CA1030071A - Blade retaining sideplate and turbine disk assembly - Google Patents

Blade retaining sideplate and turbine disk assembly

Info

Publication number
CA1030071A
CA1030071A CA235,497A CA235497A CA1030071A CA 1030071 A CA1030071 A CA 1030071A CA 235497 A CA235497 A CA 235497A CA 1030071 A CA1030071 A CA 1030071A
Authority
CA
Canada
Prior art keywords
sideplate
disk assembly
turbine disk
blade retaining
retaining
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
CA235,497A
Other languages
English (en)
French (fr)
Inventor
Donald J. Bandurick
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of CA1030071A publication Critical patent/CA1030071A/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
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CA235,497A 1974-10-29 1975-09-08 Blade retaining sideplate and turbine disk assembly Expired CA1030071A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/518,826 US3957393A (en) 1974-10-29 1974-10-29 Turbine disk and sideplate construction

Publications (1)

Publication Number Publication Date
CA1030071A true CA1030071A (en) 1978-04-25

Family

ID=24065668

Family Applications (1)

Application Number Title Priority Date Filing Date
CA235,497A Expired CA1030071A (en) 1974-10-29 1975-09-08 Blade retaining sideplate and turbine disk assembly

Country Status (8)

Country Link
US (1) US3957393A (de)
JP (1) JPS5166919A (de)
CA (1) CA1030071A (de)
DE (1) DE2542428C2 (de)
FR (1) FR2289726A1 (de)
GB (1) GB1519818A (de)
IT (1) IT1043684B (de)
SE (1) SE411060B (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1512882A (en) * 1976-02-11 1978-06-01 Rolls Royce Bladed rotor assembly for a gas turbine engine
US4523890A (en) * 1983-10-19 1985-06-18 General Motors Corporation End seal for turbine blade base
US4767276A (en) * 1986-12-19 1988-08-30 General Electric Company Retainer ring
US5030063A (en) * 1990-02-08 1991-07-09 General Motors Corporation Turbomachine rotor
FR2694046B1 (fr) * 1992-07-22 1994-09-23 Snecma Dispositif d'étanchéité et de rétention pour un rotor entaillé de brochages recevant des pieds d'aubes.
US6139277A (en) * 1998-12-22 2000-10-31 Air Concepts, Inc. Motorized fan
US7465149B2 (en) * 2006-03-14 2008-12-16 Rolls-Royce Plc Turbine engine cooling
US8128371B2 (en) * 2007-02-15 2012-03-06 General Electric Company Method and apparatus to facilitate increasing turbine rotor efficiency
EP1978211A1 (de) * 2007-04-04 2008-10-08 Siemens Aktiengesellschaft Anordnung zur Axialsicherung an Laufschaufeln in einem Rotor sowie Gasturbine mit einer solchen Anordnung
US10544677B2 (en) 2017-09-01 2020-01-28 United Technologies Corporation Turbine disk
DE112011100606B4 (de) * 2010-02-19 2022-12-08 Borgwarner Inc. Turbinenrad und Verfahren zu seiner Herstellung
US10641110B2 (en) 2017-09-01 2020-05-05 United Technologies Corporation Turbine disk
US10472968B2 (en) 2017-09-01 2019-11-12 United Technologies Corporation Turbine disk
US10550702B2 (en) 2017-09-01 2020-02-04 United Technologies Corporation Turbine disk
US10724374B2 (en) 2017-09-01 2020-07-28 Raytheon Technologies Corporation Turbine disk

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB779059A (en) * 1954-07-15 1957-07-17 Rolls Royce Improvements in or relating to axial-flow fluid machines, for example compressors orturbines of gas-turbine engines
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
US3572966A (en) * 1969-01-17 1971-03-30 Westinghouse Electric Corp Seal plates for root cooled turbine rotor blades
DE1957614C3 (de) * 1969-11-15 1974-03-14 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Laufschaufelkranz für Gasturbinentriebwerke mit hoher DrehzahL
US3666376A (en) * 1971-01-05 1972-05-30 United Aircraft Corp Turbine blade damper
BE794573A (fr) * 1972-02-02 1973-05-16 Gen Electric Dispositif de fixation d'aubes
US3887298A (en) * 1974-05-30 1975-06-03 United Aircraft Corp Apparatus for sealing turbine blade damper cavities

Also Published As

Publication number Publication date
SE411060B (sv) 1979-11-26
US3957393A (en) 1976-05-18
GB1519818A (en) 1978-08-02
DE2542428C2 (de) 1984-03-22
IT1043684B (it) 1980-02-29
DE2542428A1 (de) 1976-05-13
FR2289726A1 (fr) 1976-05-28
FR2289726B1 (de) 1979-06-29
JPS5166919A (de) 1976-06-10
SE7510642L (sv) 1976-04-30

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