IT7828046A0 - Camicia per la camera di combustione di un motore a turbina a gas. - Google Patents
Camicia per la camera di combustione di un motore a turbina a gas.Info
- Publication number
- IT7828046A0 IT7828046A0 IT7828046A IT2804678A IT7828046A0 IT 7828046 A0 IT7828046 A0 IT 7828046A0 IT 7828046 A IT7828046 A IT 7828046A IT 2804678 A IT2804678 A IT 2804678A IT 7828046 A0 IT7828046 A0 IT 7828046A0
- Authority
- IT
- Italy
- Prior art keywords
- sleeve
- combustion chamber
- gas turbine
- turbine engine
- engine
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title 1
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
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
- F23R3/04—Air inlet arrangements
- F23R3/06—Arrangement of apertures along the flame tube
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/836,119 US4132066A (en) | 1977-09-23 | 1977-09-23 | Combustor liner for gas turbine engine |
Publications (2)
Publication Number | Publication Date |
---|---|
IT7828046A0 true IT7828046A0 (it) | 1978-09-25 |
IT1099145B IT1099145B (it) | 1985-09-18 |
Family
ID=25271287
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT28046/78A IT1099145B (it) | 1977-09-23 | 1978-09-25 | Camicia per la camera di combustione di un motore a turbina a gas |
Country Status (6)
Country | Link |
---|---|
US (1) | US4132066A (it) |
BE (1) | BE870668A (it) |
DE (1) | DE2841343A1 (it) |
FR (1) | FR2404110A1 (it) |
GB (1) | GB2004592B (it) |
IT (1) | IT1099145B (it) |
Families Citing this family (47)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1979001144A1 (en) * | 1978-05-30 | 1979-12-27 | Fosroc International Ltd | Anchoring cartridges |
US4414816A (en) * | 1980-04-02 | 1983-11-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Combustor liner construction |
US4361010A (en) * | 1980-04-02 | 1982-11-30 | United Technologies Corporation | Combustor liner construction |
US4622821A (en) * | 1985-01-07 | 1986-11-18 | United Technologies Corporation | Combustion liner for a gas turbine engine |
US4989407A (en) * | 1986-08-29 | 1991-02-05 | United Technologies Corporation | Thrust augmentor flameholder |
GB8703101D0 (en) * | 1987-02-11 | 1987-03-18 | Secr Defence | Gas turbine engine combustion chambers |
US4887432A (en) * | 1988-10-07 | 1989-12-19 | Westinghouse Electric Corp. | Gas turbine combustion chamber with air scoops |
DE19528406A1 (de) * | 1995-08-02 | 1997-02-06 | Bmw Rolls Royce Gmbh | Gasturbinen-Brennkammer mit Luftübertrittsöffnungen |
US6279313B1 (en) | 1999-12-14 | 2001-08-28 | General Electric Company | Combustion liner for gas turbine having liner stops |
DE10214570A1 (de) * | 2002-04-02 | 2004-01-15 | Rolls-Royce Deutschland Ltd & Co Kg | Mischluftloch in Gasturbinenbrennkammer mit Brennkammerschindeln |
US8281600B2 (en) * | 2007-01-09 | 2012-10-09 | General Electric Company | Thimble, sleeve, and method for cooling a combustor assembly |
US20100236248A1 (en) * | 2009-03-18 | 2010-09-23 | Karthick Kaleeswaran | Combustion Liner with Mixing Hole Stub |
FR2948988B1 (fr) * | 2009-08-04 | 2011-12-09 | Snecma | Chambre de combustion de turbomachine comprenant des orifices d'entree d'air ameliores |
US9010121B2 (en) * | 2010-12-10 | 2015-04-21 | Rolls-Royce Plc | Combustion chamber |
US9062884B2 (en) | 2011-05-26 | 2015-06-23 | Honeywell International Inc. | Combustors with quench inserts |
US9360215B2 (en) | 2012-04-02 | 2016-06-07 | United Technologies Corporation | Combustor having a beveled grommet |
US20130283806A1 (en) * | 2012-04-26 | 2013-10-31 | General Electric Company | Combustor and a method for repairing the combustor |
FR2991028B1 (fr) * | 2012-05-25 | 2014-07-04 | Snecma | Virole de chambre de combustion de turbomachine |
US9625151B2 (en) * | 2012-09-25 | 2017-04-18 | United Technologies Corporation | Cooled combustor liner grommet |
US10088162B2 (en) | 2012-10-01 | 2018-10-02 | United Technologies Corporation | Combustor with grommet having projecting lip |
EP2735796B1 (en) * | 2012-11-23 | 2020-01-01 | Ansaldo Energia IP UK Limited | Wall of a hot gas path component of a gas turbine and method for enhancing operational behaviour of a gas turbine |
WO2015030927A1 (en) | 2013-08-30 | 2015-03-05 | United Technologies Corporation | Contoured dilution passages for a gas turbine engine combustor |
EP3039340B1 (en) * | 2013-08-30 | 2018-11-28 | United Technologies Corporation | Vena contracta swirling dilution passages for gas turbine engine combustor |
WO2015039074A1 (en) * | 2013-09-16 | 2015-03-19 | United Technologies Corporation | Controlled variation of pressure drop through effusion cooling in a double walled combustor of a gas turbine engine |
EP3060847B1 (en) * | 2013-10-24 | 2019-09-18 | United Technologies Corporation | Passage geometry for gas turbine engine combustor |
EP3077727B1 (en) * | 2013-12-06 | 2019-10-09 | United Technologies Corporation | An assembly for a turbine engine |
WO2015147929A2 (en) | 2013-12-20 | 2015-10-01 | United Technologies Corporation | Cooling an aperture body of a combustor wall |
EP3087266B1 (en) | 2013-12-23 | 2019-10-09 | United Technologies Corporation | Multi-streamed dilution hole configuration for a gas turbine engine and relating method of operation |
US9810430B2 (en) | 2013-12-23 | 2017-11-07 | United Technologies Corporation | Conjoined grommet assembly for a combustor |
US10151486B2 (en) | 2014-01-03 | 2018-12-11 | United Technologies Corporation | Cooled grommet for a combustor wall assembly |
EP2927595B1 (en) * | 2014-04-02 | 2019-11-13 | United Technologies Corporation | Grommet assembly and method of design |
US10112557B2 (en) * | 2014-04-03 | 2018-10-30 | United Technologies Corporation | Thermally compliant grommet assembly |
US9528705B2 (en) * | 2014-04-08 | 2016-12-27 | General Electric Company | Trapped vortex fuel injector and method for manufacture |
EP2957833B1 (en) | 2014-06-17 | 2018-10-24 | Rolls-Royce Corporation | Combustor assembly with chutes |
FR3022613B1 (fr) * | 2014-06-24 | 2019-04-19 | Safran Helicopter Engines | Bossage pour chambre de combustion. |
US9851105B2 (en) * | 2014-07-03 | 2017-12-26 | United Technologies Corporation | Self-cooled orifice structure |
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 |
US9810148B2 (en) | 2014-07-24 | 2017-11-07 | United Technologies Corporation | Self-cooled orifice structure |
US10612781B2 (en) | 2014-11-07 | 2020-04-07 | United Technologies Corporation | Combustor wall aperture body with cooling circuit |
US20160178199A1 (en) * | 2014-12-17 | 2016-06-23 | United Technologies Corporation | Combustor dilution hole active heat transfer control apparatus and system |
US10094564B2 (en) * | 2015-04-17 | 2018-10-09 | Pratt & Whitney Canada Corp. | Combustor dilution hole cooling system |
DE102015225505A1 (de) * | 2015-12-16 | 2017-06-22 | Rolls-Royce Deutschland Ltd & Co Kg | Wand eines mittels Kühlluft zu kühlenden Bauteils, insbesondere einer Gasturbinenbrennkammerwand |
US20180283695A1 (en) * | 2017-04-03 | 2018-10-04 | United Technologies Corporation | Combustion panel grommet |
US11022308B2 (en) * | 2018-05-31 | 2021-06-01 | Honeywell International Inc. | Double wall combustors with strain isolated inserts |
US11255543B2 (en) | 2018-08-07 | 2022-02-22 | General Electric Company | Dilution structure for gas turbine engine combustor |
US11085639B2 (en) * | 2018-12-27 | 2021-08-10 | Rolls-Royce North American Technologies Inc. | Gas turbine combustor liner with integral chute made by additive manufacturing process |
GB201902693D0 (en) * | 2019-02-28 | 2019-04-17 | Rolls Royce Plc | Combustion liner and gas turbine engine comprising a combustion liner |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3064425A (en) * | 1959-10-05 | 1962-11-20 | Gen Motors Corp | Combustion liner |
NL127178C (it) * | 1959-11-20 | |||
FR1273296A (fr) * | 1960-11-10 | 1961-10-06 | Rolls Royce | Appareillage de combustion pour turbo-moteur à gaz |
DE1957147A1 (de) * | 1968-11-15 | 1970-06-04 | Rolls Royce | Flammrohr fuer Verbrennungsanlagen von Gasturbinentriebwerken |
US3545202A (en) * | 1969-04-02 | 1970-12-08 | United Aircraft Corp | Wall structure and combustion holes for a gas turbine engine |
US3702058A (en) * | 1971-01-13 | 1972-11-07 | Westinghouse Electric Corp | Double wall combustion chamber |
US3899882A (en) * | 1974-03-27 | 1975-08-19 | Westinghouse Electric Corp | Gas turbine combustor basket cooling |
DE2606704A1 (de) * | 1976-02-19 | 1977-09-01 | Motoren Turbinen Union | Brennkammer fuer gasturbinentriebwerke |
GB2017827B (en) * | 1978-04-04 | 1983-02-02 | Gen Electric | Combustor liner cooling |
-
1977
- 1977-09-23 US US05/836,119 patent/US4132066A/en not_active Expired - Lifetime
-
1978
- 1978-09-21 GB GB7837688A patent/GB2004592B/en not_active Expired
- 1978-09-21 BE BE190635A patent/BE870668A/xx not_active IP Right Cessation
- 1978-09-22 DE DE19782841343 patent/DE2841343A1/de not_active Withdrawn
- 1978-09-22 FR FR7827151A patent/FR2404110A1/fr not_active Withdrawn
- 1978-09-25 IT IT28046/78A patent/IT1099145B/it active
Also Published As
Publication number | Publication date |
---|---|
FR2404110A1 (fr) | 1979-04-20 |
GB2004592B (en) | 1982-01-27 |
IT1099145B (it) | 1985-09-18 |
US4132066A (en) | 1979-01-02 |
DE2841343A1 (de) | 1979-04-05 |
GB2004592A (en) | 1979-04-04 |
BE870668A (fr) | 1979-01-15 |
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