Coating compositions are provided that eject droplets of condensed fluid from a surface. The coatings include a nanostructured coating layer and in some embodiments, also include a hydrophobic layer deposited thereon. The coating materials eject droplets from the surface in the presence of non-condensing gases such as air and may be deployed under conditions of supersaturation of the condensed fluid to be ejected. A heat exchanger design utilizing the coating is described herein.

Coating compositions are provided that eject droplets of condensed fluid from a surface. The coatings include a nanostructured coating layer and in some embodiments, also include a hydrophobic layer deposited thereon. The coating materials eject droplets from the surface in the presence of non-condensing gases such as air and may be deployed under conditions of supersaturation of the condensed fluid to be ejected. A heat exchanger design utilizing the coating is described herein.

The invention relates to a method for obtaining a functionalised sensor tip for atomic force microscopy, which is characterised in that functionalisation takes place by means of an activated vapour silanisation process, comprising: a) evaporating an organometallic compound containing at least one silicon atom and at least one functional group selected from an amine group, a hydroxyl group, a carboxyl group and a thiol group; b) activating the vapour of the organometallic compound of step a) by heating; and c) causing the activated vapour of step b) to impinge on a sensor tip for atomic force microscopy in order to deposit a film of the organometallic compound on the sensor tip, steps b) and c) taking place consecutively. The invention also relates to the functionalised sensor tip obtained using the method.

In at least one example, a composition for surface activation of an aerospace vehicle consists essentially of an organic solvent present in an amount from about 95 to about 99.5 volume percent, a transition metal alkoxide present in an amount from about 0.5 to about 5 volume percent, and a water content in an amount from about 0 to about 5 volume percent. In at least one example, a method of sealing a surface of an aerospace vehicle includes applying the composition to a surface of an aerospace vehicle. The composition applied to the surface is dried to form a transition metal oxide from the transition metal alkoxide. Excess of the transition metal oxide is removed from the surface. A sealant is applied over a remaining layer of the transition metal oxide on the surface.

The invention relates to a method for obtaining a functionalised sensor tip for atomic force microscopy, which is characterised in that functionalisation takes place by means of an activated vapour silanisation process, comprising: a) evaporating an organometallic compound containing at least one silicon atom and at least one functional group selected from an amine group, a hydroxyl group, a carboxyl group and a thiol group; b) activating the vapour of the organometallic compound of step a) by heating; and c) causing the activated vapour of step b) to impinge on a sensor tip for atomic force microscopy in order to deposit a film of the organometallic compound on the sensor tip, steps b) and c) taking place consecutively. The invention also relates to the functionalised sensor tip obtained using the method.

A turbine article includes a substrate with a geometric surface having a multiple of divots recessed into the substrate, and a ceramic topcoat disposed over the geometric surface, the topcoat including at least a first layer having a first hardness and a second layer having a second hardness, the first hardness different than the second hardness.

Provided is a method for preparing a silica layer, comprising bringing to gelation a precursor layer formed from a precursor composition comprising a silica precursor an acid catalyst and a surfactant.

A turbine article includes a substrate with a geometric surface having a multiple of divots recessed into the substrate, and a ceramic topcoat disposed over the geometric surface, the topcoat including at least a first layer having a first hardness and a second layer having a second hardness, the first hardness different than the second hardness.

During an example coating method, a metallic substrate is provided. A foundation coat precursor is applied on the metallic substrate. The foundation coat precursor includes a matrix and a plurality of capsules present in the matrix. Each capsule includes a shell and a healing agent surrounded by the shell. A basecoat precursor is applied, and a clearcoat precursor is applied. The metallic substrate, the foundation coat precursor, the basecoat precursor, and the clearcoat precursor are heated i) after each respective application or ii) simultaneously, in order to cure the foundation coat, basecoat, and clearcoat precursors and respectively form a foundation coat, a basecoat, and a clearcoat. The foundation coat is ultraviolet (UV) stable and bonds the metallic substrate to the basecoat and the clearcoat.

An object having a high temperature resistance includes an inorganic substrate, an omniphobic non-stick coating, and an adhesion-promoting coating containing amorphic silicon dioxide and located between the inorganic substrate and the omniphobic non-stick coating.