WO2007009766A1 - Compresseur radial - Google Patents

Compresseur radial Download PDF

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Publication number
WO2007009766A1
WO2007009766A1 PCT/EP2006/007100 EP2006007100W WO2007009766A1 WO 2007009766 A1 WO2007009766 A1 WO 2007009766A1 EP 2006007100 W EP2006007100 W EP 2006007100W WO 2007009766 A1 WO2007009766 A1 WO 2007009766A1
Authority
WO
WIPO (PCT)
Prior art keywords
impeller
impellers
drive shaft
motor
balancing
Prior art date
Application number
PCT/EP2006/007100
Other languages
English (en)
Inventor
Norbert Aust
Gerhard Frey
Jürgen Fischer
Original Assignee
Gardner Denver Schopfheim 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
Application filed by Gardner Denver Schopfheim Gmbh filed Critical Gardner Denver Schopfheim Gmbh
Priority to US11/993,670 priority Critical patent/US20100158679A1/en
Priority to JP2008521879A priority patent/JP2009501865A/ja
Priority to CA002614710A priority patent/CA2614710A1/fr
Priority to EP06762696A priority patent/EP1915536A1/fr
Priority to AU2006271917A priority patent/AU2006271917A1/en
Publication of WO2007009766A1 publication Critical patent/WO2007009766A1/fr

Links

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
    • F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08—Centrifugal pumps
    • F04D17/10—Centrifugal pumps for compressing or evacuating
    • F04D17/12—Multi-stage pumps
    • F04D17/122—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08—Centrifugal pumps
    • F04D17/10—Centrifugal pumps for compressing or evacuating
    • F04D17/12—Multi-stage 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
    • F04D25/02—Units comprising pumps and their driving means
    • F04D25/06—Units comprising pumps and their driving means the pump being electrically driven
    • 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
    • F04D29/002—Details, component parts, or accessories 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
    • F04D29/02—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
    • F04D29/00—Details, component parts, or accessories
    • F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/051—Axial thrust balancing
    • 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
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
    • F04D29/286—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors multi-stage rotors
    • 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
    • F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/30—Vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44—Fluid-guiding means, e.g. diffusers
    • F04D29/441—Fluid-guiding means, e.g. diffusers 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
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/662—Balancing of rotors
    • 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
    • F05D2210/00—Working fluids
    • F05D2210/10—Kind or type
    • F05D2210/12—Kind or type gaseous, i.e. compressible
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S415/00—Rotary kinetic fluid motors or pumps

Definitions

  • the invention relates a small compact radial compressor impeller and a small compact radial compressor that contains the impeller characterised by the impeller having a central bore sized to be jammed or press fitted onto a motor drive shaft.
  • Small radial compressors are known that have a drive power in the range of 5 to 10 kW and which can be used to provide compressed air to other machines such as, for example, a book binding or other production machines.
  • Standard compressors of this power range produce a total pressure differential of around 80 mbar for a volume flow rate of around 2,000 m 3 /h, the efficiency being comparatively low.
  • the small size multistage compressors have their impellers manufactured in at least two parts - a hub with impeller blades and an impeller shroud enclosing the impeller blades.
  • the first part is a cast impeller hub with a plurality of 2- dimensional blades radially extending from the impeller hub. While the 2- dimensional blades are advantageous with respect to the fabrication effort, the efficiency of the impeller suffers under this kind of simple blade design.
  • the second part is the impeller shroud which is generally welded to the impeller hub. This two part impeller makes it more difficult to balance the impeller on the motor shaft and also increases the fabrication costs.
  • the known small size multi-stage compressors generally have blades in their diffusers.
  • a two-stage radial compressor having a drive motor, a drive shaft on which there are arranged two impellers, the drive motor being a fast-running asynchronous motor with a speed in excess of 10,000 rpm and a power in the range of around 5 to 10 kW.
  • the combination of a two-stage compressor and operating at a speed above the critical speed provides a very high performing compressor that produces an overall pressure differential exceeding 200 mbar at a volume flow rate of 700 to 900 m 3 /h.
  • our two impellers are identical one piece impellers.
  • our one piece impellers are identical except for their impeller bores which are not identical.
  • Each of the impeller bores are frustums for at east 75% of the length of the bore with the second impeller bore closest to the motor being larger than the first impeller bore furthest away from the motor. This allows the impellers to be relatively easily removed from the motor drive shaft.
  • Our impellers have integral impeller blades that are integral with the impel- ler hub and are 3 dimensional blades that radially and axially extend from the impeller hub.
  • the impeller are spatially twisted. The deviation of the centre line on a small radius exceeds the deviation on a bigger radius.
  • impellers are lightweight and consist of one single piece of a cast aluminium alloy to provide integral impeller hub, impeller blades and impeller shroud. This allows the blades to be manufactured with our 3-dimensional curved shapes. To this end, lost cores are used. The low specific weight of the cast aluminium alloy used provides a low total weight. The outside sur- face of the impeller is machined to provide a smooth uniform surface i.e. by a chip-forming process.
  • impellers are attached to the motor drive shaft by jamming or press fitting the impeller onto the drive shaft. This makes it possible to dispense with feather keys etc. which, at the high drive speed of the impellers, would create special problems in terms of unbalance and strength.
  • the impeller retains a precisely de- fined and preferable centred position relative to the drive shaft, by providing a tolerance ring between the drive shaft and the impeller.
  • the compressor has a pair of one piece impellers that are identical, except for their bores.
  • the impeller hub bore of the first impeller is a frustum with its first end, which is the end furthest from the compressor motor, having a smaller diameter than its second end.
  • impeller hub bore of the second impeller is also a frustum with its first end, which is the end furthest from the compressor motor, having a smaller diameter than its second end.
  • the first end of the second impeller bore has a larger diameter than the second end of the first impeller bore.
  • the diameter of the first end of the second impeller bore is also larger than any portion of the motor drive shaft that extends beyond the second impeller so that second impeller can easily be removed from the motor drive shaft for repairs or replacement.
  • the one piece motor drive shaft has spaced frustums thereon that are slightly larger than the corresponding frustum bores of the first and second impellers so that the impeller can be press fitted thereon.
  • impellers with a plurality of balancing bores into which balancing members i.e. bolts, screws, or disks may be selectively attached. Since the impellers are driven at a speed above the critical speed, extremely careful balancing after the compressor is assembled is essential. This can only occur after the radial compressor has been assembled because even with previously perfectly balanced impellers, the unbalance which could occur during installation of the impellers, e.g. by a slight eccentric arrangement of the drive shaft, could have fatal consequences during operation.
  • the balancing bores of the first impeller, the impeller furthest away from the motor are accessible on the suction side of the compressor so that, after balancing, no work of any kind is required on rotating parts.
  • outlet diffuser which has parallel walls and no blades.
  • the outlet dif- fuser ensures a reduction of the flow velocity of the medium exiting from the impeller, which increases the static pressure. Omitting the blades in the diffuser yields a wide range of performance with good efficiency, bladed diffusers are known to improve the efficiency even further, but the range in terms of possible flows is limited.
  • the drive shaft is held in two roller bearings one of which is arranged between the impellers and the drive motor, and the other on the drive motor side facing away from the impellers.
  • the two impellers are arranged on the freely projecting drive shaft.
  • roller bearings To improve the bearing arrangement of the drive shaft the roller bearings have bearing rings made of steel and rollers made of ceramics. Hybrid bearings of this kind have low requirements in terms of lubrication and offer a long service life.
  • a balancing disk is arranged on the side of the drive motor facing away from the impellers. With respect to the speed, which is above the critical speed, of the drive motor and the impellers, it has proven advantageous to have the balancing disk as additional means of balancing the assembly comprising the drive shaft, the impellers and the electric motor.
  • the balancing disk is preferably in a heat-conducting connection with the neighbouring roller bearing such that the produced frictional heat and the heat dissipated away from the electric motor into the roller bearing may be released into the environment via the balancing disk.
  • Figure 1 a radial compressor according to the invention in a first perspective view
  • Figure 2 the radial compressor of Figure 1 in a second perspective view
  • Figure 3 one embodiment of the radial compressor of Figure 1 in a partial sectional view
  • Figure 4 a first schematic view of a blade of an impeller of the radial compressor according to the invention.
  • Figure 5 a second schematic view of the blade.
  • Figure 6 is a perspective view of the impeller of the present invention.
  • Figure 7 is a partial schematic sectional view of another embodiment of the radial compressor of the present invention.
  • our two-stage radial compressor has a drive motor 5, a drive motor external cooling fan 6, a compressor housing 7, a compressor housing outlet 22 and a compressor housing inlet 24.
  • the drive motor 5 is a fast-running asynchronous motor with a frequency inverter, the motor having a drive speed of around 15,000 rpm.
  • the drive motor 5 has a drive shaft 14 made of one single continuous piece, preferably of steel.
  • the drive shaft 14 is held in two roller bearings 16 which are in two end plates - one on the front and the other on the rear of the drive motor 5.
  • the roller bearings 16 are hybrid bearings with bearing rings made of steel and rollers made of ceramics. Since there are a low number of joints between the components accommodating the roller bearings 16, the roller bearings 16 can be aligned relative to each other with high accuracy.
  • the compressor housing 7 is made of several parts.
  • the compressor housing 7 houses our first compressor impeller 10 and our second compressor impeller 12.
  • the inlet 24 is concentric with the drive shaft 14.
  • Each of the two impellers 10, 12 are cast aluminium alloy and are produced using the sand casting method.
  • Each of the impellers is an integral one piece casting with an impeller hub 17, a cylindrical bore 13 defined by the impeller hub, a plurality of essentially radial impeller blades 26 integrally extending from an impeller hub 17 and enclosed by an integral shroud 19.
  • Flow channels extend between the impeller blades.
  • the flow channels and hence the blades 26 are defined during casting by means of lost cores.
  • Each blade 26 is designed to be three-dimensionally curved.
  • the angle of the blade when using the blade centre line with the centre line of the drive shaft 14, increases from a value of around 45 to be parallel to the center- line of the drive shaft on the outlet side. As stated above, the deviation of the centreline on a small radius exceeds the deviation on a bigger radius.
  • the blade itself is twisted in approximately a screw-shaped way. Our three- dimensional blades provide very high fluid flow efficiency.
  • Figures 4 and 5 show the three dimensional curved shape of the blades 26.
  • Figure 5 shows view Y of Figure 4 in a developed view.
  • E denotes the inlet edge
  • A denotes the outlet edge
  • D denotes the contour on the cover disk and N the contour of the hub.
  • the drive shaft 14 has a plurality of grooves 27.
  • a tolerance ring 34 is mounted in each shaft groove 27.
  • the tolerance rings 34 are arranged in each case in the area of the plane of their centre of gravity prior to the impellers and spacer ring being placed on the shaft.
  • the tolerance rings are essentially a stiff spring lock washer with a cross-section, which has a wave-shape.
  • the tolerance ring eliminates the play between the drive shaft and the impeller, which is needed for assembly.
  • the tolerance rings contribute to torque transmission between the drive shaft and the impeller and are used to as much as possible, to centrally position the two impellers 10, 12 and maintain their position during operation.
  • the diameter of the drive shaft is slightly larger than the diameter of the impeller bores.
  • the two impellers 10, 12 are identical one piece impellers and are fastened on the drive shaft 14 solely by jamming them onto the drive shaft. Prior to placing the impellers 10, 12 and spacer 30 on the drive shaft 14, they are statically balanced. After the static balancing, the second impeller 12 and spacer ring 30 are jammed onto the shaft 14 and then the first impeller 10 is jammed onto the shaft 14. The two impellers 10, 12 are fastened on the drive shaft solely by this tight fit between the drive shaft and the impeller bores 13. In this embodiment of Figure 3, the contact ring 32 is placed on the shaft to abut the shaft shoulder 35, then the second impeller 12 and spacer ring 30 are jammed onto the drive shaft and finally the first impeller 10 is jammed onto the shaft 14.
  • each impeller a plurality of balancing bores 36, into which balancing members such as screws, bolts or disks may be selec- tively attached.
  • balancing members such as screws, bolts or disks
  • the bores are appropriately threaded.
  • disks or other types of balancers are preferred, then the bores are appropriately configured.
  • the dynamic balancing is only done on the first impeller 10.
  • the balancing bores of the second impeller may exist only because, for fabrication reasons, both impellers 10, 12 are manu- factured identically.
  • a balancing disk 38 there is provided on the drive motor 5 side facing away from the impellers 10, 12 a balancing disk 38.
  • the balancing disk 38 is used so that any unbalances can be reduced further.
  • the balancing disk 38 addi- tionally serves to cool the roller bearing 16 arranged on this side.
  • the roller bearing 16 has a heat-conducting connection with the balancing disk 38, which in turn is located inside the cooling air flow of the external fan 6.
  • this is our one piece cast impeller with a plurality of balancing slots or bores 36, a hub 17, impeller blades 26, and a shroud 19.
  • our two-stage radial compressor has two one piece cast impellers 41 and 42 and a drive shaft 43.
  • Figure 7 shows only a partial view of the compressor and does not show all of the features of impellers mounted in a compressor housing.
  • Figure 7 shows the important features of our preferred impeller and motor drive shaft structure.
  • the impellers of Figure 7 have the same general structure as the impellers of Figure 3 except for the shape of the impeller hub bores.
  • the two impellers 41, 42 are cast aluminium alloy and are produced using the sand casting method.
  • Each impeller 41 and 42 has a hub 17, a plurality of spatially curved radially extending three dimensional blades 26, and a shroud 19.
  • the integral blades 26 have flow channels formed between them. The flow channels and hence the blades 26 are defined during casting by lost cores.
  • Each blade 26, as shown in Figures 4 and 5 are three dimensionally curved.
  • the two impellers 41 and 42 are identical to each other except for their bores 43 and 44.
  • the impeller bore 43 of the first impeller 41 is a frustum with a first end 46 having a smaller diameter than its second end 47.
  • the bore 44 of the second impeller 42 is a frustum with a first end 48 having a smaller diameter than its second end 49.
  • the first end 48 of the bore 44 of the second impeller 42 has a larger diameter than the second end 47 of the impeller bore 43 of the first impeller 41.
  • the diameter of the first end 48 of the bore 44 of the second impeller 42 is also larger than any portion of the drive shaft 50 which extends beyond the second impeller 42 towards the first impeller 41 so that the second impeller 42 can easily be removed in the direction of arrow 51 from the drive shaft 50 and replaced on drive shaft 50 or of course another impeller identical to the second impeller 42 placed on drive shaft 50.
  • the drive shaft 50 has a frustum section 52 that is adjacent to the shaft end connected to the motor. This frustum section 52 expands towards the mo- tor.
  • the frustum section 52 is slightly larger than the frustum bore 44 of impeller 42 so that the impeller can be press fitted thereon.
  • the drive shaft also has another frustum section 53 that is adjacent the end of the shaft that is opposite to the shaft end connected to the motor.
  • This shaft frustum section 53 is slightly larger than the frustum bore 43 of impeller 41 so that the impeller 41 can be press fitted onto the shaft 50.
  • Both frustum sections 52 and 53 of the shaft 50 each have their outer sur- faces in contact respectively with more than 75% of the surfaces of the respective impeller bores 43and 44.
  • the diameter of the shaft is slightly larger at its point of contact with the impeller bores
  • the impeller bores are preferably formed during casting but can be formed by machining after casting if desired.
  • the two impellers 41 , 42 are fastened onto the drive shaft 50 solely by press fitting them onto the drive shaft frustums 52, 53. Prior to placing the impellers 41 , 42 and spacer 55 onto drive shaft 50, they are statically bal- anced.
  • the compressor housing 7 near its end closest to the motor has a groove formed therein. The groove holds a contact ring 54 and a retainer ring 56.
  • the second impeller 42 is hand forced onto the shaft .
  • the final press fitting of the second impeller 42 onto the shaft frustum 53 is accomplished by turning the jam nut 28 (a) .
  • each impeller a plurality of balancing bores 36, into which balancing members such as screws, bolts or disks may be selectively attached.
  • balancing members such as screws, bolts or disks
  • the bores are appropriately threaded.
  • disks or other types of balancers are preferred, then the bores are appropriately configured.
  • the dynamic balancing is only done on the first impeller 41.
  • the balancing bores of the second impeller exist only for fabrication reasons and may be eliminated if desired.
  • our impellers can be driven at a speed above the critical speed although, in the area of the impellers, the drive shaft is designed in a freely projecting manner.

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

Abstract

Ce compresseur radial comporte deux rotors monoblocs en fonte pourvus de pales tridimensionnelles radiales incurvées et torsadées. Ils sont logés dans un carter relié à un moteur d'entraînement. Les rotors sont montés sur un arbre moteur par serrage ou par emmanchement à la presse sur l'arbre de façon à constituer un compresseur radial à deux niveaux. Le moteur (5) et les rotors (10, 12) sont montés sur un même arbre d'entraînement (14). Le moteur (5) est d'un modèle asynchrone rapide tournant à plus de 10.000 t/mn, avec une puissance d'environ 5 à 10 kW.
PCT/EP2006/007100 2005-07-20 2006-07-19 Compresseur radial WO2007009766A1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
US11/993,670 US20100158679A1 (en) 2005-07-20 2006-07-19 Radial compressor
JP2008521879A JP2009501865A (ja) 2005-07-20 2006-07-19 遠心圧縮機
CA002614710A CA2614710A1 (fr) 2005-07-20 2006-07-19 Compresseur radial
EP06762696A EP1915536A1 (fr) 2005-07-20 2006-07-19 Compresseur radial
AU2006271917A AU2006271917A1 (en) 2005-07-20 2006-07-19 Radial compressor

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP05015745A EP1746290A1 (fr) 2005-07-20 2005-07-20 Compresseur centrifuge
EP05015745.2 2005-07-20

Publications (1)

Publication Number Publication Date
WO2007009766A1 true WO2007009766A1 (fr) 2007-01-25

Family

ID=35464067

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2006/007100 WO2007009766A1 (fr) 2005-07-20 2006-07-19 Compresseur radial

Country Status (8)

Country Link
US (1) US20100158679A1 (fr)
EP (2) EP1746290A1 (fr)
JP (1) JP2009501865A (fr)
KR (1) KR20080024486A (fr)
CN (1) CN101218435A (fr)
AU (1) AU2006271917A1 (fr)
CA (1) CA2614710A1 (fr)
WO (1) WO2007009766A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8454299B2 (en) 2008-02-29 2013-06-04 Mitsubishi Heavy Industries, Ltd. Radial compressor
US8905737B2 (en) 2008-02-18 2014-12-09 Nanyang Technological Univerity Revolving vane compressor and method for its manufacture
WO2022053856A1 (fr) 2020-09-14 2022-03-17 Imtmedical Ag Appareil de soufflante à deux étages pour ventilateur

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CN103362860A (zh) * 2012-04-02 2013-10-23 珠海格力电器股份有限公司 高速流体动力机械、及其转子的构成方法、装配方法
DE102013208476A1 (de) * 2013-05-08 2014-11-13 Ksb Aktiengesellschaft Pumpenanordnung
JP5827978B2 (ja) * 2013-09-17 2015-12-02 ナンヤン テクノロジカル ユニヴァーシティー 回転ベーン式圧縮機及びその製造方法
GB2545269B (en) * 2015-12-11 2018-02-28 Dyson Technology Ltd An electric motor
JP6720629B2 (ja) * 2016-03-28 2020-07-08 株式会社デンソー 遠心ポンプ及び遠心ポンプの製造方法
US11754092B2 (en) 2018-05-22 2023-09-12 Micronel Ag Radial turbomachine
US11218048B2 (en) 2018-12-14 2022-01-04 Nidec Motor Corporation Shaft-mounted slinger for electric motor

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EP0651169A1 (fr) * 1993-11-03 1995-05-03 Ingersoll-Rand Company Procédé pour prévenir l'exoriation et l'écorchure d'un accouplement à section polygonale
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CN101218435A (zh) 2008-07-09
JP2009501865A (ja) 2009-01-22
AU2006271917A1 (en) 2007-01-25
US20100158679A1 (en) 2010-06-24
EP1746290A1 (fr) 2007-01-24
EP1915536A1 (fr) 2008-04-30
CA2614710A1 (fr) 2007-01-25
KR20080024486A (ko) 2008-03-18

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