IT1048355B - THERMODYNAMIC PROCEDURE FOR GENERATING COMBUSTION PRODUCTS OF HIGH THERMAL ENERGY AND PRODUCING MECHANICAL ENERGY FROM THEM IN A GAS TURBINE AND RELATED TURBINE PLANT - Google Patents

THERMODYNAMIC PROCEDURE FOR GENERATING COMBUSTION PRODUCTS OF HIGH THERMAL ENERGY AND PRODUCING MECHANICAL ENERGY FROM THEM IN A GAS TURBINE AND RELATED TURBINE PLANT

Info

Publication number
IT1048355B
IT1048355B IT51955/75A IT5195575A IT1048355B IT 1048355 B IT1048355 B IT 1048355B IT 51955/75 A IT51955/75 A IT 51955/75A IT 5195575 A IT5195575 A IT 5195575A IT 1048355 B IT1048355 B IT 1048355B
Authority
IT
Italy
Prior art keywords
high thermal
combustion products
gas turbine
producing mechanical
generating combustion
Prior art date
Application number
IT51955/75A
Other languages
Italian (it)
Original Assignee
Engelhard Min & Chem
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 Min & Chem filed Critical Engelhard Min & Chem
Application granted granted Critical
Publication of IT1048355B publication Critical patent/IT1048355B/en

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
IT51955/75A 1974-10-30 1975-10-28 THERMODYNAMIC PROCEDURE FOR GENERATING COMBUSTION PRODUCTS OF HIGH THERMAL ENERGY AND PRODUCING MECHANICAL ENERGY FROM THEM IN A GAS TURBINE AND RELATED TURBINE PLANT IT1048355B (en)

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 (1)

Publication Number Publication Date
IT1048355B true IT1048355B (en) 1980-11-20

Family

ID=24067660

Family Applications (1)

Application Number Title Priority Date Filing Date
IT51955/75A IT1048355B (en) 1974-10-30 1975-10-28 THERMODYNAMIC PROCEDURE FOR GENERATING COMBUSTION PRODUCTS OF HIGH THERMAL ENERGY AND PRODUCING MECHANICAL ENERGY FROM THEM IN A GAS TURBINE AND RELATED TURBINE PLANT

Country Status (7)

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

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 (en) * 1982-07-29 1984-02-06 Osaka Gas Co Ltd Starter of high pressure hot air generator
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

Family Cites Families (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 (en) * 1971-05-13 1973-01-05 Engelhard Min & Chem
BE795913A (en) * 1972-02-26 1973-06-18 Degussa CHLOROSILANES PREPARATION PROCESS

Also Published As

Publication number Publication date
BE835078R (en) 1976-04-30
FR2309724B2 (en) 1980-04-30
JPS5198415A (en) 1976-08-30
DE2548680A1 (en) 1976-05-06
AU8618775A (en) 1977-05-05
GB1532793A (en) 1978-11-22
FR2309724A2 (en) 1976-11-26
AU502658B2 (en) 1979-08-02

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