FR2008530A1 - - Google Patents

Info

Publication number
FR2008530A1
FR2008530A1 FR6909915A FR6909915A FR2008530A1 FR 2008530 A1 FR2008530 A1 FR 2008530A1 FR 6909915 A FR6909915 A FR 6909915A FR 6909915 A FR6909915 A FR 6909915A FR 2008530 A1 FR2008530 A1 FR 2008530A1
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.)
Withdrawn
Application number
FR6909915A
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2008530A1 publication Critical patent/FR2008530A1/fr
Withdrawn legal-status Critical Current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
    • F01D5/32Locking, e.g. by final locking blades or keys
    • F01D5/323Locking of axial insertion type blades by means of a key or the like parallel to the axis of the rotor

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)
FR6909915A 1968-05-15 1969-04-01 Withdrawn FR2008530A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US72915368A 1968-05-15 1968-05-15

Publications (1)

Publication Number Publication Date
FR2008530A1 true FR2008530A1 (fr) 1970-01-23

Family

ID=24929802

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6909915A Withdrawn FR2008530A1 (fr) 1968-05-15 1969-04-01

Country Status (6)

Country Link
US (1) US3479009A (fr)
JP (1) JPS4815324B1 (fr)
BE (1) BE730808A (fr)
DE (1) DE1915920A1 (fr)
FR (1) FR2008530A1 (fr)
GB (1) GB1255873A (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4885001U (fr) * 1972-01-21 1973-10-16
US4208170A (en) * 1978-05-18 1980-06-17 General Electric Company Blade retainer
US4470757A (en) * 1982-02-25 1984-09-11 United Technologies Corporation Sideplate retention for a turbine rotor
US4576551A (en) * 1982-06-17 1986-03-18 The Garrett Corporation Turbo machine blading
US5257908A (en) * 1991-11-15 1993-11-02 Ortolano Ralph J Turbine lashing structure
US5350279A (en) * 1993-07-02 1994-09-27 General Electric Company Gas turbine engine blade retainer sub-assembly
US6109877A (en) * 1998-11-23 2000-08-29 Pratt & Whitney Canada Corp. Turbine blade-to-disk retention device
JP2005273646A (ja) * 2004-02-25 2005-10-06 Mitsubishi Heavy Ind Ltd 動翼体及びこの動翼体を有する回転機械
FR2900437B1 (fr) * 2006-04-27 2008-07-25 Snecma Sa Systeme de retention des aubes dans un rotor
US7874804B1 (en) * 2007-05-10 2011-01-25 Florida Turbine Technologies, Inc. Turbine blade with detached platform
US8128365B2 (en) 2007-07-09 2012-03-06 Siemens Energy, Inc. Turbine airfoil cooling system with rotor impingement cooling
JP2010216289A (ja) * 2009-03-13 2010-09-30 Ihi Corp 動翼の固定装置、翼回転装置及び翼回転装置の組立方法
EP2386721A1 (fr) * 2010-05-14 2011-11-16 Siemens Aktiengesellschaft Dispositif de fixation pour pales de turbomachines pouvant s'écouler axialement et son procédé de fabrication
FR2963383B1 (fr) * 2010-07-27 2016-09-09 Snecma Aube de turbomachine, rotor, turbine basse pression et turbomachine equipes d'une telle aube
US9885368B2 (en) * 2012-05-24 2018-02-06 Carrier Corporation Stall margin enhancement of axial fan with rotating shroud
US20140199172A1 (en) * 2013-01-11 2014-07-17 General Electric Company Turbomachine and method of handling turbomachine components
DE102013214933A1 (de) * 2013-07-30 2015-02-26 MTU Aero Engines AG Verfahren zum Montieren einer Gasturbinenschaufel in einer zugeordneten Aufnahme eines Rotorgrundkörpers
CN113478180B (zh) * 2021-07-15 2022-11-25 重庆江增船舶重工有限公司 一种增压器锁紧片的加工方法及其翻边工具
US12410720B2 (en) * 2023-11-02 2025-09-09 General Electric Company Turbine engine having a rotatable disk and a blade

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US791564A (en) * 1905-01-13 1905-06-06 Oren Lynch Tire-tightener.
US2297770A (en) * 1941-03-07 1942-10-06 Jepson Percy Cotter pin
FR1031802A (fr) * 1950-03-25 1953-06-26 Armstrong Siddeley Motors Ltd Disque de rotor à aubage
US2786648A (en) * 1950-04-04 1957-03-26 United Aircraft Corp Blade locking device
GB691380A (en) * 1950-07-01 1953-05-13 Power Jets Res & Dev Ltd Improvements relating to bladed rotors for compressors, turbines or like apparatus
US2753149A (en) * 1951-03-30 1956-07-03 United Aircraft Corp Blade lock
US2971744A (en) * 1956-11-27 1961-02-14 Szydlowski Joseph Blade lock

Also Published As

Publication number Publication date
GB1255873A (en) 1971-12-01
BE730808A (fr) 1969-09-01
DE1915920A1 (de) 1970-01-15
JPS4815324B1 (fr) 1973-05-14
US3479009A (en) 1969-11-18

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Legal Events

Date Code Title Description
ST Notification of lapse