NO893887D0 - HIGH SPEED WHEELS OF COMPOSITION MATERIAL. - Google Patents

HIGH SPEED WHEELS OF COMPOSITION MATERIAL.

Info

Publication number
NO893887D0
NO893887D0 NO893887A NO893887A NO893887D0 NO 893887 D0 NO893887 D0 NO 893887D0 NO 893887 A NO893887 A NO 893887A NO 893887 A NO893887 A NO 893887A NO 893887 D0 NO893887 D0 NO 893887D0
Authority
NO
Norway
Prior art keywords
fibres
wheel
circumferentially
blades
count
Prior art date
Application number
NO893887A
Other languages
Norwegian (no)
Other versions
NO893887L (en
Inventor
Jean-Pierre Labrouche
Bernard Broquere
Jean-Marie Parenteau
Jacques Etienne
Alain Lacombe
Original Assignee
Europ Propulsion
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 Europ Propulsion filed Critical Europ Propulsion
Publication of NO893887D0 publication Critical patent/NO893887D0/en
Publication of NO893887L publication Critical patent/NO893887L/en

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
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282Selecting composite materials, e.g. blades with reinforcing filaments
    • 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
    • F01D5/34Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Ceramic Engineering (AREA)
  • Composite Materials (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Laminated Bodies (AREA)

Abstract

The wheel, comprising a central part or rim equipped with blades on its periphery, is produced in one piece from a composite material consisting of a fibrous reinforcement densified by a matrix. The fibrous reinforcement is formed by means of a helical fabric (20) with radially oriented fibres and circumferentially oriented fibres, the count of fibres in the radial direction and the count of fibres in the circumferential direction varying along a radius of the wheel as a function of the variation of the radial stresses and circumferential stresses, respectively, exerted on the wheel during its use, and at least some of the circumferentially directed fibres in the rim are made of a material having a high mechanical resistance whilst at least some of the circumferentially directed fibres in the blades and of the radially directed fibres, are made of a material having a high resistance to elevated temperatures and to chemical attacks. <IMAGE>
NO89893887A 1988-09-30 1989-09-29 HIGH SPEED WHEELS OF COMPOSITION MATERIAL. NO893887L (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8812853A FR2637319B1 (en) 1988-09-30 1988-09-30 HIGH SPEED TURBINE WHEEL IN COMPOSITE MATERIAL

Publications (2)

Publication Number Publication Date
NO893887D0 true NO893887D0 (en) 1989-09-29
NO893887L NO893887L (en) 1990-04-02

Family

ID=9370590

Family Applications (1)

Application Number Title Priority Date Filing Date
NO89893887A NO893887L (en) 1988-09-30 1989-09-29 HIGH SPEED WHEELS OF COMPOSITION MATERIAL.

Country Status (10)

Country Link
EP (1) EP0362074B1 (en)
JP (1) JP2950554B2 (en)
AT (1) ATE89364T1 (en)
CA (1) CA1315696C (en)
DE (1) DE68906498T2 (en)
ES (1) ES2041023T3 (en)
FR (1) FR2637319B1 (en)
IE (1) IE62818B1 (en)
NO (1) NO893887L (en)
PT (1) PT91839B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2723868B1 (en) * 1994-08-24 1996-09-20 Snecma PROCESS FOR OBTAINING A METAL CIRCULAR PIECE WITH BLADES
JPH09157049A (en) * 1995-11-30 1997-06-17 Senshin Zairyo Riyou Gas Jienereeta Kenkyusho:Kk Production of ceramic composite material
US6595751B1 (en) * 2000-06-08 2003-07-22 The Boeing Company Composite rotor having recessed radial splines for high torque applications
NL1024463C2 (en) * 2003-10-06 2005-04-07 Polymarin Holding B V Rotor for use in a wind turbine and method for making the rotor.

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1090721A (en) * 1964-01-15 1967-11-15 Rolls Royce Method of making a bladed rotor for a fluid flow machine, e.g. a gas turbine engine
DE1629442A1 (en) * 1966-02-25 1971-02-04 Gen Electric Impeller and process for its manufacture
US3501090A (en) * 1968-01-29 1970-03-17 Gen Electric Composite bladed rotors
FR2401888A1 (en) * 1977-09-06 1979-03-30 Europ Propulsion Impregnating porous carbon body with refractory material - esp. carbide, boride and/or nitride to improve compressive strength and erosion resistance
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
JPS5766939A (en) * 1980-10-15 1982-04-23 Komatsu Ltd Manufacture of turbine impeller
US4464097A (en) * 1982-04-01 1984-08-07 General Electric Company Turbomachinery rotor and method of manufacture
FR2568937B1 (en) * 1984-08-13 1988-10-28 Europ Propulsion PROCESS FOR MANUFACTURING A TURBINE OR COMPRESSOR WHEEL OF COMPOSITE MATERIAL, AND WHEEL THUS OBTAINED

Also Published As

Publication number Publication date
IE62818B1 (en) 1995-03-08
PT91839B (en) 1995-07-18
NO893887L (en) 1990-04-02
EP0362074B1 (en) 1993-05-12
ES2041023T3 (en) 1993-11-01
IE893099L (en) 1990-03-30
FR2637319A1 (en) 1990-04-06
CA1315696C (en) 1993-04-06
DE68906498D1 (en) 1993-06-17
JPH02176102A (en) 1990-07-09
EP0362074A1 (en) 1990-04-04
ATE89364T1 (en) 1993-05-15
JP2950554B2 (en) 1999-09-20
FR2637319B1 (en) 1994-02-25
PT91839A (en) 1990-03-30
DE68906498T2 (en) 1993-11-04

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