JPS57113923A - Intermediate duct for combustion turbine - Google Patents

Intermediate duct for combustion turbine

Info

Publication number
JPS57113923A
JPS57113923A JP56177265A JP17726581A JPS57113923A JP S57113923 A JPS57113923 A JP S57113923A JP 56177265 A JP56177265 A JP 56177265A JP 17726581 A JP17726581 A JP 17726581A JP S57113923 A JPS57113923 A JP S57113923A
Authority
JP
Japan
Prior art keywords
combustion turbine
intermediate duct
duct
turbine
combustion
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
JP56177265A
Other languages
Japanese (ja)
Other versions
JPS6027816B2 (en
Inventor
Furederitsuku Aarin Sutaaringu
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.)
CBS Corp
Original Assignee
Westinghouse Electric 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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of JPS57113923A publication Critical patent/JPS57113923A/en
Publication of JPS6027816B2 publication Critical patent/JPS6027816B2/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
    • F23R3/002Wall structures
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
JP56177265A 1980-11-06 1981-11-06 Combustion turbine intermediate duct Expired JPS6027816B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US20444180A 1980-11-06 1980-11-06
US204441 1980-11-06

Publications (2)

Publication Number Publication Date
JPS57113923A true JPS57113923A (en) 1982-07-15
JPS6027816B2 JPS6027816B2 (en) 1985-07-01

Family

ID=22757890

Family Applications (1)

Application Number Title Priority Date Filing Date
JP56177265A Expired JPS6027816B2 (en) 1980-11-06 1981-11-06 Combustion turbine intermediate duct

Country Status (8)

Country Link
JP (1) JPS6027816B2 (en)
AR (1) AR225977A1 (en)
BE (1) BE891023A (en)
BR (1) BR8106793A (en)
CA (1) CA1183695A (en)
GB (1) GB2087066B (en)
IT (1) IT1142046B (en)
MX (1) MX154157A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008531961A (en) * 2005-02-22 2008-08-14 シーメンス パワー ジェネレイション インコーポレイテッド Cooling transition duct for gas turbine engines

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0752014B2 (en) * 1986-03-20 1995-06-05 株式会社日立製作所 Gas turbine combustor
US6018950A (en) * 1997-06-13 2000-02-01 Siemens Westinghouse Power Corporation Combustion turbine modular cooling panel
CA2288557C (en) * 1998-11-12 2007-02-06 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor cooling structure
US6412268B1 (en) * 2000-04-06 2002-07-02 General Electric Company Cooling air recycling for gas turbine transition duct end frame and related method
US7310938B2 (en) * 2004-12-16 2007-12-25 Siemens Power Generation, Inc. Cooled gas turbine transition duct
JP2010085052A (en) * 2008-10-01 2010-04-15 Mitsubishi Heavy Ind Ltd Combustor tail pipe, designing method therefor, and gas turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008531961A (en) * 2005-02-22 2008-08-14 シーメンス パワー ジェネレイション インコーポレイテッド Cooling transition duct for gas turbine engines

Also Published As

Publication number Publication date
BE891023A (en) 1982-05-06
MX154157A (en) 1987-05-27
AR225977A1 (en) 1982-05-14
IT1142046B (en) 1986-10-08
IT8124871A0 (en) 1981-11-05
CA1183695A (en) 1985-03-12
BR8106793A (en) 1982-07-06
JPS6027816B2 (en) 1985-07-01
GB2087066B (en) 1984-09-19
GB2087066A (en) 1982-05-19

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