AU2001257482A1 - Annular combustor for use with an energy system - Google Patents

Annular combustor for use with an energy system

Info

Publication number
AU2001257482A1
AU2001257482A1 AU2001257482A AU5748201A AU2001257482A1 AU 2001257482 A1 AU2001257482 A1 AU 2001257482A1 AU 2001257482 A AU2001257482 A AU 2001257482A AU 5748201 A AU5748201 A AU 5748201A AU 2001257482 A1 AU2001257482 A1 AU 2001257482A1
Authority
AU
Australia
Prior art keywords
energy system
annular combustor
combustor
annular
energy
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.)
Abandoned
Application number
AU2001257482A
Inventor
J. Michael Teets
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.)
Elliott Energy Systems Inc
Original Assignee
Elliott Energy Systems Inc
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 Elliott Energy Systems Inc filed Critical Elliott Energy Systems Inc
Publication of AU2001257482A1 publication Critical patent/AU2001257482A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
    • F02C3/085—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage the turbine being of the radial-flow type (radial-radial)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M9/00—Baffles or deflectors for air or combustion products; Flame shields
    • F23M9/06—Baffles or deflectors for air or combustion products; Flame shields in fire-boxes
    • 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
    • F23R3/04—Air inlet arrangements
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
AU2001257482A 2000-05-01 2001-05-01 Annular combustor for use with an energy system Abandoned AU2001257482A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US20094600P 2000-05-01 2000-05-01
US60200946 2000-05-01
PCT/US2001/014115 WO2001083963A1 (en) 2000-05-01 2001-05-01 Annular combustor for use with an energy system

Publications (1)

Publication Number Publication Date
AU2001257482A1 true AU2001257482A1 (en) 2001-11-12

Family

ID=22743841

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001257482A Abandoned AU2001257482A1 (en) 2000-05-01 2001-05-01 Annular combustor for use with an energy system

Country Status (8)

Country Link
US (1) US6845621B2 (en)
EP (1) EP1295018A4 (en)
JP (1) JP4851674B2 (en)
KR (1) KR20030036174A (en)
CN (1) CN1502007A (en)
AU (1) AU2001257482A1 (en)
CA (1) CA2407717A1 (en)
WO (1) WO2001083963A1 (en)

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US8701416B2 (en) * 2006-06-26 2014-04-22 Joseph Michael Teets Radially staged RQL combustor with tangential fuel-air premixers
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US8113003B2 (en) * 2008-08-12 2012-02-14 Siemens Energy, Inc. Transition with a linear flow path for use in a gas turbine engine
US8616007B2 (en) * 2009-01-22 2013-12-31 Siemens Energy, Inc. Structural attachment system for transition duct outlet
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WO2015199694A1 (en) 2014-06-26 2015-12-30 Siemens Energy, Inc. Converging flow joint insert system at an intersection between adjacent transitions duct bodies
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Also Published As

Publication number Publication date
JP4851674B2 (en) 2012-01-11
EP1295018A1 (en) 2003-03-26
CA2407717A1 (en) 2001-11-08
KR20030036174A (en) 2003-05-09
WO2001083963A1 (en) 2001-11-08
JP2004507700A (en) 2004-03-11
CN1502007A (en) 2004-06-02
EP1295018A4 (en) 2004-06-02
US6845621B2 (en) 2005-01-25
US20030205050A1 (en) 2003-11-06

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