FR1579649A - - Google Patents

Info

Publication number
FR1579649A
FR1579649A FR1579649DA FR1579649A FR 1579649 A FR1579649 A FR 1579649A FR 1579649D A FR1579649D A FR 1579649DA FR 1579649 A FR1579649 A FR 1579649A
Authority
FR
France
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
Application number
Other languages
French (fr)
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
Application granted granted Critical
Publication of FR1579649A publication Critical patent/FR1579649A/fr
Expired legal-status Critical Current

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
FR1579649D 1967-06-24 1968-06-24 Expired FR1579649A (en)

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
FR1579649A true FR1579649A (en) 1969-08-29

Family

ID=10288440

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1579649D Expired FR1579649A (en) 1967-06-24 1968-06-24

Country Status (7)

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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2327858A1 (en) * 1975-10-14 1977-05-13 Messerschmitt Boelkow Blohm CONNECTION ELEMENT FOR THE DIVIDED TRANSMISSION OF STRENGTHS IN A COMPONENT
FR2524546A1 (en) * 1982-04-01 1983-10-07 Gen Electric ROTOR OF TURBOMACHINE
WO1991008893A1 (en) * 1989-12-20 1991-06-27 MTU MOTOREN- UND TURBINEN-UNION MüNCHEN GMBH Technical fibre structural member subjected to tensile stress

Families Citing this family (49)

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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
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 (en) * 1979-08-31 1981-12-24 Heraeus Quarzschmelze Gmbh, 6450 Hanau Process for the tool-free production of porous shaped bodies from quartz glass and the use of these shaped bodies
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
US4460531A (en) * 1982-05-10 1984-07-17 The Boeing Company Composite fiber reinforced propeller
US4487792A (en) * 1982-06-21 1984-12-11 E. I. Du Pont De Nemours And Company Preforms for reinforcement of battery grids
US4395449A (en) * 1982-06-21 1983-07-26 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
GB2161109B (en) * 1984-07-07 1988-12-21 Rolls Royce Integral bladed member
GB2161110B (en) * 1984-07-07 1988-03-23 Rolls Royce An annular bladed member having an integral shroud and a method of manufacture thereof
US4666753A (en) * 1985-05-16 1987-05-19 United Technologies Corporation Filament wound structure for use as a torque drive
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 (en) * 1994-09-14 1996-10-25 Snecma BLADE OF A TURBOMACHINE IN COMPOSITE MATERIAL PROVIDED WITH A SEAL AND ITS MANUFACTURING METHOD
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
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
US6261699B1 (en) 1999-04-28 2001-07-17 Allison Advanced Development Company Fiber reinforced iron-cobalt composite material system
DE69914959T2 (en) 1999-11-25 2004-12-16 Dunlop Aerospace Ltd. ABRASIVE OBJECTS
EP2302170A1 (en) 2004-11-12 2011-03-30 Board of Trustees of Michigan State University Turbomachine system and method of operation
GB2427658B (en) * 2005-06-30 2007-08-22 Rolls Royce Plc Organic matrix composite integrally bladed rotor
FR2933634B1 (en) * 2008-07-10 2010-08-27 Snecma AUBE BLOWER RECTIFIER IN COMPOSITE 3D
FR2939130B1 (en) * 2008-11-28 2011-09-16 Snecma Propulsion Solide PROCESS FOR MANUFACTURING COMPOUND FORM SHAPE PIECE OF COMPOSITE MATERIAL
FR2946999B1 (en) * 2009-06-18 2019-08-09 Safran Aircraft Engines CMC TURBINE DISPENSER ELEMENT, PROCESS FOR MANUFACTURING SAME, AND DISPENSER AND GAS TURBINE INCORPORATING SAME.
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 (en) * 2009-12-14 2012-02-10 Snecma TURBOMACHINE DRAFT IN COMPOSITE MATERIAL AND METHOD FOR MANUFACTURING THE SAME
FI20105048A (en) * 2010-01-21 2011-07-22 Runtech Systems Oy Method of manufacturing a rotor of a radial compressor
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 (en) * 2011-06-21 2015-06-05 Snecma TURBOMACHINE COMPRESSOR COMPRESSOR OR TURBINE DISPENSER PART AND METHOD FOR MANUFACTURING THE SAME
US20130052004A1 (en) * 2011-08-25 2013-02-28 Nicholas D. Stilin Structural composite fan exit guide vane for a turbomachine
FR2983428B1 (en) * 2011-12-01 2014-01-17 Snecma Propulsion Solide PROCESS FOR MANUFACTURING A TURBOMACHINE BLADE IN COMPOSITE MATERIAL WITH INTEGRATED PLATFORMS
GB201215299D0 (en) * 2012-08-29 2012-10-10 Rolls Royce Plc A Metallic foam material
US9677405B2 (en) 2013-03-05 2017-06-13 Rolls-Royce Corporation Composite gas turbine engine blade having multiple airfoils
US10193430B2 (en) 2013-03-15 2019-01-29 Board Of Trustees Of Michigan State University Electromagnetic device having discrete wires
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
US10006156B2 (en) * 2014-03-21 2018-06-26 Goodrich Corporation Systems and methods for calculated tow fiber angle

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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2327858A1 (en) * 1975-10-14 1977-05-13 Messerschmitt Boelkow Blohm CONNECTION ELEMENT FOR THE DIVIDED TRANSMISSION OF STRENGTHS IN A COMPONENT
FR2524546A1 (en) * 1982-04-01 1983-10-07 Gen Electric ROTOR OF TURBOMACHINE
WO1991008893A1 (en) * 1989-12-20 1991-06-27 MTU MOTOREN- UND TURBINEN-UNION MüNCHEN GMBH Technical fibre structural member subjected to tensile stress

Also Published As

Publication number Publication date
CH501823A (en) 1971-01-15
SE331940B (en) 1971-01-18
BE716715A (en) 1968-12-02
US3632460A (en) 1972-01-04
GB1237532A (en) 1971-06-30
JPS4639164B1 (en) 1971-11-18

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Legal Events

Date Code Title Description
TP Transmission of property
TP Transmission of property
ST Notification of lapse