FR2289726A1 - Rotor de turbine - Google Patents

Rotor de turbine

Info

Publication number
FR2289726A1
FR2289726A1 FR7531037A FR7531037A FR2289726A1 FR 2289726 A1 FR2289726 A1 FR 2289726A1 FR 7531037 A FR7531037 A FR 7531037A FR 7531037 A FR7531037 A FR 7531037A FR 2289726 A1 FR2289726 A1 FR 2289726A1
Authority
FR
France
Prior art keywords
turbine rotor
turbine
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.)
Granted
Application number
FR7531037A
Other languages
English (en)
Other versions
FR2289726B1 (fr
Inventor
Donald James 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
Publication of FR2289726A1 publication Critical patent/FR2289726A1/fr
Application granted granted Critical
Publication of FR2289726B1 publication Critical patent/FR2289726B1/fr
Granted 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)
FR7531037A 1974-10-29 1975-10-10 Rotor de turbine Granted FR2289726A1 (fr)

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 (2)

Publication Number Publication Date
FR2289726A1 true FR2289726A1 (fr) 1976-05-28
FR2289726B1 FR2289726B1 (fr) 1979-06-29

Family

ID=24065668

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7531037A Granted FR2289726A1 (fr) 1974-10-29 1975-10-10 Rotor de turbine

Country Status (8)

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

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 (fr) * 2007-04-04 2008-10-08 Siemens Aktiengesellschaft Dispositif de sécurité axiale sur des aubes mobiles d'un moteur tout comme turbine à gaz dotée d'un tel dispositif
US10544677B2 (en) 2017-09-01 2020-01-28 United Technologies Corporation Turbine disk
CN102741522A (zh) * 2010-02-19 2012-10-17 博格华纳公司 涡轮机叶轮以及用于生产其的方法
US10641110B2 (en) 2017-09-01 2020-05-05 United Technologies Corporation Turbine disk
US10550702B2 (en) 2017-09-01 2020-02-04 United Technologies Corporation Turbine disk
US10472968B2 (en) 2017-09-01 2019-11-12 United Technologies Corporation Turbine disk
US10724374B2 (en) 2017-09-01 2020-07-28 Raytheon Technologies Corporation Turbine disk

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3887298A (en) * 1974-05-30 1975-06-03 United Aircraft Corp Apparatus for sealing turbine blade damper cavities

Family Cites Families (6)

* 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

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
JPS5166919A (fr) 1976-06-10
IT1043684B (it) 1980-02-29
CA1030071A (fr) 1978-04-25
FR2289726B1 (fr) 1979-06-29
GB1519818A (en) 1978-08-02
SE411060B (sv) 1979-11-26
DE2542428C2 (de) 1984-03-22
DE2542428A1 (de) 1976-05-13
US3957393A (en) 1976-05-18
SE7510642L (sv) 1976-04-30

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Legal Events

Date Code Title Description
ST Notification of lapse