JP4097941B2 - 低延性の翼を備えたタービン翼組立体 - Google Patents
低延性の翼を備えたタービン翼組立体 Download PDFInfo
- Publication number
- JP4097941B2 JP4097941B2 JP2001400493A JP2001400493A JP4097941B2 JP 4097941 B2 JP4097941 B2 JP 4097941B2 JP 2001400493 A JP2001400493 A JP 2001400493A JP 2001400493 A JP2001400493 A JP 2001400493A JP 4097941 B2 JP4097941 B2 JP 4097941B2
- Authority
- JP
- Japan
- Prior art keywords
- wing
- support
- assembly
- cte
- opening wall
- 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
- 239000000463 material Substances 0.000 claims description 47
- 229910001092 metal group alloy Inorganic materials 0.000 claims description 12
- 239000011153 ceramic matrix composite Substances 0.000 claims description 11
- 239000000919 ceramic Substances 0.000 claims description 8
- 229910000943 NiAl Inorganic materials 0.000 claims description 7
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 claims description 7
- 239000012530 fluid Substances 0.000 claims description 7
- 229910000765 intermetallic Inorganic materials 0.000 claims description 5
- 238000001816 cooling Methods 0.000 description 12
- 229910045601 alloy Inorganic materials 0.000 description 10
- 239000000956 alloy Substances 0.000 description 10
- 229910000601 superalloy Inorganic materials 0.000 description 8
- 239000002184 metal Substances 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 238000005219 brazing Methods 0.000 description 3
- 230000015556 catabolic process Effects 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 3
- 230000008602 contraction Effects 0.000 description 3
- 238000006731 degradation reaction Methods 0.000 description 3
- 239000000835 fiber Substances 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 229910000856 hastalloy Inorganic materials 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000005272 metallurgy Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 239000011226 reinforced ceramic Substances 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3084—Fixing blades to rotors; Blade roots ; Blade spacers the blades being made of ceramics
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/801118 | 2001-03-07 | ||
| US09/801,118 US6464456B2 (en) | 2001-03-07 | 2001-03-07 | Turbine vane assembly including a low ductility vane |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2002295202A JP2002295202A (ja) | 2002-10-09 |
| JP2002295202A5 JP2002295202A5 (enExample) | 2005-05-26 |
| JP4097941B2 true JP4097941B2 (ja) | 2008-06-11 |
Family
ID=25180233
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2001400493A Expired - Lifetime JP4097941B2 (ja) | 2001-03-07 | 2001-12-28 | 低延性の翼を備えたタービン翼組立体 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6464456B2 (enExample) |
| EP (1) | EP1239119B1 (enExample) |
| JP (1) | JP4097941B2 (enExample) |
| DE (1) | DE60227307D1 (enExample) |
| ES (1) | ES2307709T3 (enExample) |
Families Citing this family (100)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6485655B1 (en) * | 2001-08-02 | 2002-11-26 | General Electric Company | Method and apparatus for retaining an internal coating during article repair |
| US6939106B2 (en) * | 2002-12-11 | 2005-09-06 | General Electric Company | Sealing of steam turbine nozzle hook leakages using a braided rope seal |
| US6832892B2 (en) * | 2002-12-11 | 2004-12-21 | General Electric Company | Sealing of steam turbine bucket hook leakages using a braided rope seal |
| US6893214B2 (en) * | 2002-12-20 | 2005-05-17 | General Electric Company | Shroud segment and assembly with surface recessed seal bridging adjacent members |
| EP1433925A1 (fr) * | 2002-12-24 | 2004-06-30 | Techspace Aero S.A. | Procédé de solidarisation d'une aube sur virole |
| US7080971B2 (en) * | 2003-03-12 | 2006-07-25 | Florida Turbine Technologies, Inc. | Cooled turbine spar shell blade construction |
| GB2400415B (en) | 2003-04-11 | 2006-03-08 | Rolls Royce Plc | Vane mounting |
| GB2402717B (en) * | 2003-06-10 | 2006-05-10 | Rolls Royce Plc | A vane assembly for a gas turbine engine |
| US7101150B2 (en) * | 2004-05-11 | 2006-09-05 | Power Systems Mfg, Llc | Fastened vane assembly |
| US7052234B2 (en) * | 2004-06-23 | 2006-05-30 | General Electric Company | Turbine vane collar seal |
| US7153096B2 (en) | 2004-12-02 | 2006-12-26 | Siemens Power Generation, Inc. | Stacked laminate CMC turbine vane |
| US7198458B2 (en) | 2004-12-02 | 2007-04-03 | Siemens Power Generation, Inc. | Fail safe cooling system for turbine vanes |
| US7247002B2 (en) * | 2004-12-02 | 2007-07-24 | Siemens Power Generation, Inc. | Lamellate CMC structure with interlock to metallic support structure |
| US7255535B2 (en) | 2004-12-02 | 2007-08-14 | Albrecht Harry A | Cooling systems for stacked laminate CMC vane |
| US7326030B2 (en) * | 2005-02-02 | 2008-02-05 | Siemens Power Generation, Inc. | Support system for a composite airfoil in a turbine engine |
| US7329087B2 (en) * | 2005-09-19 | 2008-02-12 | General Electric Company | Seal-less CMC vane to platform interfaces |
| US20070122266A1 (en) * | 2005-10-14 | 2007-05-31 | General Electric Company | Assembly for controlling thermal stresses in ceramic matrix composite articles |
| US7600970B2 (en) * | 2005-12-08 | 2009-10-13 | General Electric Company | Ceramic matrix composite vane seals |
| US7452189B2 (en) * | 2006-05-03 | 2008-11-18 | United Technologies Corporation | Ceramic matrix composite turbine engine vane |
| US7950234B2 (en) * | 2006-10-13 | 2011-05-31 | Siemens Energy, Inc. | Ceramic matrix composite turbine engine components with unitary stiffening frame |
| US7771159B2 (en) * | 2006-10-16 | 2010-08-10 | General Electric Company | High temperature seals and high temperature sealing systems |
| US7824152B2 (en) * | 2007-05-09 | 2010-11-02 | Siemens Energy, Inc. | Multivane segment mounting arrangement for a gas turbine |
| US8210803B2 (en) * | 2007-06-28 | 2012-07-03 | United Technologies Corporation | Ceramic matrix composite turbine engine vane |
| US8206098B2 (en) * | 2007-06-28 | 2012-06-26 | United Technologies Corporation | Ceramic matrix composite turbine engine vane |
| GB2455785B (en) * | 2007-12-21 | 2009-11-11 | Rolls Royce Plc | Annular component |
| US8118546B2 (en) * | 2008-08-20 | 2012-02-21 | Siemens Energy, Inc. | Grid ceramic matrix composite structure for gas turbine shroud ring segment |
| US8292580B2 (en) * | 2008-09-18 | 2012-10-23 | Siemens Energy, Inc. | CMC vane assembly apparatus and method |
| FR2948965B1 (fr) * | 2009-08-06 | 2012-11-30 | Snecma | Etage redresseur pour une turbomachine |
| US8967078B2 (en) * | 2009-08-27 | 2015-03-03 | United Technologies Corporation | Abrasive finish mask and method of polishing a component |
| EP2295722B1 (en) * | 2009-09-09 | 2019-11-06 | Ansaldo Energia IP UK Limited | Blade of a turbine |
| US9080448B2 (en) * | 2009-12-29 | 2015-07-14 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine vanes |
| US8454303B2 (en) * | 2010-01-14 | 2013-06-04 | General Electric Company | Turbine nozzle assembly |
| US8668442B2 (en) * | 2010-06-30 | 2014-03-11 | Honeywell International Inc. | Turbine nozzles and methods of manufacturing the same |
| FR2974593B1 (fr) * | 2011-04-28 | 2015-11-13 | Snecma | Moteur a turbine comportant une protection metallique d'une piece composite |
| US9726028B2 (en) | 2011-06-29 | 2017-08-08 | Siemens Energy, Inc. | Ductile alloys for sealing modular component interfaces |
| US8939727B2 (en) * | 2011-09-08 | 2015-01-27 | Siemens Energy, Inc. | Turbine blade and non-integral platform with pin attachment |
| US9097124B2 (en) * | 2012-01-24 | 2015-08-04 | United Technologies Corporation | Gas turbine engine stator vane assembly with inner shroud |
| US9951639B2 (en) * | 2012-02-10 | 2018-04-24 | Pratt & Whitney Canada Corp. | Vane assemblies for gas turbine engines |
| US9249669B2 (en) | 2012-04-05 | 2016-02-02 | General Electric Company | CMC blade with pressurized internal cavity for erosion control |
| EP2660429A1 (en) | 2012-05-03 | 2013-11-06 | Siemens Aktiengesellschaft | Sealing arrangement for a nozzle guide vane and gas turbine |
| US9080457B2 (en) | 2013-02-23 | 2015-07-14 | Rolls-Royce Corporation | Edge seal for gas turbine engine ceramic matrix composite component |
| US9556750B2 (en) * | 2013-03-04 | 2017-01-31 | Rolls-Royce North American Technologies, Inc. | Compartmentalization of cooling air flow in a structure comprising a CMC component |
| US9777584B2 (en) * | 2013-03-07 | 2017-10-03 | Rolls-Royce Plc | Outboard insertion system of variable guide vanes or stationary vanes |
| US10590798B2 (en) | 2013-03-25 | 2020-03-17 | United Technologies Corporation | Non-integral blade and platform segment for rotor |
| BR112015032787A2 (pt) * | 2013-07-19 | 2017-08-22 | Gen Electric | Aparelho de bocal de turbina |
| EP2886802B1 (fr) * | 2013-12-20 | 2019-04-10 | Safran Aero Boosters SA | Joint de virole interne de dernier étage de compresseur de turbomachine axiale |
| WO2015157751A1 (en) | 2014-04-11 | 2015-10-15 | General Electric Company | Turbine center frame fairing assembly |
| JP6372210B2 (ja) | 2014-07-14 | 2018-08-15 | 株式会社Ihi | セラミックス基複合材料よりなるタービン静翼 |
| US10563522B2 (en) * | 2014-09-22 | 2020-02-18 | Rolls-Royce North American Technologies Inc. | Composite airfoil for a gas turbine engine |
| US10294802B2 (en) | 2014-12-05 | 2019-05-21 | Rolls-Royce American Technologies, Inc. | Turbine engine components with chemical vapor infiltrated isolation layers |
| US9995160B2 (en) | 2014-12-22 | 2018-06-12 | General Electric Company | Airfoil profile-shaped seals and turbine components employing same |
| US10281045B2 (en) | 2015-02-20 | 2019-05-07 | Rolls-Royce North American Technologies Inc. | Apparatus and methods for sealing components in gas turbine engines |
| US9845692B2 (en) * | 2015-05-05 | 2017-12-19 | General Electric Company | Turbine component connection with thermally stress-free fastener |
| US9759079B2 (en) | 2015-05-28 | 2017-09-12 | Rolls-Royce Corporation | Split line flow path seals |
| US10309240B2 (en) * | 2015-07-24 | 2019-06-04 | General Electric Company | Method and system for interfacing a ceramic matrix composite component to a metallic component |
| US9850763B2 (en) | 2015-07-29 | 2017-12-26 | General Electric Company | Article, airfoil component and method for forming article |
| US10458263B2 (en) | 2015-10-12 | 2019-10-29 | Rolls-Royce North American Technologies Inc. | Turbine shroud with sealing features |
| ES2797731T3 (es) | 2016-02-22 | 2020-12-03 | MTU Aero Engines AG | Estructura de sellado de materiales compuestos de fibra cerámica |
| ES2723623T3 (es) * | 2016-02-22 | 2019-08-29 | MTU Aero Engines AG | Carcasa intermedia de turbinas de materiales compuestos de fibra cerámica |
| US10161258B2 (en) * | 2016-03-16 | 2018-12-25 | United Technologies Corporation | Boas rail shield |
| US10132184B2 (en) * | 2016-03-16 | 2018-11-20 | United Technologies Corporation | Boas spring loaded rail shield |
| US10655477B2 (en) | 2016-07-26 | 2020-05-19 | General Electric Company | Turbine components and method for forming turbine components |
| US10746038B2 (en) | 2016-11-17 | 2020-08-18 | Raytheon Technologies Corporation | Airfoil with airfoil piece having radial seal |
| US10458262B2 (en) * | 2016-11-17 | 2019-10-29 | United Technologies Corporation | Airfoil with seal between endwall and airfoil section |
| US10301955B2 (en) | 2016-11-29 | 2019-05-28 | Rolls-Royce North American Technologies Inc. | Seal assembly for gas turbine engine components |
| US10260363B2 (en) | 2016-12-08 | 2019-04-16 | General Electric Company | Additive manufactured seal for insert compartmentalization |
| US10801343B2 (en) * | 2016-12-16 | 2020-10-13 | Pratt & Whitney Canada Corp. | Self retaining face seal design for by-pass stator vanes |
| 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 |
| US10724380B2 (en) * | 2017-08-07 | 2020-07-28 | General Electric Company | CMC blade with internal support |
| FR3070422B1 (fr) | 2017-08-22 | 2021-07-23 | Safran Aircraft Engines | Attache poignard avec joint d'une aube de redresseur |
| US10746035B2 (en) * | 2017-08-30 | 2020-08-18 | General Electric Company | Flow path assemblies for gas turbine engines and assembly methods therefore |
| US10718226B2 (en) | 2017-11-21 | 2020-07-21 | Rolls-Royce Corporation | Ceramic matrix composite component assembly and seal |
| US11181005B2 (en) * | 2018-05-18 | 2021-11-23 | Raytheon Technologies Corporation | Gas turbine engine assembly with mid-vane outer platform gap |
| US10774665B2 (en) | 2018-07-31 | 2020-09-15 | General Electric Company | Vertically oriented seal system for gas turbine vanes |
| US11454128B2 (en) * | 2018-08-06 | 2022-09-27 | General Electric Company | Fairing assembly |
| US10934868B2 (en) * | 2018-09-12 | 2021-03-02 | Rolls-Royce North American Technologies Inc. | Turbine vane assembly with variable position support |
| US11149567B2 (en) | 2018-09-17 | 2021-10-19 | Rolls-Royce Corporation | Ceramic matrix composite load transfer roller joint |
| US11149568B2 (en) | 2018-12-20 | 2021-10-19 | Rolls-Royce Plc | Sliding ceramic matrix composite vane assembly for gas turbine engines |
| PL431184A1 (pl) * | 2019-09-17 | 2021-03-22 | General Electric Company Polska Spółka Z Ograniczoną Odpowiedzialnością | Zespół silnika turbinowego |
| FR3101665B1 (fr) | 2019-10-07 | 2022-04-22 | Safran Aircraft Engines | Distributeur de turbine à aubage en composite à matrice céramique traversé par un circuit de ventilation métallique |
| US11268392B2 (en) | 2019-10-28 | 2022-03-08 | Rolls-Royce Plc | Turbine vane assembly incorporating ceramic matrix composite materials and cooling |
| US11156105B2 (en) | 2019-11-08 | 2021-10-26 | Raytheon Technologies Corporation | Vane with seal |
| US11261748B2 (en) | 2019-11-08 | 2022-03-01 | Raytheon Technologies Corporation | Vane with seal |
| US11174794B2 (en) | 2019-11-08 | 2021-11-16 | Raytheon Technologies Corporation | Vane with seal and retainer plate |
| US11454127B2 (en) | 2019-11-22 | 2022-09-27 | Pratt & Whitney Canada Corp. | Vane for gas turbine engine |
| US11333037B2 (en) * | 2020-02-06 | 2022-05-17 | Raytheon Technologies Corporation | Vane arc segment load path |
| US11319822B2 (en) * | 2020-05-06 | 2022-05-03 | Rolls-Royce North American Technologies Inc. | Hybrid vane segment with ceramic matrix composite airfoils |
| US11879360B2 (en) | 2020-10-30 | 2024-01-23 | General Electric Company | Fabricated CMC nozzle assemblies for gas turbine engines |
| BE1029074B1 (fr) * | 2021-02-02 | 2022-08-29 | Safran Aero Boosters | Ensemble redresseur pour compresseur de turbomachine d'aeronef |
| US11391163B1 (en) * | 2021-03-05 | 2022-07-19 | Raytheon Technologies Corporation | Vane arc segment with seal |
| US11549385B2 (en) * | 2021-05-04 | 2023-01-10 | Raytheon Technologies Corporation | Airfoil assembly with seal plate and seal |
| US11952917B2 (en) * | 2022-08-05 | 2024-04-09 | Rtx Corporation | Vane multiplet with conjoined singlet vanes |
| US11725528B1 (en) * | 2022-08-05 | 2023-08-15 | Raytheon Technologies Corporation | Vane multiplet with common platform joining airfoils |
| US12241374B2 (en) * | 2023-05-10 | 2025-03-04 | Rolls-Royce Corporation | Ceramic matrix composite endwall sealing around vane airfoil of gas turbine engine |
| US20250003346A1 (en) * | 2023-06-28 | 2025-01-02 | General Electric Company | High temperature gas turbine engine |
| US12025029B1 (en) * | 2023-08-21 | 2024-07-02 | Rtx Corporation | Bathtub seal for damping CMC vane platform |
| US12326099B2 (en) | 2023-08-21 | 2025-06-10 | Rtx Corporation | Bathtub seal integrated into CMC vane load path |
| US12281597B2 (en) | 2023-08-21 | 2025-04-22 | Rtx Corporation | CMC vane with rotatable baffle design to accommodate re-stagger |
| US20250067187A1 (en) * | 2023-08-24 | 2025-02-27 | Rtx Corporation | Radial seal between cmc vane and vane support |
Family Cites Families (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3966353A (en) * | 1975-02-21 | 1976-06-29 | Westinghouse Electric Corporation | Ceramic-to-metal (or ceramic) cushion/seal for use with three piece ceramic stationary vane assembly |
| CA1082949A (en) * | 1976-06-03 | 1980-08-05 | William F. Schilling | High-temperature austenitic alloys and articles utilizing the same |
| GB2037901B (en) * | 1978-11-25 | 1982-07-28 | Rolls Royce | Nozzle guide vane assembly |
| DE2851507C2 (de) * | 1978-11-29 | 1982-05-19 | Aktiengesellschaft Kühnle, Kopp & Kausch, 6710 Frankenthal | Isolations-Federkörper und dessen Verwendung |
| DE3003470C2 (de) * | 1980-01-31 | 1982-02-25 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Turbinenleitschaufelaufhängung für Gasturbinenstrahltriebwerke |
| US4768924A (en) * | 1986-07-22 | 1988-09-06 | Pratt & Whitney Canada Inc. | Ceramic stator vane assembly |
| GB2236809B (en) * | 1989-09-22 | 1994-03-16 | Rolls Royce Plc | Improvements in or relating to gas turbine engines |
| US5074752A (en) * | 1990-08-06 | 1991-12-24 | General Electric Company | Gas turbine outlet guide vane mounting assembly |
| FR2685033B1 (fr) * | 1991-12-11 | 1994-02-11 | Snecma | Stator dirigeant l'entree de l'air a l'interieur d'une turbomachine et procede de montage d'une aube de ce stator. |
| US5411370A (en) * | 1994-08-01 | 1995-05-02 | United Technologies Corporation | Vibration damping shroud for a turbomachine vane |
| US5640767A (en) * | 1995-01-03 | 1997-06-24 | Gen Electric | Method for making a double-wall airfoil |
| US5820337A (en) * | 1995-01-03 | 1998-10-13 | General Electric Company | Double wall turbine parts |
| US5626462A (en) * | 1995-01-03 | 1997-05-06 | General Electric Company | Double-wall airfoil |
| US5833773A (en) * | 1995-07-06 | 1998-11-10 | General Electric Company | Nb-base composites |
| US5630700A (en) * | 1996-04-26 | 1997-05-20 | General Electric Company | Floating vane turbine nozzle |
| US5690469A (en) * | 1996-06-06 | 1997-11-25 | United Technologies Corporation | Method and apparatus for replacing a vane assembly in a turbine engine |
| US6000906A (en) * | 1997-09-12 | 1999-12-14 | Alliedsignal Inc. | Ceramic airfoil |
| IL122843A (en) * | 1998-01-02 | 2001-01-11 | Ceramight Composites Ltd | Metal-ceramic laminar-band composite |
-
2001
- 2001-03-07 US US09/801,118 patent/US6464456B2/en not_active Expired - Lifetime
- 2001-12-28 JP JP2001400493A patent/JP4097941B2/ja not_active Expired - Lifetime
-
2002
- 2002-01-04 DE DE60227307T patent/DE60227307D1/de not_active Expired - Lifetime
- 2002-01-04 EP EP02250055A patent/EP1239119B1/en not_active Expired - Lifetime
- 2002-01-04 ES ES02250055T patent/ES2307709T3/es not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| US6464456B2 (en) | 2002-10-15 |
| US20020127097A1 (en) | 2002-09-12 |
| EP1239119B1 (en) | 2008-07-02 |
| ES2307709T3 (es) | 2008-12-01 |
| DE60227307D1 (de) | 2008-08-14 |
| EP1239119A1 (en) | 2002-09-11 |
| JP2002295202A (ja) | 2002-10-09 |
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Legal Events
| Date | Code | Title | Description |
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