Sealing a turbomachine Axia

Sealing arrangement of an axial turbomachine for sealing zones in or adjacent at least two static component parts of the turbomachine, wherein the component parts are axially displaceable relative to the other, comprising a sealing element (100) and of at least two static component parts of the turbomachine, wherein the sealing element (100) is configured in a segmented manner in the peripheral direction of the turbomachine, characterized in that the sealing element (100) has a first radial zone ( 1) formed in spiral or hook, which acts stiffening, with a first stiffness and a second radial zone (5) having a second stiffness, the first stiffness greater than the second stiffness and the first radial portion being (1) as attachment component fixed sealing element in a static part of the turbomachine component.