DE60201406D1 - Integrierte Oberflächenmerkmale für Komponenten aus keramischem Matrix-Verbundwerkstoff und entsprechende Methode - Google Patents
Integrierte Oberflächenmerkmale für Komponenten aus keramischem Matrix-Verbundwerkstoff und entsprechende MethodeInfo
- Publication number
- DE60201406D1 DE60201406D1 DE60201406T DE60201406T DE60201406D1 DE 60201406 D1 DE60201406 D1 DE 60201406D1 DE 60201406 T DE60201406 T DE 60201406T DE 60201406 T DE60201406 T DE 60201406T DE 60201406 D1 DE60201406 D1 DE 60201406D1
- Authority
- DE
- Germany
- Prior art keywords
- matrix composite
- surface features
- ceramic matrix
- corresponding method
- components made
- 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.)
- Expired - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/221—Improvement of heat transfer
- F05D2260/2212—Improvement of heat transfer by creating turbulence
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M2900/00—Special features of, or arrangements for combustion chambers
- F23M2900/05004—Special materials for walls or lining
-
- 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
- Y10T29/49339—Hollow blade
- Y10T29/49341—Hollow blade with cooling passage
- Y10T29/49343—Passage contains tubular insert
-
- 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
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
- Y10T428/1352—Polymer or resin containing [i.e., natural or synthetic]
- Y10T428/1362—Textile, fabric, cloth, or pile containing [e.g., web, net, woven, knitted, mesh, nonwoven, matted, etc.]
-
- 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
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
- Y10T428/1352—Polymer or resin containing [i.e., natural or synthetic]
- Y10T428/139—Open-ended, self-supporting conduit, cylinder, or tube-type article
-
- 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.]
- Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
-
- 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
- Y10T428/24612—Composite web or sheet
-
- 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.]
- Y10T428/24777—Edge feature
-
- 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.]
- Y10T428/24802—Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.]
- Y10T428/24926—Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.] including ceramic, glass, porcelain or quartz layer
-
- 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.]
- Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
- Y10T428/2495—Thickness [relative or absolute]
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Ceramic Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US683384 | 1996-07-18 | ||
US09/683,384 US6610385B2 (en) | 2001-12-20 | 2001-12-20 | Integral surface features for CMC components and method therefor |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60201406D1 true DE60201406D1 (de) | 2004-11-04 |
DE60201406T2 DE60201406T2 (de) | 2006-03-09 |
Family
ID=24743821
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60201406T Expired - Lifetime DE60201406T2 (de) | 2001-12-20 | 2002-12-18 | Integrierte Oberflächenmerkmale für Komponenten aus keramischem Matrix-Verbundstoff und entsprechendes Verfahren |
Country Status (5)
Country | Link |
---|---|
US (1) | US6610385B2 (de) |
EP (1) | EP1321712B1 (de) |
JP (1) | JP4307059B2 (de) |
KR (1) | KR100676000B1 (de) |
DE (1) | DE60201406T2 (de) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7104067B2 (en) * | 2002-10-24 | 2006-09-12 | General Electric Company | Combustor liner with inverted turbulators |
US6984277B2 (en) * | 2003-07-31 | 2006-01-10 | Siemens Westinghouse Power Corporation | Bond enhancement for thermally insulated ceramic matrix composite materials |
US20050113229A1 (en) * | 2003-11-25 | 2005-05-26 | General Electric Company | Universal mandrel |
US20050158171A1 (en) * | 2004-01-15 | 2005-07-21 | General Electric Company | Hybrid ceramic matrix composite turbine blades for improved processibility and performance |
US7435058B2 (en) | 2005-01-18 | 2008-10-14 | Siemens Power Generation, Inc. | Ceramic matrix composite vane with chordwise stiffener |
US7776404B2 (en) * | 2006-11-30 | 2010-08-17 | General Electric Company | Methods for forming thermal oxidative barrier coatings on organic matrix composite substrates |
US7600979B2 (en) | 2006-11-28 | 2009-10-13 | General Electric Company | CMC articles having small complex features |
US20090165924A1 (en) * | 2006-11-28 | 2009-07-02 | General Electric Company | Method of manufacturing cmc articles having small complex features |
JP5378676B2 (ja) * | 2006-11-30 | 2013-12-25 | ゼネラル・エレクトリック・カンパニイ | 有機マトリックス複合材基材用の遮熱酸化防止コーティング及び被覆物品 |
US7837914B2 (en) * | 2006-12-04 | 2010-11-23 | General Electric Company | Process of producing a composite component and intermediate product thereof |
FR2912469B1 (fr) * | 2007-02-12 | 2009-05-08 | Snecma Propulsion Solide Sa | Procede de fabrication d'une structure a lobes de melangeur de flux en cmc pour moteur aeronautique a turbine de gaz. |
FR2929690B1 (fr) * | 2008-04-03 | 2012-08-17 | Snecma Propulsion Solide | Chambre de combustion sectorisee en cmc pour turbine a gaz |
FR2929689B1 (fr) * | 2008-04-03 | 2013-04-12 | Snecma Propulsion Solide | Chambre de combustion de turbine a gaz a parois interne et externe sectorisees |
CA2731373C (en) * | 2008-08-22 | 2014-07-08 | Mitsubishi Heavy Industries, Ltd. | Heat exchange bulkhead |
US8801886B2 (en) * | 2010-04-16 | 2014-08-12 | General Electric Company | Ceramic composite components and methods of fabricating the same |
JP5455962B2 (ja) * | 2011-04-06 | 2014-03-26 | 三菱重工業株式会社 | 冷却構造の製造方法 |
DE102011103106A1 (de) * | 2011-05-25 | 2012-11-29 | Erbicol S.A. | Wärmeübertrager aus keramischem Material, insbesondere für Rekuperatorbrenner, und Verfahren zu dessen Herstellung |
EP2584145A1 (de) * | 2011-10-20 | 2013-04-24 | Siemens Aktiengesellschaft | Gekühlte Turbinenleitschaufel oder gekühltes Turbinenleitblatt für eine Turbomaschine |
US8967974B2 (en) | 2012-01-03 | 2015-03-03 | General Electric Company | Composite airfoil assembly |
WO2014058502A2 (en) * | 2012-07-31 | 2014-04-17 | General Electric Company | Ceramic centerbody and method of making |
CA2897965C (en) | 2013-03-11 | 2020-02-25 | David J. Thomas | Compliant intermediate component of a gas turbine engine |
US9896954B2 (en) | 2014-10-14 | 2018-02-20 | Rolls-Royce Corporation | Dual-walled ceramic matrix composite (CMC) component with integral cooling and method of making a CMC component with integral cooling |
US10309257B2 (en) | 2015-03-02 | 2019-06-04 | Rolls-Royce North American Technologies Inc. | Turbine assembly with load pads |
US20170159487A1 (en) * | 2015-12-02 | 2017-06-08 | General Electric Company | HT Enhancement Bumps/Features on Cold Side |
US10436062B2 (en) * | 2016-11-17 | 2019-10-08 | United Technologies Corporation | Article having ceramic wall with flow turbulators |
WO2019194860A2 (en) * | 2017-09-27 | 2019-10-10 | Siemens Aktiengesellschaft | 3d cmc material having a thermal protection layer |
US11402097B2 (en) | 2018-01-03 | 2022-08-02 | General Electric Company | Combustor assembly for a turbine engine |
US11820716B2 (en) * | 2018-10-18 | 2023-11-21 | Rolls Royce North American Technologies Inc. | Method of fabricating cooling features on a ceramic matrix composite (CMC) component |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5184455A (en) * | 1991-07-09 | 1993-02-09 | The United States Of America As Represented By The Secretary Of The Air Force | Ceramic blanket augmentor liner |
US5331816A (en) * | 1992-10-13 | 1994-07-26 | United Technologies Corporation | Gas turbine engine combustor fiber reinforced glass ceramic matrix liner with embedded refractory ceramic tiles |
DE4343120A1 (de) * | 1993-12-17 | 1995-06-22 | Abb Patent Gmbh | Thermische Isolation |
WO1999006771A1 (en) * | 1997-07-31 | 1999-02-11 | Alliedsignal Inc. | Rib turbulators for combustor external cooling |
US6468669B1 (en) * | 1999-05-03 | 2002-10-22 | General Electric Company | Article having turbulation and method of providing turbulation on an article |
US6277313B1 (en) * | 1999-08-23 | 2001-08-21 | Northrop Grumman Corporation | Combination continuous woven-fiber and discontinuous ceramic-fiber structure |
-
2001
- 2001-12-20 US US09/683,384 patent/US6610385B2/en not_active Expired - Lifetime
-
2002
- 2002-12-18 KR KR1020020081090A patent/KR100676000B1/ko active IP Right Grant
- 2002-12-18 DE DE60201406T patent/DE60201406T2/de not_active Expired - Lifetime
- 2002-12-18 EP EP02258732A patent/EP1321712B1/de not_active Expired - Lifetime
- 2002-12-19 JP JP2002367431A patent/JP4307059B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US20030129338A1 (en) | 2003-07-10 |
EP1321712A1 (de) | 2003-06-25 |
KR20030053013A (ko) | 2003-06-27 |
DE60201406T2 (de) | 2006-03-09 |
US6610385B2 (en) | 2003-08-26 |
EP1321712B1 (de) | 2004-09-29 |
JP4307059B2 (ja) | 2009-08-05 |
KR100676000B1 (ko) | 2007-01-29 |
JP2003214186A (ja) | 2003-07-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8328 | Change in the person/name/address of the agent |
Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN |