GB2366589A - Fiber reinforced composite material system - Google Patents

Fiber reinforced composite material system

Info

Publication number
GB2366589A
GB2366589A GB0126003A GB0126003A GB2366589A GB 2366589 A GB2366589 A GB 2366589A GB 0126003 A GB0126003 A GB 0126003A GB 0126003 A GB0126003 A GB 0126003A GB 2366589 A GB2366589 A GB 2366589A
Authority
GB
United Kingdom
Prior art keywords
composite material
material system
fiber reinforced
reinforced composite
high strength
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.)
Granted
Application number
GB0126003A
Other versions
GB0126003D0 (en
GB2366589B (en
Inventor
Robert Anthony Ress
Mark Stephen Henry
Amit Chatterjee
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 Corp
Rolls Royce North American Technologies Inc
Original Assignee
Allison Engine Co Inc
Allison Advanced Development Co Inc
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
Priority claimed from US09/301,049 external-priority patent/US6261699B1/en
Priority claimed from US09/301,302 external-priority patent/US6232688B1/en
Priority claimed from US09/301,674 external-priority patent/US6247638B1/en
Application filed by Allison Engine Co Inc, Allison Advanced Development Co Inc filed Critical Allison Engine Co Inc
Publication of GB0126003D0 publication Critical patent/GB0126003D0/en
Publication of GB2366589A publication Critical patent/GB2366589A/en
Application granted granted Critical
Publication of GB2366589B publication Critical patent/GB2366589B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/20Making alloys containing metallic or non-metallic fibres or filaments by subjecting to pressure and heat an assembly comprising at least one metal layer or sheet and one layer of fibres or filaments
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C49/00Alloys containing metallic or non-metallic fibres or filaments
    • C22C49/02Alloys containing metallic or non-metallic fibres or filaments characterised by the matrix material
    • C22C49/08Iron group metals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/04Bearings not otherwise provided for using magnetic or electric supporting means
    • F16C32/0406Magnetic bearings
    • F16C32/044Active magnetic bearings
    • F16C32/0459Details of the magnetic circuit
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/04Bearings not otherwise provided for using magnetic or electric supporting means
    • F16C32/0406Magnetic bearings
    • F16C32/044Active magnetic bearings
    • F16C32/0459Details of the magnetic circuit
    • F16C32/0468Details of the magnetic circuit of moving parts of the magnetic circuit, e.g. of the rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/04Bearings not otherwise provided for using magnetic or electric supporting means
    • F16C32/0406Magnetic bearings
    • F16C32/044Active magnetic bearings
    • F16C32/0474Active magnetic bearings for rotary movement
    • F16C32/0476Active magnetic bearings for rotary movement with active support of one degree of freedom, e.g. axial magnetic bearings
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F1/00Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
    • H01F1/01Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
    • H01F1/03Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
    • H01F1/12Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials
    • H01F1/14Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials metals or alloys
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00Supplementary information concerning processes or compositions relating to powder metallurgy
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/50Bearings
    • F05B2240/51Bearings magnetic
    • F05B2240/511Bearings magnetic with permanent magnets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00Engines or pumps
    • F16C2360/23Gas turbine engines

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Dispersion Chemistry (AREA)
  • Power Engineering (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

The present invention contemplates a high strength magnetic composite material system (35) comprising a plurality of high strength fibers (30) coupled together by a soft magnetic alloy (31). In one embodiment an internally reinforced structure is formed of the composite material system (35) and has strengths greater than the monolithic magnetic alloy. The structure having been consolidated through a combined pressure and thermal cycle.
GB0126003A 1999-04-28 2000-04-28 Fiber reinforced composite material system Expired - Fee Related GB2366589B (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US09/301,049 US6261699B1 (en) 1999-04-28 1999-04-28 Fiber reinforced iron-cobalt composite material system
US09/301,302 US6232688B1 (en) 1999-04-28 1999-04-28 High speed magnetic thrust disk
US09/301,674 US6247638B1 (en) 1999-04-28 1999-04-28 Selectively reinforced member and method of manufacture
PCT/US2000/011574 WO2000065115A2 (en) 1999-04-28 2000-04-28 Fiber reinforced composite material system

Publications (3)

Publication Number Publication Date
GB0126003D0 GB0126003D0 (en) 2001-12-19
GB2366589A true GB2366589A (en) 2002-03-13
GB2366589B GB2366589B (en) 2003-06-18

Family

ID=27404786

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0126003A Expired - Fee Related GB2366589B (en) 1999-04-28 2000-04-28 Fiber reinforced composite material system

Country Status (3)

Country Link
AU (1) AU4679600A (en)
GB (1) GB2366589B (en)
WO (1) WO2000065115A2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2483967B (en) * 2010-09-23 2014-12-31 Dyson Technology Ltd A reinforced rotor magnet and method of manufacturing the same

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6803095B1 (en) 2000-09-28 2004-10-12 Lord Corporation Composite shims having a laminate structure
GB0119636D0 (en) * 2001-08-11 2001-10-03 Rolls Royce Plc a method of manufacturing a fibre reinforced metal component
FR2901497B1 (en) * 2006-05-24 2009-03-06 Snecma Sa PROCESS FOR PRODUCING A TURBOMACHINE ROTOR DISC
US7766623B2 (en) * 2006-11-08 2010-08-03 General Electric Company System for manufacturing a rotor having an MMC ring component and an airfoil component having monolithic airfoils

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5658125A (en) * 1995-02-28 1997-08-19 Allison Engine Company, Inc. Magnetic bearings as actuation for active compressor stability control
US5660526A (en) * 1995-06-05 1997-08-26 Allison Engine Company, Inc. Gas turbine rotor with remote support rings
US5675837A (en) * 1991-10-29 1997-10-07 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Process for the preparation of fibre reinforced metal matrix composites and novel preforms therefor
US5977677A (en) * 1996-06-26 1999-11-02 Allison Engine Company Combination bearing for gas turbine engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5675837A (en) * 1991-10-29 1997-10-07 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Process for the preparation of fibre reinforced metal matrix composites and novel preforms therefor
US5658125A (en) * 1995-02-28 1997-08-19 Allison Engine Company, Inc. Magnetic bearings as actuation for active compressor stability control
US5660526A (en) * 1995-06-05 1997-08-26 Allison Engine Company, Inc. Gas turbine rotor with remote support rings
US5977677A (en) * 1996-06-26 1999-11-02 Allison Engine Company Combination bearing for gas turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2483967B (en) * 2010-09-23 2014-12-31 Dyson Technology Ltd A reinforced rotor magnet and method of manufacturing the same

Also Published As

Publication number Publication date
GB0126003D0 (en) 2001-12-19
AU4679600A (en) 2000-11-10
WO2000065115A2 (en) 2000-11-02
WO2000065115A3 (en) 2001-05-31
GB2366589B (en) 2003-06-18

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20070428