BE705200A - - Google Patents

Info

Publication number
BE705200A
BE705200A BE705200DA BE705200A BE 705200 A BE705200 A BE 705200A BE 705200D A BE705200D A BE 705200DA BE 705200 A BE705200 A BE 705200A
Authority
BE
Belgium
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
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 filed Critical
Publication of BE705200A publication Critical patent/BE705200A/xx
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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • 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
    • F01D5/303Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
    • F01D5/3038Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
    • 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
    • F01D5/32Locking, e.g. by final locking blades or keys
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE705200D 1967-01-19 1967-10-16 Expired BE705200A (US08063081-20111122-C00102.png)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US610270A US3383094A (en) 1967-01-19 1967-01-19 Rotor blade locking means

Publications (1)

Publication Number Publication Date
BE705200A true BE705200A (US08063081-20111122-C00102.png) 1968-03-01

Family

ID=24444374

Family Applications (1)

Application Number Title Priority Date Filing Date
BE705200D Expired BE705200A (US08063081-20111122-C00102.png) 1967-01-19 1967-10-16

Country Status (6)

Country Link
US (1) US3383094A (US08063081-20111122-C00102.png)
BE (1) BE705200A (US08063081-20111122-C00102.png)
CH (1) CH467419A (US08063081-20111122-C00102.png)
DE (1) DE1576955A1 (US08063081-20111122-C00102.png)
GB (1) GB1187227A (US08063081-20111122-C00102.png)
NL (1) NL6714001A (US08063081-20111122-C00102.png)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3597112A (en) * 1970-02-02 1971-08-03 Gen Electric Compressor-blade-retaining means
US3954350A (en) * 1974-06-14 1976-05-04 Motoren-Und Turbinen-Union Munchen Gmbh Rotor having means for locking rotor blades to rotor disk
US3902824A (en) * 1974-07-29 1975-09-02 Gen Motors Corp Blade lock
FR2282038A1 (fr) * 1974-08-13 1976-03-12 Mtu Muenchen Gmbh Dispositif pour fixer les aubes mobiles de turbomachines
CA1114301A (en) * 1979-06-27 1981-12-15 Ivor J. Roberts Locking device for blade mounting
US4280795A (en) * 1979-12-26 1981-07-28 United Technologies Corporation Interblade seal for axial flow rotary machines
GB2097480B (en) * 1981-04-29 1984-06-06 Rolls Royce Rotor blade fixing in circumferential slot
GB2112465B (en) * 1981-12-30 1985-04-11 Rolls Royce Turbomachine rotor
GB2171150B (en) * 1985-02-12 1989-07-26 Rolls Royce Plc Bladed rotor assembly for a turbomachine
FR2616480B1 (fr) * 1987-06-10 1989-09-29 Snecma Dispositif de verrouillage d'aubes a pied marteau sur un disque de turbomachine et procedes de montage et de demontage
FR2758364B1 (fr) * 1997-01-16 1999-02-12 Snecma Disque aubage a aubes tripodes
US6315298B1 (en) * 1999-11-22 2001-11-13 United Technologies Corporation Turbine disk and blade assembly seal
FR2873745B1 (fr) * 2004-07-28 2008-10-10 Snecma Moteurs Sa Disque de rotor de turbomachine
EP1698759B1 (de) * 2005-02-23 2015-06-03 Alstom Technology Ltd Rotor-Schluss
GB0908502D0 (en) * 2009-05-19 2009-06-24 Rolls Royce Plc A balanced rotor for a turbine engine
FR2965008B1 (fr) * 2010-09-16 2013-08-02 Snecma Disque a aubes pour rotor de turbomachine, et turbomachine equipee d'un tel disque
GB201106050D0 (en) * 2011-04-11 2011-05-25 Rolls Royce Plc A retention device for a composite blade of a gas turbine engine
US20140199172A1 (en) * 2013-01-11 2014-07-17 General Electric Company Turbomachine and method of handling turbomachine components
ITFI20130117A1 (it) 2013-05-21 2014-11-22 Nuovo Pignone Srl "turbomachine rotor assembly and method"
DE102013223583A1 (de) * 2013-11-19 2015-05-21 MTU Aero Engines AG Schaufel-Scheiben-Verbund, Verfahren und Strömungsmaschine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1371327A (en) * 1920-07-21 1921-03-15 Schneider & Cie Turbine
US2199243A (en) * 1939-03-01 1940-04-30 Gen Electric Elastic fluid turbine rotor
US2393447A (en) * 1944-05-20 1946-01-22 Allis Chalmers Mfg Co Turbine blade locking apparatus
BE490366A (US08063081-20111122-C00102.png) * 1948-09-17
US2781962A (en) * 1951-07-26 1957-02-19 Gen Motors Corp Blade fastening means
US2994507A (en) * 1959-01-23 1961-08-01 Westinghouse Electric Corp Blade locking structure
GB903176A (en) * 1960-01-18 1962-08-15 Rolls Royce Method of mounting a multi-blade set on a support member, for example to form a gas turbine compressor rotor
US3216700A (en) * 1963-10-24 1965-11-09 Gen Electric Rotor blade locking means
US3252687A (en) * 1965-02-01 1966-05-24 Gen Motors Corp Rotor blade locking

Also Published As

Publication number Publication date
DE1576955A1 (de) 1970-05-06
GB1187227A (en) 1970-04-08
NL6714001A (US08063081-20111122-C00102.png) 1968-07-22
CH467419A (de) 1969-01-15
US3383094A (en) 1968-05-14

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