FR2933153A1 - Support de montage d'une piece de transition et procede associe. - Google Patents

Support de montage d'une piece de transition et procede associe. Download PDF

Info

Publication number
FR2933153A1
FR2933153A1 FR0953751A FR0953751A FR2933153A1 FR 2933153 A1 FR2933153 A1 FR 2933153A1 FR 0953751 A FR0953751 A FR 0953751A FR 0953751 A FR0953751 A FR 0953751A FR 2933153 A1 FR2933153 A1 FR 2933153A1
Authority
FR
France
Prior art keywords
mounting bracket
component
pair
arms
transition piece
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.)
Pending
Application number
FR0953751A
Other languages
English (en)
French (fr)
Inventor
Patrick Melton
Kyle Kidder
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 FR2933153A1 publication Critical patent/FR2933153A1/fr
Pending 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Connection Of Plates (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Portable Nailing Machines And Staplers (AREA)
FR0953751A 2008-06-25 2009-06-05 Support de montage d'une piece de transition et procede associe. Pending FR2933153A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/213,828 US7918433B2 (en) 2008-06-25 2008-06-25 Transition piece mounting bracket and related method

Publications (1)

Publication Number Publication Date
FR2933153A1 true FR2933153A1 (fr) 2010-01-01

Family

ID=41360902

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0953751A Pending FR2933153A1 (fr) 2008-06-25 2009-06-05 Support de montage d'une piece de transition et procede associe.

Country Status (5)

Country Link
US (1) US7918433B2 (enExample)
JP (1) JP2010008037A (enExample)
CN (1) CN101614406B (enExample)
DE (1) DE102009026018B4 (enExample)
FR (1) FR2933153A1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103423246A (zh) * 2013-07-31 2013-12-04 昆山维金五金制品有限公司 一种连接板

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8616007B2 (en) * 2009-01-22 2013-12-31 Siemens Energy, Inc. Structural attachment system for transition duct outlet
US8281602B2 (en) * 2009-09-11 2012-10-09 General Electric Company Circumferentially self expanding combustor support for a turbine engine
US20110271688A1 (en) * 2010-05-06 2011-11-10 General Electric Company Reduced Pressure Loss Transition Support
USD655669S1 (en) * 2010-11-02 2012-03-13 Tony Matijevich Truck cradle assembly
US8403156B1 (en) * 2010-12-10 2013-03-26 Ryan K. Boone Canister organizer
US8448444B2 (en) * 2011-02-18 2013-05-28 General Electric Company Method and apparatus for mounting transition piece in combustor
US9803868B2 (en) * 2011-05-20 2017-10-31 Siemens Energy, Inc. Thermally compliant support for a combustion system
JP5491472B2 (ja) * 2011-09-26 2014-05-14 株式会社椿本チエイン ケーブル・配管類保護案内部材用取り付けブラケット
US8567745B2 (en) 2011-12-15 2013-10-29 United Technologies Corporation Apparatuses and systems with vertically and longitudinally offset mounting flanges
USD676037S1 (en) * 2012-02-17 2013-02-12 Spur Construction Ltd. Cell phone mounting bracket
US8936228B2 (en) 2012-05-02 2015-01-20 Caterpillar Inc. Load isolation bracket
US8931184B1 (en) 2012-05-21 2015-01-13 General Electric Company Method for dimensionally inspecting a component of a gas turbine system
US9249976B2 (en) 2012-06-28 2016-02-02 General Electric Company Method for servicing a combustor cap assembly for a turbine
CN102852917A (zh) * 2012-07-31 2013-01-02 苏州柏德纳科技有限公司 带侧挡板机械安装板
US9404421B2 (en) * 2014-01-23 2016-08-02 Siemens Energy, Inc. Structural support bracket for gas flow path
EP3105439B1 (en) * 2014-02-04 2019-12-11 United Technologies Corporation Clearance control system with brackets
US9696037B2 (en) 2014-10-16 2017-07-04 General Electric Company Liner retaining feature for a combustor
US9574460B2 (en) 2014-10-30 2017-02-21 Siemens Energy, Inc. Support arrangement for a transition piece of a gas turbine engine
EP3783200B1 (en) * 2014-12-11 2024-03-06 Siemens Energy Global GmbH & Co. KG Transition duct for a gas turbine engine
EP3726008B1 (en) * 2019-04-18 2022-05-18 Ansaldo Energia Switzerland AG Transition duct for a gas turbine assembly and gas turbine assembly comprising this transition duct

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1635847A (en) * 1925-09-17 1927-07-12 Henry Y Hooper Crank-case repair arm
US2707013A (en) * 1954-03-08 1955-04-26 Tinnerman Products Inc Blind fastening nut
US3337172A (en) * 1965-10-24 1967-08-22 Randall E Jackson Fixture supporting bracket
NZ180421A (en) * 1975-04-03 1979-03-16 Mc Lay R B C Bracket for lag stacking
US4422288A (en) 1981-03-02 1983-12-27 General Electric Company Aft mounting system for combustion transition duct members
US4465284A (en) 1983-09-19 1984-08-14 General Electric Company Scalloped cooling of gas turbine transition piece frame
US4719748A (en) 1985-05-14 1988-01-19 General Electric Company Impingement cooled transition duct
US4819748A (en) * 1987-02-20 1989-04-11 Truscott Aaron S Roof drill bit
BE1005718A3 (fr) 1992-03-10 1993-12-28 Solvay Procede pour la fabrication d'une poudre microspheroidale a faible dispersite, poudre microspheroidale a faible dispersite ainsi obtenue, catalyseurs pour la polymerisation d'alpha-olefines et procede de polymerisation d'alpha-olefines.
US5265412A (en) * 1992-07-28 1993-11-30 General Electric Company Self-accommodating brush seal for gas turbine combustor
US5414999A (en) 1993-11-05 1995-05-16 General Electric Company Integral aft frame mount for a gas turbine combustor transition piece
DE19928706C1 (de) * 1999-06-23 2001-01-18 Raymond A & Cie Zweiteilige Klammer zur Verbindung von zwei Platten mit Einschluß einer Zwischenplatte
US6494044B1 (en) 1999-11-19 2002-12-17 General Electric Company Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method
KR20010059692A (ko) * 1999-12-30 2001-07-06 이계안 모듈러 클립
US6412268B1 (en) 2000-04-06 2002-07-02 General Electric Company Cooling air recycling for gas turbine transition duct end frame and related method
DE20006801U1 (de) * 2000-04-13 2001-08-30 Erbslöh AG, 42553 Velbert Vorrichtung zur verdeckten Befestigung eines Profilteiles
US6547257B2 (en) 2001-05-04 2003-04-15 General Electric Company Combination transition piece floating cloth seal and stage 1 turbine nozzle flexible sealing element
US6904756B2 (en) * 2003-02-28 2005-06-14 Power Systems Mfg, Llc Transition duct support bracket wear cover
US7310952B2 (en) * 2003-10-17 2007-12-25 General Electric Company Methods and apparatus for attaching swirlers to gas turbine engine combustors
US7373772B2 (en) 2004-03-17 2008-05-20 General Electric Company Turbine combustor transition piece having dilution holes
US7010921B2 (en) 2004-06-01 2006-03-14 General Electric Company Method and apparatus for cooling combustor liner and transition piece of a gas turbine
DE202006007437U1 (de) * 2006-05-10 2007-09-13 Heinrich Gillet Gmbh Vorrichtung zum Befestigen eines Krümmers am Block eines Verbrennungsmotors
US7909300B2 (en) * 2007-10-18 2011-03-22 General Electric Company Combustor bracket assembly

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103423246A (zh) * 2013-07-31 2013-12-04 昆山维金五金制品有限公司 一种连接板

Also Published As

Publication number Publication date
CN101614406B (zh) 2013-07-31
DE102009026018B4 (de) 2017-07-27
DE102009026018A1 (de) 2009-12-31
CN101614406A (zh) 2009-12-30
US7918433B2 (en) 2011-04-05
US20090321608A1 (en) 2009-12-31
JP2010008037A (ja) 2010-01-14

Similar Documents

Publication Publication Date Title
FR2933153A1 (fr) Support de montage d'une piece de transition et procede associe.
FR3072720B1 (fr) Carter pour turbomachine comprenant une portion centrale en saillie relativement a deux portions laterales dans une region de jonction
EP0541472B1 (fr) Joint verrouillé pour canalisations
FR2970736A1 (fr) Manchon d'impact de piece de transition pour une turbine a gaz
FR2968031A1 (fr) Ensemble de fixation pour distributeur de turbine a gaz et methode de fixation, de depose et d'installation
FR2970288A1 (fr) Plaque de refroidissement par impact pour piece de turbomachine
EP3161263B1 (fr) Ensemble rotatif pour turbomachine
CA2802821A1 (fr) Secteur angulaire de redresseur pour compresseur de turbomachine
EP2488725A1 (fr) Roue de turbine equipee d'un jonc de retenue axiale verrouillant des pales par rapport a un disque
EP2718627B1 (fr) Chambre de combustion annulaire de turbomachine
FR2901773A1 (fr) Fixation de rail de plancher pour siege d'avion
FR3071273B1 (fr) Ensemble d'etancheite de turbine pour turbomachine
CA2925438A1 (fr) Ensemble rotatif pour turbomachine
WO2012089968A1 (fr) Plot de friction souple et garniture de frein pourvue d'un tel plot
EP2048324A1 (fr) Stator de turbine pour turbomachine d'aeronef integrant un dispositif d'amortissement de vibrations
CA2577595A1 (fr) Paroi transversale de chambre de combustion munie de trous de multiperforation
FR3040765A1 (fr) Element d'appui pour amortir des deplacements axiaux de traversee coulissante de systeme d'injection pour turbomachine
CA2578701C (fr) Chambre de combustion annulaire a fond amovible
EP1580403A1 (fr) Joint d'étanchéité entre les carters intérieur et extérieur d'une section de turboréacteur
FR2951508A1 (fr) Dispositif de pose d'un element plat et profile de base pour un tel dispositif
FR3061266B1 (fr) Four de cuisson comportant une plaque de separation
FR3005971A1 (fr) Element de raccordement pour tuyau d'eau et procede de montage d'un tel element a travers un mur
WO2006106255A2 (fr) Manchon compensateur pour tubes lisses
FR2888615A1 (fr) Fixation d'un element d'echappement sur le moteur
FR2817285A1 (fr) Virole interne de stator