EP1840471A3 - Device for fastening a sequentially operated burner in a gas turbine arrangement - Google Patents

Device for fastening a sequentially operated burner in a gas turbine arrangement Download PDF

Info

Publication number
EP1840471A3
EP1840471A3 EP07103514A EP07103514A EP1840471A3 EP 1840471 A3 EP1840471 A3 EP 1840471A3 EP 07103514 A EP07103514 A EP 07103514A EP 07103514 A EP07103514 A EP 07103514A EP 1840471 A3 EP1840471 A3 EP 1840471A3
Authority
EP
European Patent Office
Prior art keywords
fastening
gas turbine
hole
sequentially operated
turbine arrangement
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
EP07103514A
Other languages
German (de)
French (fr)
Other versions
EP1840471B1 (en
EP1840471A2 (en
Inventor
Urs Benz
Thorsten Christoph Motzkus
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 Technology GmbH
Original Assignee
Alstom Technology AG
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 Alstom Technology AG filed Critical Alstom Technology AG
Priority to EP09155057.4A priority Critical patent/EP2077421B1/en
Publication of EP1840471A2 publication Critical patent/EP1840471A2/en
Publication of EP1840471A3 publication Critical patent/EP1840471A3/en
Application granted granted Critical
Publication of EP1840471B1 publication Critical patent/EP1840471B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)

Abstract

The device has a fuel mixture burned in a primary burner during formation of hot gases, which are supplied to a burner (1) for a secondary successive combustion, which is formed as a flow channel. A supporting structure is formed as a carrier plate unit (10). A hole (2) and fixing structures (5) are provided for opposite fixing. A recess is provided for the hole size in the flow channel wall. The carrier plate unit does not over lap the hole in the fixed position at the outer support (8). A collar is designed diametrically at the edge of opening.
EP07103514A 2006-03-31 2007-03-05 Device for fastening a sequentially operated burner in a gas turbine Active EP1840471B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP09155057.4A EP2077421B1 (en) 2006-03-31 2007-03-05 Device for fastening a sequentially operated burner in a gas turbine arrangement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102006015093 2006-03-31

Related Child Applications (2)

Application Number Title Priority Date Filing Date
EP09155057.4A Division EP2077421B1 (en) 2006-03-31 2007-03-05 Device for fastening a sequentially operated burner in a gas turbine arrangement
EP09155057.4 Division-Into 2009-03-12

Publications (3)

Publication Number Publication Date
EP1840471A2 EP1840471A2 (en) 2007-10-03
EP1840471A3 true EP1840471A3 (en) 2008-02-20
EP1840471B1 EP1840471B1 (en) 2011-07-27

Family

ID=38292665

Family Applications (2)

Application Number Title Priority Date Filing Date
EP09155057.4A Active EP2077421B1 (en) 2006-03-31 2007-03-05 Device for fastening a sequentially operated burner in a gas turbine arrangement
EP07103514A Active EP1840471B1 (en) 2006-03-31 2007-03-05 Device for fastening a sequentially operated burner in a gas turbine

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP09155057.4A Active EP2077421B1 (en) 2006-03-31 2007-03-05 Device for fastening a sequentially operated burner in a gas turbine arrangement

Country Status (4)

Country Link
US (1) US7937950B2 (en)
EP (2) EP2077421B1 (en)
AT (1) ATE518101T1 (en)
ES (2) ES2476916T3 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2116768B1 (en) * 2008-05-09 2016-07-27 Alstom Technology Ltd Burner
EP3029378B1 (en) * 2014-12-04 2019-08-28 Ansaldo Energia Switzerland AG Sequential burner for an axial gas turbine
EP3296638B1 (en) * 2016-09-20 2020-02-19 General Electric Technology GmbH Burner assembly and method for a burner of a gas turbine

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3147594A (en) * 1962-03-19 1964-09-08 Continental Aviat & Eng Corp Fuel injection device
EP0550126A1 (en) * 1992-01-02 1993-07-07 General Electric Company Thrust augmentor heat shield
DE4223733A1 (en) * 1992-07-18 1994-01-20 Gutehoffnungshuette Man Fastening for flame tube in gas turbine engine - accommodates thermal expansion and contraction with conical intermediate ring with outward-turned flange bolted to flange on attachment on flame tube
EP0616111A1 (en) * 1993-03-11 1994-09-21 ROLLS-ROYCE plc Gas turbine combustion chamber discharge support
EP0620362B1 (en) * 1993-04-08 1999-02-10 Asea Brown Boveri Ag Gasturbine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3565968A (en) 1967-07-31 1971-02-23 Ashland Oil Inc Cracking and recovery of hydrocarbons
FR2646880A1 (en) 1989-05-11 1990-11-16 Snecma THERMAL PROTECTION SHIRT FOR POST-COMBUSTION CHANNEL OR TRANSITION OF TURBOREACTOR
JPH0772616B2 (en) 1989-05-24 1995-08-02 株式会社日立製作所 Combustor and operating method thereof
US6339923B1 (en) * 1998-10-09 2002-01-22 General Electric Company Fuel air mixer for a radial dome in a gas turbine engine combustor
DE19948956A1 (en) 1999-10-11 2001-04-12 Asea Brown Boveri Mounting system for burner duct in gas turbine cylinder comprises internal groove in cylinder into which lugs on top and bottom retaining components fit, side pieces being fitted between retaining components and bolted into place
GB2432198B (en) * 2005-11-15 2007-10-03 Rolls Royce Plc Sealing arrangement

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3147594A (en) * 1962-03-19 1964-09-08 Continental Aviat & Eng Corp Fuel injection device
EP0550126A1 (en) * 1992-01-02 1993-07-07 General Electric Company Thrust augmentor heat shield
DE4223733A1 (en) * 1992-07-18 1994-01-20 Gutehoffnungshuette Man Fastening for flame tube in gas turbine engine - accommodates thermal expansion and contraction with conical intermediate ring with outward-turned flange bolted to flange on attachment on flame tube
EP0616111A1 (en) * 1993-03-11 1994-09-21 ROLLS-ROYCE plc Gas turbine combustion chamber discharge support
EP0620362B1 (en) * 1993-04-08 1999-02-10 Asea Brown Boveri Ag Gasturbine

Also Published As

Publication number Publication date
US20070227157A1 (en) 2007-10-04
EP2077421B1 (en) 2014-04-30
EP1840471B1 (en) 2011-07-27
EP2077421A3 (en) 2009-07-15
ES2369524T3 (en) 2011-12-01
EP2077421A2 (en) 2009-07-08
EP1840471A2 (en) 2007-10-03
ES2476916T3 (en) 2014-07-15
ATE518101T1 (en) 2011-08-15
US7937950B2 (en) 2011-05-10

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