Turbine stator assembly with a radial degree of freedom between a guide vane assembly and a sealing ring
US-12116897-B2 · Oct 15, 2024 · US
US9103223B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9103223-B2 |
| Application number | US-201214347457-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 25, 2012 |
| Priority date | Oct 26, 2011 |
| Publication date | Aug 11, 2015 |
| Grant date | Aug 11, 2015 |
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A shaft sealing device is provided in an annular space between a rotor and a stator surrounding an outer periphery of the rotor, and divides the annular space in the direction of an axis of the rotor into a high-pressure region and a low-pressure region. The shaft sealing device includes a seal body obtained by stacking a plurality of thin plate sealing pieces in a circumferential direction of the rotor; and a high-pressure side plate that extends from the stator toward the radial inner side so as to run along the high-pressure side of the seal body, and is segmented into a plurality of portions in the circumferential direction, and includes a rigidity imparting member configured to impart rigidity in the direction of the axis to a portion of the surface of the high-pressure side plate that faces the high-pressure region.
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The invention claimed is: 1. A shaft sealing device provided in an annular space between a rotor and a stator surrounding an outer periphery of the rotor to divide the annular space into a high-pressure region and a low-pressure region in a direction of an axis of the rotor, the shaft sealing device comprising: a seal body having a plurality of thin plate sealing pieces that extend from the stator toward a radial inner side of the rotor and are stacked in a circumferential direction of the rotor; a high-pressure side plate that extends from the stator toward a radial inner side so as to run along a high-pressure side of the seal body, and is segmented into a plurality of portions in the circumferential direction; and a rigidity imparting member configured to impart rigidity in the direction of the axis of the rotor to a portion of a surface of the high-pressure side plate that faces the high-pressure region, wherein the rigidity imparting member is a supporting plate portion comprising a first plate piece and a second plate piece, wherein the first plate piece is stacked on the surface of the high-pressure side plate that faces the high-pressure region, and extends from the stator toward the radial inner side, wherein a longitudinal length of the first plate piece is shorter than the high-pressure side plate, and wherein the second plate piece is stacked on the surface of the first plate piece that faces the high-pressure region, and extends from the stator toward the radial inner side, wherein a longitudinal length of the second plate piece is shorter than the first plate piece. 2. The shaft sealing device according to claim 1 , further comprising: a plurality of fins, which extend in the radial direction, is arranged at intervals in the circumferential direction, and is configured to suppress a fluid that flows in the circumferential direction, in an entire area of an inner wall surface facing the surface of the high-pressure side plate that faces the high-pressure region. 3. A shaft sealing device provided in an annular space between a rotor and a stator surrounding an outer periphery of the rotor to divide the annular space into a high-pressure region and a low-pressure region in a direction of an axis of the rotor, the shaft sealing device comprising: a seal body having a plurality of thin plate sealing pieces that extend from the stator toward a radial inner side of the rotor and are stacked in a circumferential direction of the rotor; a high-pressure side plate that extends from the stator toward the radial inner side so as to run along a high-pressure side of the seal body, and is segmented into a plurality of portions in the circumferential direction; and a rigidity imparting member configured to impart rigidity in the direction of the axis of the rotor to a portion of a surface of the high-pressure side plate that faces the high-pressure region, wherein the rigidity imparting member is a plurality of ribs formed integrally with the surface of the high-pressure side plate that faces the high-pressure region, and wherein the plurality of ribs is arranged at intervals in the circumferential direction. 4. The shaft sealing device according to claim 3 , wherein the thin plate sealing pieces extend toward a forward side in a rotational direction of the rotor as the thin plate sealing pieces extend toward the radial inner side, and wherein the ribs extend toward the forward side in the rotational direction as the ribs extend toward the radial inner side. 5. A shaft sealing device provided in an annular space between a rotor and a stator surrounding an outer periphery of the rotor to divide the annular space into a high-pressure region and a low-pressure region in a direction of an axis of the rotor, the shaft sealing device comprising: a seal body having a plurality of thin plate sealing pieces that extend from the stator toward a radial inner side of the rotor and are stacked in a circumferential direction of the rotor; a high-pressure side plate that extends from the stator toward the radial inner side so as to run along a high-pressure side of the seal body, and is segmented into a plurality of portions in the circumferential direction; and a rigidity imparting member configured to impart rigidity in the direction of the axis of the rotor to a portion of a surface of the high-pressure side plate that faces the high-pressure region, wherein the rigidity imparting member is an elastic member that presses a portion of the high-pressure side plate from the high-pressure region side toward the low-pressure region side, and wherein in an entire area of an inner wall surface facing the surface of the high-pressure side plate that faces the high-pressure region, a plurality of fins, which extend in the radial direction, is arranged at intervals in the circumferential direction, and is configured to suppress a fluid that flows in the circumferential direction. 6. A rotating machine comprising: the shaft sealing device according to claim 1 .
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