FR2728014B1 - Support d'ailettes, notamment pour turbine a gaz - Google Patents

Support d'ailettes, notamment pour turbine a gaz

Info

Publication number
FR2728014B1
FR2728014B1 FR9514396A FR9514396A FR2728014B1 FR 2728014 B1 FR2728014 B1 FR 2728014B1 FR 9514396 A FR9514396 A FR 9514396A FR 9514396 A FR9514396 A FR 9514396A FR 2728014 B1 FR2728014 B1 FR 2728014B1
Authority
FR
France
Prior art keywords
gas turbine
fin support
fin
support
turbine
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 - Fee Related
Application number
FR9514396A
Other languages
English (en)
Other versions
FR2728014A1 (fr
Inventor
James Edwin Rhoda
Thomas A Bradley
Mark Joseph Mielke
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 FR2728014A1 publication Critical patent/FR2728014A1/fr
Application granted granted Critical
Publication of FR2728014B1 publication Critical patent/FR2728014B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
    • F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
    • F01D5/3038—Fixing 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
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR9514396A 1994-12-08 1995-12-06 Support d'ailettes, notamment pour turbine a gaz Expired - Fee Related FR2728014B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/351,997 US5486095A (en) 1994-12-08 1994-12-08 Split disk blade support

Publications (2)

Publication Number Publication Date
FR2728014A1 FR2728014A1 (fr) 1996-06-14
FR2728014B1 true FR2728014B1 (fr) 1998-10-23

Family

ID=23383352

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9514396A Expired - Fee Related FR2728014B1 (fr) 1994-12-08 1995-12-06 Support d'ailettes, notamment pour turbine a gaz

Country Status (3)

Country Link
US (1) US5486095A (fr)
FR (1) FR2728014B1 (fr)
GB (1) GB2295861B (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2299834B (en) * 1995-04-12 1999-09-08 Rolls Royce Plc Gas turbine engine rotary disc
US5961287A (en) * 1997-09-25 1999-10-05 United Technologies Corporation Twin-web rotor disk
US6558121B2 (en) * 2001-08-29 2003-05-06 General Electric Company Method and apparatus for turbine blade contoured platform
DE10337868A1 (de) * 2003-08-18 2005-03-17 Mtu Aero Engines Gmbh Rotor für eine Gasturbine sowie Gasturbine
JP4911286B2 (ja) * 2006-03-14 2012-04-04 株式会社Ｉｈｉ ファンのダブテール構造
JP4807113B2 (ja) * 2006-03-14 2011-11-02 株式会社Ｉｈｉ ファンのダブテール構造
EP2128450B1 (fr) * 2007-03-27 2018-05-16 IHI Corporation Structure de soutien pour aube de rotor de ventilateur et moteur à double flux équipé de celle-ci
US8251668B2 (en) * 2009-06-30 2012-08-28 General Electric Company Method and apparatus for assembling rotating machines
FR2974863B1 (fr) * 2011-05-06 2015-10-23 Snecma Disque de soufflante de turbomachine
PL415045A1 (pl) 2015-12-03 2017-06-05 General Electric Company Tarcze turbiny i sposoby ich wytwarzania
US11231043B2 (en) 2018-02-21 2022-01-25 General Electric Company Gas turbine engine with ultra high pressure compressor
US10823191B2 (en) 2018-03-15 2020-11-03 General Electric Company Gas turbine engine arrangement with ultra high pressure compressor

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR389268A (fr) * 1907-04-20 1908-09-04 Carl Roth Système de fixation des aubes de turbines à vapeur et autres machines analogues
GB277663A (en) * 1926-09-20 1928-01-26 Lorenzen Turbinen Ag Improvements in or relating to turbines
US2751189A (en) * 1950-09-08 1956-06-19 United Aircraft Corp Blade fastening means
GB739870A (en) * 1954-04-07 1955-11-02 Parsons C A & Co Ltd Improvements in and relating to locking devices for rotor blades of turbines and the like
NL295165A (fr) * 1962-07-11
GB1052008A (fr) * 1966-06-20
GB1432875A (en) * 1973-07-11 1976-04-22 Rolls Royce Gas rotor assemblies
US4094615A (en) * 1976-12-27 1978-06-13 Electric Power Research Institute, Inc. Blade attachment structure for gas turbine rotor
FR2448626A1 (fr) * 1979-02-08 1980-09-05 Snecma Perfectionnement aux rotors de machines tournantes
GB2097480B (en) * 1981-04-29 1984-06-06 Rolls Royce Rotor blade fixing in circumferential slot
FR2535793B1 (fr) * 1982-11-08 1987-04-10 Snecma Dispositif de verrouillage axial d'aubes de soufflante
FR2637321B1 (fr) * 1988-10-05 1990-11-30 Snecma Rotor de turbomachine muni d'un dispositif de fixation des aubes
US5022822A (en) * 1989-10-24 1991-06-11 United Technologies Corporation Compressor blade attachment assembly
US5131814A (en) * 1990-04-03 1992-07-21 General Electric Company Turbine blade inner end attachment structure
US5112193A (en) * 1990-09-11 1992-05-12 Pratt & Whitney Canada Fan blade axial retention device
US5135354A (en) * 1990-09-14 1992-08-04 United Technologies Corporation Gas turbine blade and disk
US5213475A (en) * 1991-12-05 1993-05-25 General Electric Company Burst resistant rotor disk assembly
US5310317A (en) * 1992-08-11 1994-05-10 General Electric Company Quadra-tang dovetail blade

Also Published As

Publication number Publication date
US5486095A (en) 1996-01-23
GB9524098D0 (en) 1996-01-24
GB2295861A (en) 1996-06-12
FR2728014A1 (fr) 1996-06-14
GB2295861B (en) 1998-03-25

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20110831