SE8303907L - Turbinbladsaggregat - Google Patents
TurbinbladsaggregatInfo
- Publication number
- SE8303907L SE8303907L SE8303907A SE8303907A SE8303907L SE 8303907 L SE8303907 L SE 8303907L SE 8303907 A SE8303907 A SE 8303907A SE 8303907 A SE8303907 A SE 8303907A SE 8303907 L SE8303907 L SE 8303907L
- Authority
- SE
- Sweden
- Prior art keywords
- ceramic blade
- blade element
- post member
- corrugated
- ceramic
- Prior art date
Links
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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/397,267 US4519745A (en) | 1980-09-19 | 1982-07-12 | Rotor blade and stator vane using ceramic shell |
Publications (2)
Publication Number | Publication Date |
---|---|
SE8303907D0 SE8303907D0 (sv) | 1983-07-08 |
SE8303907L true SE8303907L (sv) | 1984-01-13 |
Family
ID=23570504
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8303907A SE8303907L (sv) | 1982-07-12 | 1983-07-08 | Turbinbladsaggregat |
Country Status (6)
Country | Link |
---|---|
US (1) | US4519745A (sv) |
JP (1) | JPS5923001A (sv) |
DE (1) | DE3324755A1 (sv) |
FR (1) | FR2529947B2 (sv) |
GB (1) | GB2123489B (sv) |
SE (1) | SE8303907L (sv) |
Families Citing this family (60)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3512008A1 (de) * | 1985-04-02 | 1986-10-09 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Turbinenlaufschaufel, insbesondere fuer gasturbinentriebwerke |
DE3521782A1 (de) * | 1985-06-19 | 1987-01-02 | Mtu Muenchen Gmbh | Hybridschaufel aus metall und keramik zusammengesetzt |
US4790721A (en) * | 1988-04-25 | 1988-12-13 | Rockwell International Corporation | Blade assembly |
US5667359A (en) * | 1988-08-24 | 1997-09-16 | United Technologies Corp. | Clearance control for the turbine of a gas turbine engine |
JP2602929B2 (ja) * | 1988-11-21 | 1997-04-23 | 株式会社東芝 | ターボ機械の動翼構造 |
JP2693527B2 (ja) * | 1988-11-21 | 1997-12-24 | 株式会社東芝 | ターボ機械の動翼構造 |
US5145315A (en) * | 1991-09-27 | 1992-09-08 | Westinghouse Electric Corp. | Gas turbine vane cooling air insert |
GB9607578D0 (en) * | 1996-04-12 | 1996-06-12 | Rolls Royce Plc | Turbine rotor blades |
DE59905944D1 (de) * | 1998-08-31 | 2003-07-17 | Siemens Ag | Turbinenschaufel |
US6135715A (en) * | 1999-07-29 | 2000-10-24 | General Electric Company | Tip insulated airfoil |
US6260349B1 (en) | 2000-03-17 | 2001-07-17 | Kenneth F. Griffiths | Multi-stage turbo-machines with specific blade dimension ratios |
US6378287B2 (en) | 2000-03-17 | 2002-04-30 | Kenneth F. Griffiths | Multi-stage turbomachine and design method |
WO2002027145A2 (en) * | 2000-09-29 | 2002-04-04 | Siemens Westinghouse Power Corporation | Vane assembly for a turbine and combustion turbine with this vane assembly |
US6514046B1 (en) * | 2000-09-29 | 2003-02-04 | Siemens Westinghouse Power Corporation | Ceramic composite vane with metallic substructure |
US6709230B2 (en) * | 2002-05-31 | 2004-03-23 | Siemens Westinghouse Power Corporation | Ceramic matrix composite gas turbine vane |
US6648597B1 (en) | 2002-05-31 | 2003-11-18 | Siemens Westinghouse Power Corporation | Ceramic matrix composite turbine vane |
US9068464B2 (en) * | 2002-09-17 | 2015-06-30 | Siemens Energy, Inc. | Method of joining ceramic parts and articles so formed |
US7093359B2 (en) | 2002-09-17 | 2006-08-22 | Siemens Westinghouse Power Corporation | Composite structure formed by CMC-on-insulation process |
US7080971B2 (en) * | 2003-03-12 | 2006-07-25 | Florida Turbine Technologies, Inc. | Cooled turbine spar shell blade construction |
EP1489264A1 (de) * | 2003-06-18 | 2004-12-22 | Siemens Aktiengesellschaft | Modular aufgebaute Schaufel |
US7066717B2 (en) * | 2004-04-22 | 2006-06-27 | Siemens Power Generation, Inc. | Ceramic matrix composite airfoil trailing edge arrangement |
US7435058B2 (en) * | 2005-01-18 | 2008-10-14 | Siemens Power Generation, Inc. | Ceramic matrix composite vane with chordwise stiffener |
US7648336B2 (en) * | 2006-01-03 | 2010-01-19 | General Electric Company | Apparatus and method for assembling a gas turbine stator |
US7641440B2 (en) * | 2006-08-31 | 2010-01-05 | Siemens Energy, Inc. | Cooling arrangement for CMC components with thermally conductive layer |
US7713029B1 (en) | 2007-03-28 | 2010-05-11 | Florida Turbine Technologies, Inc. | Turbine blade with spar and shell construction |
DE102007027465A1 (de) * | 2007-06-14 | 2008-12-18 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenschaufel mit modularem Aufbau |
US7993104B1 (en) | 2007-12-21 | 2011-08-09 | Florida Turbine Technologies, Inc. | Turbine blade with spar and shell |
US20100028133A1 (en) * | 2008-07-30 | 2010-02-04 | General Electric Company | Turbomachine component damping structure and method of damping vibration of a turbomachine component |
US8033790B2 (en) * | 2008-09-26 | 2011-10-11 | Siemens Energy, Inc. | Multiple piece turbine engine airfoil with a structural spar |
US8956105B2 (en) * | 2008-12-31 | 2015-02-17 | Rolls-Royce North American Technologies, Inc. | Turbine vane for gas turbine engine |
US8152468B2 (en) * | 2009-03-13 | 2012-04-10 | United Technologies Corporation | Divoted airfoil baffle having aimed cooling holes |
GB2468528B (en) | 2009-03-13 | 2011-03-30 | Rolls Royce Plc | Vibration damper |
US8256088B2 (en) * | 2009-08-24 | 2012-09-04 | Siemens Energy, Inc. | Joining mechanism with stem tension and interlocked compression ring |
US7955054B2 (en) * | 2009-09-21 | 2011-06-07 | Pratt & Whitney Rocketdyne, Inc. | Internally damped blade |
US8678764B1 (en) * | 2009-10-27 | 2014-03-25 | Florida Turbine Technologies, Inc. | Tip cap for a turbine rotor blade |
US9528382B2 (en) | 2009-11-10 | 2016-12-27 | General Electric Company | Airfoil heat shield |
US20110110772A1 (en) * | 2009-11-11 | 2011-05-12 | Arrell Douglas J | Turbine Engine Components with Near Surface Cooling Channels and Methods of Making the Same |
US8251658B1 (en) * | 2009-12-08 | 2012-08-28 | Florida Turbine Technologies, Inc. | Tip cap for turbine rotor blade |
US8740567B2 (en) | 2010-07-26 | 2014-06-03 | United Technologies Corporation | Reverse cavity blade for a gas turbine engine |
EP2426316A1 (en) | 2010-09-03 | 2012-03-07 | Siemens Aktiengesellschaft | Turbine blade |
JP5660883B2 (ja) * | 2010-12-22 | 2015-01-28 | 三菱日立パワーシステムズ株式会社 | 蒸気タービンの静翼、蒸気タービン |
US20120315139A1 (en) * | 2011-06-10 | 2012-12-13 | General Electric Company | Cooling flow control members for turbomachine buckets and method |
US9726028B2 (en) * | 2011-06-29 | 2017-08-08 | Siemens Energy, Inc. | Ductile alloys for sealing modular component interfaces |
US9186757B2 (en) * | 2012-05-09 | 2015-11-17 | Siemens Energy, Inc. | Method of providing a turbine blade tip repair |
WO2014149116A2 (en) * | 2013-02-23 | 2014-09-25 | Shuck Quinlan Y | Gas turbine engine component |
US10072503B2 (en) | 2013-08-14 | 2018-09-11 | Elwha Llc | Dual element turbine blade |
DE102013219774A1 (de) * | 2013-09-30 | 2015-04-02 | MTU Aero Engines AG | Schaufel für eine Gasturbine |
US10329918B2 (en) * | 2013-10-18 | 2019-06-25 | United Technologies Corporation | Multiple piece engine component |
US20150292540A1 (en) * | 2014-04-09 | 2015-10-15 | Natel Energy, Inc. | Wedge clamping system for beams |
FR3023317B1 (fr) * | 2014-07-04 | 2016-08-05 | Snecma | Procede de fabrication d'une aube bi-composant pour moteur a turbine a gaz et aube obtenue par un tel procede |
US10731481B2 (en) * | 2016-11-01 | 2020-08-04 | Rolls-Royce Corporation | Turbine blade with ceramic matrix composite material construction |
US10408090B2 (en) * | 2016-11-17 | 2019-09-10 | United Technologies Corporation | Gas turbine engine article with panel retained by preloaded compliant member |
US10392945B2 (en) * | 2017-05-19 | 2019-08-27 | General Electric Company | Turbomachine cooling system |
US10724380B2 (en) * | 2017-08-07 | 2020-07-28 | General Electric Company | CMC blade with internal support |
RU2740069C1 (ru) * | 2017-12-01 | 2020-12-31 | Сименс Энерджи, Инк. | Впаянный теплопередающий элемент для охлаждаемых компонентов турбины |
US11459899B2 (en) * | 2018-03-23 | 2022-10-04 | Raytheon Technologies Corporation | Turbine component with a thin interior partition |
US10519777B2 (en) * | 2018-05-14 | 2019-12-31 | General Electric Company | Tip member for blade structure and related method to form turbomachine component |
US11149568B2 (en) * | 2018-12-20 | 2021-10-19 | Rolls-Royce Plc | Sliding ceramic matrix composite vane assembly for gas turbine engines |
US11203947B2 (en) | 2020-05-08 | 2021-12-21 | Raytheon Technologies Corporation | Airfoil having internally cooled wall with liner and shell |
US20220090504A1 (en) * | 2020-09-24 | 2022-03-24 | General Electric Company | Rotor blade for a gas turbine engine having a metallic structural member and a composite fairing |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB602530A (en) * | 1945-10-16 | 1948-05-28 | Bristol Aeroplane Co Ltd | Improvements in or relating to gas turbines |
FR999820A (fr) * | 1946-01-11 | 1952-02-05 | Perfectionnements aux turbines à gaz | |
FR1007303A (fr) * | 1949-08-24 | 1952-05-05 | Perfectionnements aux aubes de rotors | |
US2787441A (en) * | 1952-03-05 | 1957-04-02 | Thompson Prod Inc | Hollow turbine bucket |
GB738656A (en) * | 1952-07-26 | 1955-10-19 | Power Jets Res & Dev Ltd | Blades for compressors, turbines and like bladed fluid flow machines |
US2851216A (en) * | 1954-01-13 | 1958-09-09 | Schwarzkopf Dev Co | Device adapted for respiration cooling and process of making same |
US2994124A (en) * | 1955-10-03 | 1961-08-01 | Gen Electric | Clad cermet body |
GB1119392A (en) * | 1966-06-03 | 1968-07-10 | Rover Co Ltd | Axial flow rotor for a turbine or the like |
GB1187978A (en) * | 1966-10-01 | 1970-04-15 | Plessey Co Ltd | Improvements in or relating to Gas-Turbine Rotors. |
JPS54106714A (en) * | 1978-02-08 | 1979-08-22 | Ishikawajima Harima Heavy Ind Co Ltd | Turbine vane |
FR2463849A1 (fr) * | 1979-08-23 | 1981-02-27 | Onera (Off Nat Aerospatiale) | Perfectionnements apportes aux aubes tournantes de turbines a gaz, et aux turbines a gaz equipees de ces aubes |
DE3003347A1 (de) * | 1979-12-20 | 1981-06-25 | BBC AG Brown, Boveri & Cie., Baden, Aargau | Gekuehlte wand |
FR2490721B1 (fr) * | 1980-09-19 | 1987-10-09 | Rockwell International Corp | Turbomachine dont les aubages mobile et fixe sont proteges par une carapace en ceramique |
DE3110098C2 (de) * | 1981-03-16 | 1983-03-17 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Turbinenleitschaufel für Gasturbinentriebwerke |
-
1982
- 1982-07-12 US US06/397,267 patent/US4519745A/en not_active Expired - Fee Related
-
1983
- 1983-07-06 FR FR838311289A patent/FR2529947B2/fr not_active Expired
- 1983-07-08 DE DE19833324755 patent/DE3324755A1/de not_active Withdrawn
- 1983-07-08 SE SE8303907A patent/SE8303907L/sv not_active Application Discontinuation
- 1983-07-12 GB GB08318857A patent/GB2123489B/en not_active Expired
- 1983-07-12 JP JP58125626A patent/JPS5923001A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
GB8318857D0 (en) | 1983-08-10 |
FR2529947B2 (fr) | 1989-03-24 |
FR2529947A2 (fr) | 1984-01-13 |
JPS5923001A (ja) | 1984-02-06 |
DE3324755A1 (de) | 1984-01-12 |
US4519745A (en) | 1985-05-28 |
GB2123489B (en) | 1985-10-23 |
SE8303907D0 (sv) | 1983-07-08 |
GB2123489A (en) | 1984-02-01 |
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Legal Events
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NAV | Patent application has lapsed |
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