Abstract: The invention relates to a blade component, a compressor or turbine stage of a gas turbine, in particular a gas turbine engine characterized in that the blade component includes at least two structural elements which can be connected together by means of a connection method, in particular sintering, and that the at least one connection face of the at least two structural elements lies on a face, wherein in particular the normal vector has, for at least a part of the face, a component perpendicular to the radial orientation of the blade component. The invention also concerns a method for manufacturing a blade component, and a gas turbine with a blade component.

Abstract: A method for producing a hybrid component including providing a first component constituent made of a metallic first material, a second component constituent in the form of a sleeve made of an electrically insulating second material, and a third component constituent made of a metallic third material and having a recess; forming a complete component assembly by arranging the first component constituent in an inner volume of the second component constituent and arranging the second component constituent in the recess of the third component constituent; and sintering the complete component assembly by heating to a sintering temperature.

Abstract: The invention relates to a production method for an electrical resistance element (for example a shunt) with the following steps: —providing a resistance alloy in powder form, and—forming the resistance element from the powdered resistance material. The invention also relates to a correspondingly produced resistance element.

Abstract: The invention relates to a production method for an electrical resistance element (for example a shunt) with the following steps: -providing a resistance alloy in powder form, and -forming the resistance element from the powdered resistance material. The invention also relates to a correspondingly produced resistance element.