FR2413541A1 - Systeme de fixation d'aubes mobiles - Google Patents

Systeme de fixation d'aubes mobiles

Info

Publication number
FR2413541A1
FR2413541A1 FR7837057A FR7837057A FR2413541A1 FR 2413541 A1 FR2413541 A1 FR 2413541A1 FR 7837057 A FR7837057 A FR 7837057A FR 7837057 A FR7837057 A FR 7837057A FR 2413541 A1 FR2413541 A1 FR 2413541A1
Authority
FR
France
Prior art keywords
disc
mobile
section
blades
aub
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
FR7837057A
Other languages
English (en)
Other versions
FR2413541B1 (fr
Inventor
Salvatore Alfred Leonardi
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.)
RTX 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 FR2413541A1 publication Critical patent/FR2413541A1/fr
Application granted granted Critical
Publication of FR2413541B1 publication Critical patent/FR2413541B1/fr
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
    • F01D5/32—Locking, e.g. by final locking blades or keys
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Toys (AREA)
  • Massaging Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'INVENTION CONCERNE UN SYSTEME DE FIXATION D'AUBES MOBILES. LES AUBES MOBILES 14 D'UN DISQUE DE ROTOR 12 COMPORTENT CHACUNE UNE SECTION DE TALON 16 ET UNE SECTION PROFILEE 18. LA SECTION DE TALON 16 DE CHAQUE AUBE 14 VIENT S'ENGAGER DANS UNE RAINURE DE FORME CORRESPONDANTE 20 PRATIQUEE A LA PERIPHERIE DU DISQUE 12. CHAQUE RAINURE 20 S'ETEND EN DESSOUS DE LA SECTION DE TALON 16 DE L'AUBE 14 POUR FORMER UNE CAVITE 22 ENTRE CETTE DERNIERE ET LE DISQUE 12. AU MOINS UN FLASQUE 24 ENTRE EN CONTACT AVEC LE DISQUE 12 POUR ENFERMER LES AUBES 14 DANS LES RAINURES CORRESPONDANTES 20 DE CE DISQUE 12. LE SYSTEME DE L'INVENTION EST UTILISE POUR FIXER LES AUBES MOBILES D'UN DISQUE DE ROTOR D'UNE TURBINE A GAZ.
FR7837057A 1977-12-27 1978-12-27 Systeme de fixation d'aubes mobiles Expired FR2413541B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/864,948 US4191509A (en) 1977-12-27 1977-12-27 Rotor blade attachment

Publications (2)

Publication Number Publication Date
FR2413541A1 true FR2413541A1 (fr) 1979-07-27
FR2413541B1 FR2413541B1 (fr) 1986-04-18

Family

ID=25344390

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7837057A Expired FR2413541B1 (fr) 1977-12-27 1978-12-27 Systeme de fixation d'aubes mobiles

Country Status (19)

Country Link
US (1) US4191509A (fr)
JP (1) JPS5496618A (fr)
KR (1) KR820000756B1 (fr)
AU (1) AU520295B2 (fr)
BE (1) BE873014A (fr)
BR (1) BR7808517A (fr)
CA (1) CA1112184A (fr)
CH (1) CH640916A5 (fr)
DE (1) DE2853856C2 (fr)
DK (1) DK581078A (fr)
FR (1) FR2413541B1 (fr)
GB (1) GB2011552B (fr)
IL (2) IL56125A (fr)
IN (1) IN149724B (fr)
IT (1) IT1101094B (fr)
NO (1) NO155159C (fr)
PL (1) PL123377B1 (fr)
SE (1) SE443184B (fr)
YU (1) YU39689B (fr)

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US4477222A (en) * 1982-09-30 1984-10-16 The United States Of America As Represented By The Secretary Of The Air Force Mounting construction for turbine vane assembly
US4692976A (en) * 1985-07-30 1987-09-15 Westinghouse Electric Corp. Method of making scalable side entry turbine blade roots
JPS63501372A (ja) * 1985-07-30 1988-05-26 ウエスチングハウス・エレクトリック・コ−ポレ−ション スケールモデルにより設計可能なサイドエントリー型タービン翼の形状決定方法
US4824328A (en) * 1987-05-22 1989-04-25 Westinghouse Electric Corp. Turbine blade attachment
GB2238581B (en) * 1989-11-30 1994-01-12 Rolls Royce Plc Improved attachment of a gas turbine engine blade to a turbine rotor disc
US5100292A (en) * 1990-03-19 1992-03-31 General Electric Company Gas turbine engine blade
US5152669A (en) * 1990-06-26 1992-10-06 Westinghouse Electric Corp. Turbomachine blade fastening
US5141401A (en) * 1990-09-27 1992-08-25 General Electric Company Stress-relieved rotor blade attachment slot
US5147180A (en) * 1991-03-21 1992-09-15 Westinghouse Electric Corp. Optimized blade root profile for steam turbine blades
US5176500A (en) * 1992-03-24 1993-01-05 Westinghouse Electric Corp. Two-lug side-entry turbine blade attachment
DE4432999C2 (de) * 1994-09-16 1998-07-30 Mtu Muenchen Gmbh Laufrad einer Turbomaschine, insbesondere einer axial durchströmten Turbine eines Gasturbinentriebwerks
DE4435268A1 (de) * 1994-10-01 1996-04-04 Abb Management Ag Beschaufelter Rotor einer Turbomaschine
US5494408A (en) * 1994-10-12 1996-02-27 General Electric Co. Bucket to wheel dovetail design for turbine rotors
DE4436727A1 (de) * 1994-10-14 1996-04-18 Abb Management Ag Trommelrotor für eine axial durchströmte Turbomaschine
US5531569A (en) * 1994-12-08 1996-07-02 General Electric Company Bucket to wheel dovetail design for turbine rotors
DE19516694C2 (de) * 1995-05-06 2001-06-28 Mtu Aero Engines Gmbh Einrichtung zur Fixierung von Laufschaufeln am Laufrad, insbesondere einer Turbine eines Gasturbinentriebwerks
DE19603388C1 (de) * 1996-01-31 1997-07-24 Mtu Muenchen Gmbh Einrichtung zur Fixierung der Laufschaufeln am Laufrad, insbesondere einer Turbine eines Gasturbinentriebwerks, durch Nietung
DE19619316C2 (de) * 1996-05-14 2002-07-18 Voith Siemens Hydro Power Laufrad für eine Freistrahlturbine
JP2000512707A (ja) * 1996-06-21 2000-09-26 シーメンス アクチエンゲゼルシヤフト 溝内に装着可能な翼を有するタービン機械のロータ及びロータの翼
AUPO729997A0 (en) * 1997-06-11 1997-07-03 Cleland, Glen Irving Engine disabling apparatus
DE19728085A1 (de) * 1997-07-02 1999-01-07 Asea Brown Boveri Fügeverbindung zwischen zwei Fügepartnern sowie deren Verwendung
US6033185A (en) * 1998-09-28 2000-03-07 General Electric Company Stress relieved dovetail
GB2345943B (en) * 1998-12-04 2003-07-09 Glenn Bruce Sinclair Precision crowning of blade attachments in gas turbines
US6139277A (en) * 1998-12-22 2000-10-31 Air Concepts, Inc. Motorized fan
US6592330B2 (en) * 2001-08-30 2003-07-15 General Electric Company Method and apparatus for non-parallel turbine dovetail-faces
US6773234B2 (en) 2002-10-18 2004-08-10 General Electric Company Methods and apparatus for facilitating preventing failure of gas turbine engine blades
US7905709B2 (en) * 2004-02-10 2011-03-15 General Electric Company Advanced firtree and broach slot forms for turbine stage 1 and 2 buckets and rotor wheels
US8079817B2 (en) * 2004-02-10 2011-12-20 General Electric Company Advanced firtree and broach slot forms for turbine stage 3 buckets and rotor wheels
EP1584792A1 (fr) * 2004-04-08 2005-10-12 Siemens Aktiengesellschaft Attachement d'aube pour un compresseur ou une turbine
DE102004051116A1 (de) * 2004-10-20 2006-04-27 Mtu Aero Engines Gmbh Rotor einer Turbomaschine, insbesondere Gasturbinenrotor
US7261518B2 (en) * 2005-03-24 2007-08-28 Siemens Demag Delaval Turbomachinery, Inc. Locking arrangement for radial entry turbine blades
JP4869616B2 (ja) * 2005-04-01 2012-02-08 株式会社日立製作所 蒸気タービン動翼と蒸気タービンロータ及びそれを用いた蒸気タービン並びにその発電プラント
US7156612B2 (en) * 2005-04-05 2007-01-02 Pratt & Whitney Canada Corp. Spigot arrangement for a split impeller
US7387494B2 (en) * 2005-04-28 2008-06-17 General Electric Company Finger dovetail attachment between a turbine rotor wheel and bucket for stress reduction
US7690896B2 (en) * 2005-05-27 2010-04-06 United Technologies Corporation Gas turbine disk slots and gas turbine engine using same
EP2019913A4 (fr) * 2006-05-12 2011-06-01 Gen Electric Contre-découpe en queue d'aronde de pale/disque pour une réduction de la contrainte pale/disque (6fa+e, étape 2)
US8038404B2 (en) * 2007-07-16 2011-10-18 Nuovo Pignone Holdings, S.P.A. Steam turbine and rotating blade
US8047797B2 (en) * 2007-07-16 2011-11-01 Nuovo Pignone Holdings, S.P.A. Steam turbine and rotating blade
US8047796B2 (en) * 2007-11-16 2011-11-01 General Electric Company Dovetail attachment for use with turbine assemblies and methods of assembling turbine assemblies
EP2546465A1 (fr) * 2011-07-14 2013-01-16 Siemens Aktiengesellschaft Pied d'aube, aube, disque de rotor et ensemble de turbomachine associés
US9359905B2 (en) 2012-02-27 2016-06-07 Solar Turbines Incorporated Turbine engine rotor blade groove
US9546556B2 (en) * 2012-09-26 2017-01-17 United Technologies Corporation Turbine blade root profile
GB201416505D0 (en) * 2014-09-18 2014-11-05 Rolls Royce Plc Gas turbine engine
CN104832220A (zh) * 2014-12-31 2015-08-12 东方电气集团东方汽轮机有限公司 涡轮机动叶片的叶根及轮槽结构
EP3093441B1 (fr) * 2015-05-12 2019-07-10 Ansaldo Energia Switzerland AG Rotor de moteur turbo comprenant une connexion aube-arbe et aube pour ledit rotor
WO2016195689A1 (fr) * 2015-06-04 2016-12-08 Siemens Energy, Inc. Système de fixation pour surface portante de turbine
CN109145335B (zh) * 2017-06-28 2023-05-30 中国航发贵阳发动机设计研究所 一种通过预旋转提高轮盘低循环疲劳寿命的方法
US12305533B2 (en) * 2023-06-23 2025-05-20 Pratt & Whitney Canada Corp. Turbine rotor dovetail structure with splines

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1500044A (en) * 1974-03-25 1978-02-08 Norbut T Turbomachinery discs

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2429215A (en) * 1943-01-16 1947-10-21 Jarvis C Marble Turbine blade
GB677142A (en) * 1949-08-24 1952-08-13 Power Jets Res & Dev Ltd Improved mounting for turbine and like blades
DE950557C (de) * 1952-12-23 1956-10-11 Svenska Turbinfab Ab Tannenbaum-Fuss fuer Laufschaufeln von Axial-Turbinen oder -Verdichtern
US4029436A (en) * 1975-06-17 1977-06-14 United Technologies Corporation Blade root feather seal

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1500044A (en) * 1974-03-25 1978-02-08 Norbut T Turbomachinery discs

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
EXBK/66 *

Also Published As

Publication number Publication date
YU295478A (en) 1982-06-30
DK581078A (da) 1979-06-28
AU4251978A (en) 1979-07-05
DE2853856A1 (de) 1979-07-05
IL62817A0 (en) 1981-07-31
JPS5496618A (en) 1979-07-31
IT7831226A0 (it) 1978-12-22
JPS6146644B2 (fr) 1986-10-15
CH640916A5 (de) 1984-01-31
AU520295B2 (en) 1982-01-21
DE2853856C2 (de) 1987-04-02
NO155159B (no) 1986-11-10
PL123377B1 (en) 1982-10-30
NO784349L (no) 1979-06-28
SE443184B (sv) 1986-02-17
GB2011552A (en) 1979-07-11
PL211564A1 (pl) 1979-07-30
US4191509A (en) 1980-03-04
BE873014A (fr) 1979-04-17
SE7812961L (sv) 1979-06-28
KR820000756B1 (ko) 1982-05-04
FR2413541B1 (fr) 1986-04-18
IL56125A (en) 1982-02-28
CA1112184A (fr) 1981-11-10
NO155159C (no) 1987-02-18
YU39689B (en) 1985-03-20
IT1101094B (it) 1985-09-28
BR7808517A (pt) 1979-08-21
GB2011552B (en) 1982-03-31
IN149724B (fr) 1982-03-27

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Legal Events

Date Code Title Description
ST Notification of lapse