US20040202539A1 - Rotor disk - Google Patents

Rotor disk Download PDF

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Publication number
US20040202539A1
US20040202539A1 US10/476,990 US47699004A US2004202539A1 US 20040202539 A1 US20040202539 A1 US 20040202539A1 US 47699004 A US47699004 A US 47699004A US 2004202539 A1 US2004202539 A1 US 2004202539A1
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US
United States
Prior art keywords
impeller
blades
full
split
different
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
US10/476,990
Other languages
English (en)
Inventor
Andreas Blank
Guenther Kiefer
Wolfgang Ladner
Michael Brandes
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.)
Rolls Royce Solutions GmbH
Original Assignee
MTU Friedrichshafen 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 MTU Friedrichshafen GmbH filed Critical MTU Friedrichshafen GmbH
Assigned to MTU FRIEDRICHSHAFEN GMBH reassignment MTU FRIEDRICHSHAFEN GMBH ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BRANDES, MICHAEL, LADNER, WOLFGANG, KIEFER, GUENTHER, BLANK, ANDREAS
Publication of US20040202539A1 publication Critical patent/US20040202539A1/en
Abandoned legal-status Critical Current

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Classifications

    • 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
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/662Balancing of rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • 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
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/281Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
    • 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
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/284Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
    • 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
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/666Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by means of rotor construction or layout, e.g. unequal distribution of blades or vanes

Definitions

  • the present invention relates generally to an impeller, in particular a radial-flow fan or a compressor impeller having a different number of full blades and split blades.
  • impellers are used, e.g., as radial-flow fans or as compressor impellers for an exhaust gas turbocharger.
  • One problem with these impellers is the generated noise, which is often perceived as unpleasant.
  • One measure commonly used for noise reduction consists of equipping the impeller with full blades and split blades. Such an embodiment is known from European Patent 0 439 267 B1.
  • the number of full blades on this impeller may be different from the number of split blades.
  • An object of the present invention is to further reduce the noise emission by an impeller.
  • This object is has been achieved by arranging the full blades and the split blades at a different angular distance and in a different order.
  • the present invention thereby greatly reduces the noise level. Due to these measures, the acoustic power is distributed among several individual tones, the intensity of which turns out to be accordingly lower. Another advantage is that the efficiency and power consumption of the impeller remain almost constant. Due to the use of an alternative material, e.g., aluminum, the mass moment of inertia of the impeller is reduced. In actual practice, this means that a much better response characteristic is achieved in an impeller having a diameter of, for example, 670 mm.
  • FIG. 1 is a perspective view of an impeller in accordance with the present invention
  • FIG. 2 is a sectional top view of the impeller of FIG. 1;
  • FIG. 3 is a sectional side view of the impeller of FIG. 1;
  • FIG. 4 is a side sectional view of an impeller having an integrated coupling.
  • FIG. 1 shows an impeller 1 , in particular a radial-flow fan or compressor impeller. It consists of a cover plate 2 , a base plate 3 , a hub 6 with a mounting hole 7 and blades.
  • the blades of the impeller 1 are configured as full blades 4 and split blades 5 .
  • the geometry of the full blades is not identical to that of the split blades here because the split blades form part of the full blades.
  • the full blades 4 and split blades 5 are arranged at a different angular distance and in a different order, the arrangement and order of which can be seen from the sectional diagram in FIG. 2. For example, the split blade 5 . 1 is followed by a full blade 4 . 1 , then a split blade 5 .
  • the noise generated is further reduced due to the different angular distance and the different order while achieving almost the same efficiency and/or power consumption.
  • the level and frequency of the noise, which is perceived as unpleasant, are reduced by these measures and distributed over a broader frequency band. Due to these structural measures, the acoustic power is distributed among several individual tones, the intensity of which turns out to be accordingly lower.
  • the impeller 1 is preferably made of an alternative material, e.g., aluminum. This results in a significant reduction in the mass moment of inertia.
  • the impeller 1 shown in FIG. 1 also has balancing holes 8 . An imbalance in the impeller 1 is compensated by these balancing holes 8 . This reduces manufacturing costs because it is no longer necessary to mount additional balancing weights.
  • FIG. 2 shows a first area 15 and a second area 16 . Only full blades 4 are arranged in the first area 15 . Both full blades and split blades are arranged in the second area 16 . The order of the full blades 4 . 1 through 4 . 6 and the split blades 5 . 1 through 5 . 4 is irregular in the second area 16 . The angles between two blades on the air intake side and the air outlet side are identical. The angle x 1 between the split blade 5 . 1 and the full blade 4 . 1 thus corresponds to the angle x 2 . The angle y 1 between the full blade 4 . 1 and the split blade 5 . 2 corresponds to the angle y 2 .
  • angles z 1 and z 2 are different from one another, i.e., x 1 is not equal to y 1 and is not equal to z 1 .
  • x 1 is not equal to y 1 and is not equal to z 1 .
  • the order of the full blades 4 and the split blades 5 is not rotationally symmetrical, not even in segments.
  • FIG. 3 shows the impeller 1 in a side view.
  • the direction of flow of the air is indicated with arrows.
  • the air is conveyed by the impeller 1 in the axial direction, i.e., radially outward, from above in the direction of the drawing.
  • FIG. 3 shows the arrangement of the full blades and the split blades between the cover plate 2 and the base plate 3 .
  • FIG. 4 shows the impeller 1 with an integrated coupling and a coupling housing 9 .
  • the coupling housing 9 is integrated into the impeller 1 on the rear side 13 .
  • Reference numeral 10 denotes the connection for a housing, e.g., a gear box.
  • the impeller 1 is detachably connected to a wheel mount 11 by a screw 14 from the front side 12 .
  • the wheel mount 11 is in turn fixedly connected to the coupling and the coupling housing 9 .
  • the impeller 1 is activated or deactivated on the basis of the status of the coupling 9 .

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
US10/476,990 2001-05-09 2002-05-04 Rotor disk Abandoned US20040202539A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10122516.4 2001-05-09
DE10122516A DE10122516B4 (de) 2001-05-09 2001-05-09 Laufrad
PCT/EP2002/004920 WO2002090776A2 (de) 2001-05-09 2002-05-04 Laufrad

Publications (1)

Publication Number Publication Date
US20040202539A1 true US20040202539A1 (en) 2004-10-14

Family

ID=7684151

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/476,990 Abandoned US20040202539A1 (en) 2001-05-09 2002-05-04 Rotor disk

Country Status (4)

Country Link
US (1) US20040202539A1 (de)
EP (1) EP1387962A2 (de)
DE (1) DE10122516B4 (de)
WO (1) WO2002090776A2 (de)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090136357A1 (en) * 2007-11-27 2009-05-28 Emerson Electric Co. Bi-Directional Cooling Fan
WO2010048905A1 (en) * 2008-10-29 2010-05-06 Vysoké Učení Technické V Brně Impeller of hydraulic machines
WO2013074393A1 (en) * 2011-11-15 2013-05-23 Borgwarner Inc. Flow rotor, in particular turbine wheel
EP2921712A1 (de) * 2014-03-17 2015-09-23 Elica S.p.A. Rotor für ein radialgebläse und radialgebläse
CN107448415A (zh) * 2017-08-23 2017-12-08 联想(北京)有限公司 一种电子设备及其散热风扇
US20180252237A1 (en) * 2017-03-01 2018-09-06 Cooler Master Co., Ltd. Impeller
RU2679061C1 (ru) * 2017-01-17 2019-02-05 Эбершпехер Клаймит Контрол Системз Гмбх Унд Ко. Кг Рабочее колесо для транспортировки воздуха для обогрева для отопителя транспортного средства
CN112460065A (zh) * 2019-09-06 2021-03-09 台达电子工业股份有限公司 叶轮及其风扇
US11105203B2 (en) 2018-01-29 2021-08-31 Carrier Corporation High efficiency centrifugal impeller with balancing weights
US20230287795A1 (en) * 2020-09-10 2023-09-14 Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. Turbine wheel, turbine, and turbocharger

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202005015357U1 (de) 2004-10-09 2006-01-05 Ebm-Papst St. Georgen Gmbh & Co. Kg Lüfter mit einem Lüfterrad
WO2008101577A2 (de) 2007-02-23 2008-08-28 Sew-Eurodrive Gmbh & Co. Kg Lüfterrad, system und getriebebaureihe
DE102007009366B4 (de) * 2007-02-23 2017-06-14 Sew-Eurodrive Gmbh & Co Kg Lüfterrad, System und Getriebebaureihe
DE102007041142A1 (de) * 2007-08-30 2009-03-05 Siemens Ag Radialverdichterlaufrad
DE102009007843A1 (de) 2009-02-06 2010-08-12 Bosch Mahle Turbo Systems Gmbh & Co. Kg Verdichterrad einer Ladeeinrichtung
DE102010039219A1 (de) * 2010-08-11 2012-02-16 Behr Gmbh & Co. Kg Lüfter, insbesondere für ein Motorkühlungsgebläse in einem Kraftfahrzeug
DE102013212341A1 (de) * 2013-06-26 2014-12-31 Behr Gmbh & Co. Kg Lüftervorrichtung und Verfahren zur Auswuchtung
DE102015112731A1 (de) * 2015-08-03 2017-02-09 Ebm-Papst St. Georgen Gmbh & Co. Kg Lüftervorrichtung und Verfahren zur Auswuchtung einer Lüftervorrichtung
DE102015112732A1 (de) * 2015-08-03 2017-02-09 Ebm-Papst St. Georgen Gmbh & Co. Kg Verfahren zur Auswuchtung einer Lüftervorrichtung und Lüftervorrichtung, welche mittels eines Verfahrens ausgewuchtet ist

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US912362A (en) * 1907-04-23 1909-02-16 George Marie Capell Centrifugal fan and pump.
US2658455A (en) * 1948-02-26 1953-11-10 Laval Steam Turbine Co Impeller with center intake
US2781963A (en) * 1950-06-16 1957-02-19 Guy S Faber Blower
US3387768A (en) * 1966-04-08 1968-06-11 Rotron Mfg Co Fastener
US3622249A (en) * 1968-08-18 1971-11-23 Aisin Seiki Fan assembly
US3627445A (en) * 1968-04-17 1971-12-14 S E R M A G Soc D Etudes Et De Ventilating device for cooling a heat engine
US4253800A (en) * 1978-08-12 1981-03-03 Hitachi, Ltd. Wheel or rotor with a plurality of blades
US4257744A (en) * 1979-03-21 1981-03-24 Westinghouse Electric Corp. Impeller and shaft assembly for high speed gas compressor
US5158435A (en) * 1991-11-15 1992-10-27 Praxair Technology, Inc. Impeller stress improvement through overspeed

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE174855C (de) * 1905-08-19 1906-10-01 Wittig Emil Laufrad für ventilatoren
DE1707136U (de) * 1955-05-20 1955-09-15 Gerhard Dr Ing Schemberger Laufrad fuer kreiselgeblaese.
GB1293553A (en) * 1969-02-18 1972-10-18 Cav Ltd Radial flow fans
GB2046360A (en) * 1979-03-31 1980-11-12 Aes Plastics Ltd Fluid impeller
US5002461A (en) * 1990-01-26 1991-03-26 Schwitzer U.S. Inc. Compressor impeller with displaced splitter blades
DE9102865U1 (de) * 1991-03-09 1992-07-16 Robert Bosch Gmbh, 7000 Stuttgart Lüfterrad
EP0516073A1 (de) * 1991-05-29 1992-12-02 Alcatel SEL Aktiengesellschaft Vorrichtung zum Fördern eines gasförmigen Mediums
DE4445671B4 (de) * 1994-12-21 2005-03-24 Behr Gmbh & Co. Kg Axiallüfter für einen Kühler eines Kraftfahrzeugmotors

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US912362A (en) * 1907-04-23 1909-02-16 George Marie Capell Centrifugal fan and pump.
US2658455A (en) * 1948-02-26 1953-11-10 Laval Steam Turbine Co Impeller with center intake
US2781963A (en) * 1950-06-16 1957-02-19 Guy S Faber Blower
US3387768A (en) * 1966-04-08 1968-06-11 Rotron Mfg Co Fastener
US3627445A (en) * 1968-04-17 1971-12-14 S E R M A G Soc D Etudes Et De Ventilating device for cooling a heat engine
US3622249A (en) * 1968-08-18 1971-11-23 Aisin Seiki Fan assembly
US4253800A (en) * 1978-08-12 1981-03-03 Hitachi, Ltd. Wheel or rotor with a plurality of blades
US4257744A (en) * 1979-03-21 1981-03-24 Westinghouse Electric Corp. Impeller and shaft assembly for high speed gas compressor
US5158435A (en) * 1991-11-15 1992-10-27 Praxair Technology, Inc. Impeller stress improvement through overspeed

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8007241B2 (en) 2007-11-27 2011-08-30 Nidec Motor Corporation Bi-directional cooling fan
US20090136357A1 (en) * 2007-11-27 2009-05-28 Emerson Electric Co. Bi-Directional Cooling Fan
WO2010048905A1 (en) * 2008-10-29 2010-05-06 Vysoké Učení Technické V Brně Impeller of hydraulic machines
US10113428B2 (en) * 2011-11-15 2018-10-30 Borgwarner Inc. Flow rotor, in particular turbine wheel
WO2013074393A1 (en) * 2011-11-15 2013-05-23 Borgwarner Inc. Flow rotor, in particular turbine wheel
US20140308137A1 (en) * 2011-11-15 2014-10-16 Borgwarner Inc. Flow rotor, in particular turbine wheel
EP2921712A1 (de) * 2014-03-17 2015-09-23 Elica S.p.A. Rotor für ein radialgebläse und radialgebläse
RU2679061C1 (ru) * 2017-01-17 2019-02-05 Эбершпехер Клаймит Контрол Системз Гмбх Унд Ко. Кг Рабочее колесо для транспортировки воздуха для обогрева для отопителя транспортного средства
US10823189B2 (en) 2017-01-17 2020-11-03 Eberspächer Climate Control Systems GmbH & Co. KG Hot air feed wheel
US20180252237A1 (en) * 2017-03-01 2018-09-06 Cooler Master Co., Ltd. Impeller
CN107448415A (zh) * 2017-08-23 2017-12-08 联想(北京)有限公司 一种电子设备及其散热风扇
US11105203B2 (en) 2018-01-29 2021-08-31 Carrier Corporation High efficiency centrifugal impeller with balancing weights
CN112460065A (zh) * 2019-09-06 2021-03-09 台达电子工业股份有限公司 叶轮及其风扇
US20230287795A1 (en) * 2020-09-10 2023-09-14 Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. Turbine wheel, turbine, and turbocharger
US12025024B2 (en) * 2020-09-10 2024-07-02 Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. Turbine wheel, turbine, and turbocharger

Also Published As

Publication number Publication date
DE10122516A1 (de) 2002-11-28
WO2002090776A2 (de) 2002-11-14
EP1387962A2 (de) 2004-02-11
DE10122516B4 (de) 2006-10-19
WO2002090776A3 (de) 2003-02-27

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AS Assignment

Owner name: MTU FRIEDRICHSHAFEN GMBH, GERMANY

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:BLANK, ANDREAS;KIEFER, GUENTHER;LADNER, WOLFGANG;AND OTHERS;REEL/FRAME:015393/0001;SIGNING DATES FROM 20031118 TO 20031205

STCB Information on status: application discontinuation

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