DE2657529A1 - Brenner fuer eine gasturbine - Google Patents
Brenner fuer eine gasturbineInfo
- Publication number
- DE2657529A1 DE2657529A1 DE19762657529 DE2657529A DE2657529A1 DE 2657529 A1 DE2657529 A1 DE 2657529A1 DE 19762657529 DE19762657529 DE 19762657529 DE 2657529 A DE2657529 A DE 2657529A DE 2657529 A1 DE2657529 A1 DE 2657529A1
- Authority
- DE
- Germany
- Prior art keywords
- burner
- jacket
- longitudinal
- ceramic material
- piece
- 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.)
- Withdrawn
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 229910010293 ceramic material Inorganic materials 0.000 claims description 35
- 238000002485 combustion reaction Methods 0.000 claims description 32
- 239000002184 metal Substances 0.000 claims description 25
- 229910052751 metal Inorganic materials 0.000 claims description 25
- 239000000919 ceramic Substances 0.000 claims description 18
- 239000000446 fuel Substances 0.000 claims description 14
- 238000001816 cooling Methods 0.000 claims description 6
- 238000011144 upstream manufacturing Methods 0.000 claims description 4
- 238000004891 communication Methods 0.000 claims description 2
- 230000004907 flux Effects 0.000 claims description 2
- 210000003608 fece Anatomy 0.000 claims 1
- 239000010871 livestock manure Substances 0.000 claims 1
- 239000007789 gas Substances 0.000 description 12
- 230000035882 stress Effects 0.000 description 6
- 239000000463 material Substances 0.000 description 5
- 230000007704 transition Effects 0.000 description 5
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 4
- 229910010271 silicon carbide Inorganic materials 0.000 description 4
- MWUXSHHQAYIFBG-UHFFFAOYSA-N Nitric oxide Chemical compound O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 3
- 230000008602 contraction Effects 0.000 description 3
- 230000001965 increasing effect Effects 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 239000000567 combustion gas Substances 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000000704 physical effect Effects 0.000 description 2
- 230000008646 thermal stress Effects 0.000 description 2
- YPFNIPKMNMDDDB-UHFFFAOYSA-K 2-[2-[bis(carboxylatomethyl)amino]ethyl-(2-hydroxyethyl)amino]acetate;iron(3+) Chemical compound [Fe+3].OCCN(CC([O-])=O)CCN(CC([O-])=O)CC([O-])=O YPFNIPKMNMDDDB-UHFFFAOYSA-K 0.000 description 1
- 229910052581 Si3N4 Inorganic materials 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 239000003245 coal Substances 0.000 description 1
- 239000003034 coal gas Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- -1 e.g. oil) are used Chemical class 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 230000000763 evoking effect Effects 0.000 description 1
- 238000002309 gasification Methods 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Classifications
-
- 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
- F23M5/00—Casings; Linings; Walls
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C3/00—Combustion apparatus characterised by the shape of the combustion chamber
-
- 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
- F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
-
- 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
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/643,540 US4030875A (en) | 1975-12-22 | 1975-12-22 | Integrated ceramic-metal combustor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE2657529A1 true DE2657529A1 (de) | 1977-06-23 |
Family
ID=24581241
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19762657529 Withdrawn DE2657529A1 (de) | 1975-12-22 | 1976-12-18 | Brenner fuer eine gasturbine |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US4030875A (enExample) |
| JP (1) | JPS5277913A (enExample) |
| CA (1) | CA1072754A (enExample) |
| DE (1) | DE2657529A1 (enExample) |
| FR (1) | FR2336554A1 (enExample) |
| GB (1) | GB1542160A (enExample) |
| NL (1) | NL7614303A (enExample) |
| NO (1) | NO764317L (enExample) |
Families Citing this family (63)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2845588A1 (de) * | 1978-10-19 | 1980-04-24 | Motoren Turbinen Union | Brennkammer fuer gasturbinentriebwerke |
| DE2937631A1 (de) * | 1979-09-18 | 1981-04-02 | Daimler-Benz Ag, 7000 Stuttgart | Brennkammer fuer gasturbinen |
| US4380896A (en) * | 1980-09-22 | 1983-04-26 | The United States Of America As Represented By The Secretary Of The Army | Annular combustor having ceramic liner |
| JPS57154856U (enExample) * | 1981-03-19 | 1982-09-29 | ||
| JPS58133526A (ja) * | 1982-02-03 | 1983-08-09 | Kenji Watanabe | 水素ガスタ−ビンエンジン |
| US4422300A (en) * | 1981-12-14 | 1983-12-27 | United Technologies Corporation | Prestressed combustor liner for gas turbine engine |
| US4787208A (en) * | 1982-03-08 | 1988-11-29 | Westinghouse Electric Corp. | Low-nox, rich-lean combustor |
| US4485630A (en) * | 1982-12-08 | 1984-12-04 | General Electric Company | Combustor liner |
| DE3422229C2 (de) * | 1984-06-15 | 1986-06-05 | WS Wärmeprozesstechnik GmbH, 7015 Korntal-Münchingen | Industriebrenner für gasförmige oder flüssige Brennstoffe |
| US4899538A (en) * | 1987-11-20 | 1990-02-13 | Sundstrand Corporation | Hot gas generator |
| US4955202A (en) * | 1989-03-12 | 1990-09-11 | Sundstrand Corporation | Hot gas generator |
| US5024058A (en) * | 1989-12-08 | 1991-06-18 | Sundstrand Corporation | Hot gas generator |
| US5117636A (en) * | 1990-02-05 | 1992-06-02 | General Electric Company | Low nox emission in gas turbine system |
| US5749229A (en) * | 1995-10-13 | 1998-05-12 | General Electric Company | Thermal spreading combustor liner |
| US5851679A (en) * | 1996-12-17 | 1998-12-22 | General Electric Company | Multilayer dielectric stack coated part for contact with combustion gases |
| US6116013A (en) * | 1998-01-02 | 2000-09-12 | Siemens Westinghouse Power Corporation | Bolted gas turbine combustor transition coupling |
| JP3478531B2 (ja) * | 2000-04-21 | 2003-12-15 | 川崎重工業株式会社 | ガスタービンのセラミック部品支持構造 |
| US6397603B1 (en) * | 2000-05-05 | 2002-06-04 | The United States Of America As Represented By The Secretary Of The Air Force | Conbustor having a ceramic matrix composite liner |
| FR2825785B1 (fr) * | 2001-06-06 | 2004-08-27 | Snecma Moteurs | Liaison de chambre de combustion cmc de turbomachine en deux parties |
| US6495207B1 (en) | 2001-12-21 | 2002-12-17 | Pratt & Whitney Canada Corp. | Method of manufacturing a composite wall |
| US7117676B2 (en) * | 2003-03-26 | 2006-10-10 | United Technologies Corporation | Apparatus for mixing fluids |
| US7007486B2 (en) * | 2003-03-26 | 2006-03-07 | The Boeing Company | Apparatus and method for selecting a flow mixture |
| US7282274B2 (en) * | 2003-11-07 | 2007-10-16 | General Electric Company | Integral composite structural material |
| US7127899B2 (en) * | 2004-02-26 | 2006-10-31 | United Technologies Corporation | Non-swirl dry low NOx (DLN) combustor |
| US7810336B2 (en) * | 2005-06-03 | 2010-10-12 | Siemens Energy, Inc. | System for introducing fuel to a fluid flow upstream of a combustion area |
| FR2887015B1 (fr) * | 2005-06-14 | 2010-09-24 | Snecma Moteurs | Assemblage d'une chambre de combustion annulaire de turbomachine |
| US7954325B2 (en) * | 2005-12-06 | 2011-06-07 | United Technologies Corporation | Gas turbine combustor |
| US7665307B2 (en) * | 2005-12-22 | 2010-02-23 | United Technologies Corporation | Dual wall combustor liner |
| DE102006042124B4 (de) * | 2006-09-07 | 2010-04-22 | Man Turbo Ag | Gasturbinenbrennkammer |
| GB2453946B (en) * | 2007-10-23 | 2010-07-14 | Rolls Royce Plc | A Wall Element for use in Combustion Apparatus |
| GB0800294D0 (en) * | 2008-01-09 | 2008-02-20 | Rolls Royce Plc | Gas heater |
| GB0801839D0 (en) * | 2008-02-01 | 2008-03-05 | Rolls Royce Plc | combustion apparatus |
| GB2457281B (en) * | 2008-02-11 | 2010-09-08 | Rolls Royce Plc | A Combustor Wall Arrangement with Parts Joined by Mechanical Fasteners |
| EP2116770B1 (en) * | 2008-05-07 | 2013-12-04 | Siemens Aktiengesellschaft | Combustor dynamic attenuation and cooling arrangement |
| GB2460634B (en) * | 2008-06-02 | 2010-07-07 | Rolls Royce Plc | Combustion apparatus |
| US8745989B2 (en) * | 2009-04-09 | 2014-06-10 | Pratt & Whitney Canada Corp. | Reverse flow ceramic matrix composite combustor |
| US8511089B2 (en) * | 2009-07-31 | 2013-08-20 | Rolls-Royce Corporation | Relief slot for combustion liner |
| US9068751B2 (en) * | 2010-01-29 | 2015-06-30 | United Technologies Corporation | Gas turbine combustor with staged combustion |
| US8966877B2 (en) | 2010-01-29 | 2015-03-03 | United Technologies Corporation | Gas turbine combustor with variable airflow |
| CN101988430A (zh) * | 2010-02-10 | 2011-03-23 | 马鞍山科达洁能股份有限公司 | 燃气轮机 |
| US8955329B2 (en) | 2011-10-21 | 2015-02-17 | General Electric Company | Diffusion nozzles for low-oxygen fuel nozzle assembly and method |
| IL219929A0 (en) * | 2012-05-22 | 2012-07-31 | Siete Technologies Ltd | Burner for fuel oils |
| MX2012006599A (es) * | 2012-06-08 | 2013-12-16 | Jorge Rivera Garza | Quemador de combustible gaseoso con elevada eficiencia energetica y de combustion, baja emision de contaminantes y mayor transferencia de calor. |
| CN104520644B (zh) | 2012-08-07 | 2017-09-08 | 日野自动车株式会社 | 燃烧器 |
| JP5584381B2 (ja) * | 2012-08-07 | 2014-09-03 | 日野自動車株式会社 | 排気浄化装置用バーナー |
| US9249704B2 (en) | 2012-08-07 | 2016-02-02 | Hino Motors, Ltd. | Burner for exhaust gas purification devices |
| US9765662B2 (en) | 2012-08-13 | 2017-09-19 | Hine Motors, Ltd. | Burner |
| AU2013219140B2 (en) * | 2012-08-24 | 2015-10-08 | Ansaldo Energia Switzerland AG | Method for mixing a dilution air in a sequential combustion system of a gas turbine |
| SE537347C2 (sv) * | 2012-08-31 | 2015-04-07 | Reformtech Heating Holding Ab | Apparat för förbränning |
| US9932831B2 (en) | 2014-05-09 | 2018-04-03 | United Technologies Corporation | High temperature compliant metallic elements for low contact stress ceramic support |
| CN107250673A (zh) | 2014-12-15 | 2017-10-13 | 诺沃皮尼奥内股份有限公司 | 燃烧器衬套柔性支撑及方法 |
| US10208955B2 (en) * | 2015-04-07 | 2019-02-19 | United Technologies Corporation | Ceramic and metal engine components with gradient transition from metal to ceramic |
| GB2540769A (en) * | 2015-07-27 | 2017-02-01 | Rolls Royce Plc | Combustor for a gas turbine engine |
| US9618207B1 (en) * | 2016-01-21 | 2017-04-11 | Siemens Energy, Inc. | Transition duct system with metal liners for delivering hot-temperature gases in a combustion turbine engine |
| US9650904B1 (en) * | 2016-01-21 | 2017-05-16 | Siemens Energy, Inc. | Transition duct system with straight ceramic liner for delivering hot-temperature gases in a combustion turbine engine |
| US10739001B2 (en) | 2017-02-14 | 2020-08-11 | Raytheon Technologies Corporation | Combustor liner panel shell interface for a gas turbine engine combustor |
| US10718521B2 (en) | 2017-02-23 | 2020-07-21 | Raytheon Technologies Corporation | Combustor liner panel end rail cooling interface passage for a gas turbine engine combustor |
| US10823411B2 (en) | 2017-02-23 | 2020-11-03 | Raytheon Technologies Corporation | Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustor |
| US10830434B2 (en) | 2017-02-23 | 2020-11-10 | Raytheon Technologies Corporation | Combustor liner panel end rail with curved interface passage for a gas turbine engine combustor |
| US10941937B2 (en) * | 2017-03-20 | 2021-03-09 | Raytheon Technologies Corporation | Combustor liner with gasket for gas turbine engine |
| US20180340687A1 (en) * | 2017-05-24 | 2018-11-29 | Siemens Aktiengesellschaft | Refractory ceramic component for a gas turbine engine |
| US11187412B2 (en) | 2018-08-22 | 2021-11-30 | General Electric Company | Flow control wall assembly for heat engine |
| US10989413B2 (en) * | 2019-07-17 | 2021-04-27 | General Electric Company | Axial retention assembly for combustor components of a gas turbine engine |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1827246A (en) * | 1927-06-07 | 1931-10-13 | Bendix Aviat Corp | Gas turbine |
| GB1240009A (en) * | 1968-07-27 | 1971-07-21 | Leyland Gas Turbines Ltd | Flame tube |
| US3589127A (en) * | 1969-02-04 | 1971-06-29 | Gen Electric | Combustion apparatus |
| GB1304177A (enExample) * | 1969-04-23 | 1973-01-24 | ||
| US3854503A (en) * | 1971-08-05 | 1974-12-17 | Lucas Industries Ltd | Flame tubes |
| FR2149287B1 (enExample) * | 1971-08-18 | 1975-02-21 | Lucas Industries Ltd | |
| US3880574A (en) * | 1974-04-15 | 1975-04-29 | Gen Motors Corp | Ceramic combustion liner |
| US3880575A (en) * | 1974-04-15 | 1975-04-29 | Gen Motors Corp | Ceramic combustion liner |
-
1975
- 1975-12-22 US US05/643,540 patent/US4030875A/en not_active Expired - Lifetime
-
1976
- 1976-12-14 CA CA267,772A patent/CA1072754A/en not_active Expired
- 1976-12-17 FR FR7638069A patent/FR2336554A1/fr not_active Withdrawn
- 1976-12-18 DE DE19762657529 patent/DE2657529A1/de not_active Withdrawn
- 1976-12-20 GB GB7653023A patent/GB1542160A/en not_active Expired
- 1976-12-21 NO NO764317A patent/NO764317L/no unknown
- 1976-12-21 JP JP51152957A patent/JPS5277913A/ja active Pending
- 1976-12-22 NL NL7614303A patent/NL7614303A/xx not_active Application Discontinuation
Also Published As
| Publication number | Publication date |
|---|---|
| NL7614303A (nl) | 1977-06-24 |
| JPS5277913A (en) | 1977-06-30 |
| US4030875A (en) | 1977-06-21 |
| GB1542160A (en) | 1979-03-14 |
| NO764317L (enExample) | 1977-06-23 |
| CA1072754A (en) | 1980-03-04 |
| FR2336554A1 (fr) | 1977-07-22 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 8139 | Disposal/non-payment of the annual fee |