US20070297907A1 - Vacuum Pump Impeller - Google Patents

Vacuum Pump Impeller Download PDF

Info

Publication number
US20070297907A1
US20070297907A1 US11/666,980 US66698005A US2007297907A1 US 20070297907 A1 US20070297907 A1 US 20070297907A1 US 66698005 A US66698005 A US 66698005A US 2007297907 A1 US2007297907 A1 US 2007297907A1
Authority
US
United States
Prior art keywords
rotor
shaft
vacuum pump
pump impeller
cavity
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.)
Abandoned
Application number
US11/666,980
Inventor
Wolfgang Giebmanns
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.)
Leybold GmbH
Original Assignee
Oerlikon Leybold Vacuum 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 Oerlikon Leybold Vacuum GmbH filed Critical Oerlikon Leybold Vacuum GmbH
Assigned to OERLIKON LEYBOLD VACUM GMBH reassignment OERLIKON LEYBOLD VACUM GMBH ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GIEBMANNS, WOLFGANG
Publication of US20070297907A1 publication Critical patent/US20070297907A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/025Fixing blade carrying members on shafts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/02Selection of particular materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/02Selection of particular materials
    • F04D29/023Selection of particular materials especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/266Rotors specially for elastic fluids mounting compressor rotors on shafts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/21Manufacture essentially without removing material by casting
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/25Manufacture essentially without removing material by forging
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • F05D2300/12Light metals
    • F05D2300/122Beryllium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • F05D2300/17Alloys
    • F05D2300/171Steel alloys
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Definitions

  • the invention relates to a vacuum pump impeller comprising a steel shaft and a one-piece rotor held by the shaft and made from a material different from the shaft steel, and to a method for producing a vacuum pump impeller.
  • Vacuum pump impellers are known in various variants, e.g. as screw impellers, turbo impellers, rolling-piston impellers, side-channel impellers, inter alia.
  • Vacuum pump impellers can be configured for cantilevered arrangement, i.e. the impeller is supported only on one axial end so that the rotor is arranged in overhung position. Impellers are partially operated at high rotational speeds so that high radial forces can occur. For these reasons, when designing the impellers, efforts are made to keep the weight particularly of the rotor as small as possible and to provide the shaft with the highest possible strength and rigidity.
  • this is realized by attaching the rotor on the outer side of the steel shaft, and by forming the rotor of a material having a particularly light weight, e.g. aluminium. Since, due to high temperature and high centrifugal forces, the rotor may in operation may expand more than the shaft, a permanent and free-from-play fixing of the rotor to the shaft can be effected only with difficulty and in a complicated manner, e.g. by welding, soldering, bonding, axially biased toothed engagement on the end sides, tie rods etc.
  • the shaft is provided with a cavity on one axial end thereof, and the rotor is provided with a corresponding axial projection seated in positive and/or non-positive engagement in the axial cavity of the shaft.
  • the rotor is not fixed to the outer side of the shaft but is fixed substantially on the inner side of a sleeve-like portion of the hollow steel shaft.
  • the rotor projection seated in the shaft can expand more than the hollow shaft. In operation and particularly in case of high rotational speeds, the connection between the rotor and the shaft will thus become stronger.
  • the rotor projection and the shaft each comprise, within the cavity, suitably shaped portions for effecting a positive engagement with each other in the axial direction and/or the circumferential direction.
  • the provision of a positive connection results in a safe and easily established connection between rotor and shaft.
  • the rotor is a cast piece whose projection is integrally cast in the shaft cavity.
  • the shaft Prior to casting the rotor, the shaft is inserted, by its portion including the cavity, into a casting box, and then the liquid rotor material is injected into the rotor casting box, with the liquid rotor material flowing into the shaft cavity.
  • the shaped portions in the cavity of the shaft are transferred to the rotor projection already when casting the rotor. No further production step for fixing the rotor to the shaft will be required. Thereby, in turn, the weight is reduced and causes of possible imbalances are avoided.
  • the above shaped portions are configured as grooves and bars.
  • the grooves and bars can be arranged in axial and circumferential directions; however, they can be arranged also in other directions.
  • the exact shape and orientation of the bars and grooves will depend, inter alia, on the thermal expansion behavior of the materials used for the rotor and the shaft, the rotational speeds and centrifugal forces occurring during operation, and other limiting conditions.
  • the wall thickness of the shaft on the rotor-side end of the shaft decreases toward the opening of the cavity, i.e. the wall thickness of the shaft casing continuously decreases towards the opening so that the stiffness of the shaft end becomes weaker towards the opening of the cavity and the axial cavity opening is relatively elastic in radial directions.
  • the danger of breakage of the rotor projection in this region is considerably reduced, so that a correspondingly small dimensioning and thus a reduction of weight of the rotor projection can be realized.
  • the region of decreasing wall thickness as compared to the overall length of the shaft can be less than 1/10 but should at least 3 mm long.
  • the vacuum pump impeller can comprise two shafts, each of them arranged at a respective axial end of the rotor. Preferably, however, only one shaft is provided, holding an axial end of the rotor. In this manner, there is obtained a vacuum pump impeller adapted for cantilevered support; in such a vacuum pump impeller, the reduction in weight which can be realized by the inventive construction is of particular advantage.
  • the rotor material is a light metal or a plastic material. If the rotor is to be produced as a cast piece, the rotor material must have a melting temperature which allows for the rotor material to be poured into the shaft cavity without causing damage to the steel shaft.
  • plastic or fiber-reinforced plastic can be used for the rotor.
  • the shaft comprising an axial cavity is laid into a rotor drop-forge die; the red-hot rotor forging material is forged into the drop-forge die for the rotor and into the shaft cavity; and finally the vacuum pump impeller is removed from the drop-forge die.
  • FIG. 1 is a longitudinal sectional view of a first embodiment of a vacuum pump impeller comprising a rotor which has been cast into the shaft and then machined,
  • FIG. 2 is a longitudinal sectional view of the shaft of the vacuum pump impeller
  • FIG. 3 is a longitudinal sectional view of second embodiment of a vacuum pump impeller
  • FIG. 4 is a longitudinal sectional view of third embodiment of a vacuum pump impeller
  • FIG. 5 is a longitudinal sectional view of fourth embodiment of a vacuum pump impeller.
  • Impeller 10 to be used as one of the two impellers of a screw vacuum pump.
  • Impeller 10 substantially consists of two parts, notably a one-piece rotor 12 made of aluminum and a one-pieced steel shaft 14 formed as a hollow shaft throughout its length.
  • the interrupted line in FIG. 1 schematically indicates the contour of shaft 14 ′ and of rotor 12 ′ presented by these components immediately after casting and prior to machining.
  • Rotor 12 comprises two parts in its longitudinal direction, notably a projection 16 and an active part 18 which on its radially outer side has a helical structure 20 .
  • Shaft 14 is throughout its length provided with a slightly conical and/or cylindrical cavity 22 having the projection 16 of rotor 12 cast thereinto with positive engagement between the cavity and the projection.
  • shaft cavity 22 Internally of shaft cavity 22 , there are arranged longitudinal bars 24 and transverse bars 26 constituting said shaped portions, engaging corresponding longitudinal grooves 28 and transverse grooves 30 of projection 16 .
  • the wall thickness of the hollow shaft continuously decreases towards the opening 34 of the cavity so that also the stiffness of shaft 14 in this region decreases towards the rotor-side shaft end 32 .
  • the shaft end 32 can be axially toothed, as illustrated, so as to be able to transmit large torques from shaft 14 to rotor 12 in case that the positive connections via the transverse bars and grooves 24 , 26 , 28 , 30 are not sufficient for this purpose.
  • the shaft end 32 both on its outer side and on its inner side is inclined by about 5° relative to the axial line.
  • a blank of shaft 14 ′ as illustrated in FIG. 4 is first laid into a molding box; the molding box is closed and aluminum as a rotor material is filled into the molding box while still in a liquid state.
  • the liquid aluminum will also flow into the shaft cavity 22 and thus assume an outer shape which is complementary to the shaft-side bars 24 , 26 .
  • rotor 12 ′ and shaft 14 ′ are removed from the molding box and supplied to a machining process which will give the rotor and the shaft their final shape on their outer and inner sides, as illustrated in FIG. 1 .
  • the hollow shaft 14 can serve as a cooling iron by which a well-aimed cooling process of the rotor and thus increased non-porosity and better cohesion in the rotor material can be obtained.
  • the impeller can also be produced by a forging method carried out in analogous manner.
  • FIG. 3 Illustrated in FIG. 3 is a second embodiment of a vacuum pump impeller 50 comprising a radial compressor rotor 52 , shown by interrupted lines, and a hollow shaft 54 .
  • the conical rotor projection 56 is cast into the conical shaft cavity 58 .
  • the positive connection between rotor 52 and shaft 54 is effected by bars and grooves in the longitudinal and circumferential directions.
  • the rotor blank 52 ′ machined into the rotor 52 is represented by continuous lines.
  • FIG. 4 there is again illustrated a radial compressor rotor 60 whose rotor 62 , by means of high-precision casting and, inter alia, by wax melting, already after the casting presents blades 66 of which only the outer contour has to be machined.
  • Shaft 67 includes a hollow portion 67 which does not extend throughout the length of the shaft but covers only about a third of the shaft length.
  • a conical or cylindrical axial cavity 65 is provided, with a conical or cylindrical axial projection 63 of rotor 62 seated therein.
  • the positive engagement between rotor 62 and shaft 64 is obtained by at least one eccentric rotor pin 68 seated in a corresponding number of eccentric recesses 69 of shaft 64 .
  • the pins have to be arranged in a manner effecting the best possible mass equilibrium, e.g. by means of two pins arranged at a relative displacement by 180° or three pins arranged at a relative displacement by 120°.
  • FIG. 4 only one pin is shown for ease of illustration.
  • the shaft blank 64 ′ and the rotor blank are shown by continuous lines, and the rotor 62 completed by machining as well as the machined shaft 64 are shown by interrupted lines.
  • FIG. 5 shows a vacuum pump impeller 80 which comprises a diagonal compressor rotor 82 and a shaft 84 provided with an axial cavity 86 extending along only about a third of the axial length of shaft 84 .
  • the shaft cavity 86 has a corresponding projection 88 of rotor 82 seated therein.
  • the unworked rotor 82 ′ and the unworked shaft 84 ′ are shown by continuous lines, and the machined rotor 82 as well as the machined shaft 84 are shown by interrupted lines.
  • the rotor 82 of impeller 80 according to FIG. 5 is a forged part which consists e.g. of aluminum and has to be hot-forged in a drop forge wherein the shaft 84 with its cavity 86 has been laid.
  • the stability of the rotor is improved not only by the forging behavior but also by a radially toothed shaft collar 90 which is effective to reduce tensions caused by centrifugal forces and can be used to compensate for imbalances by removal of material and/or placement of compensation weights such as e.g. balancing screws.
  • a collar 92 can be formed which together with a corresponding counterpart groove 94 will provide for axial guidance.
  • the corrosion resistance of the aluminum rotor can basically be improved by eloxadizing or hard-anodizing.

Abstract

The invention relates to a vacuum pump impeller (10) which comprises a shaft (14) made of steel, and a one-piece rotor (12) supported by the shaft (14) and made of a material different from the steel of the shaft. The shaft (14) comprises an axial cavity (22), and the rotor (12) comprises an axial projection (16) seated in the cavity (22) in positive and/or non-positive engagement therewith.

Description

  • The invention relates to a vacuum pump impeller comprising a steel shaft and a one-piece rotor held by the shaft and made from a material different from the shaft steel, and to a method for producing a vacuum pump impeller.
  • Vacuum pump impellers are known in various variants, e.g. as screw impellers, turbo impellers, rolling-piston impellers, side-channel impellers, inter alia. Vacuum pump impellers can be configured for cantilevered arrangement, i.e. the impeller is supported only on one axial end so that the rotor is arranged in overhung position. Impellers are partially operated at high rotational speeds so that high radial forces can occur. For these reasons, when designing the impellers, efforts are made to keep the weight particularly of the rotor as small as possible and to provide the shaft with the highest possible strength and rigidity. In practice, this is realized by attaching the rotor on the outer side of the steel shaft, and by forming the rotor of a material having a particularly light weight, e.g. aluminium. Since, due to high temperature and high centrifugal forces, the rotor may in operation may expand more than the shaft, a permanent and free-from-play fixing of the rotor to the shaft can be effected only with difficulty and in a complicated manner, e.g. by welding, soldering, bonding, axially biased toothed engagement on the end sides, tie rods etc.
  • In view of the above, it is an object of the invention to provide a vacuum pump impeller and a method for producing the same which allow for a simple and permanent fixation of the rotor the shaft.
  • According to the invention, the above object is achieved by the features of claim 1 and 9, respectively.
  • In the vacuum pump impeller of the invention, the shaft is provided with a cavity on one axial end thereof, and the rotor is provided with a corresponding axial projection seated in positive and/or non-positive engagement in the axial cavity of the shaft. Thus, the rotor is not fixed to the outer side of the shaft but is fixed substantially on the inner side of a sleeve-like portion of the hollow steel shaft. Under the effect of the centrifugal forces and the introduction of heat into the rotor as occurring during operation, the rotor projection seated in the shaft can expand more than the hollow shaft. In operation and particularly in case of high rotational speeds, the connection between the rotor and the shaft will thus become stronger. This effect obviates the need for complex connection arrangements involving the use of tie rods etc., as well as the need for holes in the shaft and the rotor so that, by the resultant homogenization of the force flows, breakage of the shaft or the rotor is avoided. Further still, by the omission of complex fastening arrangements, the weight of the impeller is kept low, so that—particularly in case of high rotational speeds at which e.g. turbo impellers are operated—the bearing support can be simplified. Thus, with the inventive impeller, higher rotational speeds and/or a lower weight and a reduced constructional size can be realized.
  • Preferably, the rotor projection and the shaft each comprise, within the cavity, suitably shaped portions for effecting a positive engagement with each other in the axial direction and/or the circumferential direction. The provision of a positive connection results in a safe and easily established connection between rotor and shaft.
  • According to a preferred embodiment, the rotor is a cast piece whose projection is integrally cast in the shaft cavity. Prior to casting the rotor, the shaft is inserted, by its portion including the cavity, into a casting box, and then the liquid rotor material is injected into the rotor casting box, with the liquid rotor material flowing into the shaft cavity. In this manner, the shaped portions in the cavity of the shaft are transferred to the rotor projection already when casting the rotor. No further production step for fixing the rotor to the shaft will be required. Thereby, in turn, the weight is reduced and causes of possible imbalances are avoided.
  • Preferably, the above shaped portions are configured as grooves and bars. The grooves and bars can be arranged in axial and circumferential directions; however, they can be arranged also in other directions. The exact shape and orientation of the bars and grooves will depend, inter alia, on the thermal expansion behavior of the materials used for the rotor and the shaft, the rotational speeds and centrifugal forces occurring during operation, and other limiting conditions.
  • According to a preferred embodiment, it is provided that the wall thickness of the shaft on the rotor-side end of the shaft decreases toward the opening of the cavity, i.e. the wall thickness of the shaft casing continuously decreases towards the opening so that the stiffness of the shaft end becomes weaker towards the opening of the cavity and the axial cavity opening is relatively elastic in radial directions. Thereby, relatively large and/or sudden changes of the moments of inertia of the shaft are avoided, which otherwise would cause high bending and/or torsional stresses and thus—particularly in case of massive variations in stress—could result in premature fatigue with generation of fissures. The danger of breakage of the rotor projection in this region is considerably reduced, so that a correspondingly small dimensioning and thus a reduction of weight of the rotor projection can be realized. The region of decreasing wall thickness as compared to the overall length of the shaft can be less than 1/10 but should at least 3 mm long.
  • In principle, the vacuum pump impeller can comprise two shafts, each of them arranged at a respective axial end of the rotor. Preferably, however, only one shaft is provided, holding an axial end of the rotor. In this manner, there is obtained a vacuum pump impeller adapted for cantilevered support; in such a vacuum pump impeller, the reduction in weight which can be realized by the inventive construction is of particular advantage.
  • Preferably, the rotor material is a light metal or a plastic material. If the rotor is to be produced as a cast piece, the rotor material must have a melting temperature which allows for the rotor material to be poured into the shaft cavity without causing damage to the steel shaft. Apart of light metal, also plastic or fiber-reinforced plastic can be used for the rotor.
  • According to a method for producing a vacuum pump impeller comprising a rotor with an axial projection and further comprising a steel shaft having a corresponding cavity formed therein, the following method steps are provided:
      • inserting the shaft having the axial cavity into a rotor mold,
      • filling in the liquid rotor molding material into the rotor mold and into the shaft cavity, and
      • removing the vacuum pump impeller from the mold after the impeller has been cooled.
  • Using the above described manufacturing method, upon provision of suitably shaped portions in the shaft cavity, a positive connection can be established between the shaft and the rotor. In this manner, no further components will be needed for effecting a positive connection between the rotor and the shaft. The method is relatively simple and thus inexpensive.
  • According to an alternative method for producing a vacuum pump impeller, the shaft comprising an axial cavity is laid into a rotor drop-forge die; the red-hot rotor forging material is forged into the drop-forge die for the rotor and into the shaft cavity; and finally the vacuum pump impeller is removed from the drop-forge die.
  • When applying this method, advantages similar to those mentioned in connection with the molding method are obtained.
  • Several embodiments of the invention will be explained in greater detail hereunder with reference to the drawings.
  • In the drawings, the following is shown:
  • FIG. 1 is a longitudinal sectional view of a first embodiment of a vacuum pump impeller comprising a rotor which has been cast into the shaft and then machined,
  • FIG. 2 is a longitudinal sectional view of the shaft of the vacuum pump impeller,
  • FIG. 3 is a longitudinal sectional view of second embodiment of a vacuum pump impeller,
  • FIG. 4 is a longitudinal sectional view of third embodiment of a vacuum pump impeller,
  • FIG. 5 is a longitudinal sectional view of fourth embodiment of a vacuum pump impeller.
  • Illustrated in FIG. 1 is a vacuum pump impeller 10 to be used as one of the two impellers of a screw vacuum pump. Impeller 10 substantially consists of two parts, notably a one-piece rotor 12 made of aluminum and a one-pieced steel shaft 14 formed as a hollow shaft throughout its length. The interrupted line in FIG. 1 schematically indicates the contour of shaft 14′ and of rotor 12′ presented by these components immediately after casting and prior to machining.
  • Rotor 12 comprises two parts in its longitudinal direction, notably a projection 16 and an active part 18 which on its radially outer side has a helical structure 20.
  • Shaft 14 is throughout its length provided with a slightly conical and/or cylindrical cavity 22 having the projection 16 of rotor 12 cast thereinto with positive engagement between the cavity and the projection. Internally of shaft cavity 22, there are arranged longitudinal bars 24 and transverse bars 26 constituting said shaped portions, engaging corresponding longitudinal grooves 28 and transverse grooves 30 of projection 16.
  • On the rotor-side end 32 of shaft 14, the wall thickness of the hollow shaft continuously decreases towards the opening 34 of the cavity so that also the stiffness of shaft 14 in this region decreases towards the rotor-side shaft end 32. The shaft end 32 can be axially toothed, as illustrated, so as to be able to transmit large torques from shaft 14 to rotor 12 in case that the positive connections via the transverse bars and grooves 24,26,28,30 are not sufficient for this purpose. The shaft end 32 both on its outer side and on its inner side is inclined by about 5° relative to the axial line. In combination with the transverse bars and grooves 24,26,28,30 of shaft 14 and rotor 12—which bars and grooves have inclined flanks when viewed in cross section—this arrangement will compensate for thermal expansion effects caused by the differing thermal expansion effects of the two different materials of which the rotor 12 and the shaft 14 are made. In this manner, the connection will always reliably free of play.
  • For manufacture of the vacuum pump impeller 10, a blank of shaft 14′ as illustrated in FIG. 4 is first laid into a molding box; the molding box is closed and aluminum as a rotor material is filled into the molding box while still in a liquid state. In the process, the liquid aluminum will also flow into the shaft cavity 22 and thus assume an outer shape which is complementary to the shaft- side bars 24,26. After cooling, rotor 12′ and shaft 14′ are removed from the molding box and supplied to a machining process which will give the rotor and the shaft their final shape on their outer and inner sides, as illustrated in FIG. 1.
  • In this manufacturing method, all shaped elements which are provided to take up forces and torques can be generated by casting technology. The use of a cast shaft will advantageously obviate the need for additional machining. Further, the casting method makes it possible to already shape all elements with cast radii which thus—because of reduced notch effect—are useful to obtain a good connection between the aluminum rotor 12 and the steel shaft 14. During the casting of rotor 12, the hollow shaft 14 can serve as a cooling iron by which a well-aimed cooling process of the rotor and thus increased non-porosity and better cohesion in the rotor material can be obtained.
  • By way of alternative to the above described casting method, the impeller can also be produced by a forging method carried out in analogous manner.
  • Illustrated in FIG. 3 is a second embodiment of a vacuum pump impeller 50 comprising a radial compressor rotor 52, shown by interrupted lines, and a hollow shaft 54. The conical rotor projection 56 is cast into the conical shaft cavity 58. The positive connection between rotor 52 and shaft 54 is effected by bars and grooves in the longitudinal and circumferential directions. The rotor blank 52′ machined into the rotor 52 is represented by continuous lines.
  • In FIG. 4, there is again illustrated a radial compressor rotor 60 whose rotor 62, by means of high-precision casting and, inter alia, by wax melting, already after the casting presents blades 66 of which only the outer contour has to be machined. Shaft 67 includes a hollow portion 67 which does not extend throughout the length of the shaft but covers only about a third of the shaft length. In the region of hollow portion 67, a conical or cylindrical axial cavity 65 is provided, with a conical or cylindrical axial projection 63 of rotor 62 seated therein. The positive engagement between rotor 62 and shaft 64 is obtained by at least one eccentric rotor pin 68 seated in a corresponding number of eccentric recesses 69 of shaft 64. To avoid imbalances caused by the different materials of the rotor and the shaft, the pins have to be arranged in a manner effecting the best possible mass equilibrium, e.g. by means of two pins arranged at a relative displacement by 180° or three pins arranged at a relative displacement by 120°. In FIG. 4, only one pin is shown for ease of illustration. The shaft blank 64′ and the rotor blank are shown by continuous lines, and the rotor 62 completed by machining as well as the machined shaft 64 are shown by interrupted lines.
  • FIG. 5 shows a vacuum pump impeller 80 which comprises a diagonal compressor rotor 82 and a shaft 84 provided with an axial cavity 86 extending along only about a third of the axial length of shaft 84. The shaft cavity 86 has a corresponding projection 88 of rotor 82 seated therein. The unworked rotor 82′ and the unworked shaft 84′ are shown by continuous lines, and the machined rotor 82 as well as the machined shaft 84 are shown by interrupted lines.
  • When subjected to high mechanical and/or thermal stresses, cast rotors may reach the limits of their stability so that other methods and materials have to be contemplated. The rotor 82 of impeller 80 according to FIG. 5 is a forged part which consists e.g. of aluminum and has to be hot-forged in a drop forge wherein the shaft 84 with its cavity 86 has been laid. The stability of the rotor is improved not only by the forging behavior but also by a radially toothed shaft collar 90 which is effective to reduce tensions caused by centrifugal forces and can be used to compensate for imbalances by removal of material and/or placement of compensation weights such as e.g. balancing screws. Additionally, for enhancing the positive connection, a collar 92 can be formed which together with a corresponding counterpart groove 94 will provide for axial guidance.
  • The corrosion resistance of the aluminum rotor can basically be improved by eloxadizing or hard-anodizing.

Claims (15)

1. A vacuum pump impeller comprising:
a shaft made of steel, and a one-piece rotor supported by the shaft and made of a material different from the steel of the shaft, shaft defining an axial cavity and the rotor including an axial projection seated in the cavity in positive and/or non-positive engagement therewith.
2. The vacuum pump impeller according to claim 1, wherein the rotor projection and the shaft comprise, within the cavity respectively shaped portions, the shaped portions effecting a positive engagement with each other in the axial direction and the circumferential direction.
3. The vacuum pump impeller according to claim, wherein the rotor is a cast part having its projection cast into the shaft cavity.
4. The vacuum pump impeller according to claim 2, wherein said shaped portions are formed as grooves and bars.
5. The vacuum pump impeller according to claim 1, wherein on a rotor-side end, the wall thickness of the shaft continuously decreases towards an opening of the cavity.
6. The vacuum pump impeller according to claim 1, wherein the rotor is supported by a single shaft.
7. The vacuum pump impeller according to claim 1, wherein the rotor is formed of a light metal or a plastic material.
8. The vacuum pump impeller according to claim 7, wherein the rotor material is aluminum.
9. A method for producing a vacuum pump impeller according to claim 1 by casting, comprising the method steps of:
inserting a shaft having an axial shaft cavity into a rotor mold,
filling in the liquid rotor molding material into the rotor mold and into the shaft cavity, and
removing the vacuum pump impeller from the mold after the rotor has set.
10. A method for producing a vacuum pump impeller according to claim 1 by forging, comprising the method steps of:
inserting a shaft having an axial shaft cavity into a drop-forge die for the rotor,
forging red-hot rotor forging material into the rotor drop-forge die and into the shaft cavity, and
removing the vacuum pump impeller from the drop-forge die.
11. A vacuum pump impeller comprising:
a shaft defining an axial cavity in at least one end thereof;
a rotor constructed of a material which expands radially outward relative to the steel shaft when drawing a vacuum, the rotor including an axial projection which extends into the shaft axial cavity such that when drawing the vacuum, the rotor axial projection expands into a tighter relationship with shift to avoid slippage.
12. The vacuum pump impeller according to claim 11, wherein a thickness of a shaft wall surrounding the axial cavity thins toward the one end that receives the rotor axial projection such that a stiffness of the shaft decreases toward the rotor to reduce fatigue and a risk of the rotor breaking from the shaft.
13. The vacuum pump impeller according to claim 11, further including:
mating ridges and grooves defined in an interior of a peripheral wall of the shaft surrounding the axial shaft cavity and the rotor axial projection.
14. The vacuum pump impeller according to claim 11, wherein the rotor axial projection is one of cast or forged into the shaft axial cavity.
15. The vacuum pump impeller according to claim 11, wherein the shaft is constructed of steel and the rotor is constructed of aluminum.
US11/666,980 2004-11-04 2005-10-10 Vacuum Pump Impeller Abandoned US20070297907A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102004053289A DE102004053289A1 (en) 2004-11-04 2004-11-04 Vacuum pump impeller
DE102004053289.3 2004-11-04
PCT/EP2005/055413 WO2006048379A1 (en) 2004-11-04 2005-10-20 Vacuum pump impeller

Publications (1)

Publication Number Publication Date
US20070297907A1 true US20070297907A1 (en) 2007-12-27

Family

ID=35645593

Family Applications (1)

Application Number Title Priority Date Filing Date
US11/666,980 Abandoned US20070297907A1 (en) 2004-11-04 2005-10-10 Vacuum Pump Impeller

Country Status (6)

Country Link
US (1) US20070297907A1 (en)
EP (1) EP1815145A1 (en)
JP (1) JP2008519191A (en)
KR (1) KR20070083878A (en)
DE (1) DE102004053289A1 (en)
WO (1) WO2006048379A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2462275A (en) * 2008-07-31 2010-02-03 Cummins Turbo Tech Ltd A method of connection a turbine shaft to a rotor
GB2473824A (en) * 2009-09-23 2011-03-30 Edwards Ltd Pump shaft and rotor materials selected for ease of disassembly
US20130062542A1 (en) * 2011-09-09 2013-03-14 Woodward, Inc. High-Flow Electro-Hydraulic Actuator
CN107061475A (en) * 2016-01-06 2017-08-18 哈米尔顿森德斯特兰德公司 Tuner-type ram-air turbine power transmission shaft
US10119478B2 (en) 2015-06-25 2018-11-06 Woodward, Inc. High reliability high flow redundant trip block

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2096317B1 (en) 2008-02-27 2012-08-15 Agilent Technologies, Inc. Method for manufacturing the rotor assembly of a rotating vacuum pump
JP6111746B2 (en) * 2013-03-07 2017-04-12 株式会社島津製作所 Vacuum pump
DE202013010209U1 (en) * 2013-11-12 2015-02-16 Oerlikon Leybold Vacuum Gmbh Vacuum wave
DE102015224603A1 (en) * 2015-12-08 2017-06-08 Mahle International Gmbh Runner for a pumping device
KR102172654B1 (en) * 2018-11-27 2020-11-02 한국가스공사 Wear ring assembly of impeller for nlg pump

Citations (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1549218A (en) * 1924-06-06 1925-08-11 Raym Willibald Casting process for incorporating shafts, journals, or the like
US2669938A (en) * 1953-02-19 1954-02-23 Bour Company Inc Impeller and shaft construction
US3063743A (en) * 1959-02-19 1962-11-13 Skf Svenska Kullagerfab Ab Press fitting joint
US3326534A (en) * 1963-11-13 1967-06-20 Pryde Alexander Willi Harrower Stirring devices
US3414966A (en) * 1964-05-27 1968-12-10 Commissariat Energie Atomique Process for joining dissimilar metals
US4337817A (en) * 1979-03-03 1982-07-06 Nissan Motor Co., Ltd. Method of joining a member to a diecast article wrapping thereabout in diecasting
US4424003A (en) * 1977-06-27 1984-01-03 AG Ku/ hnle, Kopp & Kausch Improved connection structure for joining ceramic and metallic parts of a turbine shaft
US4639194A (en) * 1984-05-02 1987-01-27 General Motors Corporation Hybrid gas turbine rotor
US4659245A (en) * 1985-05-31 1987-04-21 Nissan Motor Co., Ltd. Gas turbine
US4719074A (en) * 1984-03-29 1988-01-12 Ngk Insulators, Ltd. Metal-ceramic composite article and a method of producing the same
US4747722A (en) * 1984-12-19 1988-05-31 Honda Giken Kogyo Kabushiki Kaisha Metal-ceramic fitting assembly
US4749334A (en) * 1984-12-06 1988-06-07 Allied-Signal Aerospace Company Ceramic rotor-shaft attachment
US4761117A (en) * 1985-06-12 1988-08-02 Ngk Insulators, Ltd. Turbine rotor and a method of producing the same
US4778345A (en) * 1985-03-15 1988-10-18 Ngk Spark Plug Co., Ltd. Turbine rotor
US4784574A (en) * 1984-10-18 1988-11-15 Ngk Insulators, Ltd. Turbine rotor units and method of producing the same
US4798320A (en) * 1985-09-20 1989-01-17 Allied-Signal Inc. Ceramic-metal brazed joint for turbochargers
US4942999A (en) * 1987-08-31 1990-07-24 Ngk Insulators, Inc. Metal-ceramic joined composite bodies and joining process therefor
US5365661A (en) * 1988-02-25 1994-11-22 Ngk Insulators, Ltd. Ceramic-metal composite joint body
US5482437A (en) * 1993-11-03 1996-01-09 Ingersoll-Rand Company Method for preventing fretting and galling in a polygon coupling
US6254349B1 (en) * 1999-07-02 2001-07-03 Ingersoll-Rand Company Device and method for detachably connecting an impeller to a pinion shaft in a high speed fluid compressor
US6499958B2 (en) * 1999-07-02 2002-12-31 Ingersoll-Rand Company Device and method for detachably connecting an impeller to a pinion shaft in a high speed fluid compressor
US20040009072A1 (en) * 2002-03-02 2004-01-15 Daimlerchrysler Ag Method for manufacturing a turbine wheel rotor
US6754954B1 (en) * 2003-07-08 2004-06-29 Borgwarner Inc. Process for manufacturing forged titanium compressor wheel

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE471417C (en) * 1929-02-12 Bbc Brown Boveri & Cie Overhung impeller for single-wheel steam or gas turbines
GB536245A (en) * 1940-04-22 1941-05-07 Frederic Drury Wayre Improvements in or relating to apparatus comprising a rotary shaft and intended for dealing with corrosive fluids
GB1422426A (en) * 1973-06-22 1976-01-28 Penny Turbines Ltd Noel Compressor rotor
DE2527498A1 (en) * 1975-06-20 1976-12-30 Daimler Benz Ag RADIAL TURBINE WHEEL FOR A GAS TURBINE
JPH0646001B2 (en) * 1985-09-30 1994-06-15 京セラ株式会社 Ceramic rotor
JPH02173322A (en) * 1988-12-23 1990-07-04 Toyota Motor Corp Turbine wheel for turbo charger

Patent Citations (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1549218A (en) * 1924-06-06 1925-08-11 Raym Willibald Casting process for incorporating shafts, journals, or the like
US2669938A (en) * 1953-02-19 1954-02-23 Bour Company Inc Impeller and shaft construction
US3063743A (en) * 1959-02-19 1962-11-13 Skf Svenska Kullagerfab Ab Press fitting joint
US3326534A (en) * 1963-11-13 1967-06-20 Pryde Alexander Willi Harrower Stirring devices
US3414966A (en) * 1964-05-27 1968-12-10 Commissariat Energie Atomique Process for joining dissimilar metals
US4424003A (en) * 1977-06-27 1984-01-03 AG Ku/ hnle, Kopp & Kausch Improved connection structure for joining ceramic and metallic parts of a turbine shaft
US4337817A (en) * 1979-03-03 1982-07-06 Nissan Motor Co., Ltd. Method of joining a member to a diecast article wrapping thereabout in diecasting
US4719074A (en) * 1984-03-29 1988-01-12 Ngk Insulators, Ltd. Metal-ceramic composite article and a method of producing the same
US4639194A (en) * 1984-05-02 1987-01-27 General Motors Corporation Hybrid gas turbine rotor
US4784574A (en) * 1984-10-18 1988-11-15 Ngk Insulators, Ltd. Turbine rotor units and method of producing the same
US4749334A (en) * 1984-12-06 1988-06-07 Allied-Signal Aerospace Company Ceramic rotor-shaft attachment
US4747722A (en) * 1984-12-19 1988-05-31 Honda Giken Kogyo Kabushiki Kaisha Metal-ceramic fitting assembly
US4778345A (en) * 1985-03-15 1988-10-18 Ngk Spark Plug Co., Ltd. Turbine rotor
US4659245A (en) * 1985-05-31 1987-04-21 Nissan Motor Co., Ltd. Gas turbine
US4761117A (en) * 1985-06-12 1988-08-02 Ngk Insulators, Ltd. Turbine rotor and a method of producing the same
US4798320A (en) * 1985-09-20 1989-01-17 Allied-Signal Inc. Ceramic-metal brazed joint for turbochargers
US4942999A (en) * 1987-08-31 1990-07-24 Ngk Insulators, Inc. Metal-ceramic joined composite bodies and joining process therefor
US5365661A (en) * 1988-02-25 1994-11-22 Ngk Insulators, Ltd. Ceramic-metal composite joint body
US5482437A (en) * 1993-11-03 1996-01-09 Ingersoll-Rand Company Method for preventing fretting and galling in a polygon coupling
US6254349B1 (en) * 1999-07-02 2001-07-03 Ingersoll-Rand Company Device and method for detachably connecting an impeller to a pinion shaft in a high speed fluid compressor
US6499958B2 (en) * 1999-07-02 2002-12-31 Ingersoll-Rand Company Device and method for detachably connecting an impeller to a pinion shaft in a high speed fluid compressor
US20040009072A1 (en) * 2002-03-02 2004-01-15 Daimlerchrysler Ag Method for manufacturing a turbine wheel rotor
US6899522B2 (en) * 2002-03-02 2005-05-31 Daimlerchrysler Ag Method for manufacturing a turbine wheel rotor
US6754954B1 (en) * 2003-07-08 2004-06-29 Borgwarner Inc. Process for manufacturing forged titanium compressor wheel

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2462275A (en) * 2008-07-31 2010-02-03 Cummins Turbo Tech Ltd A method of connection a turbine shaft to a rotor
GB2473824A (en) * 2009-09-23 2011-03-30 Edwards Ltd Pump shaft and rotor materials selected for ease of disassembly
WO2011036468A3 (en) * 2009-09-23 2012-03-01 Edwards Limited Vacuum pump shaft/rotor assembly
GB2473824B (en) * 2009-09-23 2015-12-23 Edwards Ltd Preventing pump parts joining by corrosion
TWI583869B (en) * 2009-09-23 2017-05-21 愛德華有限公司 Pumps
US9695824B2 (en) 2009-09-23 2017-07-04 Emmanuel Uzoma Okoroafor Pump with corrosion resistant shaft and rotor surfaces
US20130062542A1 (en) * 2011-09-09 2013-03-14 Woodward, Inc. High-Flow Electro-Hydraulic Actuator
US9127694B2 (en) * 2011-09-09 2015-09-08 Woodward, Inc. High-flow electro-hydraulic actuator
US10487856B2 (en) 2011-09-09 2019-11-26 Woodward, Inc. High-flow electro-hydraulic actuator
US10119478B2 (en) 2015-06-25 2018-11-06 Woodward, Inc. High reliability high flow redundant trip block
CN107061475A (en) * 2016-01-06 2017-08-18 哈米尔顿森德斯特兰德公司 Tuner-type ram-air turbine power transmission shaft
US10295042B2 (en) * 2016-01-06 2019-05-21 Hamilton Sundstrand Corporation Tuned RAT driveshaft

Also Published As

Publication number Publication date
WO2006048379A1 (en) 2006-05-11
JP2008519191A (en) 2008-06-05
KR20070083878A (en) 2007-08-24
DE102004053289A1 (en) 2006-05-11
EP1815145A1 (en) 2007-08-08

Similar Documents

Publication Publication Date Title
US20070297907A1 (en) Vacuum Pump Impeller
US9316234B2 (en) Rotor disk for a turbo machine
US8794096B2 (en) Gearwheel and method for manufacturing a gearwheel
RU2331495C1 (en) Cast hollow crankshaft and its manufacturing method
US20070277645A1 (en) Lightweight Crankshaft
US8167576B2 (en) Method for manufacturing the rotor assembly of a rotating vacuum pump
US6234912B1 (en) High-stiffness composite shaft
KR20090082886A (en) Turbocharger
EP2754904B1 (en) Lightweight wheel hub rolling bearing assembly and method of assembling the assembly
US6899522B2 (en) Method for manufacturing a turbine wheel rotor
JP2003191039A (en) Method for profiling outer circumferential face of cylinder liners
US9506350B1 (en) Turbine rotor blade of the spar and shell construction
US20090304503A1 (en) Stator blade segment of a thermal turbomachine, associated production method and also thermal turbomachine
US5134900A (en) Crankshaft with hollow pins
JP2007071139A (en) Composite vacuum pump rotor
WO2014098151A1 (en) Method for manufacturing turbine rotor blade
US11891916B2 (en) Method for producing metal alloy parts with complex shape
US20110142653A1 (en) Two piece impeller
US6979173B2 (en) Turbine blade or vane
JPWO2006117847A1 (en) Micro gas turbine
JP7410193B2 (en) Rotating spindle and rotating machinery
CN219611445U (en) Rotor system of high-speed motor
JP3947433B2 (en) Forging die, closed forging production system, aluminum alloy rotor forging method and forged aluminum alloy rotor
JP5289137B2 (en) Assembly crankshaft and manufacturing method thereof
JP2014058972A (en) Rotor assembly, and refit method

Legal Events

Date Code Title Description
AS Assignment

Owner name: OERLIKON LEYBOLD VACUM GMBH, GERMANY

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:GIEBMANNS, WOLFGANG;REEL/FRAME:019291/0138

Effective date: 20070417

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION