DE60122819T2 - Brennkammer mit Brennkammerwand aus Verbundwerkstoff mit keramischer Matrix - Google Patents
Brennkammer mit Brennkammerwand aus Verbundwerkstoff mit keramischer Matrix Download PDFInfo
- Publication number
- DE60122819T2 DE60122819T2 DE60122819T DE60122819T DE60122819T2 DE 60122819 T2 DE60122819 T2 DE 60122819T2 DE 60122819 T DE60122819 T DE 60122819T DE 60122819 T DE60122819 T DE 60122819T DE 60122819 T2 DE60122819 T2 DE 60122819T2
- Authority
- DE
- Germany
- Prior art keywords
- combustion chamber
- insert
- rear seal
- holder
- thermal expansion
- 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.)
- Expired - Lifetime
Links
- 238000002485 combustion reaction Methods 0.000 title claims description 76
- 239000000919 ceramic Substances 0.000 title claims description 20
- 239000011159 matrix material Substances 0.000 title claims description 19
- 239000002131 composite material Substances 0.000 title claims description 13
- 239000000463 material Substances 0.000 claims description 29
- 239000011153 ceramic matrix composite Substances 0.000 claims description 15
- 238000001816 cooling Methods 0.000 claims description 15
- 239000000446 fuel Substances 0.000 claims description 13
- 239000007789 gas Substances 0.000 claims description 7
- 239000007769 metal material Substances 0.000 claims description 7
- 230000001590 oxidative effect Effects 0.000 claims description 4
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 3
- 239000000567 combustion gas Substances 0.000 claims description 2
- 229910052814 silicon oxide Inorganic materials 0.000 claims description 2
- 239000002184 metal Substances 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 6
- 229910010271 silicon carbide Inorganic materials 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 230000008878 coupling Effects 0.000 description 4
- 238000010168 coupling process Methods 0.000 description 4
- 238000005859 coupling reaction Methods 0.000 description 4
- 239000000835 fiber Substances 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 229910000601 superalloy Inorganic materials 0.000 description 4
- -1 Textron's SCS-6 Chemical compound 0.000 description 3
- 229920001296 polysiloxane Polymers 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- 230000035882 stress Effects 0.000 description 3
- 238000000626 liquid-phase infiltration Methods 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229920002134 Carboxymethyl cellulose Polymers 0.000 description 1
- INJRKJPEYSAMPD-UHFFFAOYSA-N aluminum;silicic acid;hydrate Chemical compound O.[Al].[Al].O[Si](O)(O)O INJRKJPEYSAMPD-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 235000010948 carboxy methyl cellulose Nutrition 0.000 description 1
- 229920006184 cellulose methylcellulose Polymers 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000012710 chemistry, manufacturing and control Methods 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- GUJOJGAPFQRJSV-UHFFFAOYSA-N dialuminum;dioxosilane;oxygen(2-);hydrate Chemical compound O.[O-2].[O-2].[O-2].[Al+3].[Al+3].O=[Si]=O.O=[Si]=O.O=[Si]=O.O=[Si]=O GUJOJGAPFQRJSV-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000011256 inorganic filler Substances 0.000 description 1
- 229910003475 inorganic filler Inorganic materials 0.000 description 1
- 239000010443 kyanite Substances 0.000 description 1
- 229910052850 kyanite Inorganic materials 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000010445 mica Substances 0.000 description 1
- 229910052618 mica group Inorganic materials 0.000 description 1
- 229910052901 montmorillonite Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 229910052903 pyrophyllite Inorganic materials 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000012783 reinforcing fiber Substances 0.000 description 1
- 229910052594 sapphire Inorganic materials 0.000 description 1
- 239000010980 sapphire Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 150000004760 silicates Chemical class 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000000454 talc Substances 0.000 description 1
- 229910052623 talc Inorganic materials 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 239000010456 wollastonite Substances 0.000 description 1
- 229910052882 wollastonite Inorganic materials 0.000 description 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
- F23R3/007—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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
-
- 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
- F05B2230/00—Manufacture
- F05B2230/60—Assembly methods
- F05B2230/604—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins
- F05B2230/606—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins using maintaining alignment while permitting differential dilatation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2212/00—Burner material specifications
- F23D2212/10—Burner material specifications ceramic
- F23D2212/103—Fibres
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Gasket Seals (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Compositions Of Oxide Ceramics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US567557 | 2000-05-05 | ||
| US09/567,557 US6397603B1 (en) | 2000-05-05 | 2000-05-05 | Conbustor having a ceramic matrix composite liner |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE60122819D1 DE60122819D1 (de) | 2006-10-19 |
| DE60122819T2 true DE60122819T2 (de) | 2007-10-11 |
Family
ID=24267649
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE60122819T Expired - Lifetime DE60122819T2 (de) | 2000-05-05 | 2001-03-05 | Brennkammer mit Brennkammerwand aus Verbundwerkstoff mit keramischer Matrix |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US6397603B1 (https=) |
| EP (1) | EP1152191B1 (https=) |
| JP (1) | JP5289653B2 (https=) |
| DE (1) | DE60122819T2 (https=) |
| PL (1) | PL203961B1 (https=) |
| RU (1) | RU2266477C2 (https=) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102013007443A1 (de) * | 2013-04-30 | 2014-10-30 | Rolls-Royce Deutschland Ltd & Co Kg | Brennerdichtung für Gasturbinen-Brennkammerkopf und Hitzeschild |
Families Citing this family (107)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3600911B2 (ja) * | 2001-01-25 | 2004-12-15 | 川崎重工業株式会社 | 環状燃焼器のライナ支持構造 |
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| FR2825784B1 (fr) * | 2001-06-06 | 2003-08-29 | Snecma Moteurs | Accrochage de chambre de combustion cmc de turbomachine utilisant les trous de dilution |
| FR2825780B1 (fr) * | 2001-06-06 | 2003-08-29 | Snecma Moteurs | Architecure de chambre de combustion de turbomachine en materiau a matrice ceramique |
| FR2825781B1 (fr) * | 2001-06-06 | 2004-02-06 | Snecma Moteurs | Montage elastique de chambre ce combustion cmc de turbomachine dans un carter metallique |
| FR2825785B1 (fr) * | 2001-06-06 | 2004-08-27 | Snecma Moteurs | Liaison de chambre de combustion cmc de turbomachine en deux parties |
| FR2825783B1 (fr) * | 2001-06-06 | 2003-11-07 | Snecma Moteurs | Accrochage de chambre de combustion cmc de turbomachine par pattes brasees |
| JP4008212B2 (ja) * | 2001-06-29 | 2007-11-14 | 三菱重工業株式会社 | フランジ付中空構造物 |
| CA2690461C (en) * | 2001-07-06 | 2010-12-21 | 3M Innovative Properties Company | Inorganic fiber substrates for exhaust systems and methods of making same |
| US20030165638A1 (en) * | 2001-07-06 | 2003-09-04 | Louks John W. | Inorganic fiber substrates for exhaust systems and methods of making same |
| JP3851161B2 (ja) * | 2001-12-25 | 2006-11-29 | 株式会社日立製作所 | ガスタービン燃焼器 |
| JP3848155B2 (ja) * | 2001-12-25 | 2006-11-22 | 株式会社日立製作所 | ガスタービン燃焼器 |
| US7572311B2 (en) | 2002-10-28 | 2009-08-11 | Geo2 Technologies, Inc. | Highly porous mullite particulate filter substrate |
| US7582270B2 (en) | 2002-10-28 | 2009-09-01 | Geo2 Technologies, Inc. | Multi-functional substantially fibrous mullite filtration substrates and devices |
| US6946013B2 (en) | 2002-10-28 | 2005-09-20 | Geo2 Technologies, Inc. | Ceramic exhaust filter |
| US7574796B2 (en) | 2002-10-28 | 2009-08-18 | Geo2 Technologies, Inc. | Nonwoven composites and related products and methods |
| US6904757B2 (en) | 2002-12-20 | 2005-06-14 | General Electric Company | Mounting assembly for the forward end of a ceramic matrix composite liner in a gas turbine engine combustor |
| US6895761B2 (en) * | 2002-12-20 | 2005-05-24 | General Electric Company | Mounting assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor |
| CA2512201A1 (en) * | 2003-01-08 | 2005-02-17 | 3M Innovative Properties Company | Ceramic fiber composite and method for making the same |
| US6775985B2 (en) | 2003-01-14 | 2004-08-17 | General Electric Company | Support assembly for a gas turbine engine combustor |
| US6920762B2 (en) * | 2003-01-14 | 2005-07-26 | General Electric Company | Mounting assembly for igniter in a gas turbine engine combustor having a ceramic matrix composite liner |
| US7007480B2 (en) * | 2003-04-09 | 2006-03-07 | Honeywell International, Inc. | Multi-axial pivoting combustor liner in gas turbine engine |
| FR2871847B1 (fr) * | 2004-06-17 | 2006-09-29 | Snecma Moteurs Sa | Montage d'un distributeur de turbine sur une chambre de combustion a parois en cmc dans une turbine a gaz |
| FR2871845B1 (fr) * | 2004-06-17 | 2009-06-26 | Snecma Moteurs Sa | Montage de chambre de combustion de turbine a gaz avec distributeur integre de turbine haute pression |
| US7237389B2 (en) * | 2004-11-18 | 2007-07-03 | Siemens Power Generation, Inc. | Attachment system for ceramic combustor liner |
| US7300621B2 (en) * | 2005-03-16 | 2007-11-27 | Siemens Power Generation, Inc. | Method of making a ceramic matrix composite utilizing partially stabilized fibers |
| US7647779B2 (en) | 2005-04-27 | 2010-01-19 | United Technologies Corporation | Compliant metal support for ceramic combustor liner in a gas turbine engine |
| FR2887015B1 (fr) * | 2005-06-14 | 2010-09-24 | Snecma Moteurs | Assemblage d'une chambre de combustion annulaire de turbomachine |
| US7546743B2 (en) * | 2005-10-12 | 2009-06-16 | General Electric Company | Bolting configuration for joining ceramic combustor liner to metal mounting attachments |
| US7762076B2 (en) * | 2005-10-20 | 2010-07-27 | United Technologies Corporation | Attachment of a ceramic combustor can |
| US7682578B2 (en) | 2005-11-07 | 2010-03-23 | Geo2 Technologies, Inc. | Device for catalytically reducing exhaust |
| US7211232B1 (en) | 2005-11-07 | 2007-05-01 | Geo2 Technologies, Inc. | Refractory exhaust filtering method and apparatus |
| US7682577B2 (en) | 2005-11-07 | 2010-03-23 | Geo2 Technologies, Inc. | Catalytic exhaust device for simplified installation or replacement |
| US7493771B2 (en) * | 2005-11-30 | 2009-02-24 | General Electric Company | Methods and apparatuses for assembling a gas turbine engine |
| US7523616B2 (en) * | 2005-11-30 | 2009-04-28 | General Electric Company | Methods and apparatuses for assembling a gas turbine engine |
| US7637110B2 (en) * | 2005-11-30 | 2009-12-29 | General Electric Company | Methods and apparatuses for assembling a gas turbine engine |
| US7665307B2 (en) * | 2005-12-22 | 2010-02-23 | United Technologies Corporation | Dual wall combustor liner |
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| US7563415B2 (en) | 2006-03-03 | 2009-07-21 | Geo2 Technologies, Inc | Catalytic exhaust filter device |
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| DE102006026969A1 (de) * | 2006-06-09 | 2007-12-13 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammerwand für eine mager-brennende Gasturbinenbrennkammer |
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| US20080149255A1 (en) * | 2006-12-20 | 2008-06-26 | General Electric Company | Ceramic composite article manufacture using thin plies |
| DE102006060857B4 (de) | 2006-12-22 | 2014-02-13 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | CMC-Brennkammerauskleidung in Doppelschichtbauweise |
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| US11149646B2 (en) | 2015-09-02 | 2021-10-19 | General Electric Company | Piston ring assembly for a turbine engine |
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| US11226099B2 (en) | 2019-10-11 | 2022-01-18 | Rolls-Royce Corporation | Combustor liner for a gas turbine engine with ceramic matrix composite components |
| FR3109430B1 (fr) * | 2020-04-17 | 2022-12-02 | Safran Aircraft Engines | Bougie pour chambre de combustion monobloc |
| US11466855B2 (en) | 2020-04-17 | 2022-10-11 | Rolls-Royce North American Technologies Inc. | Gas turbine engine combustor with ceramic matrix composite liner |
| CN112503574A (zh) * | 2020-10-30 | 2021-03-16 | 南京航空航天大学 | 陶瓷基环形火焰筒 |
| US11867402B2 (en) | 2021-03-19 | 2024-01-09 | Rtx Corporation | CMC stepped combustor liner |
| US11859819B2 (en) | 2021-10-15 | 2024-01-02 | General Electric Company | Ceramic composite combustor dome and liners |
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| US2547619A (en) * | 1948-11-27 | 1951-04-03 | Gen Electric | Combustor with sectional housing and liner |
| GB1059199A (en) * | 1965-10-20 | 1967-02-15 | Rolls Royce | Flame tube |
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| US4016718A (en) * | 1975-07-21 | 1977-04-12 | United Technologies Corporation | Gas turbine engine having an improved transition duct support |
| US4030875A (en) * | 1975-12-22 | 1977-06-21 | General Electric Company | Integrated ceramic-metal combustor |
| DE2713414A1 (de) * | 1977-03-26 | 1978-09-28 | Motoren Turbinen Union | Brennkammer fuer gasturbinentriebwerke |
| JPS56102614A (en) * | 1980-01-17 | 1981-08-17 | Nissan Motor Co Ltd | Gas turbine combustor |
| US4363208A (en) * | 1980-11-10 | 1982-12-14 | General Motors Corporation | Ceramic combustor mounting |
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| JPS62176448U (https=) * | 1986-04-30 | 1987-11-09 | ||
| FR2624953B1 (fr) * | 1987-12-16 | 1990-04-20 | Snecma | Chambre de combustion, pour turbomachines, possedant un convergent a doubles parois |
| US5553455A (en) | 1987-12-21 | 1996-09-10 | United Technologies Corporation | Hybrid ceramic article |
| US5488017A (en) * | 1989-04-14 | 1996-01-30 | General Electric Company | Fibert reinforced ceramic matrix composite member |
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| JP2597800B2 (ja) | 1992-06-12 | 1997-04-09 | ゼネラル・エレクトリック・カンパニイ | ガスタービンエンジン用燃焼器 |
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| US5851679A (en) * | 1996-12-17 | 1998-12-22 | General Electric Company | Multilayer dielectric stack coated part for contact with combustion gases |
-
2000
- 2000-05-05 US US09/567,557 patent/US6397603B1/en not_active Expired - Lifetime
-
2001
- 2001-03-02 JP JP2001057521A patent/JP5289653B2/ja not_active Expired - Fee Related
- 2001-03-05 RU RU2001106166/06A patent/RU2266477C2/ru not_active IP Right Cessation
- 2001-03-05 PL PL346261A patent/PL203961B1/pl unknown
- 2001-03-05 DE DE60122819T patent/DE60122819T2/de not_active Expired - Lifetime
- 2001-03-05 EP EP01301951A patent/EP1152191B1/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102013007443A1 (de) * | 2013-04-30 | 2014-10-30 | Rolls-Royce Deutschland Ltd & Co Kg | Brennerdichtung für Gasturbinen-Brennkammerkopf und Hitzeschild |
| US10041415B2 (en) | 2013-04-30 | 2018-08-07 | Rolls-Royce Deutschland Ltd & Co Kg | Burner seal for gas-turbine combustion chamber head and heat shield |
Also Published As
| Publication number | Publication date |
|---|---|
| PL346261A1 (en) | 2001-11-19 |
| US6397603B1 (en) | 2002-06-04 |
| EP1152191A3 (en) | 2001-12-19 |
| JP2001317739A (ja) | 2001-11-16 |
| PL203961B1 (pl) | 2009-11-30 |
| JP5289653B2 (ja) | 2013-09-11 |
| RU2266477C2 (ru) | 2005-12-20 |
| EP1152191A2 (en) | 2001-11-07 |
| DE60122819D1 (de) | 2006-10-19 |
| EP1152191B1 (en) | 2006-09-06 |
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