BR0104648A - Método e aparelho para redução de tensão em circunferência em aro de estrutura de rotor - Google Patents

Método e aparelho para redução de tensão em circunferência em aro de estrutura de rotor

Info

Publication number
BR0104648A
BR0104648A BR0104648-9A BR0104648A BR0104648A BR 0104648 A BR0104648 A BR 0104648A BR 0104648 A BR0104648 A BR 0104648A BR 0104648 A BR0104648 A BR 0104648A
Authority
BR
Brazil
Prior art keywords
rotor
rim
blades
circumference
rotor blades
Prior art date
Application number
BR0104648-9A
Other languages
English (en)
Other versions
BR0104648B1 (pt
Inventor
Mark Joseph Mielke
John Jared Decker
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BR0104648A publication Critical patent/BR0104648A/pt
Publication of BR0104648B1 publication Critical patent/BR0104648B1/pt

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • 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
    • F01D5/02Blade-carrying members, e.g. rotors
    • 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
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/06Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • 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
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • F01D5/142Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
    • F01D5/143Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S415/00Rotary kinetic fluid motors or pumps
    • Y10S415/914Device to control boundary layer
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making
    • Y10T29/49321Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member

Abstract

Patente de Invenção: "MéTODO E APARELHO PARA REDUçãO DE TENSãO EM CIRCUNFERêNCIA EM ARO DE ESTRUTURA DE ROTOR". Estrutura de rotor (10) para um motor de turbina a gás (12) opera com tensão circunferente reduzida. A estrutura de rotor inclui um rotor (14), incluindo uma pluralidade de lâminas de rotor (26), que se estendem de forma radial para o exterior, a partir de um aro anelar (20). Um filete de raiz ou base (80) se estende de forma circunferente em torno de cada lâmina, entre as lâminas e o aro. O aro inclui uma superfície externa (28), incluindo uma pluralidade de indentações cóncavos (90) que se estendem entre lâminas de rotor adjacentes e formando um raio composto. Cada indentação se estende a partir de uma borda de condução (40) das lâminas de rotor, em direção à borda de rastreamento (42) das lâminas de rotor.
BRPI0104648-9A 2000-10-20 2001-10-18 método para fabricação de uma estrutura de rotor, estrutura de rotor e motor de turbina a gás. BR0104648B1 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/693,570 US6471474B1 (en) 2000-10-20 2000-10-20 Method and apparatus for reducing rotor assembly circumferential rim stress

Publications (2)

Publication Number Publication Date
BR0104648A true BR0104648A (pt) 2002-05-28
BR0104648B1 BR0104648B1 (pt) 2010-06-15

Family

ID=24785200

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0104648-9A BR0104648B1 (pt) 2000-10-20 2001-10-18 método para fabricação de uma estrutura de rotor, estrutura de rotor e motor de turbina a gás.

Country Status (5)

Country Link
US (1) US6471474B1 (pt)
EP (1) EP1199439A3 (pt)
JP (1) JP3948926B2 (pt)
BR (1) BR0104648B1 (pt)
CA (1) CA2358673C (pt)

Families Citing this family (92)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6669445B2 (en) * 2002-03-07 2003-12-30 United Technologies Corporation Endwall shape for use in turbomachinery
JP3876195B2 (ja) * 2002-07-05 2007-01-31 本田技研工業株式会社 遠心圧縮機のインペラ
US6837685B2 (en) * 2002-12-13 2005-01-04 General Electric Company Methods and apparatus for repairing a rotor assembly of a turbine
US7269955B2 (en) * 2004-08-25 2007-09-18 General Electric Company Methods and apparatus for maintaining rotor assembly tip clearances
CA2569026C (en) * 2004-09-24 2009-10-20 Ishikawajima-Harima Heavy Industries Co., Ltd. Wall configuration of axial-flow machine, and gas turbine engine
WO2006060010A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Compressor inlet guide vane for tip turbine engine and corresponding control method
US7921636B2 (en) * 2004-12-01 2011-04-12 United Technologies Corporation Tip turbine engine and corresponding operating method
WO2006060011A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
WO2006060014A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Starter generator system for a tip turbine engine
WO2006110123A2 (en) * 2004-12-01 2006-10-19 United Technologies Corporation Vectoring transition duct for turbine engine
US8096753B2 (en) 2004-12-01 2012-01-17 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
US8468795B2 (en) * 2004-12-01 2013-06-25 United Technologies Corporation Diffuser aspiration for a tip turbine engine
US9003759B2 (en) 2004-12-01 2015-04-14 United Technologies Corporation Particle separator for tip turbine engine
WO2006059985A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Axial compressor for tip turbine engine
WO2006110122A2 (en) 2004-12-01 2006-10-19 United Technologies Corporation Inflatable bleed valve for a turbine engine and a method of operating therefore
US7882694B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Variable fan inlet guide vane assembly for gas turbine engine
US8061968B2 (en) 2004-12-01 2011-11-22 United Technologies Corporation Counter-rotating compressor case and assembly method for tip turbine engine
EP1828547B1 (en) 2004-12-01 2011-11-30 United Technologies Corporation Turbofan comprising a plurality of individually controlled inlet guide vanes and corresponding controlling method
US7874802B2 (en) 2004-12-01 2011-01-25 United Technologies Corporation Tip turbine engine comprising turbine blade clusters and method of assembly
US7921635B2 (en) * 2004-12-01 2011-04-12 United Technologies Corporation Peripheral combustor for tip turbine engine
US8152469B2 (en) 2004-12-01 2012-04-10 United Technologies Corporation Annular turbine ring rotor
WO2006059971A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine integral fan, combustor, and turbine case
WO2006059972A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
EP1825113B1 (en) 2004-12-01 2012-10-24 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
DE602004023769D1 (de) * 2004-12-01 2009-12-03 United Technologies Corp Gestapelte ringförmige bauteile für turbinenmotoren
US7882695B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Turbine blow down starter for turbine engine
WO2006059973A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine with a heat exchanger
WO2006060006A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine non-metallic tailcone
WO2006059979A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine integral case, vane, mount, and mixer
WO2006059989A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine support structure
EP1834076B1 (en) 2004-12-01 2011-04-06 United Technologies Corporation Turbine blade cluster for a fan-turbine rotor assembly and method of mounting such a cluster
US8807936B2 (en) 2004-12-01 2014-08-19 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
EP1825112B1 (en) 2004-12-01 2013-10-23 United Technologies Corporation Cantilevered tip turbine engine
WO2006060003A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
DE602004031986D1 (de) 2004-12-01 2011-05-05 United Technologies Corp Gebläse-turbinen-rotoranordnung für einen spitzenturbinenmotor
WO2006059970A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
US8024931B2 (en) 2004-12-01 2011-09-27 United Technologies Corporation Combustor for turbine engine
DE602004028528D1 (de) * 2004-12-01 2010-09-16 United Technologies Corp Tip-Turbinentriebwerk mit mehreren Gebläse- und Turbinenstufen
US7883315B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
US7980054B2 (en) * 2004-12-01 2011-07-19 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
WO2006059994A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Seal assembly for a fan-turbine rotor of a tip turbine engine
US7959532B2 (en) 2004-12-01 2011-06-14 United Technologies Corporation Hydraulic seal for a gearbox of a tip turbine engine
EP1825170B1 (en) 2004-12-01 2009-03-18 United Technologies Corporation Gearbox lubrication supply system for a tip turbine engine
US7959406B2 (en) 2004-12-01 2011-06-14 United Technologies Corporation Close coupled gearbox assembly for a tip turbine engine
WO2006062497A1 (en) 2004-12-04 2006-06-15 United Technologies Corporation Tip turbine engine mount
US7476086B2 (en) * 2005-04-07 2009-01-13 General Electric Company Tip cambered swept blade
US7374403B2 (en) * 2005-04-07 2008-05-20 General Electric Company Low solidity turbofan
JP4838733B2 (ja) * 2007-01-12 2011-12-14 三菱重工業株式会社 ガスタービンの翼構造
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
US10544677B2 (en) * 2017-09-01 2020-01-28 United Technologies Corporation Turbine disk
FR2928174B1 (fr) * 2008-02-28 2011-05-06 Snecma Aube avec plateforme non axisymetrique : creux et bosse sur extrados.
FR2928172B1 (fr) * 2008-02-28 2015-07-17 Snecma Aube avec plateforme non axisymetrique lineaire.
US8100655B2 (en) * 2008-03-28 2012-01-24 Pratt & Whitney Canada Corp. Method of machining airfoil root fillets
US8616849B2 (en) * 2009-02-18 2013-12-31 Pratt & Whitney Canada Corp. Fan blade platform
US8568102B2 (en) * 2009-02-18 2013-10-29 Pratt & Whitney Canada Corp. Fan blade anti-fretting insert
FR2946083B1 (fr) * 2009-05-28 2011-06-17 Snecma Turbine basse-pression
US8403645B2 (en) 2009-09-16 2013-03-26 United Technologies Corporation Turbofan flow path trenches
FR2950942B1 (fr) * 2009-10-02 2013-08-02 Snecma Rotor d'un compresseur de turbomachine a paroi d'extremite interne optimisee
US8636195B2 (en) * 2010-02-19 2014-01-28 General Electric Company Welding process and component formed thereby
US8356975B2 (en) * 2010-03-23 2013-01-22 United Technologies Corporation Gas turbine engine with non-axisymmetric surface contoured vane platform
US9976433B2 (en) 2010-04-02 2018-05-22 United Technologies Corporation Gas turbine engine with non-axisymmetric surface contoured rotor blade platform
DE102011006273A1 (de) 2011-03-28 2012-10-04 Rolls-Royce Deutschland Ltd & Co Kg Rotor einer Axialverdichterstufe einer Turbomaschine
DE102011006275A1 (de) 2011-03-28 2012-10-04 Rolls-Royce Deutschland Ltd & Co Kg Stator einer Axialverdichterstufe einer Turbomaschine
DE102011007767A1 (de) 2011-04-20 2012-10-25 Rolls-Royce Deutschland Ltd & Co Kg Strömungsmaschine
US8788083B2 (en) * 2011-07-22 2014-07-22 Pratt & Whitney Canada Corp. Compensation for process variables in a numerically-controlled machining operation
US8904636B2 (en) 2011-07-22 2014-12-09 Pratt & Whitney Canada Corp. Method of fabricating integrally bladed rotor using surface positioning in relation to surface priority
US8631577B2 (en) 2011-07-22 2014-01-21 Pratt & Whitney Canada Corp. Method of fabricating integrally bladed rotor and stator vane assembly
US8844132B2 (en) 2011-07-22 2014-09-30 Pratt & Whitney Canada Corp. Method of machining using an automatic tool path generator adapted to individual blade surfaces on an integrally bladed rotor
US10077663B2 (en) * 2011-09-29 2018-09-18 United Technologies Corporation Gas turbine engine rotor stack assembly
US9909425B2 (en) 2011-10-31 2018-03-06 Pratt & Whitney Canada Corporation Blade for a gas turbine engine
US9267386B2 (en) 2012-06-29 2016-02-23 United Technologies Corporation Fairing assembly
DE102012106810B4 (de) * 2012-07-26 2020-08-27 Ihi Charging Systems International Gmbh Laufrad für eine Fluidenergiemaschine
US10344601B2 (en) 2012-08-17 2019-07-09 United Technologies Corporation Contoured flowpath surface
WO2014163673A2 (en) 2013-03-11 2014-10-09 Bronwyn Power Gas turbine engine flow path geometry
US10196897B2 (en) 2013-03-15 2019-02-05 United Technologies Corporation Fan exit guide vane platform contouring
US10465519B2 (en) * 2013-10-17 2019-11-05 Pratt & Whitney Canada Corp. Fastening system for rotor hubs
US10352180B2 (en) 2013-10-23 2019-07-16 General Electric Company Gas turbine nozzle trailing edge fillet
WO2015130381A2 (en) * 2013-12-20 2015-09-03 United Technologies Corporation A gas turbine engine integrally bladed rotor with asymmetrical trench fillets
EP3012411A1 (en) * 2014-10-23 2016-04-27 United Technologies Corporation Integrally bladed rotor having axial arm and pocket
JP2016084751A (ja) * 2014-10-27 2016-05-19 三菱重工業株式会社 インペラ、遠心式流体機械、及び流体装置
US20160208626A1 (en) * 2015-01-19 2016-07-21 United Technologies Corporation Integrally bladed rotor with pressure side thickness on blade trailing edge
DE102015214854A1 (de) * 2015-08-04 2017-02-09 Bosch Mahle Turbo Systems Gmbh & Co. Kg Verdichterrad für einen Abgasturbolader
US10458426B2 (en) 2016-09-15 2019-10-29 General Electric Company Aircraft fan with low part-span solidity
ES2750815T3 (es) * 2017-07-14 2020-03-27 MTU Aero Engines AG Rejilla de alas perfiladas para turbomáquinas
US10472968B2 (en) 2017-09-01 2019-11-12 United Technologies Corporation Turbine disk
US10641110B2 (en) 2017-09-01 2020-05-05 United Technologies Corporation Turbine disk
US10724374B2 (en) 2017-09-01 2020-07-28 Raytheon Technologies Corporation Turbine disk
US10550702B2 (en) 2017-09-01 2020-02-04 United Technologies Corporation Turbine disk
KR20190046118A (ko) * 2017-10-25 2019-05-07 두산중공업 주식회사 터빈 블레이드
EP3636880B1 (de) * 2018-10-11 2023-06-07 BorgWarner, Inc. Turbinenrad
DE112019007771T5 (de) * 2019-12-09 2022-09-01 Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. Laufrad des zentrifugalverdichters, zentrifugalverdichter und turbolader
US11614028B2 (en) 2020-12-21 2023-03-28 Brp-Rotax Gmbh & Co. Kg Turbocharger and turbine wheel for a turbine of a turbocharger

Family Cites Families (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2735612A (en) 1956-02-21 hausmann
US1793468A (en) 1929-05-28 1931-02-24 Westinghouse Electric & Mfg Co Turbine blade
CH229266A (de) * 1942-03-26 1943-10-15 Sulzer Ag Turbomaschine, deren Schaufelblattflächen am Schaufelfuss mit einer Abrundung in die Grundfläche übergehen.
US2429324A (en) 1943-12-30 1947-10-21 Meisser Christian Rotor for centrifugal compressors
US2415380A (en) 1944-11-15 1947-02-04 Weber Max Propeller blade
US2790620A (en) 1952-07-09 1957-04-30 Gen Electric Multiple finger dovetail attachment for turbine bucket
US2918254A (en) 1954-05-10 1959-12-22 Hausammann Werner Turborunner
US3095180A (en) 1959-03-05 1963-06-25 Stalker Corp Blades for compressors, turbines and the like
FR1442526A (fr) 1965-05-07 1966-06-17 Rateau Soc Perfectionnements aux canaux courbes parcourus par un gaz ou une vapeur
GB1119392A (en) 1966-06-03 1968-07-10 Rover Co Ltd Axial flow rotor for a turbine or the like
US3481531A (en) 1968-03-07 1969-12-02 United Aircraft Canada Impeller boundary layer control device
US3584969A (en) 1968-05-25 1971-06-15 Aisin Seiki Flexible blade fan
GB1302036A (pt) 1969-06-26 1973-01-04
US3661475A (en) 1970-04-30 1972-05-09 Gen Electric Turbomachinery rotors
US3890062A (en) 1972-06-28 1975-06-17 Us Energy Blade transition for axial-flow compressors and the like
US3927952A (en) 1972-11-20 1975-12-23 Garrett Corp Cooled turbine components and method of making the same
US3951611A (en) 1974-11-14 1976-04-20 Morrill Wayne J Blank for fan blade
NO146029C (no) 1976-08-11 1982-07-14 Kongsberg Vapenfab As Impellerelement i et radialgassturbinhjul
US4135857A (en) 1977-06-09 1979-01-23 United Technologies Corporation Reduced drag airfoil platforms
SU756083A1 (ru) 1978-07-18 1980-08-15 Vladislav D Lubenets Рабочее колесо вихревой машины 1
US4335997A (en) 1980-01-16 1982-06-22 General Motors Corporation Stress resistant hybrid radial turbine wheel
DE3023466C2 (de) 1980-06-24 1982-11-25 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur Verminderung von Sekundärströmungsverlusten in einem beschaufelten Strömungskanal
US4671739A (en) 1980-07-11 1987-06-09 Robert W. Read One piece molded fan
DE3202855C1 (de) * 1982-01-29 1983-03-31 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur Verminderung von Sekundaerstroemungsverlusten in einem beschaufelten Stroemungskanal
US4587700A (en) 1984-06-08 1986-05-13 The Garrett Corporation Method for manufacturing a dual alloy cooled turbine wheel
US4659288A (en) 1984-12-10 1987-04-21 The Garrett Corporation Dual alloy radial turbine rotor with hub material exposed in saddle regions of blade ring
DE3514122A1 (de) 1985-04-19 1986-10-23 MAN Gutehoffnungshütte GmbH, 4200 Oberhausen Verfahren zur herstellung einer leitschaufel fuer ein turbinen- oder verdichter-leitrad und nach dem verfahren hergestellte leitschaufel
DE3710321C1 (de) 1987-03-28 1988-06-01 Mtu Muenchen Gmbh Geblaeseschaufel,insbesondere fuer Prop-Fan-Triebwerke
DE3726522A1 (de) 1987-08-10 1989-02-23 Standard Elektrik Lorenz Ag Aus einer metallblechscheibe hergestelltes luefterrad und verfahren zu seiner herstellung
US4866985A (en) 1987-09-10 1989-09-19 United States Of America As Represented By The Secretary Of Interior Bucket wheel assembly for a flow measuring device
US5018271A (en) 1988-09-09 1991-05-28 Airfoil Textron Inc. Method of making a composite blade with divergent root
US5061154A (en) 1989-12-11 1991-10-29 Allied-Signal Inc. Radial turbine rotor with improved saddle life
GB2251897B (en) 1991-01-15 1994-11-30 Rolls Royce Plc A rotor
US5215439A (en) 1991-01-15 1993-06-01 Northern Research & Engineering Corp. Arbitrary hub for centrifugal impellers
US5397215A (en) * 1993-06-14 1995-03-14 United Technologies Corporation Flow directing assembly for the compression section of a rotary machine
GB2281356B (en) 1993-08-20 1997-01-29 Rolls Royce Plc Gas turbine engine turbine
US5554004A (en) 1995-07-27 1996-09-10 Ametek, Inc. Fan impeller assembly
FR2738303B1 (fr) 1995-08-30 1997-11-28 Europ Propulsion Turbine en materiau composite thermostructural, en particulier a petit diametre, et procede pour sa fabrication
US5628621A (en) * 1996-07-26 1997-05-13 General Electric Company Reinforced compressor rotor coupling
US5735673A (en) 1996-12-04 1998-04-07 United Technologies Corporation Turbine engine rotor blade pair
DE19650656C1 (de) * 1996-12-06 1998-06-10 Mtu Muenchen Gmbh Turbomaschine mit transsonischer Verdichterstufe
KR20010005910A (ko) * 1997-04-01 2001-01-15 칼 하인쯔 호르닝어 유동 채널 또는 터빈 블레이드의 벽 표면 구조
DE19941134C1 (de) * 1999-08-30 2000-12-28 Mtu Muenchen Gmbh Schaufelkranz für eine Gasturbine
US6511294B1 (en) * 1999-09-23 2003-01-28 General Electric Company Reduced-stress compressor blisk flowpath

Also Published As

Publication number Publication date
CA2358673C (en) 2008-06-17
BR0104648B1 (pt) 2010-06-15
EP1199439A3 (en) 2003-06-18
JP2002161702A (ja) 2002-06-07
JP3948926B2 (ja) 2007-07-25
EP1199439A2 (en) 2002-04-24
CA2358673A1 (en) 2002-04-20
US6471474B1 (en) 2002-10-29

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