FR2309724A2 - Procede et appareillage d'obtention d'une combustion entretenue dans une turbine a gaz - Google Patents

Procede et appareillage d'obtention d'une combustion entretenue dans une turbine a gaz

Info

Publication number
FR2309724A2
FR2309724A2 FR7532904A FR7532904A FR2309724A2 FR 2309724 A2 FR2309724 A2 FR 2309724A2 FR 7532904 A FR7532904 A FR 7532904A FR 7532904 A FR7532904 A FR 7532904A FR 2309724 A2 FR2309724 A2 FR 2309724A2
Authority
FR
France
Prior art keywords
gas turbine
sustained combustion
obtaining sustained
obtaining
combustion
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.)
Granted
Application number
FR7532904A
Other languages
English (en)
French (fr)
Other versions
FR2309724B2 (enrdf_load_stackoverflow
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.)
Engelhard Minerals and Chemicals Corp
Original Assignee
Engelhard Minerals and Chemicals 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
Priority claimed from US05/519,288 external-priority patent/US3975900A/en
Application filed by Engelhard Minerals and Chemicals Corp filed Critical Engelhard Minerals and Chemicals Corp
Publication of FR2309724A2 publication Critical patent/FR2309724A2/fr
Application granted granted Critical
Publication of FR2309724B2 publication Critical patent/FR2309724B2/fr
Granted 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26—Controlling the air flow
    • 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
    • F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]
    • 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
    • Y02T50/678—Aviation using fuels of non-fossil origin

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
FR7532904A 1974-10-30 1975-10-28 Procede et appareillage d'obtention d'une combustion entretenue dans une turbine a gaz Granted FR2309724A2 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/519,288 US3975900A (en) 1972-02-18 1974-10-30 Method and apparatus for turbine system combustor temperature

Publications (2)

Publication Number Publication Date
FR2309724A2 true FR2309724A2 (fr) 1976-11-26
FR2309724B2 FR2309724B2 (enrdf_load_stackoverflow) 1980-04-30

Family

ID=24067660

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7532904A Granted FR2309724A2 (fr) 1974-10-30 1975-10-28 Procede et appareillage d'obtention d'une combustion entretenue dans une turbine a gaz

Country Status (7)

Country Link
JP (1) JPS5198415A (enrdf_load_stackoverflow)
AU (1) AU502658B2 (enrdf_load_stackoverflow)
BE (1) BE835078R (enrdf_load_stackoverflow)
DE (1) DE2548680A1 (enrdf_load_stackoverflow)
FR (1) FR2309724A2 (enrdf_load_stackoverflow)
GB (1) GB1532793A (enrdf_load_stackoverflow)
IT (1) IT1048355B (enrdf_load_stackoverflow)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4930454A (en) * 1981-08-14 1990-06-05 Dresser Industries, Inc. Steam generating system
JPS5923034A (ja) * 1982-07-29 1984-02-06 Osaka Gas Co Ltd 高圧熱風発生装置の起動装置
US4918915A (en) * 1987-09-21 1990-04-24 Pfefferle William C Method for clean incineration of wastes
US6357216B1 (en) * 2000-09-27 2002-03-19 Honeywell International, Inc. Flashback control for a gas turbine engine combustor having an air bypass system

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2651175A (en) * 1946-09-11 1953-09-08 Rolls Royce Controlling combustion system of gas-turbine engines
US3584459A (en) * 1968-09-12 1971-06-15 Gen Motors Corp Gas turbine engine with combustion chamber bypass for fuel-air ratio control and turbine cooling
FR2139363A5 (enrdf_load_stackoverflow) * 1971-05-13 1973-01-05 Engelhard Min & Chem
FR2172964A1 (enrdf_load_stackoverflow) * 1972-02-26 1973-10-05 Degussa

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2651175A (en) * 1946-09-11 1953-09-08 Rolls Royce Controlling combustion system of gas-turbine engines
US3584459A (en) * 1968-09-12 1971-06-15 Gen Motors Corp Gas turbine engine with combustion chamber bypass for fuel-air ratio control and turbine cooling
FR2139363A5 (enrdf_load_stackoverflow) * 1971-05-13 1973-01-05 Engelhard Min & Chem
FR2172964A1 (enrdf_load_stackoverflow) * 1972-02-26 1973-10-05 Degussa

Also Published As

Publication number Publication date
AU502658B2 (en) 1979-08-02
GB1532793A (en) 1978-11-22
AU8618775A (en) 1977-05-05
JPS5198415A (enrdf_load_stackoverflow) 1976-08-30
IT1048355B (it) 1980-11-20
FR2309724B2 (enrdf_load_stackoverflow) 1980-04-30
DE2548680A1 (de) 1976-05-06
BE835078R (fr) 1976-04-30

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