Abstract: An overlap holder for a segmented liner of a turbomachine exhaust diffuser includes stacked plates and fasteners. A main plate includes a first face, an opposite second face, a first end, and an opposite second end. A spacer, which includes respective first and second faces, engages the first face of the main plate. A top plate includes a respective first face that engages the second face of the main plate and a respective second face opposite the first face of the top plate. A fastener is disposed at each of the first end and the second end of the main plate. Each fastener extends through holes in the spacer, the main plate, and the top plate to hold the spacer, the main plate, and the top plate in mutual engagement to secure a first segment of the segmented liner to an adjacent second segment of the segmented liner.

Abstract: A device for fastening a moving blade (3) to a rotor (2) of a thermal turbomachine is described. The moving blade (3) has a blade root (36), a blade leaf (32) and a platform (31) arranged between the blade root (36) and the blade leaf (32) and having at least two side flanks (33, 34). The idea, on which the invention is based, of avoiding axial forces occurring on the rotor (2) on account of bearing faces set obliquely to the rotor axis (4) between two adjacent moving blades (3) is that adjacent moving blades (3) meet solely at axially oriented bearing faces (52).