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7351364 |
Method of manufacturing a hybrid structure
A method of manufacturing a hybrid structure ( 100 ) having a layer of CMC material ( 28 ) defining an interior passageway ( 24 ) and a layer of ceramic insulating material ( 18 ) lining the...
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7334330 |
Thermally insulating layer incorporating a distinguishing agent and method for inspecting the same
Thermally insulating layer incorporating a distinguishing agent and method for inspecting the insulating layer are provided. The distinguishing agent may be used for determining a remaining...
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EP1881156A2 |
Turbine vane with removable platform inserts
Aspects of the invention are related to a turbine vane assembly (10) in which at least one of the platforms (22, 24) is equipped with one or more removable platform inserts (34). The inserts (34)...
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7316539 |
Vane assembly with metal trailing edge segment
Embodiments of the invention relate to a vane assembly formed by a forward airfoil segment and an aft airfoil segment. The aft segment is made of metal and can define the trailing edge of the vane...
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7311790 |
Hybrid structure using ceramic tiles and method of manufacture
A hybrid structure ( 50 ) and method of manufacturing the same including a structural ceramic matrix composite (CMC) material ( 42 ) coated with a layer of ceramic insulating tiles ( 24 )....
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7300621 |
Method of making a ceramic matrix composite utilizing partially stabilized fibers
A green body ceramic matrix composite material (30) is formed using ceramic fibers (32) in an intermediate state disposed in a green body ceramic matrix material (34). The fibers may be in either a...
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7258530 |
CMC component and method of fabrication
An airfoil ( 44 ) formed of a plurality of pre-fired structural CMC panels ( 46, 48, 50, 52 ). Each panel is formed to have an open shape having opposed ends ( 54 ) that are free to move during the...
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7247002 |
Lamellate CMC structure with interlock to metallic support structure
A component ( 10 ) for a gas turbine engine formed of a stacked plurality of ceramic matrix composite (CMC) lamellae ( 12 ) supported by a metal support structure ( 20 ). Individual lamellae are...
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7108925 |
High temperature insulation utilizing zirconia-hafnia
A ceramic insulating composition including monoclinic zirconia-hafnia. The zirconia-hafnia may be used as a filler powder ( 14 ) in a ceramic composition ( 10 ), or it may be used as a protective...
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7067181 |
Insulating ceramic based on partially filled shapes
An insulating ceramic made up of a plurality of partially filled shapes (e.g., 101 ), such as oblate spheroids, spheres, and shapes free of corners, is provided. Each partially filled shape may...
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7001679 |
Protective overlayer for ceramics
A xenotime phosphate protective overlayer ( 22 ) for protecting a ceramic material ( 24 ) from a high temperature, moisture-containing environment. Yttrium phosphate may be used as a protective...
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6984277 |
Bond enhancement for thermally insulated ceramic matrix composite materials
A composite structure ( 62 ) having a bond enhancement member ( 76 ) extending across a bond joint ( 86 ) between a ceramic matrix composite (CMC) material ( 80 ) and a ceramic insulation material...
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6939603 |
Thermal barrier coating having subsurface inclusions for improved thermal shock resistance
A component ( 10 ) having a thermal barrier coating ( 14 ) exhibiting an improved resistance to thermal shock. A plurality of stress relieving cracks ( 22 ) are formed at the free surface ( 24 ) of...
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6929852 |
Protective overlayer for ceramics
An alumina comprising composition protective overlayer ( 20 ) for protecting a ceramic matrix composite material ( 12 ) from a high temperature, moisture-containing environment. Alumina may be used...
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6884384 |
Method for making a high temperature erosion resistant material containing compacted hollow geometric shapes
A method for making a thermal insulating material includes the steps of: providing a chamber, placing hollow geometric shapes in the chamber, closing the chamber, evacuating air from the chamber,...
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6846574 |
Honeycomb structure thermal barrier coating
A device having an improved thermal barrier coating ( 46 ) and a process for manufacturing the same. A support structure ( 28 ) for retaining a ceramic insulating material ( 46 ) on a substrate (...
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6767659 |
Backside radiative cooled ceramic matrix composite component
An article comprising a ceramic matrix composite component of a gas turbine engine such as a combustion liner this is adapted for backside radiative cooling is provided. The article comprises a...
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6733907 |
Hybrid ceramic material composed of insulating and structural ceramic layers
A hybrid ceramic structure ( 10 ), for use in high temperature environments such as in gas turbines, is made from an insulating layer ( 12 ) of porous ceramic that is thermally stable at...
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EP1394138A2 |
Protective overlayer for ceramics
An alumina comprising composition protective overlayer (20) for protecting a ceramic matrix composite material (12) from a high temperature, moisture-containing environment. Alumina may be used as...
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6676783 |
High temperature insulation for ceramic matrix composites
A ceramic composition is provided to insulate ceramic matrix composites under high temperature, high heat flux environments. The composition comprises a plurality of hollow oxide-based spheres of...
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6641907 |
High temperature erosion resistant coating and material containing compacted hollow geometric shapes
A material system ( 60 ) contains close packed hollow shapes ( 50, 70 ) having a dense wall structure ( 52, 66 ), which are bonded together and which may contain a matrix binder material ( 56 )...
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6617013 |
Ceramic matrix composite having improved interlaminar strength
A ceramic matrix composite material ( 10 ) having a plurality of interlaminar stitches ( 16 ) as shown in FIG. 1 . The stitches are formed by directing laser energy into the material to melt and...
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6528190 |
Fiber coating compounds for reinforced ceramic matrix composites
A composite ( 20 ) has a matrix ( 10 ), preferably of ceramic, interspersed with reinforcement structures ( 12 ), preferably ceramic fibers, coated with a material ( 14 ) selected from ZrGeO 4 ,...
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6514046 |
Ceramic composite vane with metallic substructure
A vane assembly for a turbine assembly includes an inner endcap, an outer endcap, and a body. The body includes a metallic core assembly, a ceramic shell assembly and a support assembly. The...
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6347446 |
Method of making silicon carbide-silicon composite having improved oxidation resistance
A Silicon carbide-silicon matrix composite having improved oxidation resistance at high temperatures in dry or water-containing environments is provided. A method is given for sealing matrix cracks...
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6284682 |
Process for making chemically bonded sol-gel ceramics
This invention relates to a novel method of decreasing porosity of ceramics produced by sol-gel processing. The process of preparing chemically bonded sol-gel ceramics comprises phosphating a...
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