EP2414684A1 - Geared compressor rotor for cold gas applications - Google Patents

Geared compressor rotor for cold gas applications

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Publication number
EP2414684A1
EP2414684A1 EP10716500A EP10716500A EP2414684A1 EP 2414684 A1 EP2414684 A1 EP 2414684A1 EP 10716500 A EP10716500 A EP 10716500A EP 10716500 A EP10716500 A EP 10716500A EP 2414684 A1 EP2414684 A1 EP 2414684A1
Authority
EP
European Patent Office
Prior art keywords
rotor
compressor rotor
impeller
segment
bearing
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
EP10716500A
Other languages
German (de)
French (fr)
Other versions
EP2414684B1 (en
Inventor
Volker Hütten
Andreas Peters
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.)
Siemens AG
Original Assignee
Siemens AG
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Filing date
Publication date
Application filed by Siemens AG filed Critical Siemens AG
Publication of EP2414684A1 publication Critical patent/EP2414684A1/en
Application granted granted Critical
Publication of EP2414684B1 publication Critical patent/EP2414684B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F04D29/02—Selection of particular materials
    • F04D29/023—Selection of particular materials especially adapted for elastic fluid 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
    • F04D25/00—Pumping installations or systems
    • F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
    • F04D25/163—Combinations of two or more pumps ; Producing two or more separate gas flows driven by a common gearing arrangement
    • 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
    • F04D29/102—Shaft sealings especially adapted for elastic fluid 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
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/266—Rotors specially for elastic fluids mounting compressor rotors on shafts
    • 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
    • F04D29/60—Mounting; Assembling; Disassembling
    • F04D29/62—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps
    • F04D29/624—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/502—Thermal properties
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/506—Hardness

Definitions

  • the invention relates to a transmission compressor rotor for cold gas applications with a pinion shaft having a toothed segment with a toothing, at least one impeller with an impeller hub and a sealing segment arranged between the toothed segment and the impeller hub, which carries a seal.
  • Turbo compressors are used in many ways in industry and power generation.
  • gearboxes are used for air separation, in the oxygen and nitrogen from
  • Ambient air are separated from each other.
  • an air compressor sucks in the filtered air and compresses it to the required pressure. Thereafter, the air is cooled and decomposed into the main components, ie nitrogen and oxygen and a small proportion of noble gas.
  • Compressor units then compress oxygen and nitrogen, for example, to feed them into a conduit system for further use.
  • a labyrinth seal in particular a multi-chamber seal, is usually arranged for gas separation and for maintaining the process-side pressure between a bearing and an impeller causing the compression of the rotor.
  • the impeller of the turbo-compressor is exposed to very low temperatures of below -30 0 C. In other gas separation processes temperatures below -150 0 C can be achieved. To a brittle fracture behavior at such low temperatures too avoid cold-hard materials for the production of the impeller. If low temperatures are realized in a gear compressor, not only the wheels but also the rotor shaft within the sealing areas up to the bearing points are to be protected from brittle fracture due to the low operating temperature.
  • the impeller or impellers and rotor shaft in the sealing area are typically made from a high alloy cold-strength steel in cold gas applications. For reasons of manufacturability and mountability pinion shaft and wheels are made separately. So that the pinion shaft, or the rotor shaft in the toothing region, meets high mechanical requirements, it is known to produce the pinion shaft from a different material than the impeller or its hub.
  • a gear compressor rotor of the aforementioned type form the sealing segment and the impeller hub, in particular the entire impeller, a common, integrally connected region of a first material and the toothed segment is formed of a second material.
  • a large portion of the rotor is made of the first material, which is adapted in its properties to the operating conditions of the impeller. The risk of cold embrittlement can be avoided with this design.
  • the joint between the two materials is moved very far inward in the warm-running area.
  • the toothed segment is in the operating temperature range and can be made of a conventional toothing material. This leads to very small transmission dimensions and thus at low cost and also low mechanical losses.
  • the turbocompressor is expediently a transmission compressor.
  • the gear segment may be part of a transmission that mechanically connects the gear compressor rotor to a drive, such as an electric motor.
  • the sealing segment may carry a part or a half of a seal, in particular a labyrinth seal for sealing an environment of the compressor region or impeller against a bearing of the rotor, in particular an oil bearing bearing.
  • the impeller is expediently part of an overhang stage of the turbocompressor and is expediently mounted on the fly. As a result, the impeller must be sealed only on one side with respect to a rotor bearing, so that the sealing effort is kept low.
  • the gear compressor rotor when the first material is a cold-tough material, which is cold-toughened than the second material.
  • the impeller is thus particularly well protected against brittle fracture behavior, whereas the inner portion of the rotor shaft can be designed according to the requirements placed on it.
  • the first material is in particular a cold-tough material, such as e.g. defined in the standard EN 10.269.
  • the second material is harder or higher strength than the first material.
  • the second material may be case hardened, nitrided or highly tempered steel, which accommodates the high mechanical requirements of a gear transmission.
  • a rotor bearing is arranged in the region of the second material.
  • the rotor bearing may be a radial bearing, which is designed in particular as a hydrodynamic sliding bearing.
  • Such a bearing can be supplied with warm lubricating oil at the temperature of for example 45 ° C, whereby a high heat input from the rotor bearing takes place on the rotor.
  • This heat input of the toothed area can be protected from the second material against a strong cooling. Due to the arrangement of the rotor bearing in the region of the second material also unnecessary greater heating of the first material and thus of the axially outer part of the rotor is avoided.
  • the shaft bearing is advantageously arranged between the sealing segment and the toothed segment. Due to the bearing of the rotor outside of the teeth, a stable flying bearing of the rotor can be achieved.
  • the two material areas are suitably rotatably connected to each other.
  • This non-rotatable connection can be achieved by a cohesive connection, such as a weld, a frictional connection, such as a clutch, or a positive connection.
  • this connection is formed by a spur gear, so that the two material areas engage one another positively. The risk of imbalance due to a welded joint or a slippage of the two areas against each other by an insufficiently strong frictional connection can be avoided.
  • the rotationally fixed connection is advantageously arranged between the sealing segment and a rotor bearing, for example the radial bearing.
  • Hirth connection Particularly suitable as a rotationally fixed connection between the two rotor regions or material regions of the rotor is a Hirth connection.
  • Hirtharm a fixed, self-centering and detachable connection is achieved by simple means.
  • the teeth of the Hirth toothing are in the sense of a non-positive Clutch static and surface to each other and are radially aligned, whereby the centering is achieved.
  • a very compact connection between the rotor areas can be achieved. For traction axial tension is necessary, which in turn limits the power transmission from one area to another.
  • Sealing segment 10 comprises a seal 12 in the form of a labyrinth seal.
  • the impeller 6 is cantilevered and is part of an overhang stage of
  • the gear compressor rotor 2 can be designed both with one and with two wheels.
  • Fig. 1 can be viewed as a half-view with a mirror plane in the toothed area.
  • the pinion shaft 16 ends with the lying behind the toothing second and not shown storage area.
  • the gear compressor rotor 2 is part of a turbo transmission compressor with a gear that connects a drive, such as a steam turbine or an electric motor, for power transmission with the impeller 6 by a toothing 14.
  • the toothing 14 of the rotor 2 is made on a pinion shaft 16, which can be divided into a toothed segment 18 and into a bearing region 20, which in turn form an inner region 22 of the rotor.
  • the pinion shaft 16 carries a rotor bearing 24 in the form of a radial bearing, namely a hydrodynamic sliding bearing.
  • the two areas 4, 22 are interconnected by a positive connection 26, which is indicated by an arrow. In the connection 26, the pinion shaft 16 and the impeller 6 are positively and rotatably connected to each other.
  • connection 26 is designed as a Hirth connection, wherein a screw 28 presses the two areas 4, 22 of the gear compressor rotor 2 axially against each other, so that high forces and torques can be transmitted from one to the other area 4, 22 by the Hirth connection.
  • the two areas 4, 22 are made of different materials.
  • the impeller hub 8 and the sealing segment 10 in the outer region 4 are made of a cold-tough material, such as the cold-tough steel X8Ni9.
  • the impeller hub 8 and the sealing segment 10 are made as an integral part, for example as a forging.
  • a weld between the impeller hub 8 and the seal segment 10 has been omitted to avoid the risk of imbalance due to uneven stress distribution.
  • the inner portion 22 and the pinion shaft 16 may be made of a case-hardened steel, for example 18CrNiMo7-6.
  • a high-strength tempering steel for example 56NiCrMoV7, is also advantageous. Both the case-hardened steel and the high-strength tempering steel are particularly hard and resistant to abrasion, so that the toothing 14 has a long service life. However, these steels are only partially cold-resistant, so there is a risk of brittle fracture at very low working temperatures.
  • a brittle fracture of the cold-tough steel of the outer region 4 is particularly suitable, so that the rotor shaft 2 for operation at particularly cold temperatures, for example below -30 0 C or below -120 0 C, for example, for air separation, is particularly suitable.
  • the rotor bearing 24 is supplied with warm lubricating oil, so that the hydrodynamic sliding bearing of the rotor 2 is ensured. With the warm lubricating oil heat is transferred to the inner portion 22 of the rotor 2, so that it never cools in the intended operation in a temperature range, which carries the risk of brittle fracture behavior of the pinion shaft 16.
  • the transmission can be designed to be particularly compact and wear-resistant.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)

Abstract

The invention relates to a geared compressor rotor (2) for cold gas applications having a pinion shaft (16) having a gear tooth segment (18) having gear teeth (14), at least one wheel (6) having a wheel hub (8) and a sealing segment (10) arranged between the gear tooth segment (14) and the wheel hub (8) that bears a seal (12). Said geared compressor rotor (2) also has high strength even in low temperature applications when the wheel hub (8) and the sealing segment (10) form a common, one-piece, connected region (4) made of a first material and the gear tooth segment (18) is produced from a second material.

Description

Beschreibungdescription
Getriebeverdichterrotor für KaltgasanwendungenGear compressor rotor for cold gas applications
Die Erfindung betrifft einen Getriebeverdichterrotor für Kaltgasanwendungen mit einer Ritzelwelle mit einem Verzahnungssegment mit einer Verzahnung, zumindest einem Laufrad mit einer Laufradnabe und einem zwischen dem Verzahnungssegment und der Laufradnabe angeordneten Dichtungssegment, das eine Dichtung trägt.The invention relates to a transmission compressor rotor for cold gas applications with a pinion shaft having a toothed segment with a toothing, at least one impeller with an impeller hub and a sealing segment arranged between the toothed segment and the impeller hub, which carries a seal.
Turboverdichter werden in der Industrie und in der Energieerzeugung in vielfältiger Weise eingesetzt. So werden beispielsweise Getriebeverdichter zur Luftzerlegung verwendet, bei der Sauerstoff und Stickstoff ausTurbo compressors are used in many ways in industry and power generation. For example, gearboxes are used for air separation, in the oxygen and nitrogen from
Umgebungsluft voneinander getrennt werden. Hierzu saugt ein Luftverdichter die gefilterte Luft an und komprimiert sie auf den erforderlichen Druck. Danach wird die Luft gekühlt und in die Hauptkomponenten zerlegt, also in Stickstoff und Sauerstoff sowie einen kleinen Anteil von Edelgas.Ambient air are separated from each other. For this purpose, an air compressor sucks in the filtered air and compresses it to the required pressure. Thereafter, the air is cooled and decomposed into the main components, ie nitrogen and oxygen and a small proportion of noble gas.
Verdichtereinheiten komprimieren Sauerstoff und Stickstoff anschließend, um sie beispielsweise in ein Leitungssystem zur weiteren Verwendung einzuspeisen.Compressor units then compress oxygen and nitrogen, for example, to feed them into a conduit system for further use.
Bei der Verdichtung von Sauerstoff müssen Schmieröl für die Lager des Verdichterrotors und das Fördermedium Sauerstoff wegen Explosionsgefahr sorgsam voneinander getrennt werden. Daher ist zur Gastrennung und zur Aufrechterhaltung des prozessseitigen Drucks zwischen einem Lager und einem die Verdichtung bewirkenden Laufrad des Rotors üblicherweise eine Labyrinthdichtung angeordnet, insbesondere eine Mehrkammerdichtung .When compressing oxygen, lubricating oil for the bearings of the compressor rotor and the pumped medium oxygen must be carefully separated from each other due to the risk of explosion. Therefore, a labyrinth seal, in particular a multi-chamber seal, is usually arranged for gas separation and for maintaining the process-side pressure between a bearing and an impeller causing the compression of the rotor.
Durch das Kühlen und anschließende Zerlegen der Luft ist das Laufrad des Turboverdichters sehr tiefen Temperaturen von unterhalb -300C ausgesetzt. Bei anderen Gastrennungsprozessen können Temperaturen unter -1500C erreicht werden. Um ein Sprödbruchverhalten bei solchen tiefen Temperaturen zu vermeiden, sind für die Herstellung des Laufrads kaltzähe Werkstoffe zu verwenden. Werden tiefe Temperaturen in einem Getriebeverdichter realisiert, so sind nicht nur die Laufräder sondern auch die Rotorwelle innerhalb der Dichtungsbereiche bis zu den Lagerstellen vor Sprödbruch infolge der geringen Betriebstemperatur zu schützen.By cooling and then decomposing the air, the impeller of the turbo-compressor is exposed to very low temperatures of below -30 0 C. In other gas separation processes temperatures below -150 0 C can be achieved. To a brittle fracture behavior at such low temperatures too avoid cold-hard materials for the production of the impeller. If low temperatures are realized in a gear compressor, not only the wheels but also the rotor shaft within the sealing areas up to the bearing points are to be protected from brittle fracture due to the low operating temperature.
Das Laufrad bzw. die Laufräder und die Rotorwelle im Dichtungsbereich werden bei Kaltgasanwendungen üblicherweise aus einem hoch legierten kaltzähen Stahl gefertigt. Aus Gründen der Herstellbarkeit und Montierbarkeit sind Ritzelwelle und Laufräder getrennt ausgeführt. Damit die Ritzelwelle, bzw. die Rotorwelle im Verzahnungsbereich, hohen mechanischen Anforderungen genügt, ist es bekannt, die Ritzelwelle aus einem anderen Werkstoff herzustellen als das Laufrad bzw. dessen Nabe.The impeller or impellers and rotor shaft in the sealing area are typically made from a high alloy cold-strength steel in cold gas applications. For reasons of manufacturability and mountability pinion shaft and wheels are made separately. So that the pinion shaft, or the rotor shaft in the toothing region, meets high mechanical requirements, it is known to produce the pinion shaft from a different material than the impeller or its hub.
Es ist eine Aufgabe der vorliegenden Erfindung, einen Getriebeverdichterrotor für einen Turboverdichter anzugeben, der bei Tieftemperaturanwendungen über eine hohe Festigkeit verfügt .It is an object of the present invention to provide a transmission compressor rotor for a turbocompressor having high strength in low temperature applications.
Diese Aufgabe wird durch einen Getriebeverdichterrotor der eingangs genannten Art gelöst, bei dem erfindungsgemäß das Dichtungssegment und die Laufradnabe, insbesondere das gesamte Laufrad, einen gemeinsamen, einstückig zusammenhängenden Bereich aus einem ersten Werkstoff bilden und das Verzahnungssegment aus einem zweiten Werkstoff gebildet ist. Hierdurch ist ein großer Bereich des Rotors aus dem ersten Werkstoff gefertigt, der in seinen Eigenschaften an die Betriebsbedingungen des Laufrads angepasst ist. Die Gefahr der Kaltversprödung kann mit diesem Design vermieden werden. Außerdem ist die Verbindungsstelle zwischen den beiden Werkstoffen sehr weit nach innen in den betriebswarmen Bereich verlegt. Das Verzahnungssegment liegt in dem betriebswarmen Bereich und kann aus einem konventionellen Verzahnungswerkstoff ausgeführt werden. Dies führt zu sehr kleinen Getriebeabmessungen und somit zu geringen Kosten und auch geringen mechanischen Verlusten.This object is achieved by a gear compressor rotor of the aforementioned type, according to the invention form the sealing segment and the impeller hub, in particular the entire impeller, a common, integrally connected region of a first material and the toothed segment is formed of a second material. As a result, a large portion of the rotor is made of the first material, which is adapted in its properties to the operating conditions of the impeller. The risk of cold embrittlement can be avoided with this design. In addition, the joint between the two materials is moved very far inward in the warm-running area. The toothed segment is in the operating temperature range and can be made of a conventional toothing material. This leads to very small transmission dimensions and thus at low cost and also low mechanical losses.
Der Turboverdichter ist zweckmäßigerweise ein Getriebeverdichter. Das Verzahnungssegment kann Teil eines Getriebes sein, das den Getriebeverdichterrotor mit einem Antrieb, beispielsweise einem Elektromotor, mechanisch verbindet. Das Dichtungssegment kann einen Teil oder eine Hälfte einer Dichtung tragen, insbesondere einer Labyrinthdichtung zur Abdichtung einer Umgebung des Verdichterbereichs bzw. Laufrads gegen ein Lager des Rotors, insbesondere ein Öl führendes Lager.The turbocompressor is expediently a transmission compressor. The gear segment may be part of a transmission that mechanically connects the gear compressor rotor to a drive, such as an electric motor. The sealing segment may carry a part or a half of a seal, in particular a labyrinth seal for sealing an environment of the compressor region or impeller against a bearing of the rotor, in particular an oil bearing bearing.
Das Laufrad ist zweckmäßigerweise Teil einer Überhangstufe des Turboverdichters und ist zweckmäßigerweise fliegend gelagert. Das Laufrad muss hierdurch nur an einer Seite gegenüber einem Rotorlager abgedichtet werden, sodass der Dichtungsaufwand gering gehalten ist.The impeller is expediently part of an overhang stage of the turbocompressor and is expediently mounted on the fly. As a result, the impeller must be sealed only on one side with respect to a rotor bearing, so that the sealing effort is kept low.
Besonders geeignet für die Anwendung im Tieftemperaturbereich von -30°C und tiefer ist der Getriebeverdichterrotor, wenn der erste Werkstoff ein kaltzäher Werkstoff ist, der kaltzäher ist als der zweite Werkstoff. Das Laufrad ist hierdurch besonders gut gegen ein Sprödbruchverhalten geschützt, wohingegen der innere Bereich der Rotorwelle entsprechend den an ihn gestellten Anforderungen ausgeführt sein kann. Der erste Werkstoff ist insbesondere ein kaltzäher Werkstoff, wie z.B. in der Norm EN 10.269 definiert.Particularly suitable for use in the low-temperature range of -30 ° C and lower is the gear compressor rotor, when the first material is a cold-tough material, which is cold-toughened than the second material. The impeller is thus particularly well protected against brittle fracture behavior, whereas the inner portion of the rotor shaft can be designed according to the requirements placed on it. The first material is in particular a cold-tough material, such as e.g. defined in the standard EN 10.269.
Vorteilhafterweise ist der zweite Werkstoff härter bzw. höherfester als der erste Werkstoff. Der zweite Werkstoff kann ein einsatzgehärteter, nitrierter oder hoch vergüteter Stahl sein, wodurch den hohen mechanischen Anforderungen an ein Zahnradgetriebe Rechnung getragen ist.Advantageously, the second material is harder or higher strength than the first material. The second material may be case hardened, nitrided or highly tempered steel, which accommodates the high mechanical requirements of a gear transmission.
In einer weiteren vorteilhaften Ausführungsform der Erfindung ist im Bereich des zweiten Werkstoffs ein Rotorlager angeordnet. Durch einen Wärmeeintrag des Rotorlagers kann der zweite Werkstoff vor zu starker Abkühlung geschützt werden. Das Rotorlager kann ein Radiallager sein, das insbesondere als hydrodynamisches Gleitlager ausgeführt ist. Ein solches Lager kann mit warmem Schmieröl mit der Temperatur von beispielsweise 45° C versorgt werden, wodurch ein hoher Wärmeeintrag vom Rotorlager auf den Rotor erfolgt. Durch diesen Wärmeeintrag kann der Verzahnungsbereich aus dem zweiten Werkstoff gegen eine starke Abkühlung geschützt werden. Durch die Anordnung des Rotorlagers im Bereich des zweiten Werkstoffs wird außerdem eine unnötige größere Erwärmung des ersten Werkstoffs und damit des axial äußeren Teils des Rotors vermieden.In a further advantageous embodiment of the invention, a rotor bearing is arranged in the region of the second material. By a heat input of the rotor bearing, the second material can be protected from excessive cooling. The rotor bearing may be a radial bearing, which is designed in particular as a hydrodynamic sliding bearing. Such a bearing can be supplied with warm lubricating oil at the temperature of for example 45 ° C, whereby a high heat input from the rotor bearing takes place on the rotor. By this heat input of the toothed area can be protected from the second material against a strong cooling. Due to the arrangement of the rotor bearing in the region of the second material also unnecessary greater heating of the first material and thus of the axially outer part of the rotor is avoided.
Das Wellenlager ist vorteilhafter Weise zwischen dem Dichtungssegment und dem Verzahnungssegment angeordnet. Durch die Lagerung des Rotors außerhalb der Verzahnung kann eine stabile fliegende Lagerung des Rotors erreicht werden.The shaft bearing is advantageously arranged between the sealing segment and the toothed segment. Due to the bearing of the rotor outside of the teeth, a stable flying bearing of the rotor can be achieved.
Die beiden Werkstoffbereiche sind zweckmäßigerweise drehfest miteinander verbunden. Diese drehfeste Verbindung kann durch eine Stoffschlüssige Verbindung, wie beispielsweise eine Verschweißung, eine reibschlüssige Verbindung, wie beispielsweise eine Kupplung, oder eine formschlüssige Verbindung erreicht werden. Vorteilhafterweise ist diese Verbindung durch eine Stirnverzahnung gebildet, sodass die beiden Werkstoffbereiche formschlüssig ineinander greifen. Die Gefahr einer Unwucht durch eine Schweißverbindung oder eines Rutschens der beiden Bereiche gegeneinander durch eine nicht ausreichend feste reibschlüssige Verbindung kann vermieden werden. Die drehfeste Verbindung ist vorteilhafter Weise zwischen dem Dichtungssegment und einem Rotorlager angeordnet, beispielsweise dem Radiallager.The two material areas are suitably rotatably connected to each other. This non-rotatable connection can be achieved by a cohesive connection, such as a weld, a frictional connection, such as a clutch, or a positive connection. Advantageously, this connection is formed by a spur gear, so that the two material areas engage one another positively. The risk of imbalance due to a welded joint or a slippage of the two areas against each other by an insufficiently strong frictional connection can be avoided. The rotationally fixed connection is advantageously arranged between the sealing segment and a rotor bearing, for example the radial bearing.
Besonders geeignet als drehfeste Verbindung zwischen den beiden Rotorbereichen bzw. Werkstoffbereichen des Rotors ist eine Hirthverbindung. Durch die Hirthverzahnung derParticularly suitable as a rotationally fixed connection between the two rotor regions or material regions of the rotor is a Hirth connection. By the Hirth gearing of
Hirtverbindung wird eine feste, selbst zentrierende und lösbare Verbindung mit einfachen Mitteln erreicht. Die Zähne der Hirthverzahnung liegen im Sinne einer kraftschlüssigen Kupplung statisch und flächig aneinander und sind radial ausgerichtet, wodurch die Zentrierung erreicht wird. Mit Hilfe der Hirthverbindung kann eine sehr klein bauende Verbindung zwischen den Rotorbereichen erreicht werden. Zum Kraftschluss ist eine axiale Verspannung notwendig, die wiederum die Kraftübertragung von einem Bereich zum anderen begrenzt .Hirtverbindung a fixed, self-centering and detachable connection is achieved by simple means. The teeth of the Hirth toothing are in the sense of a non-positive Clutch static and surface to each other and are radially aligned, whereby the centering is achieved. With the help of the Hirth connection, a very compact connection between the rotor areas can be achieved. For traction axial tension is necessary, which in turn limits the power transmission from one area to another.
Die Erfindung wird anhand eines Ausführungsbeispiels näher erläutert, das in einer Zeichnung dargestellt ist. Deren einzige Figur zeigt einen Abschnitt einesThe invention will be explained in more detail with reference to an embodiment which is shown in a drawing. Their only figure shows a section of a
Getriebeverdichterrotors 2, dessen axial äußerer Bereich 4 ein Laufrad 6 mit einer Laufradnabe 8 und einGetriebeverdichterrotors 2, the axially outer portion 4, an impeller 6 with an impeller hub 8 and a
Dichtungssegment 10 mit einer Dichtung 12 in Form einer Labyrinthdichtung umfasst. Das Laufrad 6 ist fliegend gelagert und ist Teil einer Überhangstufe desSealing segment 10 comprises a seal 12 in the form of a labyrinth seal. The impeller 6 is cantilevered and is part of an overhang stage of
Getriebeverdichters .Transmission compressor.
Der Getriebeverdichterrotor 2 kann sowohl mit einem als auch mit zwei Laufrädern & ausgeführt sein. Bei einem Design mit zwei Laufrädern kann Fig. 1 als halbe Darstellung mit einer Spiegelebene im Verzahnungsbereich angesehen werden. Bei einer Ausführung mit nur einem Laufrad endet die Ritzelwelle 16 mit dem hinter der Verzahnung liegenden zweiten und nicht dargestellten Lagerbereich.The gear compressor rotor 2 can be designed both with one and with two wheels. In a design with two wheels Fig. 1 can be viewed as a half-view with a mirror plane in the toothed area. In an embodiment with only one impeller, the pinion shaft 16 ends with the lying behind the toothing second and not shown storage area.
Der Getriebeverdichterrotor 2 ist Bestandteil eines Turbogetriebeverdichters mit einem Getriebe, das durch eine Verzahnung 14 einen Antrieb, beispielsweise eine Dampfturbine oder einen Elektromotor, zur Kraftübertragung mit dem Laufrad 6 verbindet. Die Verzahnung 14 des Rotors 2 ist an einer Ritzelwelle 16 gefertigt, die in ein Verzahnungssegment 18 und in einen Lagerbereich 20 eingeteilt werden kann, die wiederum einem inneren Bereich 22 des Rotors bilden. Im Lagerbereich 20 trägt die Ritzelwelle 16 ein Rotorlager 24 in Form eines Radiallagers, und zwar eines hydrodynamischen Gleitlagers . Die beiden Bereiche 4, 22 sind durch eine formschlüssige Verbindung 26 miteinander verbunden, die durch einen Pfeil angedeutet ist. In der Verbindung 26 sind die Ritzelwelle 16 und das Laufrad 6 formschlüssig und drehfest miteinander verbunden. Die Verbindung 26 ist als Hirthverbindung ausgeführt, wobei eine Verschraubung 28 die beiden Bereiche 4, 22 des Getriebeverdichterrotors 2 axial gegeneinander presst, sodass durch die Hirthverbindung hohe Kräfte und Drehmomente von einem auf den anderen Bereich 4, 22 übertragen werden können.The gear compressor rotor 2 is part of a turbo transmission compressor with a gear that connects a drive, such as a steam turbine or an electric motor, for power transmission with the impeller 6 by a toothing 14. The toothing 14 of the rotor 2 is made on a pinion shaft 16, which can be divided into a toothed segment 18 and into a bearing region 20, which in turn form an inner region 22 of the rotor. In the bearing area 20, the pinion shaft 16 carries a rotor bearing 24 in the form of a radial bearing, namely a hydrodynamic sliding bearing. The two areas 4, 22 are interconnected by a positive connection 26, which is indicated by an arrow. In the connection 26, the pinion shaft 16 and the impeller 6 are positively and rotatably connected to each other. The connection 26 is designed as a Hirth connection, wherein a screw 28 presses the two areas 4, 22 of the gear compressor rotor 2 axially against each other, so that high forces and torques can be transmitted from one to the other area 4, 22 by the Hirth connection.
Die beiden Bereiche 4, 22 sind aus unterschiedlichen Werkstoffen hergestellt. Die Laufradnabe 8 und das Dichtungssegment 10 im äußeren Bereich 4 sind aus einem kaltzähen Werkstoff hergestellt, beispielsweise dem kaltzähen Stahl X8Ni9. Hierbei sind die Laufradnabe 8 und das Dichtungssegment 10 als ein einstückiges Teil hergestellt, beispielsweise als ein Schmiedestück. Auch auf eine Verschweißung zwischen der Laufradnabe 8 und dem Dichtungssegment 10 wurde verzichtet, um die Gefahr einer Unwucht aufgrund ungleichmäßiger Spannungsverteilung zu vermeiden .The two areas 4, 22 are made of different materials. The impeller hub 8 and the sealing segment 10 in the outer region 4 are made of a cold-tough material, such as the cold-tough steel X8Ni9. Here, the impeller hub 8 and the sealing segment 10 are made as an integral part, for example as a forging. Also, a weld between the impeller hub 8 and the seal segment 10 has been omitted to avoid the risk of imbalance due to uneven stress distribution.
Der innere Bereich 22 bzw. die Ritzelwelle 16 kann aus einem einsatzgehärteten Stahl, beispielsweise 18CrNiMo7-6 hergestellt sein. Auch ein hochfester Vergütungsstahl, beispielsweise 56NiCrMoV7, ist vorteilhaft. Sowohl der einsatzgehärtete Stahl als auch der hochfeste Vergütungsstahl sind besonders hart und abriebfest, so dass die Verzahnung 14 eine hohe Lebensdauer hat. Diese Stähle sind jedoch nur bedingt kaltzäh, sodass bei sehr tiefen Arbeitstemperaturen die Gefahr eines Sprödbruchs besteht. Gegen einen Sprödbruch ist der kaltzähe Stahl des äußeren Bereichs 4 besonders geeignet, sodass die Rotorwelle 2 für einen Betrieb bei besonders kalten Temperaturen, beispielsweise unter -300C oder unter -1200C, z.B. zur Lufttrennung, besonders geeignet ist . Während des Betriebs wird das Rotorlager 24 mit warmem Schmieröl versorgt, sodass die hydrodynamische Gleitlagerung des Rotors 2 gewährleistet ist. Mit dem warmen Schmieröl wird Wärme auf den inneren Bereich 22 des Rotors 2 übertragen, sodass dieser bei vorgesehenem Betrieb nie in einen Temperaturbereich abkühlt, der die Gefahr eines Sprödbruchverhaltens der Ritzelwelle 16 birgt. Durch die Anordnung der Verbindung 26 sehr weit innen in dem betriebswarmen Bereich des Rotors 2 ist der äußere Bereiche 4 aus dem ersten und kaltzähen Werkstoff sehr lang, so dass ein großer Teil des Rotors 2 für die tiefen Betriebstemperaturen geeignet ist. Trotz dieses großen kaltzähen Bereichs verbleibt durch die Trennung des Rotors 2 in die beiden verschiedenen Bereiche 4, 22 die Möglichkeit, das Verzahnungssegment 16 aus einem geeignetenThe inner portion 22 and the pinion shaft 16 may be made of a case-hardened steel, for example 18CrNiMo7-6. A high-strength tempering steel, for example 56NiCrMoV7, is also advantageous. Both the case-hardened steel and the high-strength tempering steel are particularly hard and resistant to abrasion, so that the toothing 14 has a long service life. However, these steels are only partially cold-resistant, so there is a risk of brittle fracture at very low working temperatures. Against a brittle fracture of the cold-tough steel of the outer region 4 is particularly suitable, so that the rotor shaft 2 for operation at particularly cold temperatures, for example below -30 0 C or below -120 0 C, for example, for air separation, is particularly suitable. During operation, the rotor bearing 24 is supplied with warm lubricating oil, so that the hydrodynamic sliding bearing of the rotor 2 is ensured. With the warm lubricating oil heat is transferred to the inner portion 22 of the rotor 2, so that it never cools in the intended operation in a temperature range, which carries the risk of brittle fracture behavior of the pinion shaft 16. Due to the arrangement of the connection 26 very far inside in the operating temperature range of the rotor 2, the outer portions 4 of the first and cold-tough material is very long, so that a large part of the rotor 2 is suitable for the low operating temperatures. Despite this large cold-toughened area remains the separation of the rotor 2 in the two different areas 4, 22, the possibility of the toothed segment 16 of a suitable
Verzahnungswerkstoff herzustellen. Hierdurch kann das Getriebe besonders klein bauend und verschleißarm ausgeführt werden . To produce toothing material. As a result, the transmission can be designed to be particularly compact and wear-resistant.

Claims

Patentansprüche claims
1. Getriebeverdichterrotor (2) für Kaltgasanwendungen mit einer Ritzelwelle (16) mit einem Verzahnungssegment (18) mit einer Verzahnung (14), zumindest einem Laufrad (6) mit einer Laufradnabe (8) und einem zwischen dem Verzahnungssegment (18) und der Laufradnabe (8) angeordneten Dichtungssegment (10), das eine Dichtung (12) trägt, dadurch gekennzeichnet, dass die Laufradnabe (8) und das Dichtungssegment (10) einen gemeinsamen, einstückig zusammenhängenden Bereich (4) aus einem ersten Werkstoff bilden und das Verzahnungssegment (18) aus einem zweiten Werkstoff gebildet ist.1. gear compressor rotor (2) for cold gas applications with a pinion shaft (16) having a toothed segment (18) with a toothing (14), at least one impeller (6) with an impeller hub (8) and between the toothed segment (18) and the impeller hub (8) arranged sealing segment (10) carrying a seal (12), characterized in that the impeller hub (8) and the sealing segment (10) form a common, integrally connected region (4) of a first material and the toothed segment ( 18) is formed of a second material.
2. Getriebeverdichterrotor (2) nach Anspruch 1, dadurch gekennzeichnet, dass das Laufrad (6) fliegend gelagert ist.2. gear compressor rotor (2) according to claim 1, characterized in that the impeller (6) is cantilevered.
3. Getriebeverdichterrotor (2) nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass der erste Werkstoff kaltzäher ist als der zweite Werkstoff.Third gear compressor rotor (2) according to claim 1 or 2, characterized in that the first material is cold toughen than the second material.
4. Getriebeverdichterrotor (2) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der zweite Werkstoff härter ist als der erste Werkstoff.4. gear compressor rotor (2) according to one of the preceding claims, characterized in that the second material is harder than the first material.
5. Getriebeverdichterrotor (2) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass im Bereich (22) des zweiten Werkstoffs ein Rotorlager (24) angeordnet ist.5. gear compressor rotor (2) according to one of the preceding claims, characterized in that in the region (22) of the second material, a rotor bearing (24) is arranged.
6. Getriebeverdichterrotor (2) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass zwischen dem Dichtungssegment (10) und dem Verzahnungssegment (18) ein Rotorlager (24) angeordnet ist. 6. gear compressor rotor (2) according to any one of the preceding claims, characterized in that between the sealing segment (10) and the toothed segment (18) a rotor bearing (24) is arranged.
7. Getriebeverdichterrotor (2) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass eine drehfeste Verbindung (26) der beiden Werkstoffbereiche (4, 22) zwischen dem Dichtungssegment (10) und einem Rotorlager (24) angeordnet ist .7. Getriebeverdichterrotor (2) according to any one of the preceding claims, characterized in that a rotationally fixed connection (26) of the two material regions (4, 22) between the sealing segment (10) and a rotor bearing (24) is arranged.
8. Getriebeverdichterrotor (2) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass eine drehfeste Verbindung (26) zwischen den beiden Werkstoffbereichen (4, 22) eine Hirthverbindung ist. 8. gear compressor rotor (2) according to one of the preceding claims, characterized in that a rotationally fixed connection (26) between the two material regions (4, 22) is a Hirth connection.
EP10716500A 2009-04-01 2010-03-26 Geared compressor rotor for cold gas applications Active EP2414684B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102009015862A DE102009015862A1 (en) 2009-04-01 2009-04-01 Gear compressor rotor for cold gas applications
PCT/EP2010/054004 WO2010112423A1 (en) 2009-04-01 2010-03-26 Geared compressor rotor for cold gas applications

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EP2414684A1 true EP2414684A1 (en) 2012-02-08
EP2414684B1 EP2414684B1 (en) 2013-01-23

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EP (1) EP2414684B1 (en)
CN (1) CN102388225B (en)
DE (1) DE102009015862A1 (en)
ES (1) ES2401312T3 (en)
WO (1) WO2010112423A1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102748326A (en) * 2012-07-20 2012-10-24 湖北省风机厂有限公司 Automatic locking device for impeller with high-speed rotor
US9371835B2 (en) * 2013-07-19 2016-06-21 Praxair Technology, Inc. Coupling for directly driven compressor
DE102012223830A1 (en) 2012-12-19 2014-06-26 Siemens Aktiengesellschaft Sealing a compressor rotor
ITCO20130022A1 (en) * 2013-06-10 2014-12-11 Nuovo Pignone Srl METHOD TO CONNECT A IMPELLER TO A TREE, CONNECTION CONFIGURATION AND ROTARY MACHINE.
CN106255829B (en) * 2014-03-26 2019-05-31 株式会社 Ihi Impeller connection construction and turbo-compressor
EP3299630A1 (en) 2016-09-27 2018-03-28 Siemens Aktiengesellschaft Compressor assembly
EP3617519A1 (en) 2018-08-27 2020-03-04 Siemens Aktiengesellschaft Radially compressor rotor, radial compressor, gear-driven compressor
EP3705725A1 (en) 2019-03-05 2020-09-09 Siemens Aktiengesellschaft Assembly with transmission resistance
JP2022129728A (en) 2021-02-25 2022-09-06 三菱重工コンプレッサ株式会社 Rotating machine
EP4163501A1 (en) 2021-10-11 2023-04-12 Siemens Energy Global GmbH & Co. KG Air compression assembly for air separation
EP4163500A1 (en) 2021-10-11 2023-04-12 Siemens Energy Global GmbH & Co. KG Air compression assembly for air separation

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1808792A (en) * 1926-12-28 1931-06-09 C S Engineering Co Lubricating device
US1853973A (en) * 1927-12-08 1932-04-12 Gen Electric Centrifugal compressor or blower
US3874824A (en) * 1973-10-01 1975-04-01 Avco Corp Turbomachine rotor assembly
DE4220127C1 (en) 1992-06-17 1993-09-16 Mannesmann Ag, 40213 Duesseldorf, De
US5456818A (en) 1993-11-03 1995-10-10 Ingersoll-Rand Company Method for preventing fretting and galling in a polygon coupling
DE19612818C2 (en) * 1996-03-30 1998-04-09 Schloemann Siemag Ag Process for cooling warm-rolled steel profiles
DE10050371A1 (en) * 2000-10-11 2002-05-02 Siemens Ag Device with a ferromagnetic and mechanically resilient component in the cryogenic temperature range
GB2410982A (en) * 2004-02-14 2005-08-17 Richard Julius Gozdawa Turbomachinery electric generator arrangement with component cooling
EP1803941A1 (en) * 2004-10-19 2007-07-04 Komatsu Ltd Turbo machine, compressor impeller used for turbo machine, and method of manufacturing turbo machine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2010112423A1 *

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US9500201B2 (en) 2016-11-22
EP2414684B1 (en) 2013-01-23
DE102009015862A1 (en) 2010-10-07
CN102388225A (en) 2012-03-21
ES2401312T3 (en) 2013-04-18
WO2010112423A1 (en) 2010-10-07
US20120039722A1 (en) 2012-02-16
CN102388225B (en) 2014-09-10

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