BR112015003340A2 - processo para produzir um componente de aerofólio e componente. - Google Patents
processo para produzir um componente de aerofólio e componente.Info
- Publication number
- BR112015003340A2 BR112015003340A2 BR112015003340A BR112015003340A BR112015003340A2 BR 112015003340 A2 BR112015003340 A2 BR 112015003340A2 BR 112015003340 A BR112015003340 A BR 112015003340A BR 112015003340 A BR112015003340 A BR 112015003340A BR 112015003340 A2 BR112015003340 A2 BR 112015003340A2
- Authority
- BR
- Brazil
- Prior art keywords
- component
- produce
- airfoil
- airfoil component
- 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
-
- 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
-
- 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
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- 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
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/125—Fluid guiding means, e.g. vanes related to the tip of a stator vane
-
- 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
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/307—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the tip of a rotor blade
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
- Y10T428/24496—Foamed or cellular component
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Ceramic Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201261682870P | 2012-08-14 | 2012-08-14 | |
| US13/721,349 US9410437B2 (en) | 2012-08-14 | 2012-12-20 | Airfoil components containing ceramic-based materials and processes therefor |
| PCT/US2013/050847 WO2014058499A2 (en) | 2012-08-14 | 2013-07-17 | Airfoil components containing ceramic-based materials and processes therefor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BR112015003340A2 true BR112015003340A2 (pt) | 2017-10-10 |
Family
ID=50100230
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BR112015003340A BR112015003340A2 (pt) | 2012-08-14 | 2013-07-17 | processo para produzir um componente de aerofólio e componente. |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US9410437B2 (pt) |
| EP (1) | EP2893150B1 (pt) |
| JP (1) | JP6145167B2 (pt) |
| CN (1) | CN104541025B (pt) |
| BR (1) | BR112015003340A2 (pt) |
| CA (1) | CA2881291C (pt) |
| WO (1) | WO2014058499A2 (pt) |
Families Citing this family (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9050769B2 (en) * | 2012-04-13 | 2015-06-09 | General Electric Company | Pre-form ceramic matrix composite cavity and method of forming and method of forming a ceramic matrix composite component |
| US20140199174A1 (en) * | 2013-01-11 | 2014-07-17 | General Electric Company | Method of forming a ceramic matrix composite component, a ceramic matrix composite component and a tip member |
| US9470603B2 (en) * | 2014-04-25 | 2016-10-18 | Teledyne Scientific & Imaging, Llc | Morphing ceramic composite components for hypersonic wind tunnel |
| US10538013B2 (en) | 2014-05-08 | 2020-01-21 | United Technologies Corporation | Integral ceramic matrix composite fastener with non-polymer rigidization |
| US10371011B2 (en) * | 2014-05-08 | 2019-08-06 | United Technologies Corporation | Integral ceramic matrix composite fastener with polymer rigidization |
| US10202854B2 (en) | 2014-12-18 | 2019-02-12 | Rolls-Royce North America Technologies, Inc. | Abrasive tips for ceramic matrix composite blades and methods for making the same |
| US10294803B2 (en) | 2015-03-26 | 2019-05-21 | General Electric Company | Compositions and methods of deposition of thick environmental barrier coatings on CMC blade tips |
| US10458653B2 (en) * | 2015-06-05 | 2019-10-29 | Rolls-Royce Corporation | Machinable CMC insert |
| US10472976B2 (en) * | 2015-06-05 | 2019-11-12 | Rolls-Royce Corporation | Machinable CMC insert |
| US10465534B2 (en) | 2015-06-05 | 2019-11-05 | Rolls-Royce North American Technologies, Inc. | Machinable CMC insert |
| US10392947B2 (en) | 2015-07-13 | 2019-08-27 | General Electric Company | Compositions and methods of attachment of thick environmental barrier coatings on CMC components |
| US9926796B2 (en) * | 2015-07-28 | 2018-03-27 | General Electric Company | Ply, method for manufacturing ply, and method for manufacturing article with ply |
| US10273813B2 (en) * | 2015-10-29 | 2019-04-30 | General Electric Company | Ceramic matrix composite component and process of producing a ceramic matrix composite component |
| US20170370583A1 (en) * | 2016-06-22 | 2017-12-28 | General Electric Company | Ceramic Matrix Composite Component for a Gas Turbine Engine |
| US10358922B2 (en) | 2016-11-10 | 2019-07-23 | Rolls-Royce Corporation | Turbine wheel with circumferentially-installed inter-blade heat shields |
| US10458262B2 (en) * | 2016-11-17 | 2019-10-29 | United Technologies Corporation | Airfoil with seal between endwall and airfoil section |
| US10519781B2 (en) * | 2017-01-12 | 2019-12-31 | United Technologies Corporation | Airfoil turn caps in gas turbine engines |
| US10465528B2 (en) | 2017-02-07 | 2019-11-05 | United Technologies Corporation | Airfoil turn caps in gas turbine engines |
| US10480329B2 (en) | 2017-04-25 | 2019-11-19 | United Technologies Corporation | Airfoil turn caps in gas turbine engines |
| US10267163B2 (en) | 2017-05-02 | 2019-04-23 | United Technologies Corporation | Airfoil turn caps in gas turbine engines |
| US11897816B2 (en) * | 2018-05-15 | 2024-02-13 | Safran | Method for manufacturing a CMC part |
| US11015467B2 (en) | 2018-07-06 | 2021-05-25 | Raytheon Technologies Corporation | Porous space fillers for ceramic matrix composites |
| US11040915B2 (en) | 2018-09-11 | 2021-06-22 | General Electric Company | Method of forming CMC component cooling cavities |
| US10934854B2 (en) | 2018-09-11 | 2021-03-02 | General Electric Company | CMC component cooling cavities |
| US10760428B2 (en) | 2018-10-16 | 2020-09-01 | General Electric Company | Frangible gas turbine engine airfoil |
| US10837286B2 (en) | 2018-10-16 | 2020-11-17 | General Electric Company | Frangible gas turbine engine airfoil with chord reduction |
| US10746045B2 (en) | 2018-10-16 | 2020-08-18 | General Electric Company | Frangible gas turbine engine airfoil including a retaining member |
| US11149558B2 (en) | 2018-10-16 | 2021-10-19 | General Electric Company | Frangible gas turbine engine airfoil with layup change |
| US11111815B2 (en) | 2018-10-16 | 2021-09-07 | General Electric Company | Frangible gas turbine engine airfoil with fusion cavities |
| US11434781B2 (en) | 2018-10-16 | 2022-09-06 | General Electric Company | Frangible gas turbine engine airfoil including an internal cavity |
| US11428160B2 (en) | 2020-12-31 | 2022-08-30 | General Electric Company | Gas turbine engine with interdigitated turbine and gear assembly |
| US11506065B1 (en) * | 2021-11-12 | 2022-11-22 | Raytheon Technologies Corporation | Airfoil with serpentine fiber ply layup |
Family Cites Families (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IT1176673B (it) * | 1983-09-23 | 1987-08-18 | Gen Electric | Pala cava per turbomacchina |
| US5015540A (en) | 1987-06-01 | 1991-05-14 | General Electric Company | Fiber-containing composite |
| US5330854A (en) | 1987-09-24 | 1994-07-19 | General Electric Company | Filament-containing composite |
| US5488017A (en) | 1989-04-14 | 1996-01-30 | General Electric Company | Fibert reinforced ceramic matrix composite member |
| GB2230259B (en) * | 1989-04-14 | 1993-11-17 | Gen Electric | Fibre reinforced ceramic matrix composite member and method for making |
| US5336350A (en) | 1989-10-31 | 1994-08-09 | General Electric Company | Process for making composite containing fibrous material |
| US5628938A (en) | 1994-11-18 | 1997-05-13 | General Electric Company | Method of making a ceramic composite by infiltration of a ceramic preform |
| US6024898A (en) | 1996-12-30 | 2000-02-15 | General Electric Company | Article and method for making complex shaped preform and silicon carbide composite by melt infiltration |
| US6403158B1 (en) | 1999-03-05 | 2002-06-11 | General Electric Company | Porous body infiltrating method |
| WO2000053896A1 (de) * | 1999-03-09 | 2000-09-14 | Siemens Aktiengesellschaft | Turbinenschaufel und verfahren zur herstellung einer turbinenschaufel |
| US6503441B2 (en) | 2001-05-30 | 2003-01-07 | General Electric Company | Method for producing melt-infiltrated ceramic composites using formed supports |
| US6709230B2 (en) | 2002-05-31 | 2004-03-23 | Siemens Westinghouse Power Corporation | Ceramic matrix composite gas turbine vane |
| US20040067316A1 (en) | 2002-10-04 | 2004-04-08 | Paul Gray | Method for processing silicon-carbide materials using organic film formers |
| EP1555329A1 (de) | 2004-01-15 | 2005-07-20 | Siemens Aktiengesellschaft | Bauteil mit Druckeigenspannungen, Verfahren zur Herstellung und Vorrichtung zur Erzeugung von Druckeigenspannungen |
| US7066717B2 (en) | 2004-04-22 | 2006-06-27 | Siemens Power Generation, Inc. | Ceramic matrix composite airfoil trailing edge arrangement |
| US7153096B2 (en) | 2004-12-02 | 2006-12-26 | Siemens Power Generation, Inc. | Stacked laminate CMC turbine vane |
| US7255535B2 (en) | 2004-12-02 | 2007-08-14 | Albrecht Harry A | Cooling systems for stacked laminate CMC vane |
| US7510379B2 (en) | 2005-12-22 | 2009-03-31 | General Electric Company | Composite blading member and method for making |
| US7507466B2 (en) * | 2006-02-22 | 2009-03-24 | General Electric Company | Manufacture of CMC articles having small complex features |
| EP1895102B1 (de) | 2006-08-23 | 2009-04-22 | Siemens Aktiengesellschaft | Beschichtete Turbinenschaufel |
| US20090165924A1 (en) * | 2006-11-28 | 2009-07-02 | General Electric Company | Method of manufacturing cmc articles having small complex features |
| FR2943942B1 (fr) * | 2009-04-06 | 2016-01-29 | Snecma | Procede de fabrication d'une aube de turbomachine en materiau composite |
| US20110052406A1 (en) | 2009-08-25 | 2011-03-03 | General Electric Company | Airfoil and process for depositing an erosion-resistant coating on the airfoil |
| WO2011059064A1 (ja) * | 2009-11-13 | 2011-05-19 | 株式会社Ihi | 翼の製造方法 |
| EP2524069B1 (en) * | 2010-01-11 | 2018-03-07 | Rolls-Royce Corporation | Features for mitigating thermal or mechanical stress on an environmental barrier coating |
| US9228445B2 (en) | 2010-12-23 | 2016-01-05 | General Electric Company | Turbine airfoil components containing ceramic-based materials and processes therefor |
-
2012
- 2012-12-20 US US13/721,349 patent/US9410437B2/en active Active
-
2013
- 2013-07-17 CA CA2881291A patent/CA2881291C/en active Active
- 2013-07-17 JP JP2015527465A patent/JP6145167B2/ja active Active
- 2013-07-17 WO PCT/US2013/050847 patent/WO2014058499A2/en active Application Filing
- 2013-07-17 BR BR112015003340A patent/BR112015003340A2/pt not_active Application Discontinuation
- 2013-07-17 CN CN201380043231.4A patent/CN104541025B/zh active Active
- 2013-07-17 EP EP13826797.6A patent/EP2893150B1/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| WO2014058499A2 (en) | 2014-04-17 |
| CN104541025B (zh) | 2016-08-24 |
| WO2014058499A3 (en) | 2014-06-26 |
| US9410437B2 (en) | 2016-08-09 |
| CA2881291C (en) | 2020-07-14 |
| US20140050893A1 (en) | 2014-02-20 |
| EP2893150B1 (en) | 2016-06-29 |
| CN104541025A (zh) | 2015-04-22 |
| CA2881291A1 (en) | 2014-04-17 |
| JP6145167B2 (ja) | 2017-06-07 |
| JP2015530512A (ja) | 2015-10-15 |
| EP2893150A2 (en) | 2015-07-15 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
| B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
| B11B | Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements |