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
US9404375B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9404375-B2 |
| Application number | US-201113518559-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 28, 2011 |
| Priority date | Mar 10, 2010 |
| Publication date | Aug 2, 2016 |
| Grant date | Aug 2, 2016 |
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A shaft seal device includes a seal piece-laminated body with a plurality of thin seal pieces laminated in a circumferential direction along a rotating shaft. Outer ends of the plurality of thin seal pieces in the radial direction are connected to each other. Inner ends of the thin seal pieces in the radial direction are formed as free ends. A small gap is formed between each adjacent pair of the thin seal pieces. A small gap is formed between the rotating shaft and the seal piece-laminated body. A wear-resistant treatment layer is formed on a surface of a portion of each of the thin seal pieces close to the inner end.
Opening claim text (preview).
The invention claimed is: 1. A shaft seal device comprising a seal piece-laminated body including a high-pressure side seal plate, a low-pressure side seal plate, and a plurality of thin seal pieces, wherein the plurality of thin seal pieces are laminated in a circumferential direction to be positioned along a periphery of a rotating shaft, outer ends of the plurality of thin seal pieces in a radial direction are connected to each other, inner ends of the plurality of thin seal pieces in the radial direction are formed as free ends, a small gap is formed between each adjacent pair of the plurality of thin seal pieces, and a small gap is formed between the rotating shaft and the seal piece-laminated body, wherein a wear-resistant treatment layer is formed on a surface of a portion of each of the thin seal pieces close to the inner end and a surface of another portion of each of the thin seal pieces is free of the wear-resistant treatment layer, wherein first side end portions of the thin seal pieces, which correspond to a width direction of the thin seal pieces and are close to the inner ends, form a first small side surface corresponding to a fluid high-pressure side in an axial direction, and second side end portions of the thin seal pieces, which correspond to the width direction of the thin seal pieces and are close to the inner ends, form a second small side surface corresponding to a low-pressure side in the axial direction, wherein the high-pressure side seal plate covers a portion of an outer side of the first small side surface in the radial direction and leaves an inner portion of the first small side surface in the radial direction exposed, wherein the low-pressure side seal plate covers a portion of an outer side of the second small side surface in the radial direction and leaves an inner portion of the second small side surface in the radial direction exposed, the inner portion of the second small side surface that is exposed being larger than the inner portion of the first small side surface that is exposed, wherein the wear-resistant treatment layer is formed on the surface of the portion of each of the thin seal pieces from the inner end up to a position that overlaps the high-pressure side seal plate and is free from overlap with the low-pressure side seal plate when viewed in the axial direction, and wherein the wear-resistant treatment layer is a plating treatment layer which has a thickness. 2. The shaft seal device according to claim 1 , wherein the wear-resistant treatment layer is formed so as to be included in a range exposed from the low-pressure side seal plate when seen in the axial direction. 3. A rotary machine that includes the shaft seal devices according to claim 1 around the rotating shaft. 4. A rotary machine that includes the shaft seal devices according to claim 2 around the rotating shaft.
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