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BR8106793A - TRANSITION DUCT FOR A COMBUSTION TURBINE - Google Patents

TRANSITION DUCT FOR A COMBUSTION TURBINE

Info

Publication number
BR8106793A
BR8106793A BR8106793A BR8106793A BR8106793A BR 8106793 A BR8106793 A BR 8106793A BR 8106793 A BR8106793 A BR 8106793A BR 8106793 A BR8106793 A BR 8106793A BR 8106793 A BR8106793 A BR 8106793A
Authority
BR
Brazil
Prior art keywords
combustion turbine
transition duct
duct
transition
turbine
Prior art date
Application number
BR8106793A
Other languages
Portuguese (pt)
Inventor
Sterling F Arlington
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 BR8106793A publication Critical patent/BR8106793A/en

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
    • 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
    • F23R3/002—Wall structures
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BR8106793A 1980-11-06 1981-10-22 TRANSITION DUCT FOR A COMBUSTION TURBINE BR8106793A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
BR8106793A true BR8106793A (en) 1982-07-06

Family

ID=22757890

Family Applications (1)

Application Number Title Priority Date Filing Date
BR8106793A BR8106793A (en) 1980-11-06 1981-10-22 TRANSITION DUCT FOR A COMBUSTION TURBINE

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)

Families Citing this family (7)

* 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
US8015818B2 (en) 2005-02-22 2011-09-13 Siemens Energy, Inc. Cooled transition duct for a gas turbine engine
JP2010085052A (en) * 2008-10-01 2010-04-15 Mitsubishi Heavy Ind Ltd Combustor tail pipe, designing method therefor, and gas turbine

Also Published As

Publication number Publication date
CA1183695A (en) 1985-03-12
AR225977A1 (en) 1982-05-14
GB2087066B (en) 1984-09-19
JPS6027816B2 (en) 1985-07-01
MX154157A (en) 1987-05-27
GB2087066A (en) 1982-05-19
IT1142046B (en) 1986-10-08
IT8124871A0 (en) 1981-11-05
JPS57113923A (en) 1982-07-15
BE891023A (en) 1982-05-06

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