IT7828585A0 - Elemento di transizione raffreddato a liquido per turbina a gas e suo metodo di costruzione. - Google Patents

Elemento di transizione raffreddato a liquido per turbina a gas e suo metodo di costruzione.

Info

Publication number
IT7828585A0
IT7828585A0 IT7828585A IT2858578A IT7828585A0 IT 7828585 A0 IT7828585 A0 IT 7828585A0 IT 7828585 A IT7828585 A IT 7828585A IT 2858578 A IT2858578 A IT 2858578A IT 7828585 A0 IT7828585 A0 IT 7828585A0
Authority
IT
Italy
Prior art keywords
gas turbine
construction method
transition element
liquid cooled
cooled transition
Prior art date
Application number
IT7828585A
Other languages
English (en)
Other versions
IT1099282B (it
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT7828585A0 publication Critical patent/IT7828585A0/it
Application granted granted Critical
Publication of IT1099282B publication Critical patent/IT1099282B/it

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Compositions Of Oxide Ceramics (AREA)
IT28585/78A 1977-10-17 1978-10-10 Elemento di transizione raffreddato a liquido per turbina a gas e suo metodo di costruzione IT1099282B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/842,400 US4195474A (en) 1977-10-17 1977-10-17 Liquid-cooled transition member to turbine inlet

Publications (2)

Publication Number Publication Date
IT7828585A0 true IT7828585A0 (it) 1978-10-10
IT1099282B IT1099282B (it) 1985-09-18

Family

ID=25287208

Family Applications (1)

Application Number Title Priority Date Filing Date
IT28585/78A IT1099282B (it) 1977-10-17 1978-10-10 Elemento di transizione raffreddato a liquido per turbina a gas e suo metodo di costruzione

Country Status (8)

Country Link
US (1) US4195474A (it)
JP (1) JPS5471216A (it)
CA (1) CA1100769A (it)
DE (1) DE2844801A1 (it)
FR (1) FR2406077A1 (it)
IT (1) IT1099282B (it)
NL (1) NL7810323A (it)
NO (1) NO783498L (it)

Families Citing this family (54)

* Cited by examiner, † Cited by third party
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US4614083A (en) * 1984-04-06 1986-09-30 Agency Of Industrial Science & Technology Gas turbine
JPS62111131A (ja) * 1985-11-07 1987-05-22 Mitsubishi Heavy Ind Ltd 低カロリ−ガス焚ガスタ−ビン用燃焼器
DE4315256A1 (de) * 1993-05-07 1994-11-10 Mtu Muenchen Gmbh Einrichtung zur Verteilung sowie Zu- und Abführung eines Kühlmittels an einer Wand eines Turbo-, insbesondere Turbo-Staustrahltriebwerks
US5414999A (en) * 1993-11-05 1995-05-16 General Electric Company Integral aft frame mount for a gas turbine combustor transition piece
EP0718468B1 (en) * 1994-12-20 2001-10-31 General Electric Company Transition piece frame support
DE19643716A1 (de) * 1996-10-23 1998-04-30 Asea Brown Boveri Schaufelträger für einen Verdichter
JP3310900B2 (ja) * 1997-04-15 2002-08-05 三菱重工業株式会社 燃焼器尾筒の冷却構造
JP2002243154A (ja) * 2001-02-16 2002-08-28 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器尾筒出口構造及びガスタービン燃焼器
EP1270874B1 (de) * 2001-06-18 2005-08-31 Siemens Aktiengesellschaft Gasturbine mit einem Verdichter für Luft
EP1288441A1 (de) * 2001-09-03 2003-03-05 Siemens Aktiengesellschaft Übergangsabschnitt einer Gasturbinenbrennkammer
US6619915B1 (en) 2002-08-06 2003-09-16 Power Systems Mfg, Llc Thermally free aft frame for a transition duct
EP1398462A1 (de) * 2002-09-13 2004-03-17 Siemens Aktiengesellschaft Gasturbine sowie Übergangsbauteil
US6860108B2 (en) * 2003-01-22 2005-03-01 Mitsubishi Heavy Industries, Ltd. Gas turbine tail tube seal and gas turbine using the same
US6890148B2 (en) * 2003-08-28 2005-05-10 Siemens Westinghouse Power Corporation Transition duct cooling system
US7096668B2 (en) * 2003-12-22 2006-08-29 Martling Vincent C Cooling and sealing design for a gas turbine combustion system
US7310938B2 (en) * 2004-12-16 2007-12-25 Siemens Power Generation, Inc. Cooled gas turbine transition duct
US8015818B2 (en) * 2005-02-22 2011-09-13 Siemens Energy, Inc. Cooled transition duct for a gas turbine engine
JP4476152B2 (ja) * 2005-04-01 2010-06-09 三菱重工業株式会社 ガスタービン燃焼器
US7757492B2 (en) * 2007-05-18 2010-07-20 General Electric Company Method and apparatus to facilitate cooling turbine engines
JP4823186B2 (ja) * 2007-09-25 2011-11-24 三菱重工業株式会社 ガスタービン燃焼器
US8091365B2 (en) * 2008-08-12 2012-01-10 Siemens Energy, Inc. Canted outlet for transition in a gas turbine engine
US8549861B2 (en) * 2009-01-07 2013-10-08 General Electric Company Method and apparatus to enhance transition duct cooling in a gas turbine engine
WO2010087984A2 (en) * 2009-01-28 2010-08-05 Jonathan Feinstein Combined heat and power with a peak temperature heat load
US8402764B1 (en) * 2009-09-21 2013-03-26 Florida Turbine Technologies, Inc. Transition duct with spiral cooling channels
US8307654B1 (en) * 2009-09-21 2012-11-13 Florida Turbine Technologies, Inc. Transition duct with spiral finned cooling passage
EP2309099B1 (en) * 2009-09-30 2015-04-29 Siemens Aktiengesellschaft Transition duct
US9255484B2 (en) * 2011-03-16 2016-02-09 General Electric Company Aft frame and method for cooling aft frame
US9243506B2 (en) * 2012-01-03 2016-01-26 General Electric Company Methods and systems for cooling a transition nozzle
US20130269821A1 (en) * 2012-04-13 2013-10-17 General Electric Company Systems And Apparatuses For Hot Gas Flow In A Transition Piece
US9085981B2 (en) 2012-10-19 2015-07-21 Siemens Energy, Inc. Ducting arrangement for cooling a gas turbine structure
US9574498B2 (en) * 2013-09-25 2017-02-21 General Electric Company Internally cooled transition duct aft frame with serpentine cooling passage and conduit
KR101556532B1 (ko) * 2014-01-16 2015-10-01 두산중공업 주식회사 냉각슬리브를 포함하는 라이너, 플로우슬리브 및 가스터빈연소기
EP3221562B1 (en) * 2014-11-18 2019-01-16 Siemens Aktiengesellschaft Transition duct exit frame with insert
JP6399531B2 (ja) * 2015-02-24 2018-10-03 三菱日立パワーシステムズ株式会社 燃焼器用冷却パネル、これを備えるトランジションピース及び燃焼器、並びに燃焼器を備えるガスタービン
US10520193B2 (en) 2015-10-28 2019-12-31 General Electric Company Cooling patch for hot gas path components
US10605459B2 (en) 2016-03-25 2020-03-31 General Electric Company Integrated combustor nozzle for a segmented annular combustion system
US10584880B2 (en) 2016-03-25 2020-03-10 General Electric Company Mounting of integrated combustor nozzles in a segmented annular combustion system
US10641491B2 (en) 2016-03-25 2020-05-05 General Electric Company Cooling of integrated combustor nozzle of segmented annular combustion system
US11428413B2 (en) 2016-03-25 2022-08-30 General Electric Company Fuel injection module for segmented annular combustion system
US10584876B2 (en) 2016-03-25 2020-03-10 General Electric Company Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system
US10830442B2 (en) 2016-03-25 2020-11-10 General Electric Company Segmented annular combustion system with dual fuel capability
US11002190B2 (en) 2016-03-25 2021-05-11 General Electric Company Segmented annular combustion system
US10520194B2 (en) 2016-03-25 2019-12-31 General Electric Company Radially stacked fuel injection module for a segmented annular combustion system
US10563869B2 (en) 2016-03-25 2020-02-18 General Electric Company Operation and turndown of a segmented annular combustion system
US11156362B2 (en) 2016-11-28 2021-10-26 General Electric Company Combustor with axially staged fuel injection
US10690350B2 (en) 2016-11-28 2020-06-23 General Electric Company Combustor with axially staged fuel injection
JP6345331B1 (ja) 2017-11-20 2018-06-20 三菱日立パワーシステムズ株式会社 ガスタービンの燃焼筒及び燃焼器並びにガスタービン
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1525682A (en) * 1923-01-22 1925-02-10 Thomas K Lowry Device for extracting or transmitting heat
US1798160A (en) * 1927-12-08 1931-03-31 Holzwarth Gas Turbine Co Multistage combustion turbine
US2479573A (en) * 1943-10-20 1949-08-23 Gen Electric Gas turbine power plant
CH304143A (de) * 1950-05-09 1954-12-31 Maschf Augsburg Nuernberg Ag Verfahren zum Betrieb einer Gasturbinenanlage und Einrichtung zur Durchführung des Verfahrens.
US2992529A (en) * 1956-08-23 1961-07-18 Thompson Ramo Wooldridge Inc Turbine blade cooling
US3490747A (en) * 1967-11-29 1970-01-20 Westinghouse Electric Corp Temperature profiling means for turbine inlet
DE1951356C3 (de) * 1969-10-11 1980-08-28 Mtu Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Gasturbinentriebwerk für Flugzeuge
FR2092897A1 (en) * 1970-06-29 1972-01-28 Houlbert Rene Heat exchanger - with increased efficiency from deflector rings on wall of inner vessel
US3652181A (en) * 1970-11-23 1972-03-28 Carl F Wilhelm Jr Cooling sleeve for gas turbine combustor transition member
US3736747A (en) * 1971-07-09 1973-06-05 G Warren Combustor
US3849983A (en) * 1972-11-20 1974-11-26 Rockwell International Corp Propellant liner for active cooling

Also Published As

Publication number Publication date
NO783498L (no) 1979-04-18
JPS5471216A (en) 1979-06-07
IT1099282B (it) 1985-09-18
CA1100769A (en) 1981-05-12
DE2844801A1 (de) 1979-04-19
NL7810323A (nl) 1979-04-19
FR2406077A1 (fr) 1979-05-11
US4195474A (en) 1980-04-01

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