CA964072A - Gas turbine combustors and method of operation - Google Patents

Gas turbine combustors and method of operation

Info

Publication number
CA964072A
CA964072A CA157,092A CA157092A CA964072A CA 964072 A CA964072 A CA 964072A CA 157092 A CA157092 A CA 157092A CA 964072 A CA964072 A CA 964072A
Authority
CA
Canada
Prior art keywords
gas turbine
turbine combustors
combustors
gas
turbine
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.)
Expired
Application number
CA157,092A
Other versions
CA157092S (en
Inventor
Harold T. Quigg
Robert M. Schirmer
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.)
Phillips Petroleum Co
Original Assignee
Phillips Petroleum Co
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 Phillips Petroleum Co filed Critical Phillips Petroleum Co
Priority to CA209,737A priority Critical patent/CA971373A/en
Application granted granted Critical
Publication of CA964072A publication Critical patent/CA964072A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/005—Combined with pressure or heat exchangers
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Of Fluid Fuel (AREA)
CA157,092A 1971-12-15 1972-11-21 Gas turbine combustors and method of operation Expired CA964072A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA209,737A CA971373A (en) 1971-12-15 1974-09-23 Gas turbine combustors

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US20810271A 1971-12-15 1971-12-15
US00238317A US3826077A (en) 1971-12-15 1972-03-27 Method of introducing three streams of air into a combustor with selective heating

Publications (1)

Publication Number Publication Date
CA964072A true CA964072A (en) 1975-03-11

Family

ID=26902905

Family Applications (1)

Application Number Title Priority Date Filing Date
CA157,092A Expired CA964072A (en) 1971-12-15 1972-11-21 Gas turbine combustors and method of operation

Country Status (10)

Country Link
US (1) US3826077A (en)
JP (1) JPS512563B2 (en)
CA (1) CA964072A (en)
CH (1) CH564733A5 (en)
DE (1) DE2261596B2 (en)
ES (1) ES409277A1 (en)
FR (1) FR2197449A5 (en)
GB (1) GB1410990A (en)
IT (1) IT971654B (en)
SE (1) SE409360B (en)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3939653A (en) * 1974-03-29 1976-02-24 Phillips Petroleum Company Gas turbine combustors and method of operation
US4012902A (en) * 1974-03-29 1977-03-22 Phillips Petroleum Company Method of operating a gas turbine combustor having an independent airstream to remove heat from the primary combustion zone
US4021186A (en) * 1974-06-19 1977-05-03 Exxon Research And Engineering Company Method and apparatus for reducing NOx from furnaces
GB1490145A (en) * 1974-09-11 1977-10-26 Mtu Muenchen Gmbh Gas turbine engine
US4067681A (en) * 1975-03-10 1978-01-10 Columbia Gas System Service Corporation Gas-fired smooth top range
US4138842A (en) * 1975-11-05 1979-02-13 Zwick Eugene B Low emission combustion apparatus
EP0007424B1 (en) * 1978-06-28 1982-11-24 Smit Ovens Nijmegen B.V. Burner device for combustion of liquid fuel
US4427362A (en) * 1980-08-14 1984-01-24 Rockwell International Corporation Combustion method
JPS5829234U (en) * 1981-08-24 1983-02-25 株式会社クボタ Structure of handling torso
US4720970A (en) * 1982-11-05 1988-01-26 The United States Of America As Represented By The Secretary Of The Air Force Sector airflow variable geometry combustor
JPS60131136U (en) * 1984-02-10 1985-09-02 三菱農機株式会社 Threshing machine handling barrel
US4958488A (en) * 1989-04-17 1990-09-25 General Motors Corporation Combustion system
US6071115A (en) * 1994-03-11 2000-06-06 Gas Research Institute Apparatus for low NOx, rapid mix combustion
US5681159A (en) * 1994-03-11 1997-10-28 Gas Research Institute Process and apparatus for low NOx staged-air combustion
DE102006011727B3 (en) * 2006-03-14 2007-11-22 Webasto Ag Combined heating / hot water system for mobile applications
US9239165B2 (en) * 2012-06-07 2016-01-19 United Technologies Corporation Combustor liner with convergent cooling channel
KR102377720B1 (en) * 2019-04-10 2022-03-23 두산중공업 주식회사 Liner cooling structure with improved pressure losses and combustor for gas turbine having the same

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH417906A (en) * 1963-02-28 1966-07-31 Ghelfi Salvatore Hot gas generator that can be operated with injectable fuel
US3360929A (en) * 1966-03-10 1968-01-02 Montrose K. Drewry Gas turbine combustors
US3705492A (en) * 1971-01-11 1972-12-12 Gen Motors Corp Regenerative gas turbine system

Also Published As

Publication number Publication date
GB1410990A (en) 1975-10-22
SE409360B (en) 1979-08-13
DE2261596A1 (en) 1973-06-28
DE2261596B2 (en) 1979-07-19
CH564733A5 (en) 1975-07-31
ES409277A1 (en) 1976-03-16
US3826077A (en) 1974-07-30
DE2261596C3 (en) 1980-03-13
JPS4865314A (en) 1973-09-08
FR2197449A5 (en) 1974-03-22
JPS512563B2 (en) 1976-01-27
IT971654B (en) 1974-05-10

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