DE2333274A1 - Geblaeserad - Google Patents

Geblaeserad

Info

Publication number
DE2333274A1
DE2333274A1 DE19732333274 DE2333274A DE2333274A1 DE 2333274 A1 DE2333274 A1 DE 2333274A1 DE 19732333274 DE19732333274 DE 19732333274 DE 2333274 A DE2333274 A DE 2333274A DE 2333274 A1 DE2333274 A1 DE 2333274A1
Authority
DE
Germany
Prior art keywords
blades
blade
blade root
rotor
wheel according
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.)
Withdrawn
Application number
DE19732333274
Other languages
German (de)
English (en)
Inventor
Derek Percival Harris
David Roberts Mcmurtry
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce 1971 Ltd
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 1971 Ltd filed Critical Rolls Royce 1971 Ltd
Publication of DE2333274A1 publication Critical patent/DE2333274A1/de
Withdrawn legal-status Critical Current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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3053Fixing blades to rotors; Blade roots ; Blade spacers by means of pins
    • 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
    • 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
    • F01D7/00Rotors with blades adjustable in operation; Control thereof
    • 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
    • F04D29/322Blade mountings
    • F04D29/323Blade mountings adjustable
    • 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
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/36Application in turbines specially adapted for the fan of turbofan engines
    • 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
    • F05D2230/00Manufacture
    • F05D2230/60Assembly methods
    • F05D2230/64Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE19732333274 1972-07-06 1973-06-29 Geblaeserad Withdrawn DE2333274A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3157072A GB1430596A (en) 1972-07-06 1972-07-06 Multi-bladed fans

Publications (1)

Publication Number Publication Date
DE2333274A1 true DE2333274A1 (de) 1974-01-24

Family

ID=10325101

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19732333274 Withdrawn DE2333274A1 (de) 1972-07-06 1973-06-29 Geblaeserad

Country Status (5)

Country Link
US (1) US3860361A (hu)
JP (1) JPS558680B2 (hu)
DE (1) DE2333274A1 (hu)
FR (1) FR2192626A5 (hu)
GB (1) GB1430596A (hu)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3805586A1 (de) * 1987-03-03 1988-09-15 Rolls Royce Plc Fangehaeuse mit einer vorrichtung zur montage und demontage der fangschaufeln
EP0344671A2 (de) * 1988-05-31 1989-12-06 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Vorrichtung zur Befestigung einer verschwenkbaren Propfanschaufel

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3984194A (en) * 1974-04-12 1976-10-05 Aktiebolaget Svenska Flaktfabriken Axial flow fans
US4047840A (en) * 1975-05-29 1977-09-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Impact absorbing blade mounts for variable pitch blades
US4045149A (en) * 1976-02-03 1977-08-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Platform for a swing root turbomachinery blade
US4019832A (en) * 1976-02-27 1977-04-26 General Electric Company Platform for a turbomachinery blade
US4130381A (en) * 1977-06-08 1978-12-19 Levin Efim M Impeller of axial-flow fan
US4227129A (en) * 1979-01-29 1980-10-07 Spin Physics, Inc. Apparatus for detecting the speed of an electric motor
JPS5729617A (en) * 1980-07-30 1982-02-17 Kanai Hiroyuki Traveler for spinning frame
CH659851A5 (de) * 1981-06-05 1987-02-27 Escher Wyss Ag Turbine.
JPS58201228A (ja) * 1982-05-20 1983-11-24 Toshiba Corp カラ−受像管螢光面形成用露光装置
WO1986004385A1 (en) * 1985-01-24 1986-07-31 Sundstrand Corporation Ram air turbine
US5165856A (en) * 1988-06-02 1992-11-24 General Electric Company Fan blade mount
US5102302A (en) * 1988-06-02 1992-04-07 General Electric Company Fan blade mount
US5022825A (en) * 1988-10-07 1991-06-11 United Technologies Corporation Pitch retention member
US5102300A (en) * 1988-10-07 1992-04-07 United Technologies Corporation Pinned airfoil propeller assembly
US5022824A (en) * 1988-10-07 1991-06-11 United Technologies Corporation Pinned airfoil propeller blade
FR2654773B1 (fr) * 1989-11-22 1992-02-14 Snecma Rotor de turbomachine a flux axial.
US5277548A (en) * 1991-12-31 1994-01-11 United Technologies Corporation Non-integral rotor blade platform
US5368444A (en) * 1993-08-30 1994-11-29 General Electric Company Anti-fretting blade retention means
US6109871A (en) * 1997-03-31 2000-08-29 Horton, Inc. Integrated fan assembly with variable pitch blades
US6253716B1 (en) 1999-07-07 2001-07-03 Horton, Inc. Control system for cooling fan assembly having variable pitch blades
ITBA20010002A1 (it) * 2001-01-11 2002-07-11 Paolo Pietricola Fan a passo variabile.
US6682308B1 (en) 2002-08-01 2004-01-27 Kaz, Inc. Fan with adjustable mount
US8662846B2 (en) 2010-09-14 2014-03-04 General Electric Company Bidirectional fan having self-adjusting vane
FR2995948B1 (fr) 2012-09-24 2018-07-27 Snecma Systeme de retention d'aubes et procede d'assemblage
EP2994628A4 (en) * 2013-05-09 2017-01-18 United Technologies Corporation Turbofan engine front section
EP3957847A1 (en) 2013-05-09 2022-02-23 Raytheon Technologies Corporation Turbofan engine front section
US10288083B2 (en) * 2015-11-16 2019-05-14 General Electric Company Pitch range for a variable pitch fan
FR3053725B1 (fr) * 2016-07-07 2020-04-24 Safran Aircraft Engines Turbomachine d'avion avec des aubes mobiles en battement et en pas
GB201811861D0 (en) * 2018-07-20 2018-09-05 Rolls Royce Plc Supersonic aircraft turbofan engine
US11306601B2 (en) * 2018-10-18 2022-04-19 Raytheon Technologies Corporation Pinned airfoil for gas turbine engines

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2344266A (en) * 1941-06-27 1944-03-14 Reissner Hans Aircraft propeller construction
US2436087A (en) * 1944-12-04 1948-02-17 Ernest H Benson Cooling fan for aircraft engines
US2587247A (en) * 1948-05-28 1952-02-26 Estey M Turner Twin blade mounting for fans and propellers
GB750397A (en) * 1951-12-10 1956-06-13 Power Jets Res & Dev Ltd Damped turbine and dynamic compressor blades
US2990156A (en) * 1956-08-17 1961-06-27 Gen Electric Blade damping means
US2944787A (en) * 1957-03-20 1960-07-12 United Aircraft Corp Compressor blade limit stops
NL288322A (hu) * 1962-05-16

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3805586A1 (de) * 1987-03-03 1988-09-15 Rolls Royce Plc Fangehaeuse mit einer vorrichtung zur montage und demontage der fangschaufeln
DE3805586C2 (de) * 1987-03-03 1998-01-15 Rolls Royce Plc Ummantelter Fan für ein Turbofan-Gasturbinentriebwerk
EP0344671A2 (de) * 1988-05-31 1989-12-06 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Vorrichtung zur Befestigung einer verschwenkbaren Propfanschaufel
DE3818466C1 (hu) * 1988-05-31 1989-12-21 Mtu Muenchen Gmbh
EP0344671A3 (en) * 1988-05-31 1990-08-16 Mtu Muenchen Gmbh Attachment device for a variable pitch prop fan blade
US5015150A (en) * 1988-05-31 1991-05-14 Mtu Munchen Gmbh Arrangement for mounting a pivotable propfan blade

Also Published As

Publication number Publication date
FR2192626A5 (hu) 1974-02-08
GB1430596A (en) 1976-03-31
US3860361A (en) 1975-01-14
JPS4944307A (hu) 1974-04-26
JPS558680B2 (hu) 1980-03-05

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Legal Events

Date Code Title Description
OGA New person/name/address of the applicant
OD Request for examination
8130 Withdrawal