IT7827400A0 - COOLED AIR INLET PIPE FOR AN AGAS TURBINE COMBUSTOR. - Google Patents

COOLED AIR INLET PIPE FOR AN AGAS TURBINE COMBUSTOR.

Info

Publication number
IT7827400A0
IT7827400A0 IT7827400A IT2740078A IT7827400A0 IT 7827400 A0 IT7827400 A0 IT 7827400A0 IT 7827400 A IT7827400 A IT 7827400A IT 2740078 A IT2740078 A IT 2740078A IT 7827400 A0 IT7827400 A0 IT 7827400A0
Authority
IT
Italy
Prior art keywords
air inlet
inlet pipe
cooled air
turbine combustor
agas
Prior art date
Application number
IT7827400A
Other languages
Italian (it)
Other versions
IT1098811B (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
Publication of IT7827400A0 publication Critical patent/IT7827400A0/en
Application granted granted Critical
Publication of IT1098811B publication Critical patent/IT1098811B/en

Links

Classifications

    • 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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/045Air inlet arrangements using pipes
    • 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
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00002Gas turbine combustors adapted for fuels having low heating value [LHV]
IT27400/78A 1977-09-09 1978-09-07 AIR INLET PIPE COOLED FOR A GAS TURBINE COMBUSTER IT1098811B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US83172177A 1977-09-09 1977-09-09

Publications (2)

Publication Number Publication Date
IT7827400A0 true IT7827400A0 (en) 1978-09-07
IT1098811B IT1098811B (en) 1985-09-18

Family

ID=25259715

Family Applications (1)

Application Number Title Priority Date Filing Date
IT27400/78A IT1098811B (en) 1977-09-09 1978-09-07 AIR INLET PIPE COOLED FOR A GAS TURBINE COMBUSTER

Country Status (6)

Country Link
JP (1) JPS5450717A (en)
AR (1) AR213702A1 (en)
BE (1) BE870333A (en)
CA (1) CA1116417A (en)
GB (1) GB2003989A (en)
IT (1) IT1098811B (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4875339A (en) * 1987-11-27 1989-10-24 General Electric Company Combustion chamber liner insert
US4887432A (en) * 1988-10-07 1989-12-19 Westinghouse Electric Corp. Gas turbine combustion chamber with air scoops
US5454221A (en) * 1994-03-14 1995-10-03 General Electric Company Dilution flow sleeve for reducing emissions in a gas turbine combustor
US6499993B2 (en) 2000-05-25 2002-12-31 General Electric Company External dilution air tuning for dry low NOX combustors and methods therefor
US6331110B1 (en) * 2000-05-25 2001-12-18 General Electric Company External dilution air tuning for dry low NOx combustors and methods therefor
GB2399408B (en) 2003-03-14 2006-02-22 Rolls Royce Plc Gas turbine engine combustor
GB2431225B (en) 2005-10-15 2008-06-18 Rolls Royce Plc Combustor and component for a combustor
FR3019587B1 (en) * 2014-04-03 2019-09-13 Safran Helicopter Engines DILUTION PIPE FOR COMBUSTION CHAMBER AND ASSOCIATED COMBUSTION CHAMBER.
EP2993404B1 (en) 2014-09-08 2019-03-13 Ansaldo Energia Switzerland AG Dilution gas or air mixer for a combustor of a gas turbine
DE102016207066A1 (en) * 2016-04-26 2017-10-26 Rolls-Royce Deutschland Ltd & Co Kg Combustor shingle of a gas turbine
CN114165811B (en) * 2021-10-20 2023-03-21 中国航发四川燃气涡轮研究院 Jet sleeve with cooling structure

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS524908B1 (en) * 1969-12-24 1977-02-08

Also Published As

Publication number Publication date
CA1116417A (en) 1982-01-19
IT1098811B (en) 1985-09-18
GB2003989A (en) 1979-03-21
AR213702A1 (en) 1979-02-28
JPS5450717A (en) 1979-04-20
BE870333A (en) 1979-03-08

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