JPS57105503A - Conical aerofoil section of rotor blade and formation thereof - Google Patents

Conical aerofoil section of rotor blade and formation thereof

Info

Publication number
JPS57105503A
JPS57105503A JP56172670A JP17267081A JPS57105503A JP S57105503 A JPS57105503 A JP S57105503A JP 56172670 A JP56172670 A JP 56172670A JP 17267081 A JP17267081 A JP 17267081A JP S57105503 A JPS57105503 A JP S57105503A
Authority
JP
Japan
Prior art keywords
conical
formation
rotor blade
aerofoil section
aerofoil
Prior art date
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.)
Granted
Application number
JP56172670A
Other languages
English (en)
Other versions
JPH025882B2 (ja
Inventor
Henrii Ruubenshiyutai Jiyosefu
Kenesu Rosu Aran
Aasaa Robidoo Buraian
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of JPS57105503A publication Critical patent/JPS57105503A/ja
Publication of JPH025882B2 publication Critical patent/JPH025882B2/ja
Granted legal-status Critical Current

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
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/301Cross-sectional characteristics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/20Three-dimensional
    • F05D2250/23Three-dimensional prismatic
    • F05D2250/232Three-dimensional prismatic conical
    • 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
    • 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
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/02Formulas of curves

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP56172670A 1980-10-27 1981-10-27 Conical aerofoil section of rotor blade and formation thereof Granted JPS57105503A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/200,800 US4431376A (en) 1980-10-27 1980-10-27 Airfoil shape for arrays of airfoils

Publications (2)

Publication Number Publication Date
JPS57105503A true JPS57105503A (en) 1982-07-01
JPH025882B2 JPH025882B2 (ja) 1990-02-06

Family

ID=22743244

Family Applications (1)

Application Number Title Priority Date Filing Date
JP56172670A Granted JPS57105503A (en) 1980-10-27 1981-10-27 Conical aerofoil section of rotor blade and formation thereof

Country Status (10)

Country Link
US (1) US4431376A (ja)
JP (1) JPS57105503A (ja)
AU (1) AU547396B2 (ja)
BE (1) BE890884A (ja)
CA (1) CA1166968A (ja)
DE (1) DE3141948A1 (ja)
FR (1) FR2492885B1 (ja)
GB (1) GB2085976B (ja)
IL (1) IL63947A (ja)
IT (1) IT1139555B (ja)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH062501A (ja) * 1992-06-16 1994-01-11 Hitachi Ltd 軸流タービンの動翼

Families Citing this family (66)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3201436C1 (de) * 1982-01-19 1983-04-21 Kraftwerk Union AG, 4330 Mülheim Turbomaschinenschaufel
GB2128687B (en) * 1982-10-13 1986-10-29 Rolls Royce Rotor or stator blade for an axial flow compressor
EP0138800B1 (de) * 1983-08-17 1990-05-23 Oscar Asboth Luftschraube
US4726737A (en) * 1986-10-28 1988-02-23 United Technologies Corporation Reduced loss swept supersonic fan blade
US5088892A (en) * 1990-02-07 1992-02-18 United Technologies Corporation Bowed airfoil for the compression section of a rotary machine
US5197854A (en) * 1991-09-05 1993-03-30 Industrial Design Laboratories, Inc. Axial flow fan
US5443365A (en) * 1993-12-02 1995-08-22 General Electric Company Fan blade for blade-out protection
RU2191930C2 (ru) * 1997-06-24 2002-10-27 Сименс Акциенгезелльшафт Компрессорная лопатка (варианты) и ее применение
US6129528A (en) * 1998-07-20 2000-10-10 Nmb Usa Inc. Axial flow fan having a compact circuit board and impeller blade arrangement
US6856941B2 (en) 1998-07-20 2005-02-15 Minebea Co., Ltd. Impeller blade for axial flow fan having counter-rotating impellers
US6565334B1 (en) 1998-07-20 2003-05-20 Phillip James Bradbury Axial flow fan having counter-rotating dual impeller blade arrangement
JP3785013B2 (ja) * 2000-01-12 2006-06-14 三菱重工業株式会社 タービン動翼
US6457941B1 (en) 2001-03-13 2002-10-01 The United States Of America As Represented By The Secretary Of The Navy Fan rotor with construction and safety performance optimization
US6386830B1 (en) 2001-03-13 2002-05-14 The United States Of America As Represented By The Secretary Of The Navy Quiet and efficient high-pressure fan assembly
US6457938B1 (en) * 2001-03-30 2002-10-01 General Electric Company Wide angle guide vane
GB2384276A (en) * 2002-01-18 2003-07-23 Alstom Gas turbine low pressure stage
US6899525B2 (en) * 2002-07-22 2005-05-31 Arthur Vanmoor Blade and wing configuration
US6769879B1 (en) * 2003-07-11 2004-08-03 General Electric Company Airfoil shape for a turbine bucket
DE102005042115A1 (de) * 2005-09-05 2007-03-08 Rolls-Royce Deutschland Ltd & Co Kg Schaufel einer Strömungsarbeitsmaschine mit blockweise definierter Profilskelettlinie
DE102006055869A1 (de) 2006-11-23 2008-05-29 Rolls-Royce Deutschland Ltd & Co Kg Schaufelblattdesign für die Lauf- und Leitschaufeln einer Turbomaschine
DE102008011645A1 (de) * 2008-02-28 2009-09-03 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Rotoren mit niedrigen Rotoraustrittswinkeln
DE102008031781B4 (de) * 2008-07-04 2020-06-10 Man Energy Solutions Se Schaufelgitter für eine Strömungsmaschine und Strömungsmaschine mit einem solchen Schaufelgitter
WO2010136357A2 (en) * 2009-05-25 2010-12-02 Chongqing University Airfoils and method for designing airfoils
EP2275671A1 (en) * 2009-06-04 2011-01-19 Technical University of Denmark System and method for designing airfoils
DE102009033593A1 (de) * 2009-07-17 2011-01-20 Rolls-Royce Deutschland Ltd & Co Kg Triebwerkschaufel mit überhöhter Vorderkantenbelastung
US9309769B2 (en) * 2010-12-28 2016-04-12 Rolls-Royce Corporation Gas turbine engine airfoil shaped component
JP6030853B2 (ja) * 2011-06-29 2016-11-24 三菱日立パワーシステムズ株式会社 タービン動翼及び軸流タービン
US9340277B2 (en) * 2012-02-29 2016-05-17 General Electric Company Airfoils for use in rotary machines
JP5999348B2 (ja) 2012-10-31 2016-09-28 株式会社Ihi タービン翼
EP2811115A1 (en) * 2013-06-05 2014-12-10 Alstom Technology Ltd Airfoil for gas turbine, blade and vane
US9163517B2 (en) 2014-02-19 2015-10-20 United Technologies Corporation Gas turbine engine airfoil
EP3108123B1 (en) 2014-02-19 2023-10-04 Raytheon Technologies Corporation Turbofan engine with geared architecture and lpc airfoils
WO2015175044A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
EP3108119B1 (en) 2014-02-19 2023-10-04 RTX Corporation Turbofan engine with geared architecture and lpc blade airfoils
US9140127B2 (en) 2014-02-19 2015-09-22 United Technologies Corporation Gas turbine engine airfoil
WO2015126774A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
US10385866B2 (en) 2014-02-19 2019-08-20 United Technologies Corporation Gas turbine engine airfoil
EP3108120B1 (en) 2014-02-19 2021-03-31 Raytheon Technologies Corporation Gas turbine engine having a geared architecture and a specific fixed airfoil structure
US10557477B2 (en) 2014-02-19 2020-02-11 United Technologies Corporation Gas turbine engine airfoil
US10422226B2 (en) 2014-02-19 2019-09-24 United Technologies Corporation Gas turbine engine airfoil
US10465702B2 (en) 2014-02-19 2019-11-05 United Technologies Corporation Gas turbine engine airfoil
US10584715B2 (en) 2014-02-19 2020-03-10 United Technologies Corporation Gas turbine engine airfoil
WO2015126454A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
EP3108118B1 (en) 2014-02-19 2019-09-18 United Technologies Corporation Gas turbine engine airfoil
EP3108100B1 (en) 2014-02-19 2021-04-14 Raytheon Technologies Corporation Gas turbine engine fan blade
EP3575551B1 (en) 2014-02-19 2021-10-27 Raytheon Technologies Corporation Gas turbine engine airfoil
EP3108115B8 (en) 2014-02-19 2023-11-08 RTX Corporation Turbofan engine with geared architecture and lpc blades
EP3108121B1 (en) 2014-02-19 2023-09-06 Raytheon Technologies Corporation Turbofan engine with geared architecture and lpc airfoils
US9567858B2 (en) 2014-02-19 2017-02-14 United Technologies Corporation Gas turbine engine airfoil
WO2015126824A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
WO2015126449A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
WO2015126451A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
US10508549B2 (en) 2014-06-06 2019-12-17 United Technologies Corporation Gas turbine engine airfoil with large thickness properties
SG10201505408WA (en) 2014-07-24 2016-02-26 United Technologies Corp Gas turbine engine blade with variable density and wide chord tip
JP6468414B2 (ja) * 2014-08-12 2019-02-13 株式会社Ihi 圧縮機静翼、軸流圧縮機、及びガスタービン
US9845684B2 (en) * 2014-11-25 2017-12-19 Pratt & Whitney Canada Corp. Airfoil with stepped spanwise thickness distribution
DE102016115868A1 (de) * 2016-08-26 2018-03-01 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit hohem Ausnutzungsgrad
EP3375980B1 (de) * 2017-03-13 2019-12-11 MTU Aero Engines GmbH Dichtungsträger für eine strömungsmaschine
US10801325B2 (en) 2017-03-27 2020-10-13 Raytheon Technologies Corporation Turbine blade with tip vortex control and tip shelf
US10280756B2 (en) 2017-10-02 2019-05-07 United Technologies Corporation Gas turbine engine airfoil
US10563512B2 (en) 2017-10-25 2020-02-18 United Technologies Corporation Gas turbine engine airfoil
US11473434B2 (en) 2019-10-16 2022-10-18 Raytheon Technologies Corporation Gas turbine engine airfoil
DE102021123281A1 (de) * 2021-09-08 2023-03-09 MTU Aero Engines AG Schaufelblatt für einen Verdichter einer Strömungsmaschine
EP4332346A3 (en) * 2022-08-09 2024-06-19 RTX Corporation Fan blade or vane with improved bird impact capability
US11952912B2 (en) * 2022-08-24 2024-04-09 General Electric Company Turbine engine airfoil
US11873730B1 (en) * 2022-11-28 2024-01-16 Rtx Corporation Gas turbine engine airfoil with extended laminar flow

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH478994A (de) * 1963-05-21 1969-09-30 Jerie Jan Schaufelanordnung an Axialverdichter, Gebläse oder Ventilator
SU266475A1 (ru) * 1966-07-29 1975-10-15 Б. М. Аронов Лопатка реактивной газовой турбины
US3952971A (en) * 1971-11-09 1976-04-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Airfoil shape for flight at subsonic speeds
DE2225599A1 (de) * 1972-05-26 1973-12-06 Bosch Hausgeraete Gmbh Fluegelrad fuer einen ventilator
US4012172A (en) * 1975-09-10 1977-03-15 Avco Corporation Low noise blades for axial flow compressors

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH062501A (ja) * 1992-06-16 1994-01-11 Hitachi Ltd 軸流タービンの動翼

Also Published As

Publication number Publication date
FR2492885B1 (fr) 1986-01-17
GB2085976B (en) 1984-06-27
DE3141948C2 (ja) 1990-11-15
BE890884A (fr) 1982-02-15
IT8124706A0 (it) 1981-10-27
IT1139555B (it) 1986-09-24
IL63947A (en) 1984-08-31
JPH025882B2 (ja) 1990-02-06
US4431376A (en) 1984-02-14
AU7673581A (en) 1982-04-29
AU547396B2 (en) 1985-10-17
CA1166968A (en) 1984-05-08
FR2492885A1 (fr) 1982-04-30
GB2085976A (en) 1982-05-06
DE3141948A1 (de) 1982-04-15

Similar Documents

Publication Publication Date Title
JPS57105503A (en) Conical aerofoil section of rotor blade and formation thereof
GB2026416B (en) Multi-blade propellers and method of making same
DE3473569D1 (en) Centrifugal separator and method of operating the same
GB2067493B (en) Helicopter rotor blade tip
JPS569672A (en) Windmill blade structure and making method thereof
GB8511397D0 (en) Determining initiate cleaning of turbine blades
DE3174020D1 (en) A rotor assembly and methods of securing a rotor blade therewithin and removing a rotor blade therefrom
IL77235A (en) Radial turbine rotor and method of producing the same
JPS55156797A (en) Rotor blade made up of individual parts
DE3573291D1 (en) Turbine rotor units and method of producing the same
AU560133B2 (en) Rotor blade airfoil section
JPS5784298A (en) Section of blade for rotor for aircraft
DE3370831D1 (en) Cutting insert and method of making the same
GB2106995B (en) Turbine blades
GB2159585B (en) Turbine blade
JPS5762903A (en) Turbine blade
IL56979A (en) Helicopter rotor blades and methods of forming the same
DE3175016D1 (en) Helicopter rotor blade
JPS55114113A (en) Wire separator and method of manufacturing cutting blade therefor
EP0117721A3 (en) Ceramic radial turbine rotor and method of producing the same
GB8136625D0 (en) Method for the manufacture of monocrystalline aerodynamic blades
JPS5728802A (en) Rotor blade
GB2062102B (en) Centrifugal pump and turbine
GB8517474D0 (en) Variable-pitch bladed rotors
JPS573046A (en) Analysing rotor and method of use