Turbine
A turbine includes blades and a structure rotating relative to the blades and having a fluid flowing thereto. The turbine includes step portions that are provided in either radial tip portions of the blades or areas of the structure that face the radial tip portions; sealing fins that extend from the other of the radial tip portions of the blades or areas of the structure that face the radial tip portions toward the step portions, and form minute gaps between the sealing fins and the step portions; a flow collision surface that is provided upstream of the sealing fins in a flow direction of the fluid and against which the fluid collides; a protrusion that protrudes toward an upstream side from the flow collision surface; and a facing surface that faces the flow collision surface.
1. A turbine including a blade and a structure on a radial tip end side of the blade via a gap and rotatable relative to the blade, the turbine being configured such that a fluid flows to the gap, and the turbine comprising:
a step portion that is in either a radial tip portion of the blade or an area of the structure that faces the radial tip portion, and has a plurality of steps in a radial direction;
a plurality of sealing fins that extends from the other of the radial tip portion of the blade and the area of the structure that faces the radial tip portion, toward the step portion, and defines a minute gap between each of the plurality of sealing fins and the step portion;
a flow collision surface that is on the blade and upstream of the plurality of sealing fins in a flow direction of the fluid and against which the fluid is to collide during use of the turbine;
a protrusion that protrudes axially away from a portion of the flow collision surface which is located closest to the structure in the radial direction; and
a facing surface that faces the flow collision surface,
wherein:
each of the plurality of steps of the step portion has an axial wall surface extending along an axial direction, and a radial wall surface which is connected to the axial wall surface via a corner portion and extends along the radial direction,
the plurality of sealing fins is arranged at intervals in the axial direction such that each of the plurality of sealing fins faces a corresponding one of the plurality of steps of the step portion,
each of the plurality of sealing fins is fixed at a position downstream of the radial wall surface of the corresponding one of the plurality of steps of the step portion,
the protrusion is configured to divide a cavity into a first space which is closer to the structure and a second space which is closer to a body of the blade, the cavity being defined by one of the plurality of sealing fins which is furthest upstream, the flow collision surface, the structure, and the facing surface, and
the protrusion protrudes further axially away from the flow collision surface than the radial wall surface of one of the plurality of steps which is furthest upstream.
2. The turbine according to claim 1 ,
wherein a free-cutting material having greater machinability than each of the plurality of sealing fins is on a surface of each of the plurality of steps of the step portion.
3. The turbine according to claim 1 ,
wherein the step portion is at the structure, and the plurality of sealing fins is at the blade.
4. The turbine according to claim 1 ,
wherein the structure is a casing that holds a shaft body that is rotationally driven, and
wherein the blade is a rotor blade that is fixed to the shaft body and extends to a casing side.
5. The turbine according to claim 1 ,
wherein the structure is a shaft body that is rotationally driven, and
wherein the blade is a stator blade that is fixed to a casing holding the shaft body and extends to a shaft body side.
6. The turbine according to claim 1 ,
wherein the plurality of sealing fins is arranged such that respective lengths of each of the plurality of sealing fins become shorter in order from in the flow direction of the fluid.
7. The turbine according to claim 1 ,
wherein the radial tip portion of the blade has a substantially rectangular cross section.