DE69109648D1 - Integriertes Verbinder- und Luftrohr für eine Brennkammer einer Gasturbine. - Google Patents

Integriertes Verbinder- und Luftrohr für eine Brennkammer einer Gasturbine.

Info

Publication number
DE69109648D1
DE69109648D1 DE69109648T DE69109648T DE69109648D1 DE 69109648 D1 DE69109648 D1 DE 69109648D1 DE 69109648 T DE69109648 T DE 69109648T DE 69109648 T DE69109648 T DE 69109648T DE 69109648 D1 DE69109648 D1 DE 69109648D1
Authority
DE
Germany
Prior art keywords
combustion chamber
gas turbine
air pipe
integrated connector
connector
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
DE69109648T
Other languages
English (en)
Other versions
DE69109648T2 (de
Inventor
Edward C Able
Martin J Gibler
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 DE69109648D1 publication Critical patent/DE69109648D1/de
Application granted granted Critical
Publication of DE69109648T2 publication Critical patent/DE69109648T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F23R3/045—Air inlet arrangements using pipes
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
DE69109648T 1990-12-24 1991-12-19 Integriertes Verbinder- und Luftrohr für eine Brennkammer einer Gasturbine. Expired - Fee Related DE69109648T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/632,849 US5144793A (en) 1990-12-24 1990-12-24 Integrated connector/airtube for a turbomachine's combustion chamber walls

Publications (2)

Publication Number Publication Date
DE69109648D1 true DE69109648D1 (de) 1995-06-14
DE69109648T2 DE69109648T2 (de) 1995-09-14

Family

ID=24537203

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69109648T Expired - Fee Related DE69109648T2 (de) 1990-12-24 1991-12-19 Integriertes Verbinder- und Luftrohr für eine Brennkammer einer Gasturbine.

Country Status (4)

Country Link
US (1) US5144793A (de)
EP (1) EP0493304B1 (de)
JP (1) JP3150738B2 (de)
DE (1) DE69109648T2 (de)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2708086B1 (fr) * 1993-06-30 1995-09-01 Snecma Structure tubulaire sectorisée travaillant à l'implosion.
US5704208A (en) * 1995-12-05 1998-01-06 Brewer; Keith S. Serviceable liner for gas turbine engine
US6018950A (en) * 1997-06-13 2000-02-01 Siemens Westinghouse Power Corporation Combustion turbine modular cooling panel
US6438958B1 (en) * 2000-02-28 2002-08-27 General Electric Company Apparatus for reducing heat load in combustor panels
DE10303088B4 (de) * 2002-02-09 2015-08-20 Alstom Technology Ltd. Abgasgehäuse einer Wärmekraftmaschine
US6875476B2 (en) 2003-01-15 2005-04-05 General Electric Company Methods and apparatus for manufacturing turbine engine components
US7017334B2 (en) 2003-12-18 2006-03-28 United Technologies Corporation Compact fastening collar and stud for connecting walls of a nozzle liner and method associated therewith
US7140185B2 (en) * 2004-07-12 2006-11-28 United Technologies Corporation Heatshielded article
US8800298B2 (en) * 2009-07-17 2014-08-12 United Technologies Corporation Washer with cooling passage for a turbine engine combustor
US8979477B2 (en) * 2011-03-09 2015-03-17 General Electric Company System for cooling and purging exhaust section of gas turbine engine
US9534783B2 (en) * 2011-07-21 2017-01-03 United Technologies Corporation Insert adjacent to a heat shield element for a gas turbine engine combustor
JP5910008B2 (ja) * 2011-11-11 2016-04-27 株式会社Ihi 燃焼器ライナ
US9297307B2 (en) 2012-09-28 2016-03-29 United Technologies Corporation Power cable and connector arrangement for a gas turbine engine
DE102012022259A1 (de) * 2012-11-13 2014-05-28 Rolls-Royce Deutschland Ltd & Co Kg Brennkammerschindel einer Gasturbine sowie Verfahren zu deren Herstellung
DE102012023297A1 (de) 2012-11-28 2014-06-12 Rolls-Royce Deutschland Ltd & Co Kg Schindelbefestigungsanordnung einer Gasturbinenbrennkammer
US20140174091A1 (en) * 2012-12-21 2014-06-26 United Technologies Corporation Repair procedure for a gas turbine engine via variable polarity welding
US10112557B2 (en) * 2014-04-03 2018-10-30 United Technologies Corporation Thermally compliant grommet assembly
US10788212B2 (en) * 2015-01-12 2020-09-29 General Electric Company System and method for an oxidant passageway in a gas turbine system with exhaust gas recirculation
US10935240B2 (en) * 2015-04-23 2021-03-02 Raytheon Technologies Corporation Additive manufactured combustor heat shield
US10927555B2 (en) * 2017-05-20 2021-02-23 Interstitial Systems Inc. Method for improving the ventilation effectiveness of large conditioned air plenum environments including such environments in multilevel raised floor electro-mechanical distribution systems
JP2024091023A (ja) * 2022-12-23 2024-07-04 川崎重工業株式会社 ガスタービンの燃焼器

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2609040A (en) * 1950-03-14 1952-09-02 Elliott Co Combustion apparatus using compressed air
GB1059199A (en) * 1965-10-20 1967-02-15 Rolls Royce Flame tube
US4302941A (en) * 1980-04-02 1981-12-01 United Technologies Corporation Combuster liner construction for gas turbine engine
US4422300A (en) * 1981-12-14 1983-12-27 United Technologies Corporation Prestressed combustor liner for gas turbine engine
CA1231240A (en) * 1983-08-26 1988-01-12 Westinghouse Electric Corporation Varying thickness thermal barrier for combustion turbine baskets
US4748806A (en) * 1985-07-03 1988-06-07 United Technologies Corporation Attachment means
DE3535443C1 (de) * 1985-10-04 1986-11-20 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Brennkammer fuer ein Gasturbinentriebwerk,insbesondere Ringbrennkammer,mit mindestes einer Luftzufuhrbuchse
FR2599821B1 (fr) * 1986-06-04 1988-09-02 Snecma Chambre de combustion pour turbomachines a orifices de melange assurant le positionnement de la paroi chaude sur la paroi froide

Also Published As

Publication number Publication date
JPH04278119A (ja) 1992-10-02
EP0493304A1 (de) 1992-07-01
EP0493304B1 (de) 1995-05-10
JP3150738B2 (ja) 2001-03-26
US5144793A (en) 1992-09-08
DE69109648T2 (de) 1995-09-14

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee