CA2218692C - Turbomachines et leur procede de fabrication - Google Patents

Turbomachines et leur procede de fabrication Download PDF

Info

Publication number
CA2218692C
CA2218692C CA002218692A CA2218692A CA2218692C CA 2218692 C CA2218692 C CA 2218692C CA 002218692 A CA002218692 A CA 002218692A CA 2218692 A CA2218692 A CA 2218692A CA 2218692 C CA2218692 C CA 2218692C
Authority
CA
Canada
Prior art keywords
delta
impeller
meridional distance
dimensional
blade
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.)
Expired - Lifetime
Application number
CA002218692A
Other languages
English (en)
Other versions
CA2218692A1 (fr
Inventor
Mehrdad Zangeneh
Hideomi Harada
Akira Goto
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.)
University College London
Ebara Corp
Ebara Research Co Ltd
Original Assignee
University College London
Ebara Corp
Ebara Research Co Ltd
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 University College London, Ebara Corp, Ebara Research Co Ltd filed Critical University College London
Priority to PCT/GB1995/002904 priority Critical patent/WO1997021035A1/fr
Priority to EP95940361A priority patent/EP0865577B1/fr
Priority to CA002218692A priority patent/CA2218692C/fr
Publication of CA2218692A1 publication Critical patent/CA2218692A1/fr
Application granted granted Critical
Publication of CA2218692C publication Critical patent/CA2218692C/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • F04D29/68Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers 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
    • F04D29/18Rotors
    • F04D29/22Rotors specially for centrifugal pumps
    • F04D29/2205Conventional flow pattern
    • 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

Abstract

Rotor (6) de turbomachine muni d'ailettes (3) conçues de telle sorte que la différence de pression statique réduite DELTA Cp entre le moyeu (2) et la virole (4) sur la surface d'aspiration (3c) de l'ailette (3) présente une tendance notablement décroissante à proximité de la sortie du rotor (6b) dans la direction de la sortie du rotor (6b) entre l'entrée du rotor (6a) et la sortie du rotor (6b).
CA002218692A 1995-12-07 1995-12-07 Turbomachines et leur procede de fabrication Expired - Lifetime CA2218692C (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
PCT/GB1995/002904 WO1997021035A1 (fr) 1995-12-07 1995-12-07 Turbomachines et leur procede de fabrication
EP95940361A EP0865577B1 (fr) 1995-12-07 1995-12-07 Turbomachines et leur procede de fabrication
CA002218692A CA2218692C (fr) 1995-12-07 1995-12-07 Turbomachines et leur procede de fabrication

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
PCT/GB1995/002904 WO1997021035A1 (fr) 1995-12-07 1995-12-07 Turbomachines et leur procede de fabrication
CA002218692A CA2218692C (fr) 1995-12-07 1995-12-07 Turbomachines et leur procede de fabrication

Publications (2)

Publication Number Publication Date
CA2218692A1 CA2218692A1 (fr) 1997-06-12
CA2218692C true CA2218692C (fr) 2008-02-12

Family

ID=25679742

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002218692A Expired - Lifetime CA2218692C (fr) 1995-12-07 1995-12-07 Turbomachines et leur procede de fabrication

Country Status (3)

Country Link
EP (1) EP0865577B1 (fr)
CA (1) CA2218692C (fr)
WO (1) WO1997021035A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10962021B2 (en) 2018-08-17 2021-03-30 Rolls-Royce Corporation Non-axisymmetric impeller hub flowpath

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202005001875U1 (de) 2005-02-05 2005-05-19 Rewalux Markisenvertrieb Gmbh Verstellbares Sonnensegel mit einer Plane
KR101001056B1 (ko) 2010-02-19 2010-12-14 송길봉 구심력 동작형 수차
JP5611307B2 (ja) * 2012-11-06 2014-10-22 三菱重工業株式会社 遠心回転機械のインペラ、遠心回転機械
DE102021101419A1 (de) 2021-01-22 2022-07-28 Warema Renkhoff Se Sonnenschutzanlage mit einem Zugsystem
CN114251129A (zh) * 2021-11-29 2022-03-29 中国船舶工业集团公司第七0八研究所 用于透平机械二次流分析评估第三类流面及其设计方法
CN116306180B (zh) * 2023-05-22 2023-08-01 陕西空天信息技术有限公司 一种叶轮辅助分析方法、装置、设备及介质

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE333336C (de) * 1920-04-30 1921-02-22 Alfred P Moessner Dipl Ing Kreisel-Laufrad fuer Gase oder Fluessigkeiten
US3481531A (en) * 1968-03-07 1969-12-02 United Aircraft Canada Impeller boundary layer control device
FR2550585B1 (fr) * 1983-08-09 1987-01-16 Foueillassar Jean Marie Moyens d'uniformiser la vitesse d'un fluide a la sortie d'un rouet centrifuge
US4615659A (en) * 1983-10-24 1986-10-07 Sundstrand Corporation Offset centrifugal compressor
GB2224083A (en) * 1988-10-19 1990-04-25 Rolls Royce Plc Radial or mixed flow bladed rotors

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10962021B2 (en) 2018-08-17 2021-03-30 Rolls-Royce Corporation Non-axisymmetric impeller hub flowpath

Also Published As

Publication number Publication date
CA2218692A1 (fr) 1997-06-12
WO1997021035A1 (fr) 1997-06-12
EP0865577B1 (fr) 2002-07-03
EP0865577A1 (fr) 1998-09-23

Similar Documents

Publication Publication Date Title
US6062819A (en) Turbomachinery and method of manufacturing the same
EP0775248B1 (fr) Turbomachines centrifuges ou a circulation mixte
Zangeneh et al. Suppression of secondary flows in a mixed-flow pump impeller by application of three-dimensional inverse design method: Part 1—Design and numerical validation
Zangeneh et al. On the design criteria for suppression of secondary flows in centrifugal and mixed flow impellers
Zangeneh et al. On the role of three-dimensional inverse design methods in turbomachinery shape optimization
Wu A general theory of three-dimensional flow in subsonic and supersonic turbomachines of axial, radial, and mixed-flow types
Krain et al. Aerodynamics of a centrifugal compressor impeller with transonic inlet conditions
Senoo et al. Pressure loss due to the tip clearance of impeller blades in centrifugal and axial blowers
Casey et al. The use of 3D viscous flow calculations in the design and analysis of industrial centrifugal compressors
CA2218692C (fr) Turbomachines et leur procede de fabrication
Shin et al. Numerical investigation of the pump flow in an automotive torque converter
Goto et al. Suppression of secondary flows in a mixed-flow pump impeller by application of three-dimensional inverse design method: Part 2—Experimental Validation
Oka et al. Optimum aerodynamic design of centrifugal compressor impeller using an inverse method based on meridional viscous flow analysis
Barr et al. Improved performance of a radial turbine through the implementation of back swept blading
Hehn et al. Aerodynamic optimization of a transonic centrifugal compressor by using arbitrary blade surfaces
Zangeneh et al. On the design criteria for suppression of secondary flows in centrifugal and mixed flow impellers
Hazby et al. Design and testing of a high flow coefficient mixed flow impeller
KR100359943B1 (ko) 원심또는혼류터보기계
Itou et al. Optimum aerodynamic design of centrifugal compressor using a genetic algorithm and an inverse method based on meridional viscous flow analysis
Biedermann et al. Feasibility Study on the Effect of Blade Inclination for Heavy Duty Centrifugal Fans–Aerodynamic Aspects
Chana et al. The Effect of Reaction on Compressor Performance
Dian-Kui et al. Calculation of complete three-dimensional flow in a centrifugal rotor with splitter blades
Dunham Modelling of spanwise mixing in compressor through-flow computations
Veress Computational investigation on deswirl vanes for multistage centrifugal compressors
Wang et al. Optimization of Centrifugal Compressor Splitter Blades Design Based on Regression Kriging Algorithm

Legal Events

Date Code Title Description
EEER Examination request
MKEX Expiry

Effective date: 20151207