erfolgt gemäß dem kennzeichnenden Teil des Hauptanspruches.The invention has for its object to provide a measure for a turbomachine which is supplied with a conveying medium containing solids of the aforementioned magnitude, by means of which a space surrounding the shaft seal and the shaft seal itself can be protected against erosion wear. This object is achieved in accordance with the characterizing part of the main claim.

In praktischen Versuchen hat sich in überraschender Weise gezeigt, daß mit einem gemäß dem Hauptanspruch gestalteten Ringelement ein Erosionsverschleiß durch im Fördermedium enthaltene Feststoffe, wobei bis zu 100 mg Feststoffanteil pro dm³ gegeben war, ein Erosionsverschleiß abgestellt werden konnte. Die Unteransprüche 2 und 3 geben vorteilhafte Ausgestaltungen der Erfindung und die Lage der freien Stirnseite des Ringelementes an.In practical tests, it has surprisingly been found that with a ring element designed according to the main claim, erosion wear due to the medium being conveyed contained solids, whereby up to 100 mg solids per dm³ was given, erosion wear could be stopped. The subclaims 2 and 3 indicate advantageous embodiments of the invention and the position of the free end face of the ring element.

In den Ansprüchen 4 bis 8 beschriebene Ausgestaltungen der Erfindung bewirken, daß gefährdende Verschleißspuren weder an der Wellenabdichtung noch in dem die Wellenabdichtung umgebenden Raum feststellbar waren. Bei Versuchen mit einem Laufrad, welches auf der der Wellenabdichtung zugekehrten Seite mit einer Spaltringdichtung versehen war, wurde ohne das Ringelement die Spaltringdichtung innerhalb kürzester Zeit beschädigt. Wurde stattdessen in dem die Wellenab­dichtung aufnehmenden Raum ein erfindungsgemäßes Ringelement angeordnet, dann waren nach langer Versuchszeit selbst an der Spaltringdichtung keine Verschleißspuren feststellbar. Die Ausgestaltungen der Ansprüche 9 bis 11 beschreiben die unterschiedlichen Möglichkeiten zur Herstellung des Ringelementes.Embodiments of the invention described in claims 4 to 8 have the effect that dangerous wear marks were not detectable either on the shaft seal or in the space surrounding the shaft seal. In tests with an impeller, which was provided with a split ring seal on the side facing the shaft seal, the split ring seal was damaged within a very short time without the ring element. If an annular element according to the invention was instead arranged in the space receiving the shaft seal, no signs of wear were detectable even on the split ring seal after a long test period. The configurations of claims 9 to 11 describe the different possibilities for producing the ring element.

Ausführungsbeispiele der Erfindung sind in den Zeichnungen dargestellt und werden im folgenden näher beschrieben. Die

  • Fig. 1 bis 3 zeigen hierbei unterschiedlich geformte Ringelemente.
Embodiments of the invention are shown in the drawings and are described in more detail below. The
  • 1 to 3 show differently shaped ring elements.

Die Fig. 1 zeigt ein Gehäuse (1) einer Strömungsmaschine, welche hier als Kreiselpumpe ausgebildet ist sowie ein innerhalb des Gehäuses (1) angeordnetes Laufrad (2). Bei dem hier gewählten Ausführungsbeispiel ist das Laufrad mit saug- und druckseitigen Spaltringdichtungen (3, 4) ausgerüstet. Das Laufrad (2) ist auf einer Welle (5) befestigt, auf der weiterhin eine Wellenschutzhülse (6) und eine als Gleitring­dichtung ausgebildete Wellenabdichtung (7) befestigt ist. Desweiteren weist das Laufrad (2) im Bereich der Laufradnabe (8) in der druckseitigen Laufraddeckscheibe angebracht Axialschubausgleichsbohrungen (9) auf.1 shows a housing (1) of a turbomachine, which is designed here as a centrifugal pump, and an impeller (2) arranged inside the housing (1). In the exemplary embodiment selected here, the impeller is equipped with split ring seals (3, 4) on the suction and pressure side. The impeller (2) is attached to a shaft (5) on which a shaft protection sleeve (6) and a shaft seal (7) designed as a mechanical seal are also attached. Furthermore, the impeller (2) has axial thrust compensation bores (9) in the area of the impeller hub (8) in the impeller cover disc on the pressure side.

Innerhalb des die Wellenabdichtung (7) umgebenden Raumes (10) ist das Gehäuse (1), hier einem druckseitigen Gehäusedeckel (11), befestigte Ringelement (12) angeordnet. Es erstreckt sich im Bereich zwischen dem am Laufrad angebrachten Spaltring (13) sowie der Laufradnabe (8) und der Wellen­abdichtung (7). Die freie Stirnseite des Ringelementes (11) weist eine radial zur Welle verlaufende Fläche (14) auf, an deren kleinsten Durchmesser ein in axialer Richtung zur Wellenabdichtung (7) weisender Stutzen (15) angebracht ist. Das hier als Blechformteil ausgebildete Ringelement (12) kann auch als massives Formteil ausgebildet sein, welches auf der zur Wellenabdichtung weisenden Seite eine Hinterdrehung aufweisen würde. Desweiteren kann es mit dem gehäusefesten Spaltring (16) einteilig ausgebildet sein.Inside the space (10) surrounding the shaft seal (7), the housing (1), here a pressure-side housing cover (11), has an attached ring element (12). It extends in the area between the split ring (13) attached to the impeller and the impeller hub (8) and the shaft seal (7). The free end face of the ring element (11) has a surface (14) running radially to the shaft, on the smallest diameter of which a nozzle (15) pointing in the axial direction to the shaft seal (7) is attached. The ring element (12) formed here as a sheet metal part can also be designed as a solid part which would have a backward rotation on the side facing the shaft seal. Furthermore, it can be formed in one piece with the split ring (16) fixed to the housing.

Das Ausführungsbeispiel der Fig. 2 entspricht weitgehend dem der Fig. 1. Ein Unterschied besteht darin, daß das Ring­element (12) an seiner freien Stirnseite nur mit einer in radialer Richtung zur Welle verlaufenden Fläche (14) versehen ist.The embodiment of FIG. 2 largely corresponds to that of FIG. 1. A difference is that the ring element (12) is provided on its free end face only with a surface (14) extending in the radial direction to the shaft.

Die Fig. 3 zeigt ein im Querschnitt kegelstumpfförmig ausgebildetes Ringelement (12), welches diagonal zur Wellenachse verläuft, wobei seine freie Stirnseite (17) der Welle (5) zugekehrt ist. Infolge der kegelstumpfförmigen Ausbildung des Ringelementes (12) existiert an seiner freien Stirnseite (17), ebenso wie an den daran angebrachten, in den Fig. 1 und 2 gezeigten kleinsten Durchmessern der Fläche (14) bzw. eines daran angebrachten Stutzens (15) eine Abreißkante, mit deren Hilfe innerhalb des Raumes (10) ein Erosions­verschleiß verhindert werden kann.Fig. 3 shows a frustoconical ring element (12) which extends diagonally to the shaft axis, its free end face (17) facing the shaft (5). As a result of the frustoconical design of the ring element (12), there is one on its free end face (17), as well as on the smallest diameters of the surface (14) or a nozzle (15) attached to it shown in FIGS. 1 and 2 Tear-off edge, with the help of which erosion wear can be prevented within the space (10).

Claims (11)

1. Strömungsmaschine, insbesondere Kreiselpumpe mit innerhalb eines Gehäuses angeordnetem Laufrad und einer dem Laufrad nachgeordneten Wellenabdichtung, insbesondere Gleitringdichtung, dadurch gekennzeichnet, daß im Gehäuse (1) ein die Wellenabdichtung (7) ganz oder teilweise überdeckendes, mit seiner einen Stirnseite am Gehäuse (1,11) anliegend befestigtes Ringelement (12) angeordnet ist, daß die freie andere Stirnseite des Ringelementes (12) dem Laufrad (2) zugekehrt ist, daß zwischen der freien Stirnseite und Welle (5) und/oder Laufradnabe (8) ein Zwischenraum besteht und daß das Ringelement (12) annähernd parallel oder in Richtung der freien Stirnseite zur Welle geneigt verläuft.1. Turbomachine, in particular a centrifugal pump with an impeller arranged within a housing and a shaft seal downstream of the impeller, in particular a mechanical seal, characterized in that in the housing (1) a shaft seal (7) completely or partially overlapping, with its one end face on the housing (1 , 11) adjacent ring element (12) is arranged such that the free other end face of the ring element (12) faces the impeller (2), that there is a gap between the free end face and shaft (5) and / or impeller hub (8) and that the ring element (12) extends approximately parallel or inclined towards the free end face to the shaft. 2. Strömungsmaschine nach Anspruch 1, dadurch gekennzeichnet, daß das Ringelement (12) mit seiner freien Stirnseite im Bereich zwischen einem am Laufrad (2) angeordneten Spaltring (13) und der Welle (5) angeordnet ist.2. Turbomachine according to claim 1, characterized in that the ring element (12) is arranged with its free end face in the region between a split ring (13) arranged on the impeller (2) and the shaft (5). 3. Strömungsmaschine nach Anspruch 1, dadurch gekennzeichnet, daß die freie Stirnseite des Ringelementes (12) in einem von im Laufrad (2) angeordneten Axialschubausgleichs­bohrungen (9) überdeckten Durchmesserbereich angeordnet ist.3. Turbomachine according to claim 1, characterized in that the free end face of the ring element (12) is arranged in a diameter range covered by axial thrust compensation bores (9) arranged in the impeller (2). 4. Strömungsmaschine nach den Ansprüchen 1 bis 3, dadurch gekennzeichnet, daß das Ringelement (12) im Querschnitt kegelstumpfförmig ausgebildet ist.4. Turbomachine according to claims 1 to 3, characterized in that the ring element (12) is frustoconical in cross section. 5. Strömungsmaschine nach Anspruch 4,dadurch gekennzeichnet, daß an der freien Stirnseite des Ringelementes (12) eine radial zur Welle (5) verlaufende Fläche (14) angebracht ist.5. Turbomachine according to claim 4, characterized in that on the free end face of the ring element (12) a radially to the shaft (5) extending surface (14) is attached. 6. Strömungsmaschine nach den Ansprüchen 1 bis 3, dadurch gekennzeichnet, daß das Ringelement (12) überwiegend parallel zur Welle (5) verläuft, wobei an seiner freien Stirnseite eine radial zur Welle verlaufende Fläche (14) angebracht ist.6. Turbomachine according to claims 1 to 3, characterized in that the ring element (12) runs predominantly parallel to the shaft (5), with a radially extending to the shaft surface (14) is attached to its free end face. 7. Strömungsmaschine nach einem oder mehreren der Ansprüche 1 bis 6, dadurch gekennzeichnet, daß der Abstand zwischen einem überwiegend parallel zur Welle (5) verlaufenden Ringelement (12) und einem mit dem Laufrad (2) rotierenden Spaltring (13) um ein Vielfaches größer ist als der Abstand innerhalb der Spaltringdichtung (4).7. Fluid machine according to one or more of claims 1 to 6, characterized in that the distance between a predominantly parallel to the shaft (5) extending ring element (12) and with the impeller (2) rotating split ring (13) many times larger is the distance within the split ring seal (4). 8. Strömungsmaschine nach einem oder mehreren der Ansprüche 1 bis 7, dadurch gekennzeichnet, daß an der radial zur Welle verlaufenden Fläche (14) auf kleinstem Durchmesser ein in axialer Richtung zur Wellenabdichtung (7) weisender Stutzen (15) angebracht ist.8. Turbomachine according to one or more of claims 1 to 7, characterized in that on the radially to the shaft surface (14) on the smallest diameter in the axial direction to the shaft seal (7) pointing nozzle (15) is attached. 9. Strömungsmaschine nach einem oder mehreren der Ansprüche 1 bis 8, dadurch gekennzeichnet, daß das Ringelement (12) und ein in das Gehäuse (1, 11) eingesetzter fester Spaltring (16) einteilig ausgebildet sind.9. Turbomachine according to one or more of claims 1 to 8, characterized in that the ring element (12) and in the housing (1, 11) inserted fixed split ring (16) are integrally formed. 10. Strömungsmaschine nach einem oder mehreren der Ansprüche 1 bis 9, dadurch gekennzeichnet, daß das Ringelement (12) als Blechformteil ausgebildet ist.10. Turbomachine according to one or more of claims 1 to 9, characterized in that the ring element (12) is designed as a sheet metal part. 11. Strömungsmaschine nach einem oder mehreren der Ansprüche 1 bis 9, dadurch gekennzeichnet, daß das Ringelement (12) als massives Bauteil ausgebildet und mit einer auf der dem Laufrad (2) abgekehrten Seite angeordneten Hinterdrehung versehen ist.11. Turbomachine according to one or more of claims 1 to 9, characterized in that the ring element (12) is designed as a solid component and is provided with a rear rotation arranged on the side facing away from the impeller (2).
EP89109759A 1988-06-13 1989-05-30 Liquid-displacement machine Expired - Lifetime EP0346677B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT89109759T ATE75818T1 (en) 1988-06-13 1989-05-30 FLOW MACHINE.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3820062A DE3820062A1 (en) 1988-06-13 1988-06-13 FLOWING MACHINE
DE3820062 1988-06-13

Publications (2)

Publication Number Publication Date
EP0346677A1 true EP0346677A1 (en) 1989-12-20
EP0346677B1 EP0346677B1 (en) 1992-05-06

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Family Applications (2)

Application Number Title Priority Date Filing Date
EP89109759A Expired - Lifetime EP0346677B1 (en) 1988-06-13 1989-05-30 Liquid-displacement machine
EP89906085A Pending EP0442883A1 (en) 1988-06-13 1989-05-30 Turbine

Family Applications After (1)

Application Number Title Priority Date Filing Date
EP89906085A Pending EP0442883A1 (en) 1988-06-13 1989-05-30 Turbine

Country Status (10)

Country Link
US (1) US5171126A (en)
EP (2) EP0346677B1 (en)
JP (1) JPH0646037B2 (en)
AT (1) ATE75818T1 (en)
CA (1) CA1330908C (en)
DE (2) DE3820062A1 (en)
DK (1) DK171831B1 (en)
ES (1) ES2032073T3 (en)
GR (1) GR3005061T3 (en)
WO (1) WO1989012755A1 (en)

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EP2520804A4 (en) * 2009-12-28 2018-03-14 Ebara Corporation Pump impeller and submersible pump having such pump impeller

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DE19503318C2 (en) * 1995-02-02 1997-11-20 Kronos Titan Gmbh Rinsing the seal on a pump for pumping highly saline media
GB2307276A (en) * 1996-03-06 1997-05-21 Shell Int Research Multi-phase fluid compressor
DE50012259D1 (en) * 2000-01-11 2006-04-27 Sulzer Pumpen Ag Winterthur Turbomachine for a fluid with a radial sealing gap between stator and a rotor
PE20141829A1 (en) * 2008-05-27 2014-12-16 Weir Minerals Australia Ltd IMPROVEMENTS RELATED TO CENTRIFUGAL PUMPS
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2904038A1 (en) * 2006-07-19 2008-01-25 Snecma Sa Centrifugal compressor impeller downstream face cooling system for aircraft turbomachine e.g. turbojet and jet prop engines, has cylindrical passage and sheet guiding drawn ventilating air till neighborhood of downstream face of impeller
US7841187B2 (en) 2006-07-19 2010-11-30 Snecma Turbomachine comprising a system for cooling the downstream face of an impeller of a centrifugal compressor
EP2520804A4 (en) * 2009-12-28 2018-03-14 Ebara Corporation Pump impeller and submersible pump having such pump impeller

Also Published As

Publication number Publication date
US5171126A (en) 1992-12-15
DE3820062A1 (en) 1989-12-21
DK171831B1 (en) 1997-06-23
EP0346677B1 (en) 1992-05-06
GR3005061T3 (en) 1993-05-24
JPH0646037B2 (en) 1994-06-15
WO1989012755A1 (en) 1989-12-28
CA1330908C (en) 1994-07-26
JPH03501761A (en) 1991-04-18
ES2032073T3 (en) 1993-01-01
DK294990D0 (en) 1990-12-12
DE58901311D1 (en) 1992-06-11
EP0442883A1 (en) 1991-08-28
ATE75818T1 (en) 1992-05-15
DK294990A (en) 1990-12-12

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