IT7924987A0 - COMPOUND CERAMIC BLADE FOR GAS TURBINE. - Google Patents
COMPOUND CERAMIC BLADE FOR GAS TURBINE.Info
- Publication number
- IT7924987A0 IT7924987A0 IT7924987A IT2498779A IT7924987A0 IT 7924987 A0 IT7924987 A0 IT 7924987A0 IT 7924987 A IT7924987 A IT 7924987A IT 2498779 A IT2498779 A IT 2498779A IT 7924987 A0 IT7924987 A0 IT 7924987A0
- Authority
- IT
- Italy
- Prior art keywords
- gas turbine
- ceramic blade
- compound ceramic
- compound
- blade
- Prior art date
Links
- 239000000919 ceramic Substances 0.000 title 1
- 150000001875 compounds Chemical class 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
- 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
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/284—Selection of ceramic materials
-
- 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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19782834843 DE2834843A1 (en) | 1978-08-09 | 1978-08-09 | COMPOSED CERAMIC GAS TURBINE BLADE |
Publications (2)
Publication Number | Publication Date |
---|---|
IT7924987A0 true IT7924987A0 (en) | 1979-08-08 |
IT1122732B IT1122732B (en) | 1986-04-23 |
Family
ID=6046570
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT24987/79A IT1122732B (en) | 1978-08-09 | 1979-08-08 | COMPOSITE CERAMIC BLADE FOR GAS TURBINE |
Country Status (6)
Country | Link |
---|---|
DE (1) | DE2834843A1 (en) |
FR (1) | FR2433098A1 (en) |
GB (1) | GB2027496B (en) |
IT (1) | IT1122732B (en) |
NL (1) | NL7905608A (en) |
SE (1) | SE7905910L (en) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3203869C2 (en) * | 1982-02-05 | 1984-05-10 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Turbine rotor blades for turbo machines, in particular gas turbine engines |
US4786234A (en) * | 1982-06-21 | 1988-11-22 | Teledyne Industries, Inc. | Turbine airfoil |
FR2538029A1 (en) * | 1982-12-15 | 1984-06-22 | Onera (Off Nat Aerospatiale) | IMPROVEMENTS TO CERAMIC, ROTATING OR FIXED BLADES OF TURBOMACHINES |
DE3306896A1 (en) * | 1983-02-26 | 1984-08-30 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | HOT GAS SUPPLIED TURBINE BLADE WITH METAL SUPPORT CORE AND SURROUNDING CERAMIC BLADE |
DE3327218A1 (en) * | 1983-07-28 | 1985-02-07 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | THERMALLY HIGH-QUALITY, COOLED COMPONENT, IN PARTICULAR TURBINE BLADE |
DE3521782A1 (en) * | 1985-06-19 | 1987-01-02 | Mtu Muenchen Gmbh | HYBRID SHOVEL MADE OF METAL AND CERAMIC |
WO1991001433A1 (en) * | 1989-07-25 | 1991-02-07 | Allied-Signal Inc. | Dual alloy turbine blade |
US5106266A (en) * | 1989-07-25 | 1992-04-21 | Allied-Signal Inc. | Dual alloy turbine blade |
GB2346415A (en) * | 1999-02-05 | 2000-08-09 | Rolls Royce Plc | Vibration damping |
EP1329592A1 (en) * | 2002-01-18 | 2003-07-23 | Siemens Aktiengesellschaft | Turbine with at least four stages and utilisation of a turbine blade with reduced mass |
EP1489264A1 (en) * | 2003-06-18 | 2004-12-22 | Siemens Aktiengesellschaft | Blade consisting of moduls |
US7094021B2 (en) * | 2004-02-02 | 2006-08-22 | General Electric Company | Gas turbine flowpath structure |
US7435058B2 (en) | 2005-01-18 | 2008-10-14 | Siemens Power Generation, Inc. | Ceramic matrix composite vane with chordwise stiffener |
CH700071A1 (en) * | 2008-12-12 | 2010-06-15 | Alstom Technology Ltd | Moving blade for a gas turbine. |
GB2472572A (en) * | 2009-08-10 | 2011-02-16 | Rolls Royce Plc | Mounting for aerofoil blade using elastomeric bush |
FR2954200B1 (en) * | 2009-12-23 | 2012-03-02 | Snecma | PROCESS FOR MAKING A TURBOMACHINE METAL TURBINE REINFORCEMENT |
US8740571B2 (en) * | 2011-03-07 | 2014-06-03 | General Electric Company | Turbine bucket for use in gas turbine engines and methods for fabricating the same |
RU2510463C2 (en) * | 2012-11-12 | 2014-03-27 | Евгений Алексеевич Коняев | Gas turbine cermet blade |
DE102013219774A1 (en) * | 2013-09-30 | 2015-04-02 | MTU Aero Engines AG | Shovel for a gas turbine |
FR3023317B1 (en) | 2014-07-04 | 2016-08-05 | Snecma | METHOD FOR MANUFACTURING A BI-COMPONENT BLADE FOR A GAS-TURBINE ENGINE OBTAINED BY SUCH A METHOD |
RU2656052C1 (en) * | 2017-04-04 | 2018-05-30 | Акционерное общество "Климов" | Working blade of the gas turbine |
US11008878B2 (en) * | 2018-12-21 | 2021-05-18 | Rolls-Royce Plc | Turbine blade with ceramic matrix composite aerofoil and metallic root |
RU192858U1 (en) * | 2019-03-26 | 2019-10-03 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Санкт-Петербургский государственный архитектурно-строительный университет" | GAS TURBINE WORKING BLADE |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR869427A (en) * | 1938-11-04 | 1942-02-02 | Bmw Flugmotorenbau Gmbh | Rotor vane for exhaust gas turbines |
DE736958C (en) * | 1942-01-08 | 1943-07-02 | Turbinenfabrik Brueckner Kanis | Blade made of steel support body and sleeve made of ceramic material for centrifugal machines, especially steam or gas turbines |
US2479057A (en) * | 1945-03-27 | 1949-08-16 | United Aircraft Corp | Turbine rotor |
FR999820A (en) * | 1946-01-11 | 1952-02-05 | Improvements to gas turbines | |
FR907059A (en) * | 1946-09-20 | 1946-02-28 | High temperature gas turbine | |
US4017209A (en) * | 1975-12-15 | 1977-04-12 | United Technologies Corporation | Turbine rotor construction |
US4051585A (en) * | 1976-07-26 | 1977-10-04 | United Technologies Corporation | Method of forming a turbine rotor |
US4093399A (en) * | 1976-12-01 | 1978-06-06 | Electric Power Research Institute, Inc. | Turbine rotor with ceramic blades |
US4084922A (en) * | 1976-12-27 | 1978-04-18 | Electric Power Research Institute, Inc. | Turbine rotor with pin mounted ceramic turbine blades |
-
1978
- 1978-08-09 DE DE19782834843 patent/DE2834843A1/en not_active Withdrawn
-
1979
- 1979-07-06 SE SE7905910A patent/SE7905910L/en not_active Application Discontinuation
- 1979-07-19 NL NL7905608A patent/NL7905608A/en not_active Application Discontinuation
- 1979-07-26 FR FR7919270A patent/FR2433098A1/en not_active Withdrawn
- 1979-08-06 GB GB7927344A patent/GB2027496B/en not_active Expired
- 1979-08-08 IT IT24987/79A patent/IT1122732B/en active
Also Published As
Publication number | Publication date |
---|---|
DE2834843A1 (en) | 1980-06-26 |
SE7905910L (en) | 1980-02-10 |
FR2433098A1 (en) | 1980-03-07 |
GB2027496A (en) | 1980-02-20 |
NL7905608A (en) | 1980-02-12 |
GB2027496B (en) | 1982-08-11 |
IT1122732B (en) | 1986-04-23 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
IT7924988A0 (en) | COMPOSITE CERAMIC BLADE FOR GAS TURBINE. | |
IT7924987A0 (en) | COMPOUND CERAMIC BLADE FOR GAS TURBINE. | |
IT8221755A0 (en) | BLADE FOR A GAS TURBINE. | |
GB2030657B (en) | Blade for gas turbine engine | |
GB2028928B (en) | Aerofoil blade for a gas turbine engine | |
IT8020482A0 (en) | BLADE ROTOR FOR GAS TURBINE ENGINE. | |
JPS54160911A (en) | Blade for gas turbine engine | |
IT7921628A0 (en) | GAS TURBINE ENGINE. | |
AU2381177A (en) | Ceramic rotor blade assembly for gas turbine | |
IT7825321A0 (en) | METHOD FOR MANUFACTURING A BLADE OR BLADE FOR AGAS TURBINE ENGINES. | |
IT1076328B (en) | BLADE OR SHOVEL FOR A GAS TURBINE ENGINE | |
JPS5327714A (en) | Gas turbine rotor blade | |
IT7821288A0 (en) | GAS TURBINE ENGINE. | |
IT8020445A0 (en) | GAS TURBINE ENGINE. | |
IT7924547A0 (en) | IMPROVED TURBOMACHINE BLADE. | |
IT1089443B (en) | COMPOSITE ROTOR SHOVEL FOR TURBOMACHINES | |
IT8520834A0 (en) | BLADE FOR GAS TURBINE. | |
IT8019125A0 (en) | BREATHABLE COOLED CERAMIC BLADE FOR AN AGAS TURBINE. | |
NO784413L (en) | GAS TURBINES. | |
IT7821869A0 (en) | COOLED ROTOR BLADE FOR GAS TURBINE ENGINE. | |
IT8423829A0 (en) | BLADE FOR GAS TURBO ENGINE. | |
JPS5331012A (en) | Gas turbine blade | |
IT1109912B (en) | ROTOR BLADE OR DIRECT BLADE FOR GAS TURBINE | |
IT1142247B (en) | CERAMIC ROTOR FOR GAS TURBINES | |
IT8025620A0 (en) | MODULAR GAS TURBINE ENGINE. |