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GB2086031B - Gas turbine combustion system - Google Patents

Gas turbine combustion system

Info

Publication number
GB2086031B
GB2086031B GB8120977A GB8120977A GB2086031B GB 2086031 B GB2086031 B GB 2086031B GB 8120977 A GB8120977 A GB 8120977A GB 8120977 A GB8120977 A GB 8120977A GB 2086031 B GB2086031 B GB 2086031B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
combustion system
turbine combustion
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
GB8120977A
Other versions
GB2086031A (en
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.)
Motors Liquidation Co
Original Assignee
General Motors 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 General Motors Corp filed Critical General Motors Corp
Publication of GB2086031A publication Critical patent/GB2086031A/en
Application granted granted Critical
Publication of GB2086031B publication Critical patent/GB2086031B/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
    • F23R3/02—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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00—Geometry
    • F05B2250/40—Movement of component
    • F05B2250/41—Movement of component with one degree of freedom
    • F05B2250/411—Movement of component with one degree of freedom in rotation
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
GB8120977A 1980-10-22 1981-07-07 Gas turbine combustion system Expired GB2086031B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US19958680A 1980-10-22 1980-10-22

Publications (2)

Publication Number Publication Date
GB2086031A GB2086031A (en) 1982-05-06
GB2086031B true GB2086031B (en) 1984-04-18

Family

ID=22738169

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8120977A Expired GB2086031B (en) 1980-10-22 1981-07-07 Gas turbine combustion system

Country Status (1)

Country Link
GB (1) GB2086031B (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4343332C2 (en) * 1993-12-20 1996-06-13 Abb Management Ag Device for convective cooling of a highly loaded combustion chamber
EP0660046B1 (en) * 1993-12-22 1999-12-01 Siemens Westinghouse Power Corporation Combustor bybass system for a gas turbine
US5996351A (en) * 1997-07-07 1999-12-07 General Electric Company Rapid-quench axially staged combustor
RU2137936C1 (en) * 1997-11-10 1999-09-20 Открытое акционерное общество "Авиадвигатель" Method for controlling amount of nitrogen oxides exhausted from gas-turbine engine
US6311473B1 (en) * 1999-03-25 2001-11-06 Parker-Hannifin Corporation Stable pre-mixer for lean burn composition
DE10312971B4 (en) * 2003-03-24 2017-04-06 General Electric Technology Gmbh Method for operating a gas turbine group
RU2249121C1 (en) * 2003-08-05 2005-03-27 Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") Pulsating detonation engine
GB201501971D0 (en) 2015-02-06 2015-03-25 Rolls Royce Plc A combustion chamber
GB201613208D0 (en) 2016-08-01 2016-09-14 Rolls Royce Plc A combustion chamber assembly and a combustion chamber segment
GB202112642D0 (en) * 2021-09-06 2021-10-20 Rolls Royce Plc Controlling soot
FR3152863A1 (en) * 2023-09-12 2025-03-14 Safran Helicopter Engines Combustion chamber

Also Published As

Publication number Publication date
GB2086031A (en) 1982-05-06

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee