FR2150094A5 - - Google Patents

Info

Publication number
FR2150094A5
FR2150094A5 FR7229137A FR7229137A FR2150094A5 FR 2150094 A5 FR2150094 A5 FR 2150094A5 FR 7229137 A FR7229137 A FR 7229137A FR 7229137 A FR7229137 A FR 7229137A FR 2150094 A5 FR2150094 A5 FR 2150094A5
Authority
FR
France
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
FR7229137A
Other languages
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Application granted granted Critical
Publication of FR2150094A5 publication Critical patent/FR2150094A5/fr
Expired 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
    • F01D5/02Blade-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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR7229137A 1971-08-14 1972-08-11 Expired FR2150094A5 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2140816A DE2140816A1 (en) 1971-08-14 1971-08-14 ROTOR FOR FLOW MACHINERY

Publications (1)

Publication Number Publication Date
FR2150094A5 true FR2150094A5 (en) 1973-03-30

Family

ID=5816766

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7229137A Expired FR2150094A5 (en) 1971-08-14 1972-08-11

Country Status (4)

Country Link
US (1) US3894324A (en)
DE (1) DE2140816A1 (en)
FR (1) FR2150094A5 (en)
GB (1) GB1395957A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2456835A1 (en) * 1979-05-17 1980-12-12 United Technologies Corp ROTOR ASSEMBLY HAVING MULTI-STAGE DISC
FR2958322A1 (en) * 2010-04-01 2011-10-07 Snecma GAS TURBINE ENGINE ROTOR COMPRISING A ROTOR DRUM AND ROTOR CROWN
WO2012017168A1 (en) * 2010-08-06 2012-02-09 Snecma Process for manufacturing a turbomachine drum

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3986793A (en) * 1974-10-29 1976-10-19 Westinghouse Electric Corporation Turbine rotating blade
US4050134A (en) * 1974-10-29 1977-09-27 Westinghouse Electric Corporation Method for removing rotatable blades without removing the casting of a turbine
DE2620762C2 (en) * 1976-05-11 1977-11-17 Motoren- und Turbinen-Union München GmbH, 8000 München Gap seal for turbo machines, in particular gas turbine jet engines
FR2404134A1 (en) * 1977-09-23 1979-04-20 Snecma ROTOR FOR TURBOMACHINES
US4483054A (en) * 1982-11-12 1984-11-20 United Technologies Corporation Method for making a drum rotor
US4645424A (en) * 1984-07-23 1987-02-24 United Technologies Corporation Rotating seal for gas turbine engine
US4743165A (en) * 1986-10-22 1988-05-10 United Technologies Corporation Drum rotors for gas turbine engines
US4767272A (en) * 1987-10-14 1988-08-30 United Technologies Corporation Method for reducing blade tip variation of a bladed rotor
GB2293628B (en) * 1994-09-27 1998-04-01 Europ Gas Turbines Ltd Turbines
US5660526A (en) * 1995-06-05 1997-08-26 Allison Engine Company, Inc. Gas turbine rotor with remote support rings
US6250883B1 (en) 1999-04-13 2001-06-26 Alliedsignal Inc. Integral ceramic blisk assembly
US6908285B2 (en) * 2003-04-08 2005-06-21 General Electric Company Methods and apparatus for assembling rotatable machines
DE102004007327A1 (en) * 2004-02-14 2005-09-15 Alstom Technology Ltd rotor
US7287958B2 (en) * 2005-01-10 2007-10-30 General Electric Company Methods and apparatus for assembling rotatable machines
US8944762B2 (en) * 2011-10-28 2015-02-03 United Technologies Corporation Spoked spacer for a gas turbine engine
US9938831B2 (en) * 2011-10-28 2018-04-10 United Technologies Corporation Spoked rotor for a gas turbine engine
US8784062B2 (en) * 2011-10-28 2014-07-22 United Technologies Corporation Asymmetrically slotted rotor for a gas turbine engine
US9664058B2 (en) * 2014-12-31 2017-05-30 General Electric Company Flowpath boundary and rotor assemblies in gas turbines

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2497151A (en) * 1946-03-04 1950-02-14 Armstrong Siddeley Motors Ltd Multidisk rotor
US2548886A (en) * 1947-10-25 1951-04-17 Gen Electric Gas turbine power plant with axial flow compressor
NL72215C (en) * 1949-04-29
FR1012335A (en) * 1949-07-13 1952-07-08 Hispano Suiza Sa Improvements made to machines, especially axial compressors, with rotor equipped with several blades arranged in tandem
US2749086A (en) * 1951-08-23 1956-06-05 Rolls Royce Rotor constructions for turbo machines
US2840299A (en) * 1952-09-22 1958-06-24 Thompson Prod Inc Axial flow compressor rotor
BE541380A (en) * 1954-09-28
GB802476A (en) * 1955-09-29 1958-10-08 Rolls Royce Improvements in or relating to rotors of axial-flow fluid machines for example compressors and turbines
US3094309A (en) * 1959-12-16 1963-06-18 Gen Electric Engine rotor design
US3295825A (en) * 1965-03-10 1967-01-03 Gen Motors Corp Multi-stage turbine rotor

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2456835A1 (en) * 1979-05-17 1980-12-12 United Technologies Corp ROTOR ASSEMBLY HAVING MULTI-STAGE DISC
FR2958322A1 (en) * 2010-04-01 2011-10-07 Snecma GAS TURBINE ENGINE ROTOR COMPRISING A ROTOR DRUM AND ROTOR CROWN
US8757980B2 (en) 2010-04-01 2014-06-24 Snecma Rotor for a gas turbine engine comprising a rotor spool and a rotor ring
WO2012017168A1 (en) * 2010-08-06 2012-02-09 Snecma Process for manufacturing a turbomachine drum
FR2963577A1 (en) * 2010-08-06 2012-02-10 Snecma PROCESS FOR PRODUCING A TURBOMACHINE DRUM
US9073155B2 (en) 2010-08-06 2015-07-07 Snecma Method of fabricating a turbine engine drum
RU2585597C1 (en) * 2010-08-06 2016-05-27 Снекма Method of making turbo machine drum

Also Published As

Publication number Publication date
US3894324A (en) 1975-07-15
DE2140816A1 (en) 1973-03-01
GB1395957A (en) 1975-05-29

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Legal Events

Date Code Title Description
ST Notification of lapse