DE69632981D1 - Verschleisszusammensetzung, verfahren zur Herstellung einer Verschleisszusammensetzung und gasturbine Motor mit Verschleissdichtung - Google Patents
Verschleisszusammensetzung, verfahren zur Herstellung einer Verschleisszusammensetzung und gasturbine Motor mit VerschleissdichtungInfo
- Publication number
- DE69632981D1 DE69632981D1 DE69632981T DE69632981T DE69632981D1 DE 69632981 D1 DE69632981 D1 DE 69632981D1 DE 69632981 T DE69632981 T DE 69632981T DE 69632981 T DE69632981 T DE 69632981T DE 69632981 D1 DE69632981 D1 DE 69632981D1
- Authority
- DE
- Germany
- Prior art keywords
- wear
- composition
- producing
- gas turbine
- turbine engine
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B18/00—Layered products essentially comprising ceramics, e.g. refractory products
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B20/00—Use of materials as fillers for mortars, concrete or artificial stone according to more than one of groups C04B14/00 - C04B18/00 and characterised by shape or grain distribution; Treatment of materials according to more than one of the groups C04B14/00 - C04B18/00 specially adapted to enhance their filling properties in mortars, concrete or artificial stone; Expanding or defibrillating materials
- C04B20/0016—Granular materials, e.g. microballoons
- C04B20/002—Hollow or porous granular materials
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B28/00—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements
- C04B28/34—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements containing cold phosphate binders
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- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/127—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with a deformable or crushable structure, e.g. honeycomb
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/10—Sintering only
- B22F3/11—Making porous workpieces or articles
- B22F3/1103—Making porous workpieces or articles with particular physical characteristics
- B22F2003/1106—Product comprising closed porosity
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/00241—Physical properties of the materials not provided for elsewhere in C04B2111/00
- C04B2111/00344—Materials with friction-reduced moving parts, e.g. ceramics lubricated by impregnation with carbon
- C04B2111/00353—Sliding parts
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/00474—Uses not provided for elsewhere in C04B2111/00
- C04B2111/00612—Uses not provided for elsewhere in C04B2111/00 as one or more layers of a layered structure
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/65—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
- C04B2235/656—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/65—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
- C04B2235/656—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
- C04B2235/6567—Treatment time
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/65—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
- C04B2235/66—Specific sintering techniques, e.g. centrifugal sintering
- C04B2235/661—Multi-step sintering
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/34—Oxidic
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/34—Oxidic
- C04B2237/341—Silica or silicates
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/34—Oxidic
- C04B2237/343—Alumina or aluminates
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/38—Fiber or whisker reinforced
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- 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
- Y10T428/25—Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles
- Y10T428/252—Glass or ceramic [i.e., fired or glazed clay, cement, etc.] [porcelain, quartz, 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
- Y10T428/25—Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles
- Y10T428/256—Heavy metal or aluminum or compound thereof
-
- 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
- Y10T428/25—Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles
- Y10T428/259—Silicic material
-
- 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
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2982—Particulate matter [e.g., sphere, flake, etc.]
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Inorganic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Gasket Seals (AREA)
- Sealing Devices (AREA)
- Sealing Material Composition (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9513252 | 1995-06-29 | ||
GBGB9513252.8A GB9513252D0 (en) | 1995-06-29 | 1995-06-29 | An abradable composition |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69632981D1 true DE69632981D1 (de) | 2004-09-02 |
DE69632981T2 DE69632981T2 (de) | 2004-12-16 |
Family
ID=10776860
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69632981T Expired - Lifetime DE69632981T2 (de) | 1995-06-29 | 1996-03-27 | Verschleisszusammensetzung, verfahren zur Herstellung einer Verschleisszusammensetzung und gasturbine Motor mit Verschleissdichtung |
Country Status (6)
Country | Link |
---|---|
US (2) | US5780146A (de) |
EP (1) | EP0751104B1 (de) |
JP (1) | JPH0913007A (de) |
CA (1) | CA2177657A1 (de) |
DE (1) | DE69632981T2 (de) |
GB (1) | GB9513252D0 (de) |
Families Citing this family (69)
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GB9513252D0 (en) * | 1995-06-29 | 1995-09-06 | Rolls Royce Plc | An abradable composition |
US6733907B2 (en) * | 1998-03-27 | 2004-05-11 | Siemens Westinghouse Power Corporation | Hybrid ceramic material composed of insulating and structural ceramic layers |
US7563504B2 (en) * | 1998-03-27 | 2009-07-21 | Siemens Energy, Inc. | Utilization of discontinuous fibers for improving properties of high temperature insulation of ceramic matrix composites |
US6977060B1 (en) | 2000-03-28 | 2005-12-20 | Siemens Westinghouse Power Corporation | Method for making a high temperature erosion resistant coating and material containing compacted hollow geometric shapes |
US7179524B2 (en) * | 1998-03-27 | 2007-02-20 | Siemens Power Generation, Inc. | Insulated ceramic matrix composite and method of manufacturing |
US7067181B2 (en) * | 2003-08-05 | 2006-06-27 | Siemens Power Generation, Inc. | Insulating ceramic based on partially filled shapes |
US6197424B1 (en) * | 1998-03-27 | 2001-03-06 | Siemens Westinghouse Power Corporation | Use of high temperature insulation for ceramic matrix composites in gas turbines |
US6013592A (en) * | 1998-03-27 | 2000-01-11 | Siemens Westinghouse Power Corporation | High temperature insulation for ceramic matrix composites |
US6641907B1 (en) * | 1999-12-20 | 2003-11-04 | Siemens Westinghouse Power Corporation | High temperature erosion resistant coating and material containing compacted hollow geometric shapes |
US6315519B1 (en) * | 1998-09-28 | 2001-11-13 | General Electric Company | Turbine inner shroud and turbine assembly containing such inner shroud |
US6089825A (en) * | 1998-12-18 | 2000-07-18 | United Technologies Corporation | Abradable seal having improved properties and method of producing seal |
US6165542A (en) * | 1998-12-23 | 2000-12-26 | United Technologies Corporation | Method for fabricating and inspecting coatings |
US6235370B1 (en) | 1999-03-03 | 2001-05-22 | Siemens Westinghouse Power Corporation | High temperature erosion resistant, abradable thermal barrier composite coating |
SG90198A1 (en) * | 1999-12-23 | 2002-07-23 | United Technologies Corp | Composite abradable material |
US6365222B1 (en) | 2000-10-27 | 2002-04-02 | Siemens Westinghouse Power Corporation | Abradable coating applied with cold spray technique |
US6435824B1 (en) * | 2000-11-08 | 2002-08-20 | General Electric Co. | Gas turbine stationary shroud made of a ceramic foam material, and its preparation |
US6846574B2 (en) | 2001-05-16 | 2005-01-25 | Siemens Westinghouse Power Corporation | Honeycomb structure thermal barrier coating |
US6884384B2 (en) | 2001-09-27 | 2005-04-26 | Siemens Westinghouse Power Corporation | Method for making a high temperature erosion resistant material containing compacted hollow geometric shapes |
GB2388161A (en) * | 2002-05-02 | 2003-11-05 | Rolls Royce Plc | Gas turbine engine compressor casing |
GB0226997D0 (en) * | 2002-11-19 | 2002-12-24 | Welding Inst | Heat resistant product |
FR2840839B1 (fr) * | 2002-06-14 | 2005-01-14 | Snecma Moteurs | Materiau metallique susceptible d'etre use par abrasion; pieces, carter; procede d'elaboration dudit materiau |
US6929852B2 (en) * | 2002-08-08 | 2005-08-16 | Siemens Westinghouse Power Corporation | Protective overlayer for ceramics |
US6702553B1 (en) | 2002-10-03 | 2004-03-09 | General Electric Company | Abradable material for clearance control |
US20040188323A1 (en) * | 2003-03-24 | 2004-09-30 | Tzatzov Konstantin K. | Active coating system for reducing or eliminating coke build-up during petrochemical processes |
US7311790B2 (en) * | 2003-04-25 | 2007-12-25 | Siemens Power Generation, Inc. | Hybrid structure using ceramic tiles and method of manufacture |
US7255929B2 (en) * | 2003-12-12 | 2007-08-14 | General Electric Company | Use of spray coatings to achieve non-uniform seal clearances in turbomachinery |
US7351364B2 (en) * | 2004-01-29 | 2008-04-01 | Siemens Power Generation, Inc. | Method of manufacturing a hybrid structure |
FR2887890B1 (fr) * | 2005-06-30 | 2007-10-12 | Snecma | Composition de materiau abradable, piece thermomecanique ou carter comprenant un revetement et procede de fabrication ou de reparation d'un revetement presentant cette composition |
US7628951B1 (en) * | 2005-10-21 | 2009-12-08 | Ceramatec, Inc. | Process for making ceramic insulation |
US7604867B2 (en) * | 2005-12-20 | 2009-10-20 | General Electric Company | Particulate corrosion resistant coating composition, coated turbine component and method for coating same |
US8349111B2 (en) * | 2006-08-14 | 2013-01-08 | Ceramatec, Inc. | Method for joining ceramic components |
US20080061515A1 (en) * | 2006-09-08 | 2008-03-13 | Eric Durocher | Rim seal for a gas turbine engine |
US8017240B2 (en) | 2006-09-28 | 2011-09-13 | United Technologies Corporation | Ternary carbide and nitride thermal spray abradable seal material |
US20100119777A1 (en) * | 2006-11-16 | 2010-05-13 | Siemens Power Generation, Inc. | Ceramic matrix composite surfaces with open features for improved bonding to coatings |
GB0703827D0 (en) * | 2007-02-28 | 2007-04-11 | Rolls Royce Plc | Rotor seal segment |
GB2449249B (en) * | 2007-05-14 | 2009-10-21 | Rolls Royce Plc | Seal assembley |
US20080286459A1 (en) * | 2007-05-17 | 2008-11-20 | Pratt & Whitney Canada Corp. | Method for applying abradable coating |
US9447503B2 (en) * | 2007-05-30 | 2016-09-20 | United Technologies Corporation | Closed pore ceramic composite article |
WO2009146189A1 (en) | 2008-04-17 | 2009-12-03 | Christopher Sortore | High-speed permanent magnet motor and generator with low-loss metal rotor |
US20110168450A1 (en) * | 2010-01-12 | 2011-07-14 | Halliburton Energy Services, Inc. | Drill bit bearing contact pressure reduction |
US9598972B2 (en) | 2010-03-30 | 2017-03-21 | United Technologies Corporation | Abradable turbine air seal |
DE102010026312B4 (de) | 2010-07-06 | 2022-10-20 | Phoenix Contact Gmbh & Co. Kg | Anschlusskontakt und Verfahren zur Herstellung von Anschlusskontakten |
WO2013081606A1 (en) * | 2011-11-30 | 2013-06-06 | Halliburton Energy Services, Inc. | Drill bit with seal having spheres in a matrix seal material |
US9726043B2 (en) | 2011-12-15 | 2017-08-08 | General Electric Company | Mounting apparatus for low-ductility turbine shroud |
US20130236302A1 (en) * | 2012-03-12 | 2013-09-12 | Charles Alexander Smith | In-situ gas turbine rotor blade and casing clearance control |
GB201213109D0 (en) | 2012-07-24 | 2012-09-05 | Rolls Royce Plc | Seal segment |
EP2951241A4 (de) * | 2013-01-29 | 2016-08-24 | United Technologies Corp | Klingenabriebmaterial |
GB201303995D0 (en) | 2013-03-06 | 2013-04-17 | Rolls Royce Plc | CMC turbine engine component |
GB201305702D0 (en) | 2013-03-28 | 2013-05-15 | Rolls Royce Plc | Seal segment |
GB201305701D0 (en) * | 2013-03-28 | 2013-05-15 | Rolls Royce Plc | Wall section for the working gas annulus of a gas turbine engine |
WO2014186099A1 (en) | 2013-05-17 | 2014-11-20 | General Electric Company | Cmc shroud support system of a gas turbine |
WO2015088869A1 (en) | 2013-12-12 | 2015-06-18 | General Electric Company | Cmc shroud support system |
EP3155230B1 (de) | 2014-06-12 | 2022-06-01 | General Electric Company | Mehrteilige ummantelungsaufhängungsanordnung |
EP3155231B1 (de) | 2014-06-12 | 2019-07-03 | General Electric Company | Ummantelungsaufhängeranordnung |
CA2951425C (en) | 2014-06-12 | 2019-12-24 | General Electric Company | Shroud hanger assembly |
US9874104B2 (en) | 2015-02-27 | 2018-01-23 | General Electric Company | Method and system for a ceramic matrix composite shroud hanger assembly |
US20160305319A1 (en) * | 2015-04-17 | 2016-10-20 | General Electric Company | Variable coating porosity to influence shroud and rotor durability |
US9951642B2 (en) * | 2015-05-08 | 2018-04-24 | United Technologies Corporation | Intermittent grooved soft abradable material to reduce blade tip temperature |
US10100656B2 (en) | 2015-08-25 | 2018-10-16 | General Electric Company | Coated seal slot systems for turbomachinery and methods for forming the same |
US10294962B2 (en) * | 2017-06-30 | 2019-05-21 | United Technologies Corporation | Turbine engine seal for high erosion environment |
US11149744B2 (en) * | 2017-09-19 | 2021-10-19 | Raytheon Technologies Corporation | Turbine engine seal for high erosion environment |
GB201813086D0 (en) | 2018-08-10 | 2018-09-26 | Rolls Royce Plc | Efficient gas turbine engine |
GB201813082D0 (en) | 2018-08-10 | 2018-09-26 | Rolls Royce Plc | Efficient gas turbine engine |
GB201813081D0 (en) | 2018-08-10 | 2018-09-26 | Rolls Royce Plc | Efficient gas turbine engine |
FR3085172B1 (fr) | 2018-08-22 | 2021-03-05 | Safran Aircraft Engines | Revetement abradable pour aubes tournantes d'une turbomachine |
GB201820224D0 (en) | 2018-12-12 | 2019-01-23 | Rolls Royce Plc | Seal segment for shroud ring of a gas turbine engine |
EP3683406B1 (de) * | 2019-01-18 | 2023-11-29 | Ansaldo Energia Switzerland AG | Abreibbares hybrides material, insbesondere für dichtungselemente in gasturbinen, und herstellungsverfahren dafür |
US11149354B2 (en) | 2019-02-20 | 2021-10-19 | General Electric Company | Dense abradable coating with brittle and abradable components |
DE102023002027A1 (de) | 2023-05-19 | 2024-01-18 | Mercedes-Benz Group AG | Verfahren zur Herstellung eines Metall-Keramik-Komposit-Bauteils sowie das Metall-Keramik-Komposit-Bauteil |
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DE2053765A1 (en) * | 1969-11-04 | 1971-05-13 | G Hutmacher & Co Dr | Insulating material for lining chill tops |
FR2157106A5 (de) * | 1971-10-18 | 1973-06-01 | Electro Refractaire | |
US3975165A (en) * | 1973-12-26 | 1976-08-17 | Union Carbide Corporation | Graded metal-to-ceramic structure for high temperature abradable seal applications and a method of producing said |
GB1448320A (en) * | 1974-03-04 | 1976-09-02 | Univ Washington | Lightweight inorganic material |
FR2264789A1 (en) * | 1974-03-21 | 1975-10-17 | Thomson Csf | Rigid syntactic foam for electronic use - mfd from inorganic spheres and inorganic binders |
DE2729077A1 (de) * | 1977-06-28 | 1979-01-11 | Bayer Ag | Anorganische formkoerper und verfahren zu ihrer herstellung |
US4177308A (en) * | 1978-08-10 | 1979-12-04 | The United States Of America As Represented By The Secretary Of The Air Force | Non-combustible high temperature abradable seal material |
GB2056502B (en) * | 1979-08-21 | 1983-11-02 | Rolls Royce | Metal coated glass particles for flame spraying |
JPS5632360A (en) * | 1979-08-28 | 1981-04-01 | Asahi Chemical Ind | Lightweight refractory formed body |
GB2072222B (en) * | 1980-03-22 | 1983-02-16 | Rolls Royce | Coating compositions containing metal and glass |
GB2081246B (en) * | 1980-07-25 | 1984-03-14 | Rolls Royce | Thermal barrier coating composition |
FR2507729B1 (fr) * | 1981-06-12 | 1986-08-22 | Snecma | Joint susceptible d'etre use par abrasion et son procede de realisation |
US4450184A (en) * | 1982-02-16 | 1984-05-22 | Metco Incorporated | Hollow sphere ceramic particles for abradable coatings |
US4440865A (en) * | 1982-03-08 | 1984-04-03 | Salazar Paul V | Refractory compositions and method |
US4639388A (en) * | 1985-02-12 | 1987-01-27 | Chromalloy American Corporation | Ceramic-metal composites |
US5204289A (en) * | 1991-10-18 | 1993-04-20 | Minnesota Mining And Manufacturing Company | Glass-based and glass-ceramic-based composites |
GB9513252D0 (en) * | 1995-06-29 | 1995-09-06 | Rolls Royce Plc | An abradable composition |
-
1995
- 1995-06-29 GB GBGB9513252.8A patent/GB9513252D0/en active Pending
-
1996
- 1996-03-27 DE DE69632981T patent/DE69632981T2/de not_active Expired - Lifetime
- 1996-03-27 EP EP96302094A patent/EP0751104B1/de not_active Expired - Lifetime
- 1996-05-22 US US08/651,486 patent/US5780146A/en not_active Expired - Lifetime
- 1996-05-29 CA CA002177657A patent/CA2177657A1/en not_active Abandoned
- 1996-06-03 JP JP8139903A patent/JPH0913007A/ja not_active Withdrawn
-
1998
- 1998-04-22 US US09/064,143 patent/US5962076A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US5780146A (en) | 1998-07-14 |
EP0751104A2 (de) | 1997-01-02 |
CA2177657A1 (en) | 1996-12-30 |
DE69632981T2 (de) | 2004-12-16 |
EP0751104A3 (de) | 1997-03-26 |
GB9513252D0 (en) | 1995-09-06 |
JPH0913007A (ja) | 1997-01-14 |
US5962076A (en) | 1999-10-05 |
EP0751104B1 (de) | 2004-07-28 |
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8364 | No opposition during term of opposition |