AR225977A1 - Ducto de transicion para turbina de combustion - Google Patents

Ducto de transicion para turbina de combustion

Info

Publication number
AR225977A1
AR225977A1 AR287296A AR28729681A AR225977A1 AR 225977 A1 AR225977 A1 AR 225977A1 AR 287296 A AR287296 A AR 287296A AR 28729681 A AR28729681 A AR 28729681A AR 225977 A1 AR225977 A1 AR 225977A1
Authority
AR
Argentina
Prior art keywords
combustion turbine
transition duct
duct
transition
turbine
Prior art date
Application number
AR287296A
Other languages
English (en)
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
Application granted granted Critical
Publication of AR225977A1 publication Critical patent/AR225977A1/es

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)
AR287296A 1980-11-06 1981-10-30 Ducto de transicion para turbina de combustion AR225977A1 (es)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
AR225977A1 true AR225977A1 (es) 1982-05-14

Family

ID=22757890

Family Applications (1)

Application Number Title Priority Date Filing Date
AR287296A AR225977A1 (es) 1980-11-06 1981-10-30 Ducto de transicion para turbina de combustion

Country Status (8)

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

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
GB2087066A (en) 1982-05-19
MX154157A (es) 1987-05-27
JPS6027816B2 (ja) 1985-07-01
IT1142046B (it) 1986-10-08
IT8124871A0 (it) 1981-11-05
BE891023A (fr) 1982-05-06
GB2087066B (en) 1984-09-19
BR8106793A (pt) 1982-07-06
JPS57113923A (en) 1982-07-15
CA1183695A (en) 1985-03-12

Similar Documents

Publication Publication Date Title
BR8004198A (pt) Pa de turbina refrigerada
BR8101054A (pt) Turbina centripeta
DK142282A (da) Vindmotor
IT1151036B (it) Turbina particolarmente per turbocompressori
FR2451453B1 (fr) Ailette de turbine
BE78T1 (fr) Turbomachine
ES498630A0 (es) Rotor ceramico para turbina de gas
JPS5612019A (en) Vane assembly for combustion turbine
ES501205A0 (es) Turbina enturbada
AR225977A1 (es) Ducto de transicion para turbina de combustion
SE8005285L (sv) Transmission for vindmotorer
DE2966663D1 (de) Turbomachine
AR230756A1 (es) Turbina de combustion
NO812892L (no) Luftturbingenerator.
DK5584A (da) Turbine
BR8203361A (pt) Combustor para turbina de combustao
BR7902134A (pt) Conjunto de valvulas para turbinas
BR8203784A (pt) Combustor para sistema de turbina de combustao
NO156579C (no) Overladet forbrenningsmotor.
MX156590A (es) Mejoras en camara de combustion para turbina
DK511280A (da) Gasturbinemotor
SU898792A1 (ru) Система регулирования газотурбинного двигателя
SU702755A1 (ru) Система автоматического регулирования газотурбинного двигателя
SU666935A1 (ru) Система автоматического регулирования газотурбинного двигателя
BR7908227A (pt) Turbina aeolica