DE602008001849D1 - Keramik-Matrix-Verbund-Turbinenleitschaufel - Google Patents
Keramik-Matrix-Verbund-TurbinenleitschaufelInfo
- Publication number
- DE602008001849D1 DE602008001849D1 DE602008001849T DE602008001849T DE602008001849D1 DE 602008001849 D1 DE602008001849 D1 DE 602008001849D1 DE 602008001849 T DE602008001849 T DE 602008001849T DE 602008001849 T DE602008001849 T DE 602008001849T DE 602008001849 D1 DE602008001849 D1 DE 602008001849D1
- Authority
- DE
- Germany
- Prior art keywords
- matrix composite
- ceramic matrix
- turbine vane
- composite turbine
- vane
- 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.)
- Active
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
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
-
- 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
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- 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
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
- F05D2230/314—Layer deposition by chemical vapour deposition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/22—Non-oxide ceramics
- F05D2300/226—Carbides
- F05D2300/2261—Carbides of silicon
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49337—Composite blade
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/824,173 US8210803B2 (en) | 2007-06-28 | 2007-06-28 | Ceramic matrix composite turbine engine vane |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602008001849D1 true DE602008001849D1 (de) | 2010-09-02 |
Family
ID=39832786
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602008001849T Active DE602008001849D1 (de) | 2007-06-28 | 2008-02-11 | Keramik-Matrix-Verbund-Turbinenleitschaufel |
Country Status (3)
Country | Link |
---|---|
US (1) | US8210803B2 (de) |
EP (1) | EP2039884B1 (de) |
DE (1) | DE602008001849D1 (de) |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2943942B1 (fr) * | 2009-04-06 | 2016-01-29 | Snecma | Procede de fabrication d'une aube de turbomachine en materiau composite |
US8024932B1 (en) * | 2010-04-07 | 2011-09-27 | General Electric Company | System and method for a combustor nozzle |
US8790067B2 (en) | 2011-04-27 | 2014-07-29 | United Technologies Corporation | Blade clearance control using high-CTE and low-CTE ring members |
US8864492B2 (en) | 2011-06-23 | 2014-10-21 | United Technologies Corporation | Reverse flow combustor duct attachment |
US8739547B2 (en) | 2011-06-23 | 2014-06-03 | United Technologies Corporation | Gas turbine engine joint having a metallic member, a CMC member, and a ceramic key |
US8511975B2 (en) | 2011-07-05 | 2013-08-20 | United Technologies Corporation | Gas turbine shroud arrangement |
US9335051B2 (en) | 2011-07-13 | 2016-05-10 | United Technologies Corporation | Ceramic matrix composite combustor vane ring assembly |
US8920127B2 (en) | 2011-07-18 | 2014-12-30 | United Technologies Corporation | Turbine rotor non-metallic blade attachment |
DE102011081112A1 (de) | 2011-08-17 | 2013-02-21 | Rolls-Royce Deutschland Ltd & Co Kg | Verfahren zur Herstellung eines Bauteils für hohe thermische Belastungen, ein Bauteil herstellbar mit dem Verfahren und ein Flugzeugtriebwerk mit dem Bauteil |
JP6189432B2 (ja) | 2012-07-03 | 2017-08-30 | ゲーコーエヌ エアロスペース スウェーデン アーベー | ガスタービンエンジン用支持構造 |
US10605086B2 (en) | 2012-11-20 | 2020-03-31 | Honeywell International Inc. | Turbine engines with ceramic vanes and methods for manufacturing the same |
US9598967B2 (en) | 2012-12-18 | 2017-03-21 | United Technologies Corporation | Airfoil member and composite platform having contoured endwall |
US9650898B2 (en) | 2012-12-27 | 2017-05-16 | United Technologies Corporation | Airfoil with variable profile responsive to thermal conditions |
US9617857B2 (en) * | 2013-02-23 | 2017-04-11 | Rolls-Royce Corporation | Gas turbine engine component |
EP2971584B1 (de) | 2013-03-11 | 2019-08-28 | Rolls-Royce Corporation | Nachgiebiges mittleres teil eines gasturbinentriebwerks und verfahren zum einbauen eines solchen teils |
WO2014143339A1 (en) | 2013-03-15 | 2014-09-18 | Thomas David J | Gas turbine engine airflow member, corresponding turbomachine component and manufacturing method |
EP3074601B1 (de) * | 2013-11-25 | 2019-11-13 | Ansaldo Energia IP UK Limited | Leitschaufelanordnung auf der basis einer modularen struktur |
FR3021698B1 (fr) * | 2014-05-28 | 2021-07-02 | Snecma | Aube de turbine, comprenant un conduit central de refroidissement isole thermiquement de parois de l'aube par deux cavites laterales jointives en aval du conduit central |
US9970317B2 (en) | 2014-10-31 | 2018-05-15 | Rolls-Royce North America Technologies Inc. | Vane assembly for a gas turbine engine |
EP3048254B1 (de) * | 2015-01-22 | 2017-12-27 | Rolls-Royce Corporation | Schaufelanordnung für einen gasturbinenmotor |
US10093586B2 (en) * | 2015-02-26 | 2018-10-09 | General Electric Company | Ceramic matrix composite articles and methods for forming same |
US10309257B2 (en) | 2015-03-02 | 2019-06-04 | Rolls-Royce North American Technologies Inc. | Turbine assembly with load pads |
US10358939B2 (en) | 2015-03-11 | 2019-07-23 | Rolls-Royce Corporation | Turbine vane with heat shield |
US10329950B2 (en) * | 2015-03-23 | 2019-06-25 | Rolls-Royce North American Technologies Inc. | Nozzle guide vane with composite heat shield |
US10519779B2 (en) * | 2016-03-16 | 2019-12-31 | General Electric Company | Radial CMC wall thickness variation for stress response |
US10724380B2 (en) * | 2017-08-07 | 2020-07-28 | General Electric Company | CMC blade with internal support |
US10927677B2 (en) * | 2018-03-15 | 2021-02-23 | General Electric Company | Composite airfoil assembly with separate airfoil, inner band, and outer band |
US11085302B2 (en) | 2018-03-20 | 2021-08-10 | Rolls-Royce North American Technologies Inc. | Blade tip for ceramic matrix composite blade |
DE102018211193A1 (de) | 2018-07-06 | 2020-01-09 | MTU Aero Engines AG | Gasturbinenschaufel |
US10605103B2 (en) | 2018-08-24 | 2020-03-31 | Rolls-Royce Corporation | CMC airfoil assembly |
US10767497B2 (en) | 2018-09-07 | 2020-09-08 | Rolls-Royce Corporation | Turbine vane assembly with ceramic matrix composite components |
US10934868B2 (en) | 2018-09-12 | 2021-03-02 | Rolls-Royce North American Technologies Inc. | Turbine vane assembly with variable position support |
US11149568B2 (en) | 2018-12-20 | 2021-10-19 | Rolls-Royce Plc | Sliding ceramic matrix composite vane assembly for gas turbine engines |
US11193381B2 (en) | 2019-05-17 | 2021-12-07 | Rolls-Royce Plc | Turbine vane assembly having ceramic matrix composite components with sliding support |
US10883371B1 (en) * | 2019-06-21 | 2021-01-05 | Rolls-Royce Plc | Ceramic matrix composite vane with trailing edge radial cooling |
US10890076B1 (en) | 2019-06-28 | 2021-01-12 | Rolls-Royce Plc | Turbine vane assembly having ceramic matrix composite components with expandable spar support |
US11286798B2 (en) | 2019-08-20 | 2022-03-29 | Rolls-Royce Corporation | Airfoil assembly with ceramic matrix composite parts and load-transfer features |
US11149560B2 (en) | 2019-08-20 | 2021-10-19 | Rolls-Royce Plc | Airfoil assembly with ceramic matrix composite parts and load-transfer features |
US11255204B2 (en) | 2019-11-05 | 2022-02-22 | Rolls-Royce Plc | Turbine vane assembly having ceramic matrix composite airfoils and metallic support spar |
US10975709B1 (en) | 2019-11-11 | 2021-04-13 | Rolls-Royce Plc | Turbine vane assembly with ceramic matrix composite components and sliding support |
US11519280B1 (en) | 2021-09-30 | 2022-12-06 | Rolls-Royce Plc | Ceramic matrix composite vane assembly with compliance features |
US11560799B1 (en) | 2021-10-22 | 2023-01-24 | Rolls-Royce High Temperature Composites Inc. | Ceramic matrix composite vane assembly with shaped load transfer features |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5356265A (en) * | 1992-08-25 | 1994-10-18 | General Electric Company | Chordally bifurcated turbine blade |
US5279111A (en) * | 1992-08-27 | 1994-01-18 | Inco Limited | Gas turbine cooling |
US5630700A (en) * | 1996-04-26 | 1997-05-20 | General Electric Company | Floating vane turbine nozzle |
CA2307496A1 (en) * | 1997-10-27 | 1999-07-08 | Gary W. Swartzbeck | Turbine components with skin bonded to substrates |
US6280550B1 (en) * | 1998-12-15 | 2001-08-28 | General Electric Company | Fabrication of composite articles having an infiltrated matrix |
US6393331B1 (en) * | 1998-12-16 | 2002-05-21 | United Technologies Corporation | Method of designing a turbine blade outer air seal |
US6283708B1 (en) * | 1999-12-03 | 2001-09-04 | United Technologies Corporation | Coolable vane or blade for a turbomachine |
US6514046B1 (en) * | 2000-09-29 | 2003-02-04 | Siemens Westinghouse Power Corporation | Ceramic composite vane with metallic substructure |
US6464456B2 (en) * | 2001-03-07 | 2002-10-15 | General Electric Company | Turbine vane assembly including a low ductility vane |
US6648597B1 (en) * | 2002-05-31 | 2003-11-18 | Siemens Westinghouse Power Corporation | Ceramic matrix composite turbine vane |
US6709230B2 (en) * | 2002-05-31 | 2004-03-23 | Siemens Westinghouse Power Corporation | Ceramic matrix composite gas turbine vane |
US7093359B2 (en) * | 2002-09-17 | 2006-08-22 | Siemens Westinghouse Power Corporation | Composite structure formed by CMC-on-insulation process |
GB2402717B (en) * | 2003-06-10 | 2006-05-10 | Rolls Royce Plc | A vane assembly for a gas turbine engine |
US20050158171A1 (en) * | 2004-01-15 | 2005-07-21 | General Electric Company | Hybrid ceramic matrix composite turbine blades for improved processibility and performance |
US7223465B2 (en) * | 2004-12-29 | 2007-05-29 | General Electric Company | SiC/SiC composites incorporating uncoated fibers to improve interlaminar strength |
US7258530B2 (en) * | 2005-01-21 | 2007-08-21 | Siemens Power Generation, Inc. | CMC component and method of fabrication |
US7754126B2 (en) * | 2005-06-17 | 2010-07-13 | General Electric Company | Interlaminar tensile reinforcement of SiC/SiC CMC's using fugitive fibers |
US7967570B2 (en) * | 2007-07-27 | 2011-06-28 | United Technologies Corporation | Low transient thermal stress turbine engine components |
-
2007
- 2007-06-28 US US11/824,173 patent/US8210803B2/en active Active
-
2008
- 2008-02-11 DE DE602008001849T patent/DE602008001849D1/de active Active
- 2008-02-11 EP EP08250494A patent/EP2039884B1/de active Active
Also Published As
Publication number | Publication date |
---|---|
US8210803B2 (en) | 2012-07-03 |
EP2039884A1 (de) | 2009-03-25 |
EP2039884B1 (de) | 2010-07-21 |
US20100021290A1 (en) | 2010-01-28 |
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