EP2558726A2 - Compressor flange for screw-type compressor - Google Patents

Compressor flange for screw-type compressor

Info

Publication number
EP2558726A2
EP2558726A2 EP11716393A EP11716393A EP2558726A2 EP 2558726 A2 EP2558726 A2 EP 2558726A2 EP 11716393 A EP11716393 A EP 11716393A EP 11716393 A EP11716393 A EP 11716393A EP 2558726 A2 EP2558726 A2 EP 2558726A2
Authority
EP
European Patent Office
Prior art keywords
compressor
flange
housing
drive
compressor flange
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
EP11716393A
Other languages
German (de)
French (fr)
Other versions
EP2558726B2 (en
EP2558726B1 (en
Inventor
Engelbert KÖCK
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.)
Knorr Bremse Systeme fuer Schienenfahrzeuge GmbH
Original Assignee
Knorr Bremse Systeme fuer Schienenfahrzeuge GmbH
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=44626006&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP2558726(A2) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Knorr Bremse Systeme fuer Schienenfahrzeuge GmbH filed Critical Knorr Bremse Systeme fuer Schienenfahrzeuge GmbH
Publication of EP2558726A2 publication Critical patent/EP2558726A2/en
Application granted granted Critical
Publication of EP2558726B1 publication Critical patent/EP2558726B1/en
Publication of EP2558726B2 publication Critical patent/EP2558726B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/08Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
    • F04C18/082Details specially related to intermeshing engagement type pumps
    • F04C18/086Carter
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/0042Driving elements, brakes, couplings, transmissions specially adapted for pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/08Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
    • F04C18/12Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
    • F04C18/14Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
    • F04C18/16Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with helical teeth, e.g. chevron-shaped, screw type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C27/00Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
    • F04C27/005Axial sealings for working fluid
    • F04C27/006Elements specially adapted for sealing of the lateral faces of intermeshing-engagement type pumps, e.g. gear pumps

Definitions

  • the invention relates to a compressor flange for connecting a
  • Screw compressor with a drive having the features of the preamble of claim 1. Furthermore, the invention relates to a screw compressor with such a compressor flange.
  • the connecting elements regularly comprise a connecting flange, which is connectable to a front cover of the screw compressor.
  • the front cover closes and seals the compressor housing to the outside.
  • a refrigeration compressor with horizontally flanged electric motor emerges, which in the closed design a Flange member for connecting the compressor with the electric motor comprises.
  • the compressor housing has a hub-like projection for receiving the drive shaft and for receiving a centrally arranged projection of the flange component, so that upon insertion of the flange component, a centering thereof takes place.
  • a further centering of the compressor in relation to the electric motor is intended to take place by means of a further annular step designed concentrically for the centric approach.
  • On a Gleitringwellenabdichtung is omitted here, as a certain leakage is accepted or desired. Furthermore, there is a hole in the
  • Flange member provided to supply lubricant from the electric motor to the interior of the compressor housing.
  • the object of the present invention is to provide a compressor flange for connecting a screw compressor with a drive, which requires little manufacturing and assembly work and combines several functions in one component.
  • the stated compressor flange for connecting a screw compressor to a drive has a central opening for receiving a shaft and / or a bearing and has a first annular contact surface for engagement with a housing of the compressor and a second annular contact surface for engagement with a housing of the drive.
  • the compressor flange further comprises axially and / or radially effective seals for sealing against the Compressor housing and / or the shaft, so that an open compressor housing by use of the compressor flange is closed and sealed.
  • the seals form components of the connecting flange, so that the use of separate sealing means, which must be mounted separately from the flange, is not required.
  • the compressor flange thus simultaneously assumes the function of an end cover, which is usually provided for closing and sealing a screw compressor.
  • the number of required components can therefore be reduced, so that consequently the manufacturing and assembly costs are reduced.
  • the axially and / or radially effective seals can in grooves on
  • Compressor flange used or molded or molded.
  • the seal against the shaft in the region of the bearing of the shaft, so that the seal is not exposed to dynamic stress.
  • the seal thus has a long service life.
  • the compressor flange has an axially effective seal for sealing against the housing of the drive.
  • a tight connection of the screw compressor is ensured on the housing of the drive.
  • an annular step is formed on at least one end face of the compressor flange for centering the compressor flange with respect to the compressor housing, the shaft, the bearing and / or the housing of the drive.
  • the compressor flange at the same time has a centering function and makes additional connecting elements, for example in the form of centering pins, dispensable.
  • an annular step for centering with respect to the compressor housing and the drive is formed on both end faces of the compressor flange.
  • an axial projection for axially fixing the position of the bearing is formed on the end facing the compressor housing. That is, after connection of the compressor flange with the compressor housing, the axial projection is supported on a radially extending surface of the bearing.
  • the axial projection can also be designed in such a way that it replaces a ring stage arranged on the compressor side for centering.
  • the axial projection is preferably used in such a manner formed in a recess formed on the compressor housing or the bearing, which is not only axially, but also radially supported the axial approach.
  • the axial approach to the compressor in this way fulfills a holding and a centering function.
  • the flange may have an annular step in the form that it receives the lateral surface of the shaft bearing and fixes its axial position. As a result, a centering of the flange is reached at the camp. The latter can be achieved in that the bearing end protrudes axially beyond the compressor housing or in that the compressor housing a corresponding
  • the compressor flange can preferably be fastened by means of screws to the compressor housing.
  • bores for receiving the screws are provided in the region of the first annular abutment surface for abutment of the compressor flange on the compressor housing.
  • the compressor flange is pot-shaped and limited in contact with the compressor housing and the housing of the drive has a cavity for receiving a coupling which connects the shaft of the compressor with a shaft of the drive.
  • the housing of the coupling through the compressor flange allows the elimination of a clutch bell and thus the use of a simple coupling.
  • the number of component be further reduced.
  • the space requirement is reduced due to the smaller overall size. Finally, weight can be saved.
  • the end face forms in the region of the bottom of the pot-shaped compressor Fiansches the first annular contact surface for conditioning of the
  • Compressor fins on the compressor housing off are also in the area of the bottom of the cup-shaped
  • the cavity radially delimiting and the bottom of the cup-shaped Verêtrfiansches opposite end face forms the second annular contact surface for abutment of the Kompressorfiansches on the housing of the drive.
  • Compressor flange further openings, in particular maintenance and / or
  • Vents own. These are preferably designed such that the sealing function of the compressor flange is ensured.
  • the single FIGURE shows the section of a screw compressor 2 in the region of the connection to a drive 3, the connection being effected via a compressor flange 1.
  • the compressor flange 1 combines several functions in one component, since it not only establishes a connection between the compressor 2 and the drive 3, but also at its end faces 16, 17 annular stages 14, 15 at the same time a centering of the compressor 2 with respect to the drive 3 allows. At the same time, the compressor flange 1 replaces a front cover for
  • the radially effective seal 12 is sealingly against a bearing 6, which is provided for supporting the shaft 5 of the compressor 2.
  • the seal against the shaft 5 of the compressor 2 thus takes place indirectly via the bearing 6. This has the advantage that the radially effective seal 12 is not exposed to any dynamic load.
  • Another axially effective seal 13 is provided in the end face 17 for sealing the compressor skirt 1 with respect to the housing 10 of the drive 3.
  • the end face 17 also forms a second annular 6.3fiambae 9 for conditioning of the compressor fins 1 on the housing 10 of the drive 3 from.
  • screws 19 are provided, which are guided by bores in the end face 16 for screwing the Kompressorfiansches 1 with the compressor housing 8. The screws 19 ensure axial prestressing of the compressor skirt 1 relative to the compressor housing 8, whereby the axially effective seal 11 is pressed against the compressor housing 8.
  • the compressor case 1 further satisfies a
  • the axial projection 18 engages positively in an annular recess of the compressor housing 8.
  • a centering of the compressor Fibers against the compressor housing 8 and / or the shaft 5 of the compressor 2 is given.
  • an axial receptacle 23 for axially fixing the position of the bearing 6 in the area of the end face 16 can also be provided.
  • the bearing 6 is designed such that it protrudes in the axial direction, so that it in the axial
  • Recess 23 is at least partially used (not shown).
  • the compressor flange 1 of the illustrated embodiment is further cup-shaped, so that between a bottom portion axially on the
  • Compressor housing 8 is struck and a side wall portion, a cavity 20 is formed, the present case of receiving a coupling 21 for
  • the compressor flange 1 thus also assumes a protective function, which the
  • the compressor flange according to the invention shown in the figure thus can combine the functions of a front cover, a flange and a protective cover in itself, while he takes care of a centering, holding and sealing function. All these functions are realized by a single component, so that the number of required components are significantly reduced and the

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
  • Compressor (AREA)

Abstract

The invention relates to a compressor flange (1) for connecting a screw-type compressor (2) to a drive (3), wherein the compressor flange (1) has a central opening (4) for receiving a shaft (5) and/or a bearing (6) and a first annular bearing face (7) for bearing on a housing (8) of the compressor (2) and a second annular bearing face (9) for bearing on a housing (10) of the drive (3). According to the invention, the compressor flange (1) also comprises axially and/or radially effective seals (11, 12) for forming a seal with respect to the compressor housing (8) and/or the shaft (5), with the result that an open compressor housing (8) can be closed off and sealed by insertion of the compressor flange (1). In addition, the device relates to a screw-type compressor with such a compressor flange.

Description

Verdichterflansch für Schraubenverdichter  Compressor flange for screw compressors
Gebiet der Erfindung Field of the invention
Die Erfindung betrifft ein Verdichterflansch zur Verbindung eines The invention relates to a compressor flange for connecting a
Schraubenverdichters mit einem Antrieb mit den Merkmalen des Oberbegriffs des Anspruchs 1. Ferner betrifft die Erfindung einen Schraubenverdichter mit einem solchen Verdichter flansch. Screw compressor with a drive having the features of the preamble of claim 1. Furthermore, the invention relates to a screw compressor with such a compressor flange.
Derzeit verfügbare Schraubenkompressoren weisen zur Verbindung mit einem Antrieb Verbindungselemente auf, die zur Zentrierung mit einem Zentrierbund oder Zentrierstiften versehen sind. Die Verbindungselemente umfassen regelmäßig einen Verbindungsflansch, der mit einem Stirndeckel des Schraubenkompressors verbindbar ist. Der Stirndeckel schließt und dichtet das Verdichtergehäuse nach außen ab. Es sind somit regelmäßig mehrere Bauteile erforderlich, die zur Currently available screw compressors for connection to a drive on connecting elements, which are provided for centering with a centering or centering pins. The connecting elements regularly comprise a connecting flange, which is connectable to a front cover of the screw compressor. The front cover closes and seals the compressor housing to the outside. There are thus regularly several components required for
Verbindung des Schraubenkompressors mit einem Antrieb entsprechend positioniert und befestigt werden müssen. Der Fertigungs- und Montageaufwand ist somit sehr hoch. Connection of the screw compressor with a drive must be positioned and secured accordingly. The production and assembly costs are therefore very high.
Stand der Technik State of the art
Aus der Auslegeschrift DE 10 44 122 A geht ein Kälteverdichter mit waagerecht angeflanschtem Elektromotor hervor, der in der geschlossenen Ausführung ein Flanschbauteil zur Verbindung des Verdichters mit dem Elektromotor umfasst. Das Verdichtergehäuse weist einen nabenartigen Ansatz zur Aufnahme der Antriebswelle und zur Aufnahme eines zentrisch angeordneten Ansatzes des Flanschbauteils auf, so dass bei Einsetzen des Flanschbauteils eine Zentrierung desselben erfolgt. Durch eine weitere zum zentrischen Ansatz konzentrisch ausgebildete Ringstufe soll eine Zentrierung des Verdichters in Bezug auf den Elektromotor erfolgen. Auf eine Gleitringwellenabdichtung wird vorliegend verzichtet, da eine gewisse Leckage hingenommen wird bzw. erwünscht ist. Des Weiteren ist eine Bohrung im From the patent application DE 10 44 122 A, a refrigeration compressor with horizontally flanged electric motor emerges, which in the closed design a Flange member for connecting the compressor with the electric motor comprises. The compressor housing has a hub-like projection for receiving the drive shaft and for receiving a centrally arranged projection of the flange component, so that upon insertion of the flange component, a centering thereof takes place. A further centering of the compressor in relation to the electric motor is intended to take place by means of a further annular step designed concentrically for the centric approach. On a Gleitringwellenabdichtung is omitted here, as a certain leakage is accepted or desired. Furthermore, there is a hole in the
Flanschbauteil vorgesehen, um Schmiermittel aus dem Elektromotor dem Innern des Verdichtergehäuses zuzuführen. Flange member provided to supply lubricant from the electric motor to the interior of the compressor housing.
Aufgabe der vorliegenden Erfindung ist es, einen Verdichterflansch zur Verbindung eines Schraubenverdichters mit einem Antrieb bereitzustellen, der einen geringen Fertigungs- und Montageaufwand erfordert und mehrere Funktionen in einem Bauteil vereint. The object of the present invention is to provide a compressor flange for connecting a screw compressor with a drive, which requires little manufacturing and assembly work and combines several functions in one component.
Die Aufgabe wird gelöst durch einen Verdichterflansch mit den Merkmalen des Anspruchs 1. Vorteilhafte Weiterbildungen der Erfindung werden in den auf Anspruch 1 direkt oder indirekt rückbezogenen Unteransprüchen angegeben. Des Weiteren wird ein Schraubenverdichter mit einem solchen Verdichterflansch zur Lösung der Aufgabe vorgeschlagen. The object is achieved by a compressor flange with the features of claim 1. Advantageous developments of the invention are specified in the dependent claim 1 directly or indirectly dependent claims. Furthermore, a screw compressor with such a compressor flange is proposed for achieving the object.
Offenbarung der Erfindung Der angegebene Verdichterflansch zur Verbindung eines Schraubenverdichters mit einem Antrieb weist eine zentrale Öffnung zur Aufnahme einer Welle und/oder eines Lagers auf und besitzt eine erste ringförmige Anlagefläche zur Anlage an einem Gehäuse des Verdichters und eine zweite ringförmige Anlagefläche zur Anlage an einem Gehäuse des Antriebs. Erfindungsgemäß umfasst der Verdichterflansch ferner axial und/oder radial wirksame Dichtungen zur Abdichtung gegenüber dem Verdichtergehäuse und/oder der Welle, so dass ein offenes Verdichtergehäuse durch Einsatz des Verdichterflansches verschließbar und abdichtbar ist. Die Dichtungen bilden Bestandteile des Verbindungsflansches aus, so dass der Einsatz separater Dichtmittel, die getrennt vom Flanschbauteil montiert werden müssen, nicht erforderlich ist. Der Verdichterflansch übernimmt somit gleichzeitig die Funktion eines Stirndeckels, der üblicherweise zum Verschließen und Abdichten eines Schraubenverdichters vorgesehen ist. D.h., der Verdichterflansch übernimmt neben der Verbindungsfunktion auch eine Verschluss- und eine Abdichtungsfunktion. Die Anzahl der erforderlichen Bauteile kann demnach reduziert werden, so dass folglich auch der Fertigungs- und der Montageaufwand verringert werden. DISCLOSURE OF THE INVENTION The stated compressor flange for connecting a screw compressor to a drive has a central opening for receiving a shaft and / or a bearing and has a first annular contact surface for engagement with a housing of the compressor and a second annular contact surface for engagement with a housing of the drive. According to the invention, the compressor flange further comprises axially and / or radially effective seals for sealing against the Compressor housing and / or the shaft, so that an open compressor housing by use of the compressor flange is closed and sealed. The seals form components of the connecting flange, so that the use of separate sealing means, which must be mounted separately from the flange, is not required. The compressor flange thus simultaneously assumes the function of an end cover, which is usually provided for closing and sealing a screw compressor. This means that the compressor flange not only performs the connection function but also a closing and sealing function. The number of required components can therefore be reduced, so that consequently the manufacturing and assembly costs are reduced.
Die axial und/oder radial wirksamen Dichtungen können in Nuten am The axially and / or radially effective seals can in grooves on
Verdichterflansch eingesetzt oder angespritzt bzw. angeformt sein. Vorzugsweise erfolgt die Abdichtung gegenüber der Welle im Bereich des Lagers der Welle, so dass die Dichtung keiner dynamischen Belastung ausgesetzt ist. Die Dichtung weist somit eine hohe Lebensdauer auf. Compressor flange used or molded or molded. Preferably, the seal against the shaft in the region of the bearing of the shaft, so that the seal is not exposed to dynamic stress. The seal thus has a long service life.
Bevorzugt ist ferner vorgesehen, dass der Verdichterflansch eine axial wirksame Dichtung zur Abdichtung gegenüber dem Gehäuse des Antriebs besitzt. Somit ist auch ein dichter Anschluss des Schraubenverdichters am Gehäuse des Antriebs gewährleistet. Preferably, it is further provided that the compressor flange has an axially effective seal for sealing against the housing of the drive. Thus, a tight connection of the screw compressor is ensured on the housing of the drive.
Des Weiteren bevorzugt ist eine Ringstufe an wenigstens einer Stirnfläche des Verdichterflansches zur Zentrierung des Verdichterflansches in Bezug auf das Verdichtergehäuse, die Welle, das Lager und/oder das Gehäuse des Antriebs ausgebildet. Somit weist der Verdichterflansch zugleich eine Zentrierfunktion auf und macht weitere Verbindungselemente, beispielsweise in Form von Zentrierstiften, entbehrlich. Vorzugsweise ist an beiden Stirnflächen des Verdichterflansches jeweils eine Ringstufe zur Zentrierung gegenüber dem Verdichtergehäuse und dem Antrieb ausgebildet. Vorteilhafterweise ist an der dem Verdichtergehäuse zugewandten Stirnfläche ein axialer Ansatz zur axialen Lagefixierung des Lagers ausgebildet. D.h., dass nach Verbindung des Verdichterflansches mit dem Verdichtergehäuse der axiale Ansatz an einer radial verlaufenden Fläche des Lagers abgestützt ist. Der axiale Ansatz kann ferner derart ausgebildet sein, dass er eine verdichterseitig angeordnete Ringstufe zur Zentrierung ersetzt. Hierzu ist der axiale Ansatz vorzugsweise derart in eine am Verdichtergehäuse oder dem Lager ausgebildete Ausnehmung einsetzbar, das der axiale Ansatz nicht nur axial, sondern auch radial abgestützt ist. Der axiale Ansatz am Verdichterflansch erfüllt auf diese Weise eine Halte- und eine Zentrierfunktion. Further preferably, an annular step is formed on at least one end face of the compressor flange for centering the compressor flange with respect to the compressor housing, the shaft, the bearing and / or the housing of the drive. Thus, the compressor flange at the same time has a centering function and makes additional connecting elements, for example in the form of centering pins, dispensable. Preferably, an annular step for centering with respect to the compressor housing and the drive is formed on both end faces of the compressor flange. Advantageously, an axial projection for axially fixing the position of the bearing is formed on the end facing the compressor housing. That is, after connection of the compressor flange with the compressor housing, the axial projection is supported on a radially extending surface of the bearing. The axial projection can also be designed in such a way that it replaces a ring stage arranged on the compressor side for centering. For this purpose, the axial projection is preferably used in such a manner formed in a recess formed on the compressor housing or the bearing, which is not only axially, but also radially supported the axial approach. The axial approach to the compressor in this way fulfills a holding and a centering function.
Alternativ kann auch der Flansch eine Ringstufe in der Form aufweisen, dass diese die Mantelfläche des Wellenlagers aufnimmt und dessen axiale Position fixiert. Hierdurch wird auch eine Zentrierung des Flansches am Lager erreicht. Letzteres kann dadurch erreicht werden, dass das Lagerende axial über das Verdichtergehäuse herausragt oder dadurch, dass das Verdichtergehäuse eine entsprechende Alternatively, the flange may have an annular step in the form that it receives the lateral surface of the shaft bearing and fixes its axial position. As a result, a centering of the flange is reached at the camp. The latter can be achieved in that the bearing end protrudes axially beyond the compressor housing or in that the compressor housing a corresponding
Ausnehmung aufweist. Has recess.
Der Verdichterflansch ist vorzugsweise mittels Schrauben am Verdichtergehäuse befestigbar. Hierzu sind im Bereich der ersten ringförmigen Anlagefläche zur Anlage des Verdichterflansches am Verdichtergehäuse Bohrungen zur Aufnahme der Schrauben vorgesehen. The compressor flange can preferably be fastened by means of screws to the compressor housing. For this purpose, bores for receiving the screws are provided in the region of the first annular abutment surface for abutment of the compressor flange on the compressor housing.
Gemäß einem bevorzugten Ausführungsbeispiel ist der Verdichterflansch topfförmig ausgebildet und begrenzt in Anlage am Verdichtergehäuse und am Gehäuse des Antriebs einen Hohlraum zur Aufnahme einer Kupplung, welche die Welle des Verdichters mit einer Welle des Antriebs verbindet. Die Einhausung der Kupplung durch den Verdichterflansch ermöglicht den Wegfall einer Kupplungsglocke und damit den Einsatz einer einfachen Kupplung. Somit kann die Anzahl der Bauteil weiter reduziert werden. Ferner verringert sich der Platzbedarf, aufgrund der geringeren Gesamtbaugröße. Schließlich kann auch Gewicht eingespart werden. According to a preferred embodiment, the compressor flange is pot-shaped and limited in contact with the compressor housing and the housing of the drive has a cavity for receiving a coupling which connects the shaft of the compressor with a shaft of the drive. The housing of the coupling through the compressor flange allows the elimination of a clutch bell and thus the use of a simple coupling. Thus, the number of component be further reduced. Furthermore, the space requirement is reduced due to the smaller overall size. Finally, weight can be saved.
Mit einer Reduzierung der Anzahl der Bauteile geht ferner ein reduzierter With a reduction in the number of components is also a reduced
Montageaufwand einher, da weniger Bauteile zueinander ausgerichtet und miteinander befestigt werden müssen. Zudem reduzieren sich die Stellen, die zusätzlich abgedichtet werden müssen. Auch eine Aufsummierung von Fertigungsund/oder Montagetoleranzen wird hierdurch sicher vermieden. Die am Verdichterfiansch vorgesehenen Dichtungen gewährleisten auch bei Wegfall einer Kupplungsglocke, dass die im Hohlraum des topfförmigen Verdichterflansches aufgenommene Kupplung ausreichend geschützt ist. Dieser Schutz kann auch gewährleistet werden, wenn beispielsweise der Einsatz des Schraubenverdichters in teilweise eingetauchtem Betrieb erfolgt. Des Weiteren kann der Hohlraum zur Aufnahme eines Schmiermediums dienen, da über die Dichtungen des Assembly costs associated with fewer components aligned with each other and must be secured together. In addition, the places that need to be additionally sealed are reduced. Even a summation of manufacturing and / or assembly tolerances is thereby safely avoided. The seals provided on the compressor flange ensure, even if a clutch bell is removed, that the coupling received in the cavity of the cup-shaped compressor flange is sufficiently protected. This protection can also be ensured if, for example, the screw compressor is used in partially submerged operation. Furthermore, the cavity can serve to receive a lubricant, since the seals of the
Verdichterfiansches sichergestellt ist, dass kein Schmiermedium nach außen gelangt. Sofern im Bereich der Welle eine Schmiermittelleckage auftreten sollte, dient der Hohlraum des topfförmigen Verdichterflansches dem Auffangen des ausgetretenen Schmiermittels.  It is ensured by the compressor that no lubricating medium escapes to the outside. If a lubricant leakage should occur in the area of the shaft, the cavity of the cup-shaped compressor flange serves to catch the leaked lubricant.
Vorzugsweise bildet die Stirnfläche im Bereich des Bodens des topfförmigen Verdichterfiansches die erste ringförmige Anlagefläche zur Anlage des Preferably, the end face forms in the region of the bottom of the pot-shaped compressor Fiansches the first annular contact surface for conditioning of the
Verdichterfiansches am Verdichtergehäuse aus. Somit kann in einfacher Weise die Deckelfunktion des Verdichterfiansches realisiert werden. Die zentrale Öffnung zur Aufnahme der Welle ist ebenfalls im Bereich des Bodens des topfförmigen Compressor fins on the compressor housing off. Thus, the cover function of the compressor fins can be realized in a simple manner. The central opening for receiving the shaft is also in the area of the bottom of the cup-shaped
Verdichterfiansches vorgesehen. Weiterhin vorzugsweise bildet die den Hohlraum radial begrenzende und dem Boden des topfförmigen Verdichterfiansches gegenüberliegende Stirnfläche die zweite ringförmige Anlagefläche zur Anlage des Verdichterfiansches am Gehäuse des Antriebs aus. Zur Wartung und/oder zur Entlüftung des Schraubenverdichters kann der Compressor finssches provided. Further preferably, the cavity radially delimiting and the bottom of the cup-shaped Verdichterfiansches opposite end face forms the second annular contact surface for abutment of the Kompressorfiansches on the housing of the drive. For maintenance and / or ventilation of the screw compressor, the
Verdichterflansch ferner Öffnungen, insbesondere Wartungs- und/oder Compressor flange further openings, in particular maintenance and / or
Entlüftungsöffnungen, besitzen. Diese sind vorzugsweise derart ausgebildet, dass die Dichtfunktion des Verdichterflansches gewährleistet bleibt. Vents, own. These are preferably designed such that the sealing function of the compressor flange is ensured.
Zur Lösung der Aufgabe wird ferner ein Schraubenverdichter mit einem To solve the problem is also a screw compressor with a
erfindungsgemäßen Verdichterflansch vorgeschlagen, wobei der Verdichterflansch zugleich als Stirndeckel zum Verschließen und Abdichten des Verdichtergehäuses und als Verbindungsflansch zur Verbindung des Verdichtergehäuses mit dem proposed compressor flange according to the invention, wherein the compressor flange at the same time as an end cover for closing and sealing the compressor housing and as a connecting flange for connecting the compressor housing with the
Gehäuse des Antriebes dient. Dabei kann der vom Verdichterflansch umschlossene Raum - in Abhängigkeit von den Anforderungen der verwendeten Kupplungsart, der Art der Wellenverbindung oder weiteren sich aus der Anwendung ergebenden Anforderungen - als offener oder geschlossener Verdichter ausgeführt sein. Eine bevorzugte Ausführungsform der Erfindung wird nachfolgend anhand der einzigen Figur näher erläutert. Diese zeigt einen erfindungsgemäßen Housing of the drive is used. In this case, the space enclosed by the compressor flange - depending on the requirements of the type of coupling used, the type of shaft connection or other requirements resulting from the application - be designed as an open or closed compressor. A preferred embodiment of the invention will be explained in more detail with reference to the single figure. This shows an inventive
Verdichtungsflansch in Anlage an einen Verdichtergehäuse und einem Gehäuse eines Antriebs. Ausführliche Beschreibung der Zeichnung Compression flange in contact with a compressor housing and a housing of a drive. Detailed description of the drawing
Die einzige Figur zeigt den Ausschnitt eines Schraubenverdichters 2 im Bereich des Anschlusses an einen Antrieb 3, wobei der Anschluss über einen Verdichterflansch 1 bewirkt wird. Der Verdichterflansch 1 vereint mehrere Funktionen in einem Bauteil, da er nicht nur eine Verbindung zwischen dem Verdichter 2 und dem Antrieb 3 herstellt, sondern über an seinen Stirnflächen 16, 17 ausgebildete Ringstufen 14, 15 gleichzeitig eine Zentrierung des Verdichters 2 in Bezug auf den Antrieb 3 ermöglicht. Zugleich ersetzt der Verdichterflansch 1 einen Stirndeckel zum The single FIGURE shows the section of a screw compressor 2 in the region of the connection to a drive 3, the connection being effected via a compressor flange 1. The compressor flange 1 combines several functions in one component, since it not only establishes a connection between the compressor 2 and the drive 3, but also at its end faces 16, 17 annular stages 14, 15 at the same time a centering of the compressor 2 with respect to the drive 3 allows. At the same time, the compressor flange 1 replaces a front cover for
Verschließen und Abdichten des Gehäuses 8 des Verdichters 2, indem in einer ersten ringförmigen Anlagefläche 7 zur Anlage des Verdichterflansches 1 am Verdichtergehäuse 8 eine axial wirksame Dichtung 1 1 eingelassen ist. Des Weiteren dichtet der Verdichterfiansch 1 gegenüber einer Welle 5 des Verdichters 2 ab, welche durch eine zentrale Öffnung 4 des Verdichterfiansches 1 hindurchgeführt ist. Hierzu ist im Bereich der zentralen Öffnung 4 eine radial wirksame Dichtung 12 im Closing and sealing the housing 8 of the compressor 2, by in a first annular bearing surface 7 for conditioning the compressor flange 1 on Compressor housing 8 an axially effective seal 1 1 is inserted. Furthermore, the compressor skirt 1 seals against a shaft 5 of the compressor 2, which is passed through a central opening 4 of the compressor rotor 1. For this purpose, in the region of the central opening 4, a radially effective seal 12 in
Verdichterfiansch 1 eingelassen. Die radial wirksame Dichtung 12 liegt dichtend an einem Lager 6 an, das zur Lagerung der Welle 5 des Verdichters 2 vorgesehen ist. Die Abdichtung gegenüber der Welle 5 des Verdichters 2 erfolgt somit mittelbar über das Lager 6. Dies hat den Vorteil, dass die radial wirksame Dichtung 12 keiner dynamischen Belastung ausgesetzt ist. Compressor fiansch 1 inserted. The radially effective seal 12 is sealingly against a bearing 6, which is provided for supporting the shaft 5 of the compressor 2. The seal against the shaft 5 of the compressor 2 thus takes place indirectly via the bearing 6. This has the advantage that the radially effective seal 12 is not exposed to any dynamic load.
Eine weitere axial wirksame Dichtung 13 ist in der Stirnfläche 17 zur Abdichtung des Verdichterfiansches 1 gegenüber dem Gehäuse 10 des Antriebs 3 vorgesehen. Die Stirnfläche 17 bildet zudem eine zweite ringförmige Anlagefiäche 9 zur Anlage des Verdichterfiansches 1 am Gehäuse 10 des Antriebs 3 aus. Zur Fixierung des Verdichterfiansches 1 am Verdichtergehäuse 8 sind Schrauben 19 vorgesehen, die durch Bohrungen in der Stirnfläche 16 zur Verschraubung des Verdichterfiansches 1 mit dem Verdichtergehäuse 8 geführt werden. Die Schrauben 19 gewährleisten eine axiale Vorspannung des Verdichterfiansches 1 gegenüber dem Verdichtergehäuse 8, wobei auch die axial wirksame Dichtung 11 an das Verdichtergehäuse 8 gedrückt wird. Another axially effective seal 13 is provided in the end face 17 for sealing the compressor skirt 1 with respect to the housing 10 of the drive 3. The end face 17 also forms a second annular Anlagefiäche 9 for conditioning of the compressor fins 1 on the housing 10 of the drive 3 from. To fix the compressor Fiansches 1 on the compressor housing 8 screws 19 are provided, which are guided by bores in the end face 16 for screwing the Kompressorfiansches 1 with the compressor housing 8. The screws 19 ensure axial prestressing of the compressor skirt 1 relative to the compressor housing 8, whereby the axially effective seal 11 is pressed against the compressor housing 8.
Die Ringstufe 14 im Bereich der Stirnfläche 16 ist bei der dargestellten The annular step 14 in the region of the end face 16 is shown in the illustrated
Ausführungsform als axialer Ansatz 18 ausgebildet, mittels derer das Lager 6 in Position gehalten wird. Somit erfüllt der Verdichterfiansch 1 ferner eine Embodiment designed as an axial projection 18, by means of which the bearing 6 is held in position. Thus, the compressor case 1 further satisfies a
Haltefunktion, wobei das Halten des Lagers 6 durch die Verbindung mittels derHolding function, wherein the holding of the bearing 6 by the connection by means of
Schrauben 19 gewährleistet wird. Der axiale Ansatz 18 greift hierzu formschlüssig in eine ringförmige Ausnehmung des Verdichtergehäuses 8 ein. Somit ist gleichzeitig über den axialen Ansatz 18 auch eine Zentrierung des Verdichterfiansches gegenüber dem Verdichtergehäuse 8 und/oder der Welle 5 des Verdichters 2 gegeben. Alternativ oder ergänzend zum axialen Ansatz 18 kann im Bereich der Stirnfläche 16 zudem eine axiale Aufnahme 23 zur axialen Lagefixierung des Lagers 6 im Screw 19 is guaranteed. For this purpose, the axial projection 18 engages positively in an annular recess of the compressor housing 8. Thus, at the same time via the axial projection 18 and a centering of the compressor Fibers against the compressor housing 8 and / or the shaft 5 of the compressor 2 is given. As an alternative or in addition to the axial projection 18, an axial receptacle 23 for axially fixing the position of the bearing 6 in the area of the end face 16 can also be provided
Verdichterflansch ausgebildet sein. Vorteilhafterweise ist hierzu das Lager 6 derart ausgebildet, dass es in axialer Richtung vorsteht, so dass es in die axiale Be formed compressor flange. Advantageously, for this purpose, the bearing 6 is designed such that it protrudes in the axial direction, so that it in the axial
Ausnehmung 23 zumindest teilweise einsetzbar ist (nicht dargestellt). Recess 23 is at least partially used (not shown).
Der Verdichterflansch 1 der dargestellten Ausführungsform ist ferner topfförmig ausgebildet, so dass zwischen einem Bodenbereich, der axial an dem The compressor flange 1 of the illustrated embodiment is further cup-shaped, so that between a bottom portion axially on the
Verdichtergehäuse 8 angeschlagen ist und einem Seitenwandbereich ein Hohlraum 20 ausgebildet wird, der vorliegend der Aufnahme einer Kupplung 21 zur Compressor housing 8 is struck and a side wall portion, a cavity 20 is formed, the present case of receiving a coupling 21 for
Verbindung der Welle 5 des Verdichters 2 mit der Welle 22 des Antriebs 3 dient. Der Verdichterflansch 1 übernimmt somit auch eine Schutzfunktion, welche die  Connection of the shaft 5 of the compressor 2 with the shaft 22 of the drive 3 is used. The compressor flange 1 thus also assumes a protective function, which the
Anordnung einer Kupplungsglocke entbehrlich macht. Die Dichtungen 11, 13 stellen dabei sicher, dass der zwischen dem Verdichter 2 und dem Antrieb 3 ausgebildete Hohlraum 20 nach außen abgedichtet ist. Disposal of a clutch bell makes unnecessary. The seals 11, 13 ensure that the cavity 20 formed between the compressor 2 and the drive 3 is sealed to the outside.
Der in der Figur dargestellte erfindungsgemäße Verdichterflansch vermag somit die Funktionen eines Stirndeckels, eines Flansches und einer Schutzhaube in sich zu vereinen, wobei er gleichzeitig eine Zentrier-, Halte- und Dichtungsfunktion übernimmt. Alle diese Funktionen werden durch ein einziges Bauteil verwirklicht, so dass die Anzahl erforderlicher Bauteile deutlich reduziert werden und der The compressor flange according to the invention shown in the figure thus can combine the functions of a front cover, a flange and a protective cover in itself, while he takes care of a centering, holding and sealing function. All these functions are realized by a single component, so that the number of required components are significantly reduced and the
Fertigungs- und Montageaufwand deutlich verringert werden kann. Zugleich werden Baugröße und Gewicht eines Schraubenverdichters reduziert, so dass dieser weniger Bauraum erfordert. Bezugszeichenliste Manufacturing and assembly costs can be significantly reduced. At the same time size and weight of a screw compressor are reduced, so that this requires less space. LIST OF REFERENCE NUMBERS
1 Verdichterflansch 1 compressor flange
2 Verdichter  2 compressors
3 Antrieb  3 drive
4 zentrale Öffnung  4 central opening
5 Welle des Verdichters  5 shaft of the compressor
6 Lager  6 bearings
7 erste ringförmige Anlagefläche  7 first annular contact surface
8 Gehäuse des Verdichters  8 housing of the compressor
9 zweite ringförmige Anlagefläche  9 second annular contact surface
10 Gehäuse des Antriebs  10 housing of the drive
11 axial wirksame Dichtung  11 axially effective seal
12 radial wirksame Dichtung  12 radially effective seal
13 axial wirksame Dichtung  13 axially effective seal
14 Ringstufe  14 ring step
15 Ringstufe  15 ring step
16 Stirnfläche  16 face
17 Stirnfläche  17 face
18 axialer Ansatz  18 axial approach
19 Schrauben  19 screws
20 Hohlraum  20 cavity
21 Kupplung  21 clutch
22 Welle des Antriebs  22 shaft of the drive
23 Aufnahme  23 recording

Claims

A n s p r ü c h e Claims
1. Verdichterflansch (1) zur Verbindung eines Schraubenverdichters (2) mit einem Antrieb (3), wobei der Verdichterflansch (1) eine zentrale Öffnung (4) zur Aufnahme einer Welle (5) und/oder eines Lagers (6) aufweist und eine erste ringförmige Anlagefläche (7) zur Anlage an einem Gehäuse (8) des Verdichters (2) und eine zweite ringförmige Anlagefläche (9) zur Anlage an einem Gehäuse (10) des Antriebs (3) besitzt, Compressor flange (1) for connecting a screw compressor (2) with a drive (3), wherein the compressor flange (1) has a central opening (4) for receiving a shaft (5) and / or a bearing (6) and a first annular abutment surface (7) for abutment with a housing (8) of the compressor (2) and a second annular abutment surface (9) for abutment with a housing (10) of the drive (3),
dadurch gekennzeichnet, dass der Verdichterflansch (1) ferner axial und/oder radial wirksame Dichtungen (11, 12) zur Abdichtung gegenüber dem characterized in that the compressor flange (1) further comprises axially and / or radially effective seals (11, 12) for sealing against the
Verdichtergehäuse (8) und/oder der Welle (5) umfasst, so dass ein offenes  Compressor housing (8) and / or the shaft (5), so that an open
Verdichtergehäuse (8) durch Einsatz des Verdichterflansches (1) verschließbar und abdichtbar ist. Compressor housing (8) by use of the compressor flange (1) can be closed and sealed.
2. Verdichterflansch nach Anspruch 1 , 2. compressor flange according to claim 1,
dadurch gekennzeichnet, dass der Verdichterflansch (1) ferner eine axial wirksame Dichtung (13) zur Abdichtung gegenüber dem Gehäuse (10) des Antriebs (3) besitzt. characterized in that the compressor flange (1) further comprises an axially effective seal (13) for sealing against the housing (10) of the drive (3).
3. Verdichterflansch nach Anspruch 1 oder 2, 3. compressor flange according to claim 1 or 2,
dadurch gekennzeichnet, dass eine Ringstufe (14, 15) an wenigstens einer characterized in that an annular step (14, 15) on at least one
Stirnfläche (16, 17) des Verdichterflansches (1) zur Zentrierung des End face (16, 17) of the compressor flange (1) for centering the
Verdichterflansches (1) in Bezug auf das Verdichtergehäuse (8), die Welle (5) und/oder das Gehäuse (10) des Antriebs (3) ausgebildet ist. Compressor flange (1) with respect to the compressor housing (8), the shaft (5) and / or the housing (10) of the drive (3) is formed.
4. Verdichterflansch nach einem der vorhergehenden Ansprüche, 4. compressor flange according to one of the preceding claims,
dadurch gekennzeichnet, dass an der dem Verdichtergehäuse (8) zugewandten Stirnfläche (16) ein axialer Ansatz (18) zur axialen Lagefixierung des Lagers (6) ausgebildet ist. characterized in that on the compressor housing (8) facing end face (16) an axial projection (18) for the axial positional fixing of the bearing (6) is formed.
5. Verdichterflansch nach einem der vorhergehenden Ansprüche, 5. compressor flange according to one of the preceding claims,
dadurch gekennzeichnet, dass an der dem Verdichtergehäuse (8) zugewandten Stirnfläche (16) eine axiale Aufnahme (23) zur axialen Lagefixierung des Lagers (6) ausgebildet ist. characterized in that on the compressor housing (8) facing end face (16) an axial receptacle (23) for the axial positional fixing of the bearing (6) is formed.
6. Verdichterflansch nach einem der vorhergehenden Ansprüche, 6. compressor flange according to one of the preceding claims,
dadurch gekennzeichnet, dass der Verdichterflansch (1) mittels Schrauben (19) am Verdichtergehäuse (8) befestigbar ist. characterized in that the compressor flange (1) by means of screws (19) on the compressor housing (8) can be fastened.
7. Verdichterflansch nach einem der vorhergehenden Ansprüche, 7. compressor flange according to one of the preceding claims,
dadurch gekennzeichnet, dass der Verdichterflansch (1) topfförmig ausgebildet ist und in Anlage am Verdichtergehäuse (8) und am Gehäuse (10) des Antriebs (3) einen Hohlraum (20) zur Aufnahme einer Kupplung (21) begrenzt, welche die Welle (5) des Verdichters (2) mit einer Welle (22) des Antriebs (3) verbindet. characterized in that the compressor flange (1) is cup-shaped and in abutment on the compressor housing (8) and the housing (10) of the drive (3) defines a cavity (20) for receiving a coupling (21), which the shaft (5 ) of the compressor (2) with a shaft (22) of the drive (3) connects.
8. Verdichterflansch nach Anspruch 7, 8. compressor flange according to claim 7,
dadurch gekennzeichnet, dass die Stirnfläche (16) im Bereich des Bodens des topfförmigen Verdichterflansches (1) die erste ringförmige Anlagefläche (7) ausbildet und die den Hohlraum (20) radial begrenzende und dem Boden characterized in that the end face (16) in the region of the bottom of the cup-shaped compressor flange (1), the first annular abutment surface (7) and the cavity (20) radially bounding and the bottom
gegenüberliegende Stirnfläche (17) die zweite ringförmige Anlagefläche (8) ausbildet. opposite end face (17) forms the second annular abutment surface (8).
9. Verdichterflansch nach einem der vorhergehenden Ansprüche, 9. compressor flange according to one of the preceding claims,
dadurch gekennzeichnet, dass der Verdichterflansch (1) ferner Öffnungen, insbesondere Wartungs- und/oder Entlüftungsöffhungen, besitzt. characterized in that the compressor flange (1) further openings, in particular maintenance and / or Entlüftungsöffhungen possesses.
10. Schraubenverdichter mit einem Verdichterflansch (1) nach einem der vorhergehenden Ansprüche, wobei der Verdichterflansch (1) zugleich als Stirndeckel zum Verschließen und Abdichten des Verdichtergehäuses (8) und als 10. Screw compressor with a compressor flange (1) according to one of the preceding claims, wherein the compressor flange (1) at the same time as a front cover for closing and sealing the compressor housing (8) and as
Verbindungsflansch zur Verbindung des Verdichtergehäuses (8) mit dem Connecting flange for connecting the compressor housing (8) with the
Gehäuse (10) des Antriebes (3) dient. Housing (10) of the drive (3) is used.
EP11716393.1A 2010-04-16 2011-04-13 Compressor flange for screw-type compressor Active EP2558726B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102010015151A DE102010015151A1 (en) 2010-04-16 2010-04-16 Compressor flange for screw compressors
PCT/EP2011/055754 WO2011128349A2 (en) 2010-04-16 2011-04-13 Compressor flange for screw-type compressor

Publications (3)

Publication Number Publication Date
EP2558726A2 true EP2558726A2 (en) 2013-02-20
EP2558726B1 EP2558726B1 (en) 2017-10-18
EP2558726B2 EP2558726B2 (en) 2023-03-29

Family

ID=44626006

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11716393.1A Active EP2558726B2 (en) 2010-04-16 2011-04-13 Compressor flange for screw-type compressor

Country Status (10)

Country Link
US (1) US9523363B2 (en)
EP (1) EP2558726B2 (en)
JP (1) JP5868387B2 (en)
CN (1) CN103154520B (en)
BR (1) BR112012026459B1 (en)
CA (1) CA2796626C (en)
DE (1) DE102010015151A1 (en)
MX (1) MX342998B (en)
RU (1) RU2561515C2 (en)
WO (1) WO2011128349A2 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010015151A1 (en) 2010-04-16 2011-10-20 Knorr-Bremse Systeme für Schienenfahrzeuge GmbH Compressor flange for screw compressors
DE102016011504A1 (en) 2016-09-21 2018-03-22 Knorr-Bremse Systeme für Nutzfahrzeuge GmbH System for a commercial vehicle comprising a screw compressor and an electric motor
DE102016011442A1 (en) 2016-09-21 2018-03-22 Knorr-Bremse Systeme für Nutzfahrzeuge GmbH System for a commercial vehicle comprising a screw compressor and an electric motor
DE102016011503A1 (en) 2016-09-21 2018-03-22 Knorr-Bremse Systeme für Nutzfahrzeuge GmbH System for a commercial vehicle comprising a screw compressor and an electric motor
CN106451843A (en) * 2016-10-27 2017-02-22 驰美电机(上海)有限公司 Special bearingless direct-connection sealing permanent-magnet synchronous motor with graphene winding for compressor
US20220145880A1 (en) * 2020-11-11 2022-05-12 Server Products, Inc. Flexible impeller pump for flowable food product

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE456832C (en) 1924-08-05 1928-03-02 Fikentscher Fa F Surface planer
AT196893B (en) 1956-07-07 1958-03-25 Raimund Culk Refrigeration compressor with horizontally flanged electric motor
US3209990A (en) 1962-01-18 1965-10-05 Atlas Copco Ab Two stage screw rotor machines
CH456832A (en) * 1966-11-04 1968-05-31 Wissenschaftl Techn Zentrum Wt Drive and bearing arrangement for screw compressors
GB1438324A (en) 1973-07-20 1976-06-03 Svenska Rotor Maskiner Ab Meshing-screw compressors
AR207639A1 (en) 1973-12-26 1976-10-22 Pfizer A PROCEDURE FOR PREPARING PIRIDO (3,2-D) 1,3-DIOXIN-6-EPOXYETHANS AND INTERMEDIARY COMPOUNDS UNPROVED OF THERAPEUTIC ACTIVITY
DE7927054U1 (en) * 1979-09-24 1981-10-15 Isartaler Schraubenkompressoren GmbH, 8192 Geretsried COMPRESSOR SYSTEM
DE3161646D1 (en) 1980-09-05 1984-01-19 British Nuclear Fuels Plc Pump for heavy gases
DE3149245A1 (en) 1981-12-11 1983-06-16 Isartaler Schraubenkompressoren GmbH, 8192 Geretsried "COMPRESSOR SYSTEM"
EP0408791B1 (en) * 1989-07-20 1994-03-16 Leybold Aktiengesellschaft Drag pump with a bell-shaped rotor
SE506513C2 (en) 1995-10-23 1997-12-22 Lysholm Techn Ab Transmission with a two-piece connector
DE19716549C2 (en) * 1997-04-19 2000-02-10 Compair Drucklufttechnik Gmbh Screw compressors for stationary or mobile compressors
DE19728434C2 (en) * 1997-07-03 1999-07-29 Busch Sa Atel Screw compressors for compressible media
JP2000170680A (en) * 1998-09-30 2000-06-20 Aisin Seiki Co Ltd Vacuum pump
ITBO20000668A1 (en) 2000-11-17 2002-05-17 Fini Elettrocostruzioni Meccan SCREW COMPRESSOR
WO2004053311A1 (en) 2002-12-10 2004-06-24 Ingersoll-Rand Energy Systems Corporation Hermetic motor and gas booster
JP2004301054A (en) 2003-03-31 2004-10-28 Toyota Industries Corp Hybrid compressor
JP2005163713A (en) 2003-12-04 2005-06-23 Toyota Industries Corp Fluid compressor
JP2005188326A (en) 2003-12-24 2005-07-14 Toyota Industries Corp Fluid compressor
EP1944273A1 (en) 2007-01-15 2008-07-16 Rockwool International A/S Process and apparatus for making mineral fibers
CN101624984B (en) 2009-08-05 2011-07-13 徐道敏 Vertical single screw air compressor
DE102010015151A1 (en) 2010-04-16 2011-10-20 Knorr-Bremse Systeme für Schienenfahrzeuge GmbH Compressor flange for screw compressors

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2011128349A2 *

Also Published As

Publication number Publication date
CA2796626C (en) 2018-06-26
RU2561515C2 (en) 2015-08-27
JP2013534582A (en) 2013-09-05
CA2796626A1 (en) 2011-10-20
DE102010015151A1 (en) 2011-10-20
EP2558726B2 (en) 2023-03-29
CN103154520A (en) 2013-06-12
US9523363B2 (en) 2016-12-20
MX2012011978A (en) 2012-12-17
US20130064694A1 (en) 2013-03-14
CN103154520B (en) 2016-03-16
BR112012026459A2 (en) 2016-08-09
BR112012026459B1 (en) 2021-01-26
WO2011128349A2 (en) 2011-10-20
EP2558726B1 (en) 2017-10-18
MX342998B (en) 2016-10-21
JP5868387B2 (en) 2016-02-24
WO2011128349A3 (en) 2013-05-02
RU2012148731A (en) 2014-05-27

Similar Documents

Publication Publication Date Title
EP2558726A2 (en) Compressor flange for screw-type compressor
DE19805003B4 (en) electric motor
EP2994644B1 (en) Pump arrangement comprising a plain bearing arrangement
DE102007025202A1 (en) Storage facility
EP1423630B1 (en) Sealing arrangement, especially for sealing the shaft of a spindle
EP3983691B1 (en) Gear motor comprising a gear, an electric motor, an adapter and a bellows coupling
DE112017005841T5 (en) VANE PUMP
DE102017211037A1 (en) Device for the axial mounting of a shaft in a housing and compressor device
EP3735536A1 (en) Blocking device of a fan
DE102022106059B3 (en) Flat gasket and rotary electric machine
DE102017007533A1 (en) Sealing arrangement of a stator of an electric machine to a housing
DE102017128360A1 (en) Electromotive drive unit
DE102008058284A1 (en) Hydraulic unit with a stator and a rotor having a hydraulic pump
DE102016102911B4 (en) Refrigerant compressor
EP2350460B1 (en) Hydraulic assembly with tank
DE102019127086A1 (en) Electric axle arrangement
DE102022127140A1 (en) Automotive thermal management valve seal and automotive thermal management valve
WO2022073548A1 (en) Sealing arrangement for wheel bearings, and wheel bearing unit comprising a sealing arrangement
WO2019063281A1 (en) Drive module of a motor vehicle with two receiving spaces sealed around a drive shaft
WO2020253920A1 (en) Electric motor
DE102019118697A1 (en) Gear pump
DE102022208141A1 (en) Pump, especially gear oil pump
WO2021254658A1 (en) Transmission comprising a shaft
DE102022111377A1 (en) Displacement machine based on the spiral principle
DE102020124063A1 (en) Release system

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

R17D Deferred search report published (corrected)

Effective date: 20130502

17P Request for examination filed

Effective date: 20131104

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

DAX Request for extension of the european patent (deleted)
REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Ref document number: 502011013151

Country of ref document: DE

Free format text: PREVIOUS MAIN CLASS: F04C0029000000

Ipc: F04C0018160000

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

RIC1 Information provided on ipc code assigned before grant

Ipc: F04C 29/00 20060101ALI20170515BHEP

Ipc: F04C 18/16 20060101AFI20170515BHEP

INTG Intention to grant announced

Effective date: 20170609

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 938194

Country of ref document: AT

Kind code of ref document: T

Effective date: 20171115

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502011013151

Country of ref document: DE

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: NL

Ref legal event code: FP

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 8

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180118

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180218

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180118

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180119

REG Reference to a national code

Ref country code: DE

Ref legal event code: R026

Ref document number: 502011013151

Country of ref document: DE

PLBI Opposition filed

Free format text: ORIGINAL CODE: 0009260

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

26 Opposition filed

Opponent name: BOGE KOMPRESSOREN OTTO BOGE GMBH CO. KG

Effective date: 20180718

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

PLAX Notice of opposition and request to file observation + time limit sent

Free format text: ORIGINAL CODE: EPIDOSNOBS2

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20180430

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20180413

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180413

PLBB Reply of patent proprietor to notice(s) of opposition received

Free format text: ORIGINAL CODE: EPIDOSNOBS3

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180413

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180430

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180430

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180430

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180413

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 938194

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180413

PLAY Examination report in opposition despatched + time limit

Free format text: ORIGINAL CODE: EPIDOSNORE2

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180413

PLBC Reply to examination report in opposition received

Free format text: ORIGINAL CODE: EPIDOSNORE3

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20110413

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20171018

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171018

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 20200420

Year of fee payment: 10

Ref country code: FR

Payment date: 20200421

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20200423

Year of fee payment: 10

Ref country code: IT

Payment date: 20200423

Year of fee payment: 10

REG Reference to a national code

Ref country code: SE

Ref legal event code: EUG

REG Reference to a national code

Ref country code: NL

Ref legal event code: MM

Effective date: 20210501

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210430

Ref country code: SE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210414

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210501

REG Reference to a national code

Ref country code: CH

Ref legal event code: PK

Free format text: BERICHTIGUNGEN

RIC2 Information provided on ipc code assigned after grant

Ipc: F04C 27/00 20060101ALI20220422BHEP

Ipc: F04C 18/16 20060101ALI20220422BHEP

Ipc: F04C 29/00 20060101ALI20220422BHEP

Ipc: F04C 18/08 20060101AFI20220422BHEP

PUAH Patent maintained in amended form

Free format text: ORIGINAL CODE: 0009272

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: PATENT MAINTAINED AS AMENDED

27A Patent maintained in amended form

Effective date: 20230329

AK Designated contracting states

Kind code of ref document: B2

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: DE

Ref legal event code: R102

Ref document number: 502011013151

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200413

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230530

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20230418

Year of fee payment: 13