The invention relates to a ceramic sealing system between a rotor blade (120) and a housing (I). A small porous zirconium oxide layer (II) on a turbine rotor blade, which zirconium oxide layer faces a ceramic layer system (15′, 15″) of higher porosity, achieves durable sealing systems. The housing (I″) has a metal substrate (7), a metal adhesion-promoting layer (10), and a thick, outer, ceramic layer (15′, 15″) based on zirconium oxide, in particular having a porosity 2≥14%.

A mineral wool insulating product which comprises a layer, notably a continuous layer, of mixed mineral wool fibres, the mixed mineral wool fibres comprising a binder, first mineral wool fibres and second mineral wool fibres, the first mineral wool fibres and the second mineral wool fibres have a difference of softening point.

A dry composition formulated to be combined with water to form a jamb spray mix, the dry composition comprising, by weight: 0.1% to 10% phosphate by weight based on total weight of the dry composition; 5% to 15% plasticizer by weight based on total weight of the dry composition; and the balance including fused silica particles and impurities.

The present invention relates to a thermal emissivity coating composition comprising: a) an emissivity agent in an amount from 30 to 65% by weight with respect to the total weight of the thermal emissivity coating composition; b) a filler selected from the group consisting of oxides of aluminum, silicon, magnesium, calcium, boron and mixtures of two or more thereof, in an amount from 10 to 35 wt % with respect to the total weight of the thermal emissivity coating composition; and c) a binder in an amount from 12 to 52 wt % with respect to the total weight of the thermal emissivity coating composition; wherein the emissivity agent comprises cobalt oxide in an amount from 10 to 25 wt %, preferably 12 to 25 wt % with respect to the total weight of the thermal emissivity coating composition and further comprises chromium oxide and titanium oxide.

The present invention relates to a dry refractory particulate composition comprising a zeolithic microstructure, to a green body and to a refractory lining formed therefrom, and to uses thereof.

A porous refractory in the K.sub.2O—SiO.sub.2—B.sub.2O.sub.3 system is formed by chemical direct foaming by heating to over 600° C., resulting in adherent black or white foam. The foam can function as highly porous thermal insulation, a high or low thermal emissivity surface, as a sealant for deteriorated refractory surfaces, as a filler for pockmarks/holes/gaps or as a bonding agent for parts with large gaps between them.

A method for preparing aerogel particles and a coated component are provided. The coated component includes a substrate and a coating. The coating includes aerogel particles sprayed from a hot gas jet or plasma jet. The method includes the step of feeding one or a plurality of gel particles into a hot gas jet or plasma j et. The one or a plurality of gel particles are sufficiently small to permit supercritical drying during the time the particles are in the jet. The method further includes the step of exposing the one or a plurality of gel particles to the temperatures and pressures of the hot gas jet or plasma jet to create the aerogel particles outside of a jet emitter and/or without a sealed pressure vessel.

Disclosed is a hydraulically and chemically bonding refractory cement, which includes a caustic magnesia component having a BET specific surface area of at least 0.5 m.sup.2/g, and a carboxylic acid component, wherein the carboxylic acid component consists of at least one carboxylic acid that is only slightly water soluble and/or has a low dissolution rate in aqueous solutions, and which carboxylic acid component is capable of generating at least one soluble magnesium salt upon contact of the cement with water. Also disclosed is a corresponding refractory material containing the magnesia cement and to uses thereof for the manufacture of products useful in various industries.

A ceramic sealing system between a rotor blade and a housing is provided. By means of the combination of a small porous zirconium oxide layer on a turbine rotor blade, which zirconium oxide layer faces a ceramic layer system of higher porosity, durable sealing systems are achieved. The housing has a metal substrate, a metal adhesion-promoting layer, and a thick, outer, ceramic layer based on zirconium oxide, in particular having a porosity 214%.

The present invention relates, in part, to a discovery of a method for using atomic layer deposition (ALD) to improve the stability of refractory materials in high temperature steam, and compositions produced by the method.