Liquid-displacement machine
Abstract
This record has no abstract on file.
Term
Term ended
Expired 30 May 2009, 17.3 years ago.
- Priority
- Filed
- Granted
- Expired
- Today
11 claims: 11 independent, 0 dependent
- 1A turbomachine, more particularly a centrifugal pump with an impeller arranged within a housing, a shaft seal arranged downstream from the impeller, more particularly a mechanical seal, in the case of which the housing has a space surrounding the shaft seal, characterized in that within the space (10) a ring element (12) is arranged which partly or completely covers over the shaft seal (7) and is attached so that its one end side is in engagement with the wall of the space, in that the free other end side of the ring element (12) is turned towards the impeller (2), in that between the free end side and the shaft (5) and/or the hub (8) of the impeller an intermediate space is present and in that the ring element (12) extends approximately parallel or inclined towards the free end side in relation to the shaft. 1. Strömungsmaschine, insbesondere Kreiselpumpe mit innerhalb eines Gehäuses angeordnetem Laufrad, einer dem Laufrad nachgeordneten Wellenabdichtung, insbesondere Gleitringdichtung und wobei das Gehäuse einen die Wellenabdichtung umgebenden Raum aufweist, dadurch gekennzeichnet, daß in dem Raum (10) ein die Wellenabdichtung (7) ganz oder teilweise überdeckendes, mit seiner einen Stirnseite an der Raumwandung 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. Turbo machine, en particulier pompe centrifuge avec roue située à l'intérieur d'un corps, avec un système d'étanchéité de l'arbre situé en aval de la roue, en particulier une garniture étanche à anneau glissant, dans laquelle le corps présente un espace entourant le système d'étanchéité de l'arbre, caractérisée en ce que dans l'espace (10) est situé un élément annulaire (12) qui recouvre entièrement ou en partie le système d'étanchéité (7) et est fixé à la paroi adjacente de l'espace par une de ses faces, en ce que l'autre face libre de l'élément annulaire (12) est tournée vers la roue (2), en ce qu'il existe un espace intermédiaire entre la face libre et l'arbre (5) et/ou le moyeu de la roue (8) et en ce que l'élément annulaire (12) est de forme presque parallèle ou inclinée en direction de la face libre vers l'arbre.
- 2Strömungsmaschine 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. The turbomachine as claimed in claim 1, characterized in that the ring element (12) is arranged so that its free end side is in the part between a gap ring (13), which is arranged on the impeller (2), and the shaft (5). 2. Turbo machine selon la revendication 1 caractérisée en ce que l'élément annulaire (12) avec sa face libre est placé dans la zone située entre une bague à fente (13) placée sur la roue (2) et l'arbre (5).
- 3Strömungsmaschine 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. The turbomachine as claimed in claim 1, characterized in that the free end side of the ring element (12) is arranged in a diameter range occupied by axial thrust compensation holes (9) provided in the impeller (2). 3. Turbo machine selon la revendication 1 caractérisée en ce que la face libre de l'élément annulaire (12) est située dans une zone diamétrale couverte d'alésages (9) de compensation de la poussée axiale placés dans la roue (2).
- 4Strömungsmaschine nach den Ansprüchen 1 bis 3, dadurch gekennzeichnet, daß das Ringelement (12) im Querschnitt kegelstumpfförmig ausgebildet ist. 4. The turbomachine as claimed in any one of the preceding claims 1 through 3, characterized in that the ring element (12) is frustoconical in cross section. 4. Turbo machine selon les revendications 1 à 3 caractérisée en ce que l'élément annulaire (12) a une section de la forme d'un tronc de cône.
- 5Strömungsmaschine nach Anspruch 4,dadurch gekennzeichnet, daß an der freien Stirnseite des Ringelementes (12) eine radial zur Welle (5) verlaufende Fläche (14) angebracht ist. 5. The turbomachine as claimed in claim 4, characterized in that a surface (14), which extends radially in relation to the shaft (5), is arranged on the free end side of the ring element (12). 5. Turbo machine selon la revendication 4 caractérisée en ce qu'une surface (14) radiale à l'arbre (5) est placée sur la face de l'élément annulaire (12).
- 6Strömungsmaschine 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. The turbomachine as claimed in any one of the preceding claims 1 through 3, characterized in that the ring element (12) extends predominantly parallel to'the shaft (5), a surface (14) extending parallel to the shaft being arranged on the free end side of the ring element. 6. Turbo machine selon les revendications 1 à 3 caractérisée en ce que l'élément annulaire (12) est en grande partie parallèle à l'arbre (5) et que, sur sa face libre, est placée une surface (14) radiale à l'arbre.
- 7Strömungsmaschine 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. The turbomachine as claimed in any one or more of the preceding claims 1 through 6, characterized in that the distance between a ring element (12), which predominantly extends parallel to the shaft (5) and a gap ring (13), which rotates with the impeller (5) is many times greater than the distance within the gap ring seal (4). 7. Turbo machine selon une ou plusieurs des revendications 1 à 6 caractérisée en ce que l'écart entre un élément annulaire (12) qui est en grande partie parallèle à l'arbre (5) et la bague à fente (13) tournant avec la roue (2) est beaucoup plus grand que l'écart à l'intérieur du joint de la bague à fente (4).
- 8Strömungsmaschine 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. The turbomachine as claimed in any one or more of the preceding claims 1 through 7, characterized in that a hollow stud (15) is arranged on the surface (14) which extends radially towards the shaft, on a minimum diameter, such stud extending in the axial direction in relation to the shaft seal (7). 8. Turbo machine selon une ou plusieurs des revendications 1 à 7 caractérisée en ce qu'une tubulure (15) dirigée axialement en direction du système d'étanchéité (7) de l'arbre est placée-sur la surface (14) radiale à l'arbre là où le diamètre est le plus petit.
- 9Strömungsmaschine 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. The turbomachine as claimed in any one or more of the preceding claims 1 through 8, characterized in that the ring element (12) and a fixed gap ring (16), which is inserted into the housing (1 and 11), are integral. 9. Turbo machine selon une ou plusieurs des revendications 1 à 8 caractérisée en ce que l'élément annulaire (12) une bague fixe à fente (16) placée dans le corps (1, 11) sont en une pièce.
- 10Strömungsmaschine nach einem oder mehreren der Ansprüche 1 bis 9, dadurch gekennzeichnet, daß das Ringelement (12) als Blechformteil ausgebildet ist. 10. The turbomachine as claimed in any one or more of the preceding claims 1 through 9, characterized in that the ring element (12) is in the form of a sheet metal pressing. 10. Turbo machine selon une ou plusieurs des revendications 1 à 9 caractérisée en ce que l'élément annulaire (12) a la forme d'une pièce de tôle.
- 11Strömungsmaschine 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. The turbomachine as claimed in any one or more of the preceding claims 1 through 9, characterized in that the ring element (12) is constituted by a solid component and is provided with an undercut on the side thereof turned away from the impeller (2). 11. Turbo machine selon une ou plusieurs des revendications 1 à 9 caractérisée en ce que l'élément annulaire (12) a la forme d'une pièce massive et qu'il est tourné vers l'arrière sur le côté tournant dos à la roue (2).
Independent claims11
12 paragraphs, as filed
The invention relates to a flow machine according to the preamble of the main claim.
In flow machines, which are subjected to a solids-containing fluid handled Risk of Erosionsverschleisses within the turbomachine. Although argument can be countered by a corresponding lining of the body, however, there is a particularly vulnerable point in the region of the shaft seal. In conveying medium solids contained, which may have a size of up to 1 mm, the shaft seal itself or the shaft seal will be able to destroy holding housing parts. Premature failure of the turbo machine would thereby given
From US-A 17 22 439 is a cartridge mechanical seal, which is flanged with the aid of a flange on a shaft passage having a housing opening, is known. The medium to be shut off from the exposed cover mechanical seal cartridge has an inlet opening, in which a pump impeller hub fits sealing. A rotating the pressure-side impeller side contains solids conveying medium would destroy the cover and then the sealing rubber bellows of the mechanical seal in the shortest time. There is also the risk that the sealing rings are destroyed due to dry running due to the lack of possibility for fluid communication within the mechanical seal.
The invention is based on the object for a flow machine, which is subjected to a solids conveying medium containing the aforementioned order to provide a measure by which a shaft seal surrounding space and the shaft seal can be protected even against erosion wear. This object is performed in accordance with the characterizing part of the main claim.
In practical tests it has surprisingly been found that an erosion wear, an erosive wear was a designed according to the main claim ring element are turned off by contained in the medium solids, up to 100 mg solids was added per dm. Dependent claims 2 and 3 indicate advantageous embodiments of the invention and the position of the free end of the annular element.
In the claims 4 to 8 described embodiments of the invention cause hazardous wear marks neither the shaft sealing even where the shaft seal surrounding space were observed. In experiments with an impeller, which was provided on the shaft seal side facing a split ring seal, the split ring seal has been damaged within a short time without the ring member. Was instead placed in the shaft sealing space receiving an inventive ring element, then even on the split ring seal no wear marks were observed after a long test period. The embodiments of claims 9 to 11 describe the various possibilities for the production of the ring element.
Embodiments of the invention are illustrated in the drawings and will be described in more detail below. The
Figs. 1 to 3 show in this case differently shaped ring elements.
Fig. 1 shows a housing (1) of a turbomachine, which is designed here as a centrifugal pump, as well as within the housing (1) disposed impeller (2). In the embodiment selected here, the impeller suction and discharge gap ring seals (3, 4) is equipped. The impeller (2) is mounted on a shaft (5), is mounted on the further comprising a shaft sleeve (6) and constructed as a shaft seal shaft seal (7). Furthermore, the impeller (2) has in the region of the impeller hub (8) in the pressure-side impeller cover plate mounted on Axialschubausgleichsbohrungen (9).
Within the shaft seal (7) surrounding the chamber (10), here a pressure-side housing cover (11) is disposed in the housing (1) fixed ring element (12). It extends in the area between the mounted on the impeller wear ring (13) and the wheel hub (8) and the shaft seal (7). The free end of the annular element (11) has a radially extending to the shaft surface (14), pointing to the smallest diameter in the axial direction to the shaft seal (7) port (15) is mounted. The here designed as sheet-metal molding ring member (12) may also be formed as a solid molding, which would have on the side facing the shaft seal side a back rotation. Furthermore, it may be formed integrally with the housing-fixed ring gap (16).
The embodiment of FIG. 2 corresponds largely to that of FIG. 1. A difference is that the ring element (12) is provided at its free end face with a straight line extending in radial direction towards the shaft surface (14).
FIG. 3 shows a cross-sectionally frustoconical formed ring member (12) which runs diagonally to the shaft axis, with its free end face (17) facing the shaft (5). Due to the frusto-conical configuration of the ring element (12) exists at its free end face (17), as well as to the attached thereto, in Figs. 1 and 2, the smallest diameter of the surface (14) or an attached piece (15) a tear-off edge, by means of which within the space (10), an erosion wear can be prevented.
Every citation, both ways
| Document | Relation | Office | Cited during |
|---|---|---|---|
| US5984629A | Cited by | United States of America | Search report |
| DE4431947A1 | Cited by | Germany | Search report |
16 members in 10 offices
Priority claims4
| Document | Office | Kind | Date |
|---|---|---|---|
| 3820062 | Germany | A | |
| 3820062 | Germany | – | |
| 3820062 | – | – | – |
| DE19883820062 | – | – | – |
Members16
| Document | Office | Kind | |
|---|---|---|---|
| EP0346677A1 | European Patent Office (EPO) | A1 | |
| DE3820062A1 | Germany | A1 | |
| WO8912755A1 | World Intellectual Property Organization (WIPO) | A1 | |
| DK294990A | Denmark | A | |
| DK294990D0 | Denmark | D0 | |
| JPH03501761A | Japan | A | |
| EP0442883A1 | European Patent Office (EPO) | A1 | |
| EP0346677B1This record | European Patent Office (EPO) | B1 | |
| AT75818T | Austria | T | |
| DE58901311D1 | Germany | D1 | |
| US5171126A | United States of America | A | |
| ES2032073T3 | Spain | T3 | |
| GR3005061T3 | Greece | T3 | |
| JPH0646037B2 | Japan | B2 | |
| CA1330908C | Canada | C | |
| DK171831B1 | Denmark | B1 |
47 legal events, as 4 offices reported them to INPADOC
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| Se: european patent in force in swedenEAL | EAL | EP | |
| No opposition filedOpposition26N | 26N | EP | |
| No opposition filed within time limitOppositionORIGINAL CODE: 0009261PLBE | PLBE | EP | |
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| Validation in greece3005061FG4A | FG4A | GR | |
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| Designated contracting statesAK | AK | EP | |
| Corresponds to:REF | REF | EP | |
| Miscellaneous (additional remarks)VERBUNDEN MIT 89906085.9/0442883 (EUROPAEISCHE ANMELDENUMMER/VEROEFFENTLICHUNGSNUMMER) DURCH ENTSCHEIDUNG VOM 23.10.91.XX | XX | EP | |
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| Miscellaneous (additional remarks)VERBUNDEN MIT 89906085.9/0442883 (EUROPAEISCHE ANMELDENUMMER/VEROEFFENTLICHUNGSNUMMER) DURCH ENTSCHEIDUNG VOM 23.10.91.XX | XX | EP | |
| Designated contracting states (corrected)RBV | RBV | EP | |
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Numbers
- Publication
- 0346677
- Publication, DOCDB
- 0346677
- Publication, EPODOC
- EP0346677
- Application
- 89109759
- Application, DOCDB
- 89109759
- Application, EPODOC
- EP19890109759
Titles3
- German
- Strömungsmaschine
- English
- LIQUID-DISPLACEMENT MACHINE
- French
- Machine à fluide dynamique
Classification
- CPC, 3
- F04D29/426
- F04D7/04
- F04D29/126
- IPC, 3
- F04D29 12
- F04D7 04
- F04D29 42
Designated states12
- Contracting states, 12
- Austria
- Belgium
- Switzerland
- Germany
- Spain
- France
- United Kingdom
- Greece
- Italy
- Liechtenstein
- Netherlands (Kingdom of the)
- Sweden