SE8102134L - Brennarinsatskonstruktion - Google Patents
BrennarinsatskonstruktionInfo
- Publication number
- SE8102134L SE8102134L SE8102134A SE8102134A SE8102134L SE 8102134 L SE8102134 L SE 8102134L SE 8102134 A SE8102134 A SE 8102134A SE 8102134 A SE8102134 A SE 8102134A SE 8102134 L SE8102134 L SE 8102134L
- Authority
- SE
- Sweden
- Prior art keywords
- panels
- liner
- finwall
- introducing
- cooling air
- 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
- F23R3/002—Wall structures
-
- 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
- F05B2260/00—Function
- F05B2260/20—Heat transfer, e.g. cooling
- F05B2260/221—Improvement of heat transfer
- F05B2260/224—Improvement of heat transfer by increasing the heat transfer surface
- F05B2260/2241—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
- Spray-Type Burners (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/136,848 US4361010A (en) | 1980-04-02 | 1980-04-02 | Combustor liner construction |
Publications (2)
Publication Number | Publication Date |
---|---|
SE8102134L true SE8102134L (sv) | 1981-10-03 |
SE457372B SE457372B (sv) | 1988-12-19 |
Family
ID=22474647
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8102134A SE457372B (sv) | 1980-04-02 | 1981-04-02 | Braennkammarfoder foer en gasturbinmotor |
Country Status (8)
Country | Link |
---|---|
US (1) | US4361010A (sv) |
JP (1) | JPS56168041A (sv) |
CA (1) | CA1156843A (sv) |
DE (1) | DE3113380A1 (sv) |
FR (1) | FR2479951A1 (sv) |
GB (1) | GB2074715B (sv) |
IL (1) | IL62557A (sv) |
SE (1) | SE457372B (sv) |
Families Citing this family (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4622821A (en) * | 1985-01-07 | 1986-11-18 | United Technologies Corporation | Combustion liner for a gas turbine engine |
US4790140A (en) * | 1985-01-18 | 1988-12-13 | Ishikawajima-Harima Jukogyo Kabushiki Kaisha | Liner cooling construction for gas turbine combustor or the like |
US4642993A (en) * | 1985-04-29 | 1987-02-17 | Avco Corporation | Combustor liner wall |
EP0224817B1 (de) * | 1985-12-02 | 1989-07-12 | Siemens Aktiengesellschaft | Hitzeschildanordnung, insbesondere für Strukturteile von Gasturbinenanlagen |
US4800718A (en) * | 1986-12-24 | 1989-01-31 | The United States Of America As Represented By The Secretary Of The Air Force | Surface cooling system |
US4928479A (en) * | 1987-12-28 | 1990-05-29 | Sundstrand Corporation | Annular combustor with tangential cooling air injection |
DE3942271A1 (de) * | 1989-12-21 | 1991-07-04 | Mtu Maintenance Gmbh | Verfahren zur reparatur eines flammrohres |
DE4242721A1 (de) * | 1992-12-17 | 1994-06-23 | Asea Brown Boveri | Gasturbinenbrennkammer |
US5363654A (en) * | 1993-05-10 | 1994-11-15 | General Electric Company | Recuperative impingement cooling of jet engine components |
GB2355301A (en) * | 1999-10-13 | 2001-04-18 | Rolls Royce Plc | A wall structure for a combustor of a gas turbine engine |
US6345441B1 (en) * | 2000-07-18 | 2002-02-12 | General Electric Company | Method of repairing combustion chamber liners |
CA2364238A1 (en) * | 2000-12-04 | 2002-06-04 | Katsunori Tanaka | Plate fin and combustor using the plate fin |
US6581285B2 (en) * | 2001-06-11 | 2003-06-24 | General Electric Co. | Methods for replacing nuggeted combustor liner panels |
US6568079B2 (en) * | 2001-06-11 | 2003-05-27 | General Electric Company | Methods for replacing combustor liner panels |
US6530225B1 (en) | 2001-09-21 | 2003-03-11 | Honeywell International, Inc. | Waffle cooling |
DE102004001393A1 (de) * | 2004-01-09 | 2005-08-04 | Mtu Aero Engines Gmbh | Vorrichtung zur Aufhängung von Gaskanalelementen |
US7278256B2 (en) * | 2004-11-08 | 2007-10-09 | United Technologies Corporation | Pulsed combustion engine |
DE102005059502A1 (de) * | 2005-12-06 | 2007-06-14 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Heißkammer |
EP2116770B1 (en) * | 2008-05-07 | 2013-12-04 | Siemens Aktiengesellschaft | Combustor dynamic attenuation and cooling arrangement |
JP5484707B2 (ja) * | 2008-10-10 | 2014-05-07 | 三菱重工業株式会社 | 燃焼器およびガスタービン |
US8549861B2 (en) * | 2009-01-07 | 2013-10-08 | General Electric Company | Method and apparatus to enhance transition duct cooling in a gas turbine engine |
US7712314B1 (en) * | 2009-01-21 | 2010-05-11 | Gas Turbine Efficiency Sweden Ab | Venturi cooling system |
JP5260402B2 (ja) * | 2009-04-30 | 2013-08-14 | 三菱重工業株式会社 | 板状体の製造方法、板状体、ガスタービン燃焼器およびガスタービン |
RU2530685C2 (ru) * | 2010-03-25 | 2014-10-10 | Дженерал Электрик Компани | Структуры ударного воздействия для систем охлаждения |
US8894363B2 (en) | 2011-02-09 | 2014-11-25 | Siemens Energy, Inc. | Cooling module design and method for cooling components of a gas turbine system |
US8959886B2 (en) | 2010-07-08 | 2015-02-24 | Siemens Energy, Inc. | Mesh cooled conduit for conveying combustion gases |
US20120227408A1 (en) * | 2011-03-10 | 2012-09-13 | Delavan Inc. | Systems and methods of pressure drop control in fluid circuits through swirling flow mitigation |
WO2014029512A2 (en) * | 2012-08-24 | 2014-02-27 | Alstom Technology Ltd | Sequential combustion with dilution gas mixer |
WO2015116360A1 (en) * | 2014-01-30 | 2015-08-06 | United Technologies Corporation | Cooling flow for leading panel in a gas turbine engine combustor |
US10309652B2 (en) * | 2014-04-14 | 2019-06-04 | Siemens Energy, Inc. | Gas turbine engine combustor basket with inverted platefins |
JP6470135B2 (ja) | 2014-07-14 | 2019-02-13 | ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation | 付加製造された表面仕上げ |
US10480787B2 (en) * | 2015-03-26 | 2019-11-19 | United Technologies Corporation | Combustor wall cooling channel formed by additive manufacturing |
US10094564B2 (en) | 2015-04-17 | 2018-10-09 | Pratt & Whitney Canada Corp. | Combustor dilution hole cooling system |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH255541A (de) * | 1947-05-12 | 1948-06-30 | Bbc Brown Boveri & Cie | Gekühlte metallische Brennkammer zur Erzeugung von Heiz- und Treibgasen. |
BE535497A (sv) * | 1954-02-26 | |||
US3064424A (en) * | 1959-09-30 | 1962-11-20 | Gen Motors Corp | Flame tube |
US3333414A (en) * | 1965-10-13 | 1967-08-01 | United Aircraft Canada | Aerodynamic-flow reverser and smoother |
US3572031A (en) * | 1969-07-11 | 1971-03-23 | United Aircraft Corp | Variable area cooling passages for gas turbine burners |
US3706203A (en) * | 1970-10-30 | 1972-12-19 | United Aircraft Corp | Wall structure for a gas turbine engine |
GB1424197A (en) * | 1972-06-09 | 1976-02-11 | Lucas Industries Ltd | Combustion chambers for gas turbine engines |
GB1438379A (en) * | 1973-08-16 | 1976-06-03 | Rolls Royce | Cooling arrangement for duct walls |
GB1552132A (en) * | 1975-11-29 | 1979-09-12 | Rolls Royce | Combustion chambers for gas turbine engines |
FR2340453A1 (fr) * | 1976-02-06 | 1977-09-02 | Snecma | Corps de chambre de combustion, notamment pour turboreacteurs |
US4132066A (en) * | 1977-09-23 | 1979-01-02 | United Technologies Corporation | Combustor liner for gas turbine engine |
-
1980
- 1980-04-02 US US06/136,848 patent/US4361010A/en not_active Expired - Lifetime
-
1981
- 1981-03-19 CA CA000373415A patent/CA1156843A/en not_active Expired
- 1981-04-01 GB GB8110149A patent/GB2074715B/en not_active Expired
- 1981-04-02 JP JP5046081A patent/JPS56168041A/ja active Granted
- 1981-04-02 DE DE19813113380 patent/DE3113380A1/de active Granted
- 1981-04-02 IL IL62557A patent/IL62557A/xx not_active IP Right Cessation
- 1981-04-02 FR FR8106597A patent/FR2479951A1/fr active Granted
- 1981-04-02 SE SE8102134A patent/SE457372B/sv not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
GB2074715A (en) | 1981-11-04 |
JPH0229935B2 (sv) | 1990-07-03 |
CA1156843A (en) | 1983-11-15 |
IL62557A0 (en) | 1981-06-29 |
FR2479951A1 (fr) | 1981-10-09 |
US4361010A (en) | 1982-11-30 |
DE3113380A1 (de) | 1982-04-08 |
DE3113380C2 (sv) | 1990-09-27 |
IL62557A (en) | 1984-01-31 |
FR2479951B1 (sv) | 1984-02-10 |
SE457372B (sv) | 1988-12-19 |
JPS56168041A (en) | 1981-12-24 |
GB2074715B (en) | 1983-10-05 |
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Legal Events
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