BE811568A - COMBUSTION CHAMBER - Google Patents
COMBUSTION CHAMBERInfo
- Publication number
- BE811568A BE811568A BE141381A BE141381A BE811568A BE 811568 A BE811568 A BE 811568A BE 141381 A BE141381 A BE 141381A BE 141381 A BE141381 A BE 141381A BE 811568 A BE811568 A BE 811568A
- Authority
- BE
- Belgium
- Prior art keywords
- combustion chamber
- combustion
- chamber
- Prior art date
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
- F23R3/42—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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Combustion Of Fluid Fuel (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US00335684A US3854285A (en) | 1973-02-26 | 1973-02-26 | Combustor dome assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
BE811568A true BE811568A (en) | 1974-06-17 |
Family
ID=23312822
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE141381A BE811568A (en) | 1973-02-26 | 1974-02-26 | COMBUSTION CHAMBER |
Country Status (7)
Country | Link |
---|---|
US (1) | US3854285A (en) |
JP (1) | JPS5024617A (en) |
BE (1) | BE811568A (en) |
CA (1) | CA1005242A (en) |
DE (1) | DE2408818A1 (en) |
FR (1) | FR2219311A1 (en) |
GB (1) | GB1459591A (en) |
Families Citing this family (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1438379A (en) * | 1973-08-16 | 1976-06-03 | Rolls Royce | Cooling arrangement for duct walls |
US3903754A (en) * | 1974-06-07 | 1975-09-09 | Pino International Ltd | Bicycle crank hub assembly |
US3990232A (en) * | 1975-12-11 | 1976-11-09 | General Electric Company | Combustor dome assembly having improved cooling means |
JPS5363208U (en) * | 1976-10-30 | 1978-05-29 | ||
US4222230A (en) * | 1978-08-14 | 1980-09-16 | General Electric Company | Combustor dome assembly |
JPS5556521A (en) * | 1978-10-23 | 1980-04-25 | Hitachi Ltd | Combustion device |
JPS58106541U (en) * | 1982-01-13 | 1983-07-20 | アイシン精機株式会社 | Combustor for Stirling engine |
US4532762A (en) * | 1982-07-22 | 1985-08-06 | The Garrett Corporation | Gas turbine engine variable geometry combustor apparatus |
US5012645A (en) * | 1987-08-03 | 1991-05-07 | United Technologies Corporation | Combustor liner construction for gas turbine engine |
US5142871A (en) * | 1991-01-22 | 1992-09-01 | General Electric Company | Combustor dome plate support having uniform thickness arcuate apex with circumferentially spaced coolant apertures |
US5181377A (en) * | 1991-04-16 | 1993-01-26 | General Electric Company | Damped combustor cowl structure |
CA2070518C (en) * | 1991-07-01 | 2001-10-02 | Adrian Mark Ablett | Combustor dome assembly |
JP2597800B2 (en) * | 1992-06-12 | 1997-04-09 | ゼネラル・エレクトリック・カンパニイ | Gas turbine engine combustor |
US5329772A (en) * | 1992-12-09 | 1994-07-19 | General Electric Company | Cast slot-cooled single nozzle combustion liner cap |
US5265409A (en) * | 1992-12-18 | 1993-11-30 | United Technologies Corporation | Uniform cooling film replenishment thermal liner assembly |
DE4244303A1 (en) * | 1992-12-28 | 1994-06-30 | Abb Research Ltd | Impact cooling system for cooling surface e.g. of combustion chamber wall |
DE4244302C2 (en) * | 1992-12-28 | 2002-08-29 | Alstom | Impact cooling device |
JP3415663B2 (en) * | 1992-12-28 | 2003-06-09 | アルストム | Equipment for cooling the cooling surface in an impact manner |
US5924288A (en) * | 1994-12-22 | 1999-07-20 | General Electric Company | One-piece combustor cowl |
JP3924136B2 (en) * | 2001-06-27 | 2007-06-06 | 三菱重工業株式会社 | Gas turbine combustor |
US7013647B2 (en) * | 2001-12-21 | 2006-03-21 | Mitsubishi Heavy Industries, Ltd. | Outer casing covering gas turbine combustor |
US6672067B2 (en) * | 2002-02-27 | 2004-01-06 | General Electric Company | Corrugated cowl for combustor of a gas turbine engine and method for configuring same |
US6725667B2 (en) | 2002-08-22 | 2004-04-27 | General Electric Company | Combustor dome for gas turbine engine |
US6711900B1 (en) * | 2003-02-04 | 2004-03-30 | Pratt & Whitney Canada Corp. | Combustor liner V-band design |
US7051532B2 (en) * | 2003-10-17 | 2006-05-30 | General Electric Company | Methods and apparatus for film cooling gas turbine engine combustors |
US7219498B2 (en) * | 2004-09-10 | 2007-05-22 | Honeywell International, Inc. | Waffled impingement effusion method |
FR2885201B1 (en) * | 2005-04-28 | 2010-09-17 | Snecma Moteurs | EASILY DISMANTLING COMBUSTION CHAMBER WITH IMPROVED AERODYNAMIC PERFORMANCE |
FR2897144B1 (en) * | 2006-02-08 | 2008-05-02 | Snecma Sa | COMBUSTION CHAMBER FOR TURBOMACHINE WITH TANGENTIAL SLOTS |
FR2897145B1 (en) * | 2006-02-08 | 2013-01-18 | Snecma | ANNULAR COMBUSTION CHAMBER FOR TURBOMACHINE WITH ALTERNATE FIXINGS. |
FR2905166B1 (en) * | 2006-08-28 | 2008-11-14 | Snecma Sa | ANNULAR COMBUSTION CHAMBER OF A TURBOMACHINE. |
FR2906350B1 (en) * | 2006-09-22 | 2009-03-20 | Snecma Sa | ANNULAR COMBUSTION CHAMBER OF A TURBOMACHINE |
US7765809B2 (en) * | 2006-11-10 | 2010-08-03 | General Electric Company | Combustor dome and methods of assembling such |
US7856826B2 (en) * | 2006-11-10 | 2010-12-28 | General Electric Company | Combustor dome mixer retaining means |
FR2914399B1 (en) * | 2007-03-27 | 2009-10-02 | Snecma Sa | FURNITURE FOR BOTTOM OF COMBUSTION CHAMBER. |
DE102007050664A1 (en) * | 2007-10-24 | 2009-04-30 | Man Turbo Ag | Burner for a turbomachine, baffle for such a burner and a turbomachine with such a burner |
US20100050640A1 (en) * | 2008-08-29 | 2010-03-04 | General Electric Company | Thermally compliant combustion cap device and system |
JP4815513B2 (en) * | 2009-07-06 | 2011-11-16 | 川崎重工業株式会社 | Gas turbine combustor |
US8899051B2 (en) * | 2010-12-30 | 2014-12-02 | Rolls-Royce Corporation | Gas turbine engine flange assembly including flow circuit |
DE102013204307A1 (en) * | 2013-03-13 | 2014-09-18 | Siemens Aktiengesellschaft | Jet burner with cooling channel in the base plate |
DE102015213629A1 (en) * | 2015-07-20 | 2017-01-26 | Rolls-Royce Deutschland Ltd & Co Kg | Cover member and combustion chamber assembly for a gas turbine |
US10619856B2 (en) * | 2017-03-13 | 2020-04-14 | Rolls-Royce Corporation | Notched gas turbine combustor cowl |
US10982852B2 (en) | 2018-11-05 | 2021-04-20 | Rolls-Royce Corporation | Cowl integration to combustor wall |
US11859819B2 (en) | 2021-10-15 | 2024-01-02 | General Electric Company | Ceramic composite combustor dome and liners |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2549858A (en) * | 1946-07-30 | 1951-04-24 | Westinghouse Electric Corp | Annular combustion chamber having telescoping walls with corrugated ends for spacing |
US2537033A (en) * | 1947-07-18 | 1951-01-09 | Westinghouse Electric Corp | Gas turbine combustion chamber construction |
GB697027A (en) * | 1950-11-27 | 1953-09-16 | Lucas Ltd Joseph | Combustion chambers for prime movers |
GB710353A (en) * | 1951-06-18 | 1954-06-09 | Rolls Royce | Improvements in or relating to combustion equipment for gas-turbine engines |
GB736028A (en) * | 1952-11-29 | 1955-08-31 | Lucas Industries Ltd | Combustion chambers for prime movers |
US3038309A (en) * | 1959-07-21 | 1962-06-12 | Gen Electric | Cooling liner for jet engine afterburner |
US3064425A (en) * | 1959-10-05 | 1962-11-20 | Gen Motors Corp | Combustion liner |
US3307354A (en) * | 1965-10-01 | 1967-03-07 | Gen Electric | Cooling structure for overlapped panels |
GB1127637A (en) * | 1966-08-18 | 1968-09-18 | Lucas Industries Ltd | Supports for fuel burners |
US3385055A (en) * | 1966-11-23 | 1968-05-28 | United Aircraft Corp | Combustion chamber with floating swirler rings |
US3408812A (en) * | 1967-02-24 | 1968-11-05 | Gen Electric | Cooled joint construction for combustion wall means |
-
1973
- 1973-02-26 US US00335684A patent/US3854285A/en not_active Expired - Lifetime
-
1974
- 1974-02-05 CA CA191,797A patent/CA1005242A/en not_active Expired
- 1974-02-14 GB GB669974A patent/GB1459591A/en not_active Expired
- 1974-02-23 DE DE19742408818 patent/DE2408818A1/en active Pending
- 1974-02-26 JP JP49022010A patent/JPS5024617A/ja active Pending
- 1974-02-26 FR FR7406495A patent/FR2219311A1/fr not_active Withdrawn
- 1974-02-26 BE BE141381A patent/BE811568A/en unknown
Also Published As
Publication number | Publication date |
---|---|
US3854285A (en) | 1974-12-17 |
DE2408818A1 (en) | 1974-09-05 |
GB1459591A (en) | 1976-12-22 |
JPS5024617A (en) | 1975-03-15 |
FR2219311A1 (en) | 1974-09-20 |
CA1005242A (en) | 1977-02-15 |
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