CH497641A - Verfahren zur Herstellung eines Schaufelkranzes für Strömungsmaschinen - Google Patents

Verfahren zur Herstellung eines Schaufelkranzes für Strömungsmaschinen

Info

Publication number
CH497641A
CH497641A CH532168A CH532168A CH497641A CH 497641 A CH497641 A CH 497641A CH 532168 A CH532168 A CH 532168A CH 532168 A CH532168 A CH 532168A CH 497641 A CH497641 A CH 497641A
Authority
CH
Switzerland
Prior art keywords
blade
fibers
dependent
blades
rotor
Prior art date
Application number
CH532168A
Other languages
German (de)
English (en)
Inventor
Palfreyman Jack
Edward Middleton Henry
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of CH497641A publication Critical patent/CH497641A/de

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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3023Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
    • F01D5/303Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
    • F01D5/3038Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
    • 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
    • F01D21/00Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH532168A 1967-04-12 1968-04-09 Verfahren zur Herstellung eines Schaufelkranzes für Strömungsmaschinen CH497641A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB06873/67A GB1170593A (en) 1967-04-12 1967-04-12 Method of making a Bladed Rotor

Publications (1)

Publication Number Publication Date
CH497641A true CH497641A (de) 1970-10-15

Family

ID=10085214

Family Applications (1)

Application Number Title Priority Date Filing Date
CH532168A CH497641A (de) 1967-04-12 1968-04-09 Verfahren zur Herstellung eines Schaufelkranzes für Strömungsmaschinen

Country Status (6)

Country Link
US (1) US3515501A (enrdf_load_stackoverflow)
BE (1) BE713585A (enrdf_load_stackoverflow)
CH (1) CH497641A (enrdf_load_stackoverflow)
DE (1) DE1751156A1 (enrdf_load_stackoverflow)
FR (1) FR1575682A (enrdf_load_stackoverflow)
GB (1) GB1170593A (enrdf_load_stackoverflow)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1357295A3 (de) * 2002-04-25 2004-03-10 MTU Aero Engines GmbH Verdichter in mehrstufiger Axialbauart
WO2005056983A1 (de) * 2003-12-13 2005-06-23 Mtu Aero Engines Gmbh Faserverstärkter rotor für eine turbomaschine
DE102006015838A1 (de) * 2006-04-03 2007-10-04 Rolls-Royce Deutschland Ltd & Co Kg Axialkompressor für ein Gasturbinentriebwerk
US8677622B2 (en) 2006-03-10 2014-03-25 Rolls-Royce Deutschland Ltd & Co Kg Intake cone in a fiber compound material for a gas turbine engine and method for its manufacture

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3610772A (en) * 1970-05-04 1971-10-05 Gen Motors Corp Bladed rotor
DE2046486C3 (de) * 1970-09-21 1974-03-07 Fa. Willi Seeber, Kardaun, Bozen (Italien) Schaufelrad für Lüfter
FR2143561B1 (enrdf_load_stackoverflow) * 1971-06-29 1974-03-08 Snecma
GB1428365A (en) * 1972-03-15 1976-03-17 Rolls Royce Fluid flow machines
IT1066506B (it) * 1973-12-17 1985-03-12 Seeber Willi Ruota a pale per ventilatori e procedimento per produrla
GB1553038A (en) * 1977-04-28 1979-09-19 Snecma Drum for an axial flow compressor rotor and process for its manufacture
FR2448626A1 (fr) * 1979-02-08 1980-09-05 Snecma Perfectionnement aux rotors de machines tournantes
DE2915201C2 (de) * 1979-04-14 1986-02-27 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Laufrad für Axialströmungsmaschinen, insbesondere Verdichter
DE3037388C1 (de) * 1980-10-03 1982-06-16 Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5300 Bonn Bandage zur radialen Spannung der Segmente eines aus Einzelsegmenten aufgebauten Verdichterlaufrades fuer Gasturbinen
DE3101250C2 (de) * 1981-01-16 1983-12-01 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Verdichterrotor für Gasturbinentriebwerke
FR2539824A1 (fr) * 1983-01-26 1984-07-27 Applic Rationnelles Physiq Roue pour compresseur centrifuge et procede pour sa fabrication
DE3446732C2 (de) * 1984-12-21 1986-10-23 Süddeutsche Kühlerfabrik Julius Fr. Behr GmbH & Co KG, 7000 Stuttgart Lüfterrad
FR2605586B1 (fr) * 1986-10-22 1990-11-30 Snecma Anneau porte-pales pour aubage d'helice de grande dimension
DE3711764A1 (de) * 1987-04-07 1988-10-27 Mtu Muenchen Gmbh Axialleitgitter fuer verdichter
JPH02246897A (ja) * 1988-12-29 1990-10-02 General Electric Co <Ge> 航空機推進装置及び方法
DE4321173C2 (de) * 1993-06-25 1996-02-22 Inst Luft Kaeltetech Gem Gmbh Radiallaufrad
FR2712630B1 (fr) * 1993-11-17 1995-12-15 Snecma Rotor de turbomachine segmenté.
DE19525829A1 (de) * 1995-07-15 1997-01-16 Abb Research Ltd Lüfter
FR2755468B1 (fr) * 1996-11-07 1998-12-04 Snecma Etage de rotor de turbomachine renforce par des fibres
US5971706A (en) * 1997-12-03 1999-10-26 General Electric Company Inter-rotor bearing assembly
US6213720B1 (en) 1999-06-11 2001-04-10 Alliedsignal, Inc. High strength composite reinforced turbomachinery disk
FR2943985B1 (fr) * 2009-04-07 2011-05-13 Airbus France Helice pour turbomachine d'aeronef comprenant un anneau de retention d'aubes monte autour du moyeu.
US8182213B2 (en) * 2009-04-22 2012-05-22 Pratt & Whitney Canada Corp. Vane assembly with removable vanes
US8540482B2 (en) 2010-06-07 2013-09-24 United Technologies Corporation Rotor assembly for gas turbine engine
US10710317B2 (en) * 2016-06-16 2020-07-14 Rolls-Royce North American Technologies Inc. Composite rotatable assembly for an axial-flow compressor
FR3057905B1 (fr) * 2016-10-25 2020-06-12 Safran Aircraft Engines Piece tournante de turbomachine
US10294954B2 (en) * 2016-11-09 2019-05-21 Rolls-Royce North American Technologies Inc. Composite blisk
RU181073U1 (ru) * 2018-01-09 2018-07-04 Федеральное государственное бюджетное образовательное учреждение высшего образования "Санкт-Петербургский государственный архитектурно-строительный университет" Ротор барабанного типа осевого компрессора
CN114934815B (zh) * 2022-05-12 2023-10-31 中国航发四川燃气涡轮研究院 一种金属基复合材料箍环式发动机转子叶环结构
WO2025132987A1 (en) * 2023-12-19 2025-06-26 Lilium GmbH Bladed disk for a driven rotor of an engine of an aircraft propulsion unit, propulsion unit for an aircraft and aircraft

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA611006A (en) * 1960-12-20 P. Warnken Elmer Rotating shroud
US1544318A (en) * 1923-09-12 1925-06-30 Westinghouse Electric & Mfg Co Turbine-blade lashing
US2155231A (en) * 1936-06-01 1939-04-18 Gen Electric Fan and method of making same
US2713991A (en) * 1951-05-05 1955-07-26 A V Roe Canada Ltd Rotor blade locking device
US2873088A (en) * 1953-05-21 1959-02-10 Gen Electric Lightweight rotor construction
US2857094A (en) * 1955-07-19 1958-10-21 John R Erwin Integral plastic rotors
US3279967A (en) * 1961-04-07 1966-10-18 Carrier Corp Method of fabricating a rotor shroud
FR1455278A (fr) * 1965-08-05 1966-04-01 Snecma Turboréacteur à double flux
GB1054608A (enrdf_load_stackoverflow) * 1965-09-16
US3403844A (en) * 1967-10-02 1968-10-01 Gen Electric Bladed member and method for making

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1357295A3 (de) * 2002-04-25 2004-03-10 MTU Aero Engines GmbH Verdichter in mehrstufiger Axialbauart
US7011490B2 (en) 2002-04-25 2006-03-14 Mtu Aero Engines Gmbh Compressor in a multi-stage axial form of construction
CN100339557C (zh) * 2002-04-25 2007-09-26 Mtu飞机发动机有限公司 多级轴向结构形式的压缩机
WO2005056983A1 (de) * 2003-12-13 2005-06-23 Mtu Aero Engines Gmbh Faserverstärkter rotor für eine turbomaschine
US8123487B2 (en) 2003-12-13 2012-02-28 Mtu Aero Engines Gmbh Rotor for a turbo engine
US8677622B2 (en) 2006-03-10 2014-03-25 Rolls-Royce Deutschland Ltd & Co Kg Intake cone in a fiber compound material for a gas turbine engine and method for its manufacture
DE102006015838A1 (de) * 2006-04-03 2007-10-04 Rolls-Royce Deutschland Ltd & Co Kg Axialkompressor für ein Gasturbinentriebwerk
US7918644B2 (en) 2006-04-03 2011-04-05 Rolls-Royce Deutschland Ltd & Co Kg Axial-flow compressor for a gas turbine engine

Also Published As

Publication number Publication date
BE713585A (enrdf_load_stackoverflow) 1968-08-16
US3515501A (en) 1970-06-02
GB1170593A (en) 1969-11-12
DE1751156A1 (de) 1970-10-01
FR1575682A (enrdf_load_stackoverflow) 1969-07-25

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