Seal segment for a turbine, assembly for externally delimiting a flow path of a turbine, and stator/rotor seal
A seal segment for a turbine and an assembly for sealing the gaps between seal segments and stator vanes of a turbine. The seal segments have a plate-shaped wall, the first lateral surface of which faces the vane tips in the assembled state of the seal segments, is surrounded by a closed circumferential edge, and can be divided into four lateral wall sections, and the plate-shaped wall has a seal element which is arranged over the entire surface of the lateral surface. A number of seal lamellae which are secured on one side are provided on at least one of the lateral wall sections and/or on at least one of the seal lateral wall sections facing adjacent seal segments when the seal segments are assembled in a turbine so as to form a ring in order to reduce a flow along the corresponding lateral wall section.
1. A sealing segment for a turbine, for assembly with further sealing segments in the turbine, for sealing off a gap between the sealing segments and rotor blades of the turbine or to form a seal constituent part of a stator-rotor seal, the sealing segment comprising:
a plate-like wall which comprises a first side surface which, in an installed state of the sealing segment, faces blade tips of the rotor blades or the other seal constituent part, and an edge which surrounds the first side surface in a closed, peripheral manner and on which multiple side wall sections abut the first side surface, and
a sealing element which is arranged on the first side surface over a full surface area thereof and which, analogously to the plate-like wall, comprises sealing side wall sections, and
a number of sealing lamellae provided on at least one of the side wall sections, and/or on at least one of the sealing side wall sections, and for sealing segments assembled to form a ring in a turbine face adjacent sealing segments of the respective ring, wherein the number of sealing lamellae are adapted for reducing flow along the respective side wall section in an axial direction from upstream to downstream,
wherein the respective sealing lamellae project at an angle of less than 90° from the side wall sections or sealing side wall sections.
2. The sealing segment as claimed in claim 1 ,
wherein the respective sealing lamellae extend transversely with respect to the flow direction of a working medium flowing in the turbine, or to a leakage flow.
3. The sealing segment as claimed in claim 2 ,
wherein the respective sealing lamellae extend transversely with respect to the flow direction of a working medium flowing in the turbine, or to a leakage flow, and relative to their installation position in a turbine, in a circumferential direction and in a radial direction.
4. The sealing segment as claimed in claim 1 ,
wherein the sealing lamellae are curved toward their free end.
5. The sealing segment as claimed in claim 1 ,
wherein the sealing element is designed in the form of a honeycomb structure.
6. The sealing segment as claimed in claim 5 ,
wherein the sealing lamellae are parts of the honeycomb structure.
7. The sealing segment as claimed in claim 1 ,
wherein the sealing element is designed in the form of a strippable coating system having one or more layers.
8. The sealing segment as claimed in claim 1 ,
wherein at least the sealing lamellae are produced by an additive manufacturing method.
9. An arrangement for sealing off the gaps between sealing segments and rotor blades of a turbine, comprising:
a multiplicity of sealing segments as claimed in claim 1 arranged so as to form a segmented ring, such that the sealing lamellae of a first sealing segment bear against an opposite side wall section or sealing side wall section of a further sealing segment, which is directly adjacent to the first sealing segment, in a pre-stressed manner and a longitudinal flow through the abutting joint, which joint forms between the adjacently arranged first and second sealing segments, in an axial direction from upstream to downstream is able to be avoided to the greatest extent.
10. A stator-rotor seal, comprising:
a multiplicity of sealing segments as claimed in claim 1 arranged so as to form a segmented ring, such that the sealing lamellae of a first sealing segment bear against an opposite side wall section or sealing side wall section of a further sealing segment, which is directly adjacent to the first sealing segment, in a pre-stressed manner and a longitudinal flow through the abutting joint, which joint forms between the adjacently arranged first and second sealing segments, in an axial direction from upstream to downstream is able to be avoided to the greatest extent.