Abstract: An abradable composite material comprising a matrix of sintered metallic particles and non-metallic solid lubricants disposed within the interstitial spaces of the matrix is described. The abradable composite material is capable of being used with, e.g., titanium-alloy blades of a gas turbine at least in part because the abradable composite material does not cause excessive wear or damage to the blades of the gas turbine. Methods of forming the abradable composite material are also described.

Abstract: The technology of the present application provides an apparatus for sealing and filtering. The apparatus includes a sealing component and a filtering component. The sealing component has an annular structure and a first connecting component. The annular structure includes a sidewall defining a recess. The first connecting component extends from the annular structure in a first direction. The filtering component has a filtering material and a second connecting component. The filtering material has a flat structure. The filter material is configured to filter fluid passing therein in a second direction. The sealing component and the filtering component are coupled by the first connecting component and the second connecting component.