CA619513A - Bladed rotor assembly - Google Patents

Bladed rotor assembly

Info

Publication number
CA619513A
CA619513A CA619513A CA619513DA CA619513A CA 619513 A CA619513 A CA 619513A CA 619513 A CA619513 A CA 619513A CA 619513D A CA619513D A CA 619513DA CA 619513 A CA619513 A CA 619513A
Authority
CA
Canada
Prior art keywords
rotor assembly
bladed rotor
bladed
assembly
rotor
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
CA619513A
Inventor
Morita Saburo
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.)
Orenda Engines Ltd
Original Assignee
Orenda Engines Ltd
Publication date
Application granted granted Critical
Publication of CA619513A publication Critical patent/CA619513A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3053—Fixing blades to rotors; Blade roots ; Blade spacers by means of pins

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
CA619513A Bladed rotor assembly Expired CA619513A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA619513T

Publications (1)

Publication Number Publication Date
CA619513A true CA619513A (en) 1961-05-02

Family

ID=210630

Family Applications (1)

Application Number Title Priority Date Filing Date
CA619513A Expired CA619513A (en) Bladed rotor assembly

Country Status (1)

Country Link
CA (1) CA619513A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4008000A (en) * 1974-08-28 1977-02-15 Motoren-Und Turbinen-Union Munich Gmbh Axial-flow rotor wheel for high-speed turbomachines
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
US5007800A (en) * 1988-10-05 1991-04-16 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Rotor blade fixing for turbomachine rotors
EP0736668A1 (en) * 1995-03-06 1996-10-09 Solar Turbines Incorporated Ceramic blade attachment system
CN102213108A (en) * 2010-04-06 2011-10-12 通用电气公司 Composite turbine bucket assembly
EP3208425A3 (en) * 2011-05-26 2017-11-08 United Technologies Corporation Hybrid rotor disk assembly with ceramic matrix composites platform for a gas turbine engine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4008000A (en) * 1974-08-28 1977-02-15 Motoren-Und Turbinen-Union Munich Gmbh Axial-flow rotor wheel for high-speed turbomachines
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
US5007800A (en) * 1988-10-05 1991-04-16 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Rotor blade fixing for turbomachine rotors
EP0736668A1 (en) * 1995-03-06 1996-10-09 Solar Turbines Incorporated Ceramic blade attachment system
CN102213108A (en) * 2010-04-06 2011-10-12 通用电气公司 Composite turbine bucket assembly
EP3208425A3 (en) * 2011-05-26 2017-11-08 United Technologies Corporation Hybrid rotor disk assembly with ceramic matrix composites platform for a gas turbine engine

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