JP2014001723A5 - - Google Patents
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- Publication number
- JP2014001723A5 JP2014001723A5 JP2013016278A JP2013016278A JP2014001723A5 JP 2014001723 A5 JP2014001723 A5 JP 2014001723A5 JP 2013016278 A JP2013016278 A JP 2013016278A JP 2013016278 A JP2013016278 A JP 2013016278A JP 2014001723 A5 JP2014001723 A5 JP 2014001723A5
- Authority
- JP
- Japan
- Prior art keywords
- ceramic matrix
- matrix composite
- base ply
- cmc plies
- cavity
- 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.)
- Granted
Links
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/446,465 | 2012-04-13 | ||
| US13/446,465 US9050769B2 (en) | 2012-04-13 | 2012-04-13 | Pre-form ceramic matrix composite cavity and method of forming and method of forming a ceramic matrix composite component |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2014001723A JP2014001723A (ja) | 2014-01-09 |
| JP2014001723A5 true JP2014001723A5 (enExample) | 2016-03-17 |
| JP6325192B2 JP6325192B2 (ja) | 2018-05-16 |
Family
ID=47666059
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2013016278A Active JP6325192B2 (ja) | 2012-04-13 | 2013-01-31 | 予備成形セラミックマトリクス複合材キャビティ、予備成形セラミックマトリクス複合材キャビティを形成する方法、及びセラミックマトリクス複合材部品を形成する方法 |
Country Status (4)
| Country | Link |
|---|---|
| US (2) | US9050769B2 (enExample) |
| EP (1) | EP2650478B1 (enExample) |
| JP (1) | JP6325192B2 (enExample) |
| RU (1) | RU2013105722A (enExample) |
Families Citing this family (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10450235B2 (en) | 2012-04-27 | 2019-10-22 | General Electric Company | Method of producing an internal cavity in a ceramic matrix composite and mandrel therefor |
| US10011043B2 (en) * | 2012-04-27 | 2018-07-03 | General Electric Company | Method of producing an internal cavity in a ceramic matrix composite |
| US9845688B2 (en) * | 2013-03-15 | 2017-12-19 | Rolls-Royce Corporation | Composite blade with an integral blade tip shroud and method of forming the same |
| US9896945B2 (en) * | 2013-11-25 | 2018-02-20 | General Electric Company | Process of producing a ceramic matrix composite turbine bucket, insert for a ceramic matrix composite turbine bucket and ceramic matrix composite turbine bucket |
| US10457020B2 (en) * | 2014-01-17 | 2019-10-29 | General Electric Company | Ceramic matrix composite turbine blade squealer tip with flare |
| EP2902588B1 (en) * | 2014-01-31 | 2020-06-24 | Ansaldo Energia IP UK Limited | Composite turbine blade for high-temperature applications |
| US20160214283A1 (en) * | 2015-01-26 | 2016-07-28 | General Electric Company | Composite tool and method for forming composite components |
| US20160251272A1 (en) * | 2015-02-27 | 2016-09-01 | General Electric Company | Laminate structure fabricated using chemical vapor infiltration (cvi) |
| US9926796B2 (en) * | 2015-07-28 | 2018-03-27 | General Electric Company | Ply, method for manufacturing ply, and method for manufacturing article with ply |
| US10018054B2 (en) | 2015-10-23 | 2018-07-10 | General Electric Company | Fabrication of gas turbine engine components using multiple processing steps |
| US10273813B2 (en) * | 2015-10-29 | 2019-04-30 | General Electric Company | Ceramic matrix composite component and process of producing a ceramic matrix composite component |
| US10207471B2 (en) * | 2016-05-04 | 2019-02-19 | General Electric Company | Perforated ceramic matrix composite ply, ceramic matrix composite article, and method for forming ceramic matrix composite article |
| US10605095B2 (en) * | 2016-05-11 | 2020-03-31 | General Electric Company | Ceramic matrix composite airfoil cooling |
| US10329927B2 (en) * | 2016-08-15 | 2019-06-25 | General Electric Company | Hollow ceramic matrix composite article, mandrel for forming hollow ceramic matrix composite article, and method for forming hollow ceramic matrix composite article |
| US10391724B2 (en) * | 2017-02-15 | 2019-08-27 | General Electric Company | Method of forming pre-form ceramic matrix composite mold and method of forming a ceramic matrix composite component |
| US10569481B2 (en) | 2017-06-26 | 2020-02-25 | General Electric Company | Shaped composite ply layups and methods for shaping composite ply layups |
| US10801108B2 (en) * | 2017-08-28 | 2020-10-13 | Raytheon Technologies Corporation | Method for fabricating ceramic matrix composite components |
| US10329201B2 (en) * | 2017-09-21 | 2019-06-25 | General Electric Company | Ceramic matrix composite articles formation method |
| FR3071830B1 (fr) * | 2017-10-02 | 2021-03-12 | Safran Ceram | Procede pour la realisation d'une piece creuse en materiau composite a matrice ceramique |
| US11035239B2 (en) | 2018-10-25 | 2021-06-15 | General Electric Company | Ceramic matrix composite turbine nozzle shell and method of assembly |
| US11174203B2 (en) | 2018-10-25 | 2021-11-16 | General Electric Company | Ceramic matrix composite turbine nozzle shell and method of assembly |
| US11149561B2 (en) | 2019-08-12 | 2021-10-19 | Rolls-Royce Plc | System and method for making ceramic matrix composite vane with profiled end walls |
| CN112123515B (zh) * | 2020-09-07 | 2022-04-19 | 中国航发北京航空材料研究院 | 一种陶瓷基复合材料开口壳体一体成型方法与模具 |
| US20250264026A1 (en) * | 2024-02-15 | 2025-08-21 | Rtx Corporation | Forming gas turbine engine airfoils from cmcs with a kickback to facilitate mandrel removal |
Family Cites Families (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5710414A (en) | 1991-04-05 | 1998-01-20 | The Boeing Company | Internal tooling for induction heating |
| US6431255B1 (en) * | 1998-07-21 | 2002-08-13 | General Electric Company | Ceramic shell mold provided with reinforcement, and related processes |
| US6056915A (en) | 1998-10-21 | 2000-05-02 | Alliedsignal Inc. | Rapid manufacture of metal and ceramic tooling |
| GB9827889D0 (en) * | 1998-12-18 | 2000-03-29 | Rolls Royce Plc | A method of manufacturing a ceramic matrix composite |
| US6274078B1 (en) | 1999-01-27 | 2001-08-14 | General Electric Company | Method of removing cores from ceramic matrix composite articles |
| US7093359B2 (en) * | 2002-09-17 | 2006-08-22 | Siemens Westinghouse Power Corporation | Composite structure formed by CMC-on-insulation process |
| 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 |
| US7556477B2 (en) * | 2005-10-04 | 2009-07-07 | General Electric Company | Bi-layer tip cap |
| US7600979B2 (en) * | 2006-11-28 | 2009-10-13 | General Electric Company | CMC articles having small complex features |
| US20080149255A1 (en) * | 2006-12-20 | 2008-06-26 | General Electric Company | Ceramic composite article manufacture using thin plies |
| FR2913053B1 (fr) | 2007-02-23 | 2009-05-22 | Snecma Sa | Procede de fabrication d'un carter de turbine a gaz en materiau composite et carter ainsi obtenu |
| DE102007015909A1 (de) | 2007-04-02 | 2008-10-09 | Mt Aerospace Ag | Verfahren zur Herstellung faserverstärkter Hohlkörper |
| US8357323B2 (en) * | 2008-07-16 | 2013-01-22 | Siemens Energy, Inc. | Ceramic matrix composite wall with post laminate stitching |
| FR2934014B1 (fr) * | 2008-07-17 | 2011-05-13 | Snecma Propulsion Solide | Procede de realisation d'une tuyere ou d'un divergent de tuyere en materiau composite. |
| US8714932B2 (en) | 2008-12-31 | 2014-05-06 | General Electric Company | Ceramic matrix composite blade having integral platform structures and methods of fabrication |
| GB0901189D0 (en) * | 2009-01-26 | 2009-03-11 | Rolls Royce Plc | Manufacturing a composite component |
| US20120279631A1 (en) | 2009-11-13 | 2012-11-08 | Ihi Corporation | Method for manufacturing vane |
| GB201006625D0 (en) * | 2010-04-21 | 2010-06-02 | Rolls Royce Plc | A method of manufacturing a ceramic matrix composite article |
| US8834125B2 (en) * | 2011-05-26 | 2014-09-16 | United Technologies Corporation | Hybrid rotor disk assembly with a ceramic matrix composite airfoil for a gas turbine engine |
| US8734107B2 (en) * | 2011-05-31 | 2014-05-27 | General Electric Company | Ceramic-based tip cap for a turbine bucket |
| US9663404B2 (en) * | 2012-01-03 | 2017-05-30 | General Electric Company | Method of forming a ceramic matrix composite and a ceramic matrix component |
| US9410437B2 (en) * | 2012-08-14 | 2016-08-09 | General Electric Company | Airfoil components containing ceramic-based materials and processes therefor |
| 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 |
-
2012
- 2012-04-13 US US13/446,465 patent/US9050769B2/en active Active
-
2013
- 2013-01-31 JP JP2013016278A patent/JP6325192B2/ja active Active
- 2013-02-11 EP EP13154858.8A patent/EP2650478B1/en active Active
- 2013-02-12 RU RU2013105722/03A patent/RU2013105722A/ru not_active Application Discontinuation
-
2015
- 2015-06-09 US US14/734,028 patent/US9981438B2/en active Active
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