DE69509793T2 - Schutzplatte mit vorspringendem rand - Google Patents

Schutzplatte mit vorspringendem rand

Info

Publication number
DE69509793T2
DE69509793T2 DE69509793T DE69509793T DE69509793T2 DE 69509793 T2 DE69509793 T2 DE 69509793T2 DE 69509793 T DE69509793 T DE 69509793T DE 69509793 T DE69509793 T DE 69509793T DE 69509793 T2 DE69509793 T2 DE 69509793T2
Authority
DE
Germany
Prior art keywords
protective plate
projecting edge
projecting
edge
protective
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 - Lifetime
Application number
DE69509793T
Other languages
English (en)
Other versions
DE69509793D1 (de
Inventor
Thomas Johnson
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.)
Raytheon Technologies 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 DE69509793D1 publication Critical patent/DE69509793D1/de
Application granted granted Critical
Publication of DE69509793T2 publication Critical patent/DE69509793T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Spray-Type Burners (AREA)
DE69509793T 1994-12-15 1995-11-30 Schutzplatte mit vorspringendem rand Expired - Lifetime DE69509793T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/356,088 US5581999A (en) 1994-12-15 1994-12-15 Bulkhead liner with raised lip
PCT/US1995/015412 WO1996018852A1 (en) 1994-12-15 1995-11-30 Bulkhead liner with raised lip

Publications (2)

Publication Number Publication Date
DE69509793D1 DE69509793D1 (de) 1999-06-24
DE69509793T2 true DE69509793T2 (de) 1999-12-23

Family

ID=23400079

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69509793T Expired - Lifetime DE69509793T2 (de) 1994-12-15 1995-11-30 Schutzplatte mit vorspringendem rand

Country Status (5)

Country Link
US (1) US5581999A (de)
EP (1) EP0797746B1 (de)
JP (1) JP3692145B2 (de)
DE (1) DE69509793T2 (de)
WO (1) WO1996018852A1 (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5974805A (en) * 1997-10-28 1999-11-02 Rolls-Royce Plc Heat shielding for a turbine combustor
US6351949B1 (en) 1999-09-03 2002-03-05 Allison Advanced Development Company Interchangeable combustor chute
US6499993B2 (en) * 2000-05-25 2002-12-31 General Electric Company External dilution air tuning for dry low NOX combustors and methods therefor
EP1400751A1 (de) * 2002-09-17 2004-03-24 Siemens Aktiengesellschaft Brennkammer für eine Gasturbine
US7384075B2 (en) * 2004-05-14 2008-06-10 Allison Advanced Development Company Threaded joint for gas turbine components
FR2897107B1 (fr) * 2006-02-09 2013-01-18 Snecma Paroi transversale de chambre de combustion munie de trous de multiperforation
US7721548B2 (en) 2006-11-17 2010-05-25 Pratt & Whitney Canada Corp. Combustor liner and heat shield assembly
US7681398B2 (en) 2006-11-17 2010-03-23 Pratt & Whitney Canada Corp. Combustor liner and heat shield assembly
US7748221B2 (en) 2006-11-17 2010-07-06 Pratt & Whitney Canada Corp. Combustor heat shield with variable cooling
FR2909748B1 (fr) 2006-12-07 2009-07-10 Snecma Sa Fond de chambre, procede de realisation de celui-ci, chambre de combustion le comportant et turboreacteur en etant equipe
US8590313B2 (en) * 2008-07-30 2013-11-26 Rolls-Royce Corporation Precision counter-swirl combustor
US9121609B2 (en) * 2008-10-14 2015-09-01 General Electric Company Method and apparatus for introducing diluent flow into a combustor
US20100089022A1 (en) * 2008-10-14 2010-04-15 General Electric Company Method and apparatus of fuel nozzle diluent introduction
US8567199B2 (en) * 2008-10-14 2013-10-29 General Electric Company Method and apparatus of introducing diluent flow into a combustor
US20100089020A1 (en) * 2008-10-14 2010-04-15 General Electric Company Metering of diluent flow in combustor
US8689563B2 (en) * 2009-07-13 2014-04-08 United Technologies Corporation Fuel nozzle guide plate mistake proofing
US9021675B2 (en) 2011-08-15 2015-05-05 United Technologies Corporation Method for repairing fuel nozzle guides for gas turbine engine combustors using cold metal transfer weld technology
US10041675B2 (en) 2014-06-04 2018-08-07 Pratt & Whitney Canada Corp. Multiple ventilated rails for sealing of combustor heat shields
EP2957833B1 (de) 2014-06-17 2018-10-24 Rolls-Royce Corporation Brennkammeranordnung mit rinnen
US9534785B2 (en) 2014-08-26 2017-01-03 Pratt & Whitney Canada Corp. Heat shield labyrinth seal
US10670272B2 (en) 2014-12-11 2020-06-02 Raytheon Technologies Corporation Fuel injector guide(s) for a turbine engine combustor
GB2543803B (en) * 2015-10-29 2019-10-30 Rolls Royce Plc A combustion chamber assembly
US10677465B2 (en) * 2017-05-16 2020-06-09 General Electric Company Combustor mounting assembly having a spring finger for forming a seal with a fuel injector assembly

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2107448B (en) * 1980-10-21 1984-06-06 Rolls Royce Gas turbine engine combustion chambers
GB2247522B (en) * 1990-09-01 1993-11-10 Rolls Royce Plc Gas turbine engine combustor
GB2257781B (en) * 1991-04-30 1995-04-12 Rolls Royce Plc Combustion chamber assembly in a gas turbine engine
GB9112324D0 (en) * 1991-06-07 1991-07-24 Rolls Royce Plc Gas turbine engine combustor
US5353599A (en) * 1993-04-29 1994-10-11 United Technologies Corporation Fuel nozzle swirler for combustors
US5419115A (en) * 1994-04-29 1995-05-30 United Technologies Corporation Bulkhead and fuel nozzle guide assembly for an annular combustion chamber

Also Published As

Publication number Publication date
EP0797746B1 (de) 1999-05-19
DE69509793D1 (de) 1999-06-24
US5581999A (en) 1996-12-10
EP0797746A1 (de) 1997-10-01
JP3692145B2 (ja) 2005-09-07
JPH10510910A (ja) 1998-10-20
WO1996018852A1 (en) 1996-06-20

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition