JP2008095106A5 - - Google Patents
Download PDFInfo
- Publication number
- JP2008095106A5 JP2008095106A5 JP2007265189A JP2007265189A JP2008095106A5 JP 2008095106 A5 JP2008095106 A5 JP 2008095106A5 JP 2007265189 A JP2007265189 A JP 2007265189A JP 2007265189 A JP2007265189 A JP 2007265189A JP 2008095106 A5 JP2008095106 A5 JP 2008095106A5
- Authority
- JP
- Japan
- Prior art keywords
- high temperature
- temperature seal
- swelling
- short side
- matrix composite
- 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.)
- Granted
Links
- 230000008961 swelling Effects 0.000 claims 5
- 239000011153 ceramic matrix composite Substances 0.000 claims 4
- 239000011248 coating agent Substances 0.000 claims 4
- 238000000576 coating method Methods 0.000 claims 4
- 230000003647 oxidation Effects 0.000 claims 3
- 238000007254 oxidation reaction Methods 0.000 claims 3
- 230000004888 barrier function Effects 0.000 claims 1
- 230000007613 environmental effect Effects 0.000 claims 1
- 239000000835 fiber Substances 0.000 claims 1
- 230000001590 oxidative effect Effects 0.000 claims 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims 1
- 229910010271 silicon carbide Inorganic materials 0.000 claims 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/581,250 | 2006-10-16 | ||
| US11/581,250 US7771159B2 (en) | 2006-10-16 | 2006-10-16 | High temperature seals and high temperature sealing systems |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2008095106A JP2008095106A (ja) | 2008-04-24 |
| JP2008095106A5 true JP2008095106A5 (enExample) | 2012-10-18 |
| JP5512076B2 JP5512076B2 (ja) | 2014-06-04 |
Family
ID=38896150
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2007265189A Expired - Fee Related JP5512076B2 (ja) | 2006-10-16 | 2007-10-11 | 高温シール及び高温封止系 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US7771159B2 (enExample) |
| EP (1) | EP1914454B1 (enExample) |
| JP (1) | JP5512076B2 (enExample) |
| CN (1) | CN101165374B (enExample) |
Families Citing this family (48)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100061847A1 (en) * | 2008-09-09 | 2010-03-11 | General Electric Company | Steam turbine part including ceramic matrix composite (cmc) |
| SI2598263T1 (sl) * | 2010-07-26 | 2019-09-30 | Corts Engineering Gmbh & Co. Kg | Tekočinsko izravnana plošča ležaja |
| US8613451B2 (en) * | 2010-11-29 | 2013-12-24 | General Electric Company | Cloth seal for turbo-machinery |
| FR2974401B1 (fr) * | 2011-04-22 | 2013-06-14 | Commissariat Energie Atomique | Joint d'etancheite metallique a ame ceramique |
| US9534783B2 (en) * | 2011-07-21 | 2017-01-03 | United Technologies Corporation | Insert adjacent to a heat shield element for a gas turbine engine combustor |
| US9353635B2 (en) | 2011-08-16 | 2016-05-31 | General Electric Company | Seal end attachment |
| US9188228B2 (en) * | 2011-10-26 | 2015-11-17 | General Electric Company | Layered seal for turbomachinery |
| US20130134678A1 (en) * | 2011-11-29 | 2013-05-30 | General Electric Company | Shim seal assemblies and assembly methods for stationary components of rotary machines |
| US9169567B2 (en) | 2012-03-30 | 2015-10-27 | General Electric Company | Components having tab members |
| US9671030B2 (en) | 2012-03-30 | 2017-06-06 | General Electric Company | Metallic seal assembly, turbine component, and method of regulating airflow in turbo-machinery |
| US9587632B2 (en) | 2012-03-30 | 2017-03-07 | General Electric Company | Thermally-controlled component and thermal control process |
| US9316109B2 (en) * | 2012-04-10 | 2016-04-19 | General Electric Company | Turbine shroud assembly and method of forming |
| WO2014130147A1 (en) * | 2013-02-23 | 2014-08-28 | Jun Shi | Edge seal for gas turbine engine ceramic matrix composite component |
| WO2014158276A2 (en) * | 2013-03-05 | 2014-10-02 | Rolls-Royce Corporation | Structure and method for providing compliance and sealing between ceramic and metallic structures |
| US9757920B2 (en) | 2013-03-15 | 2017-09-12 | Rolls-Royce Corporation | Flexible ceramic matrix composite seal |
| US9719420B2 (en) * | 2014-06-02 | 2017-08-01 | General Electric Company | Gas turbine component and process for producing gas turbine component |
| US9926790B2 (en) | 2014-07-21 | 2018-03-27 | Rolls-Royce Corporation | Composite turbine components adapted for use with strip seals |
| US10281045B2 (en) | 2015-02-20 | 2019-05-07 | Rolls-Royce North American Technologies Inc. | Apparatus and methods for sealing components in gas turbine engines |
| EP3088679A1 (en) | 2015-04-30 | 2016-11-02 | Rolls-Royce Corporation | Seal for a gas turbine engine assembly |
| FR3036435B1 (fr) * | 2015-05-22 | 2020-01-24 | Safran Ceramics | Ensemble d'anneau de turbine |
| US9759079B2 (en) | 2015-05-28 | 2017-09-12 | Rolls-Royce Corporation | Split line flow path seals |
| US20170030211A1 (en) * | 2015-07-28 | 2017-02-02 | General Electric Company | Seals with a conformable coating for turbomachinery |
| US10458263B2 (en) | 2015-10-12 | 2019-10-29 | Rolls-Royce North American Technologies Inc. | Turbine shroud with sealing features |
| US10301955B2 (en) | 2016-11-29 | 2019-05-28 | Rolls-Royce North American Technologies Inc. | Seal assembly for gas turbine engine components |
| US10443420B2 (en) | 2017-01-11 | 2019-10-15 | Rolls-Royce North American Technologies Inc. | Seal assembly for gas turbine engine components |
| US10577977B2 (en) | 2017-02-22 | 2020-03-03 | Rolls-Royce Corporation | Turbine shroud with biased retaining ring |
| US10718226B2 (en) | 2017-11-21 | 2020-07-21 | Rolls-Royce Corporation | Ceramic matrix composite component assembly and seal |
| FR3085708B1 (fr) * | 2018-09-12 | 2020-11-27 | Safran Helicopter Engines | Dispositif d'etancheite ameliore pour ensemble rotatif de turbomachine |
| US20200095880A1 (en) * | 2018-09-24 | 2020-03-26 | United Technologies Corporation | Featherseal formed of cmc materials |
| US11220924B2 (en) * | 2019-09-26 | 2022-01-11 | Raytheon Technologies Corporation | Double box composite seal assembly with insert for gas turbine engine |
| US11519282B2 (en) | 2019-11-11 | 2022-12-06 | Raytheon Technologies Corporation | Ceramic matrix composite-based seal |
| US20240173743A1 (en) * | 2022-11-29 | 2024-05-30 | Raytheon Technologies Corporation | Slot with coating and method of coating a slot |
| US12138720B2 (en) | 2022-12-13 | 2024-11-12 | Rtx Corporation | Article and method of making an article by chemical vapor infiltration |
| US12188365B1 (en) | 2023-12-04 | 2025-01-07 | Rolls-Royce Corporation | Method and apparatus for ceramic matrix composite turbine shroud assembly |
| US12286906B1 (en) | 2023-12-04 | 2025-04-29 | Rolls-Royce Corporation | Locating plate for use with turbine shroud assemblies |
| US12152499B1 (en) | 2023-12-04 | 2024-11-26 | Rolls-Royce Corporation | Turbine shroud segments with strip seal assemblies having dampened ends |
| US12241376B1 (en) | 2023-12-04 | 2025-03-04 | Rolls-Royce Corporation | Locating plate for use with turbine shroud assemblies |
| US12286885B1 (en) | 2023-12-04 | 2025-04-29 | Rolls-Royce Corporation | Turbine assembly with confronting vane and turbine shroud segment |
| US12158072B1 (en) | 2023-12-04 | 2024-12-03 | Rolls-Royce Corporation | Turbine shroud segments with damping strip seals |
| US12421862B2 (en) | 2023-12-04 | 2025-09-23 | Rolls-Royce Corporation | Turbine shroud assembly with angled cooling holes |
| US12421870B1 (en) | 2024-04-30 | 2025-09-23 | Rolls-Royce Corporation | Pin mounted ceramic matrix composite heat shields with impingement cooling |
| US12258880B1 (en) | 2024-05-30 | 2025-03-25 | Rolls-Royce Corporation | Turbine shroud assemblies with inter-segment strip seal |
| US12416241B1 (en) | 2024-05-30 | 2025-09-16 | Rolls-Royce Corporation | Turbine shroud assemblies with strip seals |
| US12305525B1 (en) | 2024-05-30 | 2025-05-20 | Rolls-Royce Corporation | Turbine shroud assemblies with rod seal and strip seals |
| US12215593B1 (en) | 2024-05-30 | 2025-02-04 | Rolls-Royce Corporation | Turbine shroud assembly with inter-segment damping |
| US12410725B1 (en) | 2024-05-31 | 2025-09-09 | Rolls-Royce Corporation | Turbine shroud assemblies with air activated pistons for biasing buffer cavity seals |
| US12352176B1 (en) | 2024-05-31 | 2025-07-08 | Rolls-Royce Corporation | Turbine shroud assemblies with channels for buffer cavity seal thermal management |
| US12228044B1 (en) | 2024-06-26 | 2025-02-18 | Rolls-Royce Corporation | Turbine shroud system with ceramic matrix composite segments and dual inter-segment seals |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3322433A (en) * | 1964-03-10 | 1967-05-30 | Minnesota Rubber Co | Sealing ring and method of making same |
| FR2724973B1 (fr) * | 1982-12-31 | 1996-12-13 | Snecma | Dispositif d'etancheite d'aubages mobiles de turbomachine avec controle actif des jeux en temps reel et methode de determination dudit dispositif |
| JPH053964Y2 (enExample) * | 1987-11-06 | 1993-01-29 | ||
| JP2639674B2 (ja) * | 1988-02-09 | 1997-08-13 | 三菱電線工業株式会社 | エンジンの排気系用ガスケット |
| FR2635773B1 (fr) * | 1988-08-31 | 1992-02-14 | Aerospatiale | Materiau composite a fibres de renforcement en carbone et son procede de fabrication |
| JP3303642B2 (ja) * | 1995-03-30 | 2002-07-22 | 三菱自動車工業株式会社 | 蓄熱式熱交換器、該熱交換器等に使用する耐熱摺動体 |
| US6410148B1 (en) * | 1999-04-15 | 2002-06-25 | General Electric Co. | Silicon based substrate with environmental/ thermal barrier layer |
| US6464456B2 (en) * | 2001-03-07 | 2002-10-15 | General Electric Company | Turbine vane assembly including a low ductility vane |
| JP2003321277A (ja) * | 2002-04-30 | 2003-11-11 | Ishikawajima Harima Heavy Ind Co Ltd | セラミックス基複合材料とその製造方法 |
| US6893214B2 (en) * | 2002-12-20 | 2005-05-17 | General Electric Company | Shroud segment and assembly with surface recessed seal bridging adjacent members |
| US7004375B2 (en) * | 2003-05-23 | 2006-02-28 | National Starch And Chemical Investment Holding Corporation | Pre-applied fluxing underfill composition having pressure sensitive adhesive properties |
| EP1484427A3 (en) * | 2003-06-06 | 2005-10-26 | General Electric Company | Top coating system for industrial turbine nozzle airfoils and other hot gas path components and related method |
| US6942203B2 (en) | 2003-11-04 | 2005-09-13 | General Electric Company | Spring mass damper system for turbine shrouds |
| JP4470708B2 (ja) * | 2004-11-22 | 2010-06-02 | 宇部興産株式会社 | 複合材料およびその製造方法 |
| US7238002B2 (en) * | 2005-11-03 | 2007-07-03 | General Electric Company | Damper seal system and method |
-
2006
- 2006-10-16 US US11/581,250 patent/US7771159B2/en not_active Expired - Fee Related
-
2007
- 2007-10-11 JP JP2007265189A patent/JP5512076B2/ja not_active Expired - Fee Related
- 2007-10-12 EP EP07254046.1A patent/EP1914454B1/en not_active Not-in-force
- 2007-10-16 CN CN200710162674.1A patent/CN101165374B/zh not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP2008095106A5 (enExample) | ||
| BR112012005997A2 (pt) | artigos que incluem um substrato poroso que tem uma camada conformal sobre os mesmos | |
| JP6730034B2 (ja) | Cmcタービン構成部品及びcmcタービン構成部品の形成方法 | |
| WO2007084564A3 (en) | Insulated glass unit with sealant composition having reduced permeability to gas | |
| EP2434102A3 (en) | Gas turbine shroud with ceramic abradable layer | |
| EP1889949A3 (en) | Sodium containing thermal barrier coating | |
| WO2008051261A3 (en) | Sealant composition containing inorganic-organic nanocomposite filler | |
| WO2014150082A8 (en) | Unidirectional multi-path lumber kilns | |
| BRPI0805089A2 (pt) | defletor térmico | |
| EP2325543B8 (de) | Gasbehälter und verfahren zur herstellung des gasbehälters | |
| BRPI0909078A8 (pt) | forno de fundição de vidro | |
| WO2011139582A3 (en) | Exhaust-gas turbocharger | |
| JP2013139816A5 (enExample) | ||
| WO2010075386A3 (en) | Rotary vane engines with movable rotors,and engine systems comprising same | |
| WO2012021270A3 (en) | Mounting mat with flexible edge protection and exhaust gas treatment device incorporating the mounting mat | |
| BRPI0700671A (pt) | método para o revestimento de componentes de turbinas a gás | |
| JP2005315264A5 (enExample) | ||
| BR112012002162A2 (pt) | peça comportando uma substrato formado de um material condutor de elétrons, e, sobre pelo menos uma parte da superfície do substrato, um revestimento comportando uma camada de revestimento cerâmico, e, utilização de uma peça | |
| JP2009007185A5 (enExample) | ||
| EA201001666A1 (ru) | Буровой двигатель в сборе | |
| EP1734025A3 (en) | Thermal/Environmental barrier coating system for silicon-containing materials | |
| AU2003253028A1 (en) | Composition for producing a thermal insulation coating | |
| WO2007037854A3 (en) | Gas-filled shroud for arctube | |
| WO2007087115A3 (en) | Molecular fan | |
| MX2012006236A (es) | Capas multiples de oxido para aplicaciones y lamparas de alta temperatura. |