IT8124871A0 - Condotto di passaggio raffreddato efficacemente per una grande turbina a combustione per impianti. - Google Patents

Condotto di passaggio raffreddato efficacemente per una grande turbina a combustione per impianti.

Info

Publication number
IT8124871A0
IT8124871A0 IT8124871A IT2487181A IT8124871A0 IT 8124871 A0 IT8124871 A0 IT 8124871A0 IT 8124871 A IT8124871 A IT 8124871A IT 2487181 A IT2487181 A IT 2487181A IT 8124871 A0 IT8124871 A0 IT 8124871A0
Authority
IT
Italy
Prior art keywords
plants
combustion turbine
effectively cooled
large combustion
cooled connector
Prior art date
Application number
IT8124871A
Other languages
English (en)
Other versions
IT1142046B (it
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 IT8124871A0 publication Critical patent/IT8124871A0/it
Application granted granted Critical
Publication of IT1142046B publication Critical patent/IT1142046B/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
    • 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)
IT24871/81A 1980-11-06 1981-11-05 Condotto di passaggio raffreddato efficacemente per una grande turbina a combustione per impianti IT1142046B (it)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
IT8124871A0 true IT8124871A0 (it) 1981-11-05
IT1142046B IT1142046B (it) 1986-10-08

Family

ID=22757890

Family Applications (1)

Application Number Title Priority Date Filing Date
IT24871/81A IT1142046B (it) 1980-11-06 1981-11-05 Condotto di passaggio raffreddato efficacemente per una grande turbina a combustione per impianti

Country Status (8)

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

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0752014B2 (ja) * 1986-03-20 1995-06-05 株式会社日立製作所 ガスタ−ビン燃焼器
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 (ja) * 2008-10-01 2010-04-15 Mitsubishi Heavy Ind Ltd 燃焼器尾筒およびその設計方法ならびにガスタービン

Also Published As

Publication number Publication date
BR8106793A (pt) 1982-07-06
GB2087066B (en) 1984-09-19
GB2087066A (en) 1982-05-19
AR225977A1 (es) 1982-05-14
BE891023A (fr) 1982-05-06
IT1142046B (it) 1986-10-08
JPS6027816B2 (ja) 1985-07-01
JPS57113923A (en) 1982-07-15
CA1183695A (en) 1985-03-12
MX154157A (es) 1987-05-27

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19931119