BE716715A - - Google Patents

Info

Publication number
BE716715A
BE716715A BE716715DA BE716715A BE 716715 A BE716715 A BE 716715A BE 716715D A BE716715D A BE 716715DA BE 716715 A BE716715 A BE 716715A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE716715A publication Critical patent/BE716715A/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/34—Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/02—Selection of particular materials
    • F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2307/00—Use of elements other than metals as reinforcement
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/20—Oxide or non-oxide ceramics
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F05D2300/6034—Orientation of fibres, weaving, ply angle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/611—Coating
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/612—Foam
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/615—Filler

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Materials Engineering (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Moulding By Coating Moulds (AREA)
BE716715D 1967-06-24 1968-06-17 BE716715A (en:Method)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2924467A GB1237532A (en) 1967-06-24 1967-06-24 Improvements in turbines and compresser rotors

Publications (1)

Publication Number Publication Date
BE716715A true BE716715A (en:Method) 1968-12-02

Family

ID=10288440

Family Applications (1)

Application Number Title Priority Date Filing Date
BE716715D BE716715A (en:Method) 1967-06-24 1968-06-17

Country Status (7)

Country Link
US (1) US3632460A (en:Method)
JP (1) JPS4639164B1 (en:Method)
BE (1) BE716715A (en:Method)
CH (1) CH501823A (en:Method)
FR (1) FR1579649A (en:Method)
GB (1) GB1237532A (en:Method)
SE (1) SE331940B (en:Method)

Families Citing this family (53)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3827118A (en) * 1970-11-27 1974-08-06 Garrett Corp Airfoil and method of forming the same
US3903578A (en) * 1972-02-28 1975-09-09 United Aircraft Corp Composite fan blade and method of construction
US3799701A (en) * 1972-02-28 1974-03-26 United Aircraft Corp Composite fan blade and method of construction
US3787141A (en) * 1972-11-30 1974-01-22 United Aircraft Corp Filament reinforced motor assembly
GB1533551A (en) * 1974-11-08 1978-11-29 Gen Electric Gas turbofan engines
US4046489A (en) * 1975-10-08 1977-09-06 Eagle Motive Industries, Inc. Aerodynamic fan blade
DE2545929C2 (de) * 1975-10-14 1977-04-28 Messerschmitt-Bölkow-Blohm GmbH, 8000 München AnscMuBelement zur Einleitung von Kräften in ein Bauteil
US4098559A (en) * 1976-07-26 1978-07-04 United Technologies Corporation Paired blade assembly
GB1553038A (en) * 1977-04-28 1979-09-19 Snecma Drum for an axial flow compressor rotor and process for its manufacture
DE2935198C2 (de) * 1979-08-31 1981-12-24 Heraeus Quarzschmelze Gmbh, 6450 Hanau Verfahren zur werkzeugfreien Herstellung von porösen Formkörpern aus Quarzglas und Verwendung dieser Formkörper
US4354804A (en) * 1979-11-30 1982-10-19 Williams Research Corporation Composite turbine wheel, method of manufacture and fixture therefor
US4363602A (en) * 1980-02-27 1982-12-14 General Electric Company Composite air foil and disc assembly
EP0089809A1 (en) * 1982-03-23 1983-09-28 The British Petroleum Company p.l.c. Method for the production of fibre reinforced articles
US4464097A (en) * 1982-04-01 1984-08-07 General Electric Company Turbomachinery rotor and method of manufacture
US4460531A (en) * 1982-05-10 1984-07-17 The Boeing Company Composite fiber reinforced propeller
US4395449A (en) * 1982-06-21 1983-07-26 E. I. Du Pont De Nemours And Company Preforms for reinforcement of battery grids
US4487792A (en) * 1982-06-21 1984-12-11 E. I. Du Pont De Nemours And Company Preforms for reinforcement of battery grids
US4589176A (en) * 1983-11-25 1986-05-20 Rockwell International Corporation Fiber-composite turbine blade and method for its construction
US4584226A (en) * 1984-04-30 1986-04-22 Mcdonnell Douglas Corporation Load transfer structure and method of making the same
GB2161108B (en) * 1984-07-07 1988-03-23 Rolls Royce A compressor rotor assembly and a method of manufacture of such an assembly
GB2161110B (en) * 1984-07-07 1988-03-23 Rolls Royce An annular bladed member having an integral shroud and a method of manufacture thereof
GB2161109B (en) * 1984-07-07 1988-12-21 Rolls Royce Integral bladed member
US4666753A (en) * 1985-05-16 1987-05-19 United Technologies Corporation Filament wound structure for use as a torque drive
JPH05505148A (ja) * 1989-12-20 1993-08-05 エムティーユー・モトレン―ウント・タービネン―ユニオン・ミュンヘン・ジーエムビーエッチ 引張荷重が負荷される繊維技術的部材
US5413851A (en) * 1990-03-02 1995-05-09 Minnesota Mining And Manufacturing Company Coated fibers
US5448883A (en) * 1993-02-26 1995-09-12 The Boeing Company Ion thruster with ion optics having carbon-carbon composite elements
US5548953A (en) * 1993-02-26 1996-08-27 The Boeing Company Carbon-carbon grid elements for ion thruster ion optics
FR2724412B1 (fr) * 1994-09-14 1996-10-25 Snecma Aube de turbomachine en materiau composite munie d'un joint d'etancheite et son procede de realisation
US5921754A (en) * 1996-08-26 1999-07-13 Foster-Miller, Inc. Composite turbine rotor
US5735673A (en) * 1996-12-04 1998-04-07 United Technologies Corporation Turbine engine rotor blade pair
US6261699B1 (en) 1999-04-28 2001-07-17 Allison Advanced Development Company Fiber reinforced iron-cobalt composite material system
US6232688B1 (en) 1999-04-28 2001-05-15 Allison Advanced Development Company High speed magnetic thrust disk
US6247638B1 (en) 1999-04-28 2001-06-19 Allison Advanced Development Company Selectively reinforced member and method of manufacture
ATE259763T1 (de) 1999-11-25 2004-03-15 Dunlop Aerospace Ltd Abriebsbeständige gegenstände
EP2302172A1 (en) * 2004-11-12 2011-03-30 Board of Trustees of Michigan State University Machine comprising an electromagnetic woven rotor and manufacturing method
GB2427658B (en) * 2005-06-30 2007-08-22 Rolls Royce Plc Organic matrix composite integrally bladed rotor
FR2933634B1 (fr) * 2008-07-10 2010-08-27 Snecma Aube redresseur de soufflante en composite 3d
FR2939130B1 (fr) * 2008-11-28 2011-09-16 Snecma Propulsion Solide Procede de fabrication de piece de forme de forme complexe en materiau composite.
FR2946999B1 (fr) * 2009-06-18 2019-08-09 Safran Aircraft Engines Element de distributeur de turbine en cmc, procede pour sa fabrication, et distributeur et turbine a gaz l'incorporant.
US9506355B2 (en) 2009-12-14 2016-11-29 Snecma Turbine engine blade or vane made of composite material, turbine nozzle or compressor stator incorporating such vanes and method of fabricating same
FR2953885B1 (fr) * 2009-12-14 2012-02-10 Snecma Aube de turbomachine en materiau composite et procede pour sa fabrication
FI20105048L (fi) * 2010-01-21 2011-07-22 Runtech Systems Oy Menetelmä radiaalikompressorin juoksupyörän valmistamiseksi
US9151166B2 (en) * 2010-06-07 2015-10-06 Rolls-Royce North American Technologies, Inc. Composite gas turbine engine component
EP2522808A1 (en) * 2011-05-10 2012-11-14 Aella SA Turbo-engine, particularly internal combustion engine
FR2976968B1 (fr) * 2011-06-21 2015-06-05 Snecma Piece de turbomachine formant redresseur de compresseur ou distributeur de turbine et procede pour sa fabrication
US20130052004A1 (en) * 2011-08-25 2013-02-28 Nicholas D. Stilin Structural composite fan exit guide vane for a turbomachine
FR2983428B1 (fr) * 2011-12-01 2014-01-17 Snecma Propulsion Solide Procede de fabrication d'une aube de turbomachine en materiau composite a plates-formes integrees
GB201215299D0 (en) * 2012-08-29 2012-10-10 Rolls Royce Plc A Metallic foam material
CA2896753A1 (en) 2013-03-05 2015-04-02 Rolls-Royce North American Technologies, Inc. Composite gas turbine engine blade having multiple airfoils
US9845688B2 (en) 2013-03-15 2017-12-19 Rolls-Royce Corporation Composite blade with an integral blade tip shroud and method of forming the same
US10193430B2 (en) 2013-03-15 2019-01-29 Board Of Trustees Of Michigan State University Electromagnetic device having discrete wires
US10006156B2 (en) * 2014-03-21 2018-06-26 Goodrich Corporation Systems and methods for calculated tow fiber angle
GB202303505D0 (en) 2023-03-10 2023-04-26 Rolls Royce Plc Method for manufacturing a composite bladed disk or rotor

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1537790A (en) * 1923-09-17 1925-05-12 Alpe Robert John Universal coupling and the manufacture thereof
US2152373A (en) * 1935-12-26 1939-03-28 Dill Mfg Co Valve stem and method of constructing same
US3279967A (en) * 1961-04-07 1966-10-18 Carrier Corp Method of fabricating a rotor shroud
US3403844A (en) * 1967-10-02 1968-10-01 Gen Electric Bladed member and method for making

Also Published As

Publication number Publication date
FR1579649A (en:Method) 1969-08-29
JPS4639164B1 (en:Method) 1971-11-18
US3632460A (en) 1972-01-04
GB1237532A (en) 1971-06-30
CH501823A (fr) 1971-01-15
SE331940B (en:Method) 1971-01-18

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