FR1056070A - Rotor de compresseur axial - Google Patents

Rotor de compresseur axial

Info

Publication number
FR1056070A
FR1056070A FR1056070DA FR1056070A FR 1056070 A FR1056070 A FR 1056070A FR 1056070D A FR1056070D A FR 1056070DA FR 1056070 A FR1056070 A FR 1056070A
Authority
FR
France
Prior art keywords
compressor rotor
axial compressor
axial
rotor
compressor
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.)
Expired
Application number
Other languages
English (en)
French (fr)
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.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors 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 Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Application granted granted Critical
Publication of FR1056070A publication Critical patent/FR1056070A/fr
Expired legal-status Critical Current

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
    • F04D29/02Selection of particular materials
    • F04D29/023Selection of particular materials especially adapted for elastic fluid pumps
    • 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
    • F01D5/066Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
    • 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
    • F01D5/3069Fixing blades to rotors; Blade roots ; Blade spacers between two discs or rings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • 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
    • 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
    • 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
    • F05D2230/70Disassembly methods

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1056070D 1950-12-08 1951-11-15 Rotor de compresseur axial Expired FR1056070A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB316506X 1950-12-08

Publications (1)

Publication Number Publication Date
FR1056070A true FR1056070A (fr) 1954-02-24

Family

ID=10326335

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1056070D Expired FR1056070A (fr) 1950-12-08 1951-11-15 Rotor de compresseur axial

Country Status (6)

Country Link
US (1) US2738126A (de)
BE (1) BE507205A (de)
CH (1) CH316506A (de)
DE (1) DE967778C (de)
FR (1) FR1056070A (de)
GB (1) GB695221A (de)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2804323A (en) * 1954-08-19 1957-08-27 Rolls Royce Axial-flow compressors and turbines
US2884186A (en) * 1954-04-23 1959-04-28 Stalker Corp Rotor construction for axial flow compressors
DE1062881B (de) * 1956-08-24 1959-08-06 Krantz H Fa Axialventilator mit bei Stillstand im Nabenkranz auf verschiedene Anstellwinkel einstellbaren Laufschaufeln
FR2607866A1 (fr) * 1986-12-03 1988-06-10 Snecma Axes de fixation de rotors de turbomachine, procede de montage et rotors ainsi montes
US5378110A (en) * 1992-09-14 1995-01-03 United Technologies Corporation Composite compressor rotor with removable airfoils
DE19627386A1 (de) * 1995-07-13 1997-01-16 Bmw Rolls Royce Gmbh Verbindungs-Anordnung für zwei Turbinen-Laufradscheiben

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB741550A (en) * 1952-07-10 1955-12-07 Havilland Engine Co Ltd Improvements in or relating to the rotors of multi-stage axial flow compressors or turbines
DE1095453B (de) * 1955-07-18 1960-12-22 Rolls Royce Mehrstufige Axialstroemungsmaschine
DE1067971B (de) * 1955-10-18 1959-10-29
DE1080255B (de) * 1957-01-17 1960-04-21 Andreas Harold Andersen Axialventilator
FR1245518A (fr) * 1957-04-19 1960-11-10 Perfectionnements apportés aux turbines à fluide gazeux chaud
US3345035A (en) * 1965-04-30 1967-10-03 Gen Motors Corp Turbine wheel
US4688992A (en) * 1985-01-25 1987-08-25 General Electric Company Blade platform
EP1319805A1 (de) * 2001-12-17 2003-06-18 Techspace aero Rotor oder Rototelement für Turbokompressoren
EP1319842A1 (de) * 2001-12-17 2003-06-18 Techspace Aero S.A. Rotor oder rotierendes Element für Turboverdichter
US6887043B2 (en) 2003-03-28 2005-05-03 General Electric Company Methods and apparatus for assembling gas turbine engines
FR2869374B1 (fr) * 2004-04-23 2009-01-30 Snecma Moteurs Sa Systeme de fixation de pieces par des goujons a collerettes
FR2933887B1 (fr) * 2008-07-18 2010-09-17 Snecma Procede de reparation ou de reprise d'un disque de turbomachine et disque de turbomachine repare ou repris
FR2935429B1 (fr) * 2008-08-26 2011-11-25 Snecma Aubage fixe de turbomachine a masse reduite et turbomachine comportant au moins un tel aubage fixe
US8162615B2 (en) * 2009-03-17 2012-04-24 United Technologies Corporation Split disk assembly for a gas turbine engine
US10233941B2 (en) * 2013-07-12 2019-03-19 United Technologies Corporation Plastic variable inlet guide vane

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB599809A (en) * 1945-01-15 1948-03-22 Bristol Aeroplane Co Ltd Improvements in axial flow compressors, turbines and the like
US768597A (en) * 1902-08-21 1904-08-30 Gen Electric Turbine-bucket.
US980732A (en) * 1910-07-09 1911-01-03 Gen Electric Bucket structure for turbines.
US1118361A (en) * 1914-06-19 1914-11-24 Gen Electric Wheel for elastic-fluid turbines.
GB394001A (en) * 1931-12-18 1933-06-19 Parsons C A & Co Ltd Improvements in and relating to built-up rotors, suitable for steam turbines
DE729493C (de) * 1941-01-07 1942-12-17 Siemens Ag Aus axial miteinander verschraubten Drehkoerpern zusammengesetzter Laeufer fuer Kreiselmaschinen, insbesondere Dampf- oder Gasturbinen
DE840880C (de) * 1941-09-08 1952-06-09 Daimler Benz Ag Laufrad fuer Axialturbomaschinen, insbesondere fuer Axialverdichter
GB578191A (en) * 1941-11-21 1946-06-19 Frank Bernard Halford Improvements in or relating to turbines
FR895583A (fr) * 1942-05-21 1945-01-29 Roue motrice ou rotor pour turbines à gaz refroidies
GB579425A (en) * 1943-10-06 1946-08-02 Frank Robert Bell Improvements in blade drums for axial-flow compressors and turbines
US2452782A (en) * 1945-01-16 1948-11-02 Power Jets Res & Dev Ltd Construction of rotors for compressors and like machines
GB642287A (en) * 1948-07-01 1950-08-30 English Electric Co Ltd Improvements in and relating to the connection of spigotted components of multi-stage compressor rotors
FR1012335A (fr) * 1949-07-13 1952-07-08 Hispano Suiza Sa Perfectionnements apportés aux engins, notamment aux compresseurs axiaux, à rotor équipé de plusieurs aubages disposés en tandem

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2884186A (en) * 1954-04-23 1959-04-28 Stalker Corp Rotor construction for axial flow compressors
US2804323A (en) * 1954-08-19 1957-08-27 Rolls Royce Axial-flow compressors and turbines
DE1062881B (de) * 1956-08-24 1959-08-06 Krantz H Fa Axialventilator mit bei Stillstand im Nabenkranz auf verschiedene Anstellwinkel einstellbaren Laufschaufeln
FR2607866A1 (fr) * 1986-12-03 1988-06-10 Snecma Axes de fixation de rotors de turbomachine, procede de montage et rotors ainsi montes
EP0272966A1 (de) * 1986-12-03 1988-06-29 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Verbindungselement für die Rotorscheiben einer Turbomaschine
US4844694A (en) * 1986-12-03 1989-07-04 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) Fastening spindle and method of assembly for attaching rotor elements of a gas-turbine engine
US5378110A (en) * 1992-09-14 1995-01-03 United Technologies Corporation Composite compressor rotor with removable airfoils
DE19627386A1 (de) * 1995-07-13 1997-01-16 Bmw Rolls Royce Gmbh Verbindungs-Anordnung für zwei Turbinen-Laufradscheiben

Also Published As

Publication number Publication date
US2738126A (en) 1956-03-13
CH316506A (fr) 1956-10-15
DE967778C (de) 1958-01-16
BE507205A (de)
GB695221A (en) 1953-08-05

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