Patent classifications
C23C18/04
Sintered-bonded high temperature coatings for ceramic turbomachine components
Methods for forming sintered-bonded high temperature coatings over ceramic turbomachine components are provided, as are ceramic turbomachine components having such high temperature coatings formed thereover. In one embodiment, the method includes the step or process of removing a surface oxide layer from the ceramic component body of a turbomachine component to expose a treated surface of the ceramic component body. A first layer of coating precursor material, which has a solids content composed predominately of at least one rare earth silicate by weight percentage, is applied to the treated surface. The first layer of the coating precursor material is then heat treated to sinter the solids content and form a first sintered coating layer bonded to the treated surface. The steps of applying and sintering the coating precursor may be repeated, as desired, to build a sintered coating body to a desired thickness over the ceramic component body.
MESOPOROUS SILICA FILM STRUCTURE HAVING ULTRA-LARGE PORE AND METHOD OF MANUFACTURING THE SAME
The present invention relates to a mesoporous film structure having ultra-large pores therein and a method of manufacturing the same. More particularly, the present invention relates to a mesoporous film structure having ultra-large pores therein and a method of manufacturing the same, in which a mesoporous film having ultra-large pores therein is formed on supports including various materials and having various shapes under chemically mild conditions. The size of the pores in the film is capable of being adjusted, and a patterned mesoporous structure is formed on the upper surface of the support rather than throughout the entire support.
SINTERED-BONDED HIGH TEMPERATURE COATINGS FOR CERAMIC TURBOMACHINE COMPONENTS
A coated turbomachine component includes a ceramic component body having a principal surface. The component includes a high temperature coating. The high temperature coating includes a sintered coating body bonded directly to and intimately contacting the principal surface of the ceramic component body. The sintered coating body has a minimum porosity adjacent the principal surface and a maximum porosity at a location further from the principal surface, as taken along an axis orthogonal to the principal surface.
SINTERED-BONDED HIGH TEMPERATURE COATINGS FOR CERAMIC TURBOMACHINE COMPONENTS
A coated turbomachine component includes a ceramic component body having a principal surface. The component includes a high temperature coating. The high temperature coating includes a sintered coating body bonded directly to and intimately contacting the principal surface of the ceramic component body. The sintered coating body has a minimum porosity adjacent the principal surface and a maximum porosity at a location further from the principal surface, as taken along an axis orthogonal to the principal surface.
TRANSITION-METAL CHALCOGENIDE THIN FILM AND PREPARING METHOD OF THE SAME
A method of manufacturing transition metal chalcogenide thin films, includes the operations of forming a transition metal chalcogenides precursor on a substrate, and irradiating light onto the transition metal chalcogenides precursor. The transition metal chalcogenides precursor includes an amine-based ligand.
TRANSITION-METAL CHALCOGENIDE THIN FILM AND PREPARING METHOD OF THE SAME
A method of manufacturing transition metal chalcogenide thin films, includes the operations of forming a transition metal chalcogenides precursor on a substrate, and irradiating light onto the transition metal chalcogenides precursor. The transition metal chalcogenides precursor includes an amine-based ligand.
POLYMER COATINGS FOR SHAPE MEMORY ALLOYS FOR USE IN PERCUTANEOUS HEART PUMPS
The present disclosure relates generally to percutaneous heart pumps including a self-expandable and collapsible impeller housing fabricated from a mesh of a shape memory alloy, such as nitinol, and a base polymer coating and a top polymer coating. Specifically, the present disclosure relates to highly flexible and fluid-impermissible polymer coatings having improved adherence and performance properties on the metallic surfaces of the impeller housing mesh thus improving the overall performance of the percutaneous heart pumps.
POLYMER COATINGS FOR SHAPE MEMORY ALLOYS FOR USE IN PERCUTANEOUS HEART PUMPS
The present disclosure relates generally to percutaneous heart pumps including a self-expandable and collapsible impeller housing fabricated from a mesh of a shape memory alloy, such as nitinol, and a base polymer coating and a top polymer coating. Specifically, the present disclosure relates to highly flexible and fluid-impermissible polymer coatings having improved adherence and performance properties on the metallic surfaces of the impeller housing mesh thus improving the overall performance of the percutaneous heart pumps.
Method and Wet Chemical Compositions for Diffusion Barrier Formation
A method of forming a diffusion barrier layer on a dielectric or semiconductor substrate by a wet process. The method includes the steps of treating the dielectric or semiconductor substrate with an aqueous pretreatment solution comprising one or more adsorption promoting ingredients capable of preparing the substrate for deposition of the diffusion barrier layer thereon; and contacting the treated dielectric or semiconductor substrate with a deposition solution comprising manganese compounds and an inorganic pH buffer (optionally, with one or more doping metals) to the diffusion barrier layer thereon, wherein the diffusion barrier layer comprises manganese oxide. Also included is a two-part kit for treating a dielectric or semiconductor substrate to form a diffusion barrier layer thereon.
HOT-STAMPED BODY
There is provided a hot-stamped body including: a steel base metal; and a metallic layer formed on a surface of the steel base metal, wherein the metallic layer includes: an interface layer that contains, in mass %, Al: 30.0 to 36.0%, has a thickness of 100 nm to 5 m, and is located in an interface between the metallic layer and the steel base metal; and a principal layer that includes coexisting MgZn.sub.2 phases and insular FeAl.sub.2 phases, is located on the interface layer, and has a thickness of 3 m to 40 m.