GB201200404D0 - Turbocharger impeller - Google Patents

Turbocharger impeller

Info

Publication number
GB201200404D0
GB201200404D0 GBGB1200404.0A GB201200404A GB201200404D0 GB 201200404 D0 GB201200404 D0 GB 201200404D0 GB 201200404 A GB201200404 A GB 201200404A GB 201200404 D0 GB201200404 D0 GB 201200404D0
Authority
GB
United Kingdom
Prior art keywords
impeller
connector
shaft
composite material
particulate reinforcement
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.)
Withdrawn
Application number
GBGB1200404.0A
Other versions
GB2498361A (en
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.)
Napier Turbochargers Ltd
Original Assignee
Napier Turbochargers 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 Napier Turbochargers Ltd filed Critical Napier Turbochargers Ltd
Priority to GB1200404.0A priority Critical patent/GB2498361A/en
Publication of GB201200404D0 publication Critical patent/GB201200404D0/en
Publication of GB2498361A publication Critical patent/GB2498361A/en
Withdrawn legal-status Critical Current

Links

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
    • F01D5/04Blade-carrying members, e.g. rotors for radial-flow machines or engines
    • F01D5/043Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
    • 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
    • F01D5/04Blade-carrying members, e.g. rotors for radial-flow machines or engines
    • F01D5/043Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
    • F01D5/048Form or construction
    • 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
    • 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
    • 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
    • F05D2220/00Application
    • F05D2220/40Application in turbochargers
    • 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
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/24Rotors for turbines
    • 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
    • F05D2300/121Aluminium
    • 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
    • F05D2300/173Aluminium alloys, e.g. AlCuMgPb
    • 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
    • F05D2300/20Oxide or non-oxide ceramics
    • F05D2300/22Non-oxide ceramics
    • F05D2300/222Silicon
    • 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
    • F05D2300/20Oxide or non-oxide ceramics
    • F05D2300/22Non-oxide ceramics
    • F05D2300/226Carbides
    • F05D2300/2261Carbides of silicon
    • 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
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603Composites; e.g. fibre-reinforced
    • F05D2300/6032Metal matrix composites [MMC]
    • 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
    • F05D2300/70Treatment or modification of materials
    • F05D2300/702Reinforcement

Landscapes

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

Abstract

A turbocharger impeller 1, for connection to a shaft 2, is formed from a metal matrix composite material having an aluminium alloy matrix and silicon carbide particulate reinforcement. The average particle diameter of the particulate reinforcement may be 2 microns or less. The particulate reinforcement may be from 10% to 30% of the composite by volume. The impeller may be fitted with a connector 3. The connector may frictionally engage an inner or outer surface of a shaft-side hub extension H of the impeller. The connector may have a threaded portion 12 which screws onto a corresponding threaded portion 7 of the shaft. The material of the connector may have a coefficient of thermal expansion which is equal to or greater than that of the composite material of the impeller. The material of the connector may have a greater strength than the composite material of the impeller.
GB1200404.0A 2012-01-10 2012-01-10 Silicon carbide reinforced aluminium alloy turbocharger impeller Withdrawn GB2498361A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1200404.0A GB2498361A (en) 2012-01-10 2012-01-10 Silicon carbide reinforced aluminium alloy turbocharger impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1200404.0A GB2498361A (en) 2012-01-10 2012-01-10 Silicon carbide reinforced aluminium alloy turbocharger impeller

Publications (2)

Publication Number Publication Date
GB201200404D0 true GB201200404D0 (en) 2012-02-22
GB2498361A GB2498361A (en) 2013-07-17

Family

ID=45788759

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1200404.0A Withdrawn GB2498361A (en) 2012-01-10 2012-01-10 Silicon carbide reinforced aluminium alloy turbocharger impeller

Country Status (1)

Country Link
GB (1) GB2498361A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112084683A (en) * 2020-07-22 2020-12-15 国网江西省电力有限公司电力科学研究院 Plastic deformation analysis method of aluminum alloy material hardware fitting for power transmission line

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6232713B2 (en) * 2013-03-06 2017-11-22 株式会社島津製作所 Vacuum pump
CN110360131A (en) * 2018-04-10 2019-10-22 南通大通宝富风机有限公司 Vapour compression machine
US11754115B1 (en) * 2022-04-18 2023-09-12 Pratt & Whitney Canada Corp. Multi-material bushing for rotatably mounting a rotating structure to a stationary structure

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0417493A3 (en) * 1989-08-14 1991-04-03 Aluminum Company Of America Fiber reinforced composite having an aluminum phosphate bonded matrix
US6592687B1 (en) * 1998-09-08 2003-07-15 The United States Of America As Represented By The National Aeronautics And Space Administration Aluminum alloy and article cast therefrom
US6345503B1 (en) * 2000-09-21 2002-02-12 Caterpillar Inc. Multi-stage compressor in a turbocharger and method of configuring same
GB2392477A (en) * 2002-08-24 2004-03-03 Alstom Turbocharger
WO2006043556A1 (en) * 2004-10-19 2006-04-27 Komatsu Ltd. Turbo machine, compressor impeller used for turbo machine, and method of manufacturing turbo machine
WO2008017156A1 (en) * 2006-08-07 2008-02-14 Cardarelli Francois Composite metallic materials, uses thereof and process for making same

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112084683A (en) * 2020-07-22 2020-12-15 国网江西省电力有限公司电力科学研究院 Plastic deformation analysis method of aluminum alloy material hardware fitting for power transmission line
CN112084683B (en) * 2020-07-22 2022-07-08 国网江西省电力有限公司电力科学研究院 Plastic deformation analysis method of aluminum alloy material hardware fitting for power transmission line

Also Published As

Publication number Publication date
GB2498361A (en) 2013-07-17

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)