Turbine rotor and steam turbine
원문보기
IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0956083
(2007-12-13)
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등록번호 |
US-8277173
(2012-10-02)
|
우선권정보 |
JP-2006-338937 (2006-12-15) |
발명자
/ 주소 |
- Yamashita, Katsuya
- Inukai, Takao
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출원인 / 주소 |
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대리인 / 주소 |
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인용정보 |
피인용 횟수 :
0 인용 특허 :
7 |
초록
▼
A turbine rotor 300 includes: a high-temperature turbine rotor constituent part 301 where high-temperature steam passes; low-temperature turbine rotor constituent parts 302 sandwiching and weld-connected to the high-temperature turbine rotor constituent part 301 and made of a material different from
A turbine rotor 300 includes: a high-temperature turbine rotor constituent part 301 where high-temperature steam passes; low-temperature turbine rotor constituent parts 302 sandwiching and weld-connected to the high-temperature turbine rotor constituent part 301 and made of a material different from a material of the high-temperature turbine rotor constituent part 301; and a cooling part cooling the high-temperature turbine rotor constituent part 301 by ejecting cooling steam 240 to a position, of the high-temperature turbine rotor constituent part 301, near a welded portion 120 between the high-temperature turbine rotor constituent part 301 and the low-temperature turbine rotor constituent part 302. A value equal to a distance divided by a diameter is equal to or more than 0.3, where the distance is a distance from the position, of the high-temperature turbine rotor constituent part 301, ejected the cooling steam 240 up to the welded portion 120, and the diameter is a turbine rotor diameter of the high-temperature turbine rotor constituent part 301.
대표청구항
▼
1. A turbine rotor penetratingly provided in a steam turbine to which high-temperature steam is introduced, the turbine rotor comprising: a high-temperature turbine rotor constituent part where the high-temperature steam passes;low-temperature turbine rotor constituent parts sandwiching and weld-con
1. A turbine rotor penetratingly provided in a steam turbine to which high-temperature steam is introduced, the turbine rotor comprising: a high-temperature turbine rotor constituent part where the high-temperature steam passes;low-temperature turbine rotor constituent parts sandwiching and weld-connected to said high-temperature turbine rotor constituent part and made of a material different from a material of said high-temperature turbine rotor constituent part; anda cooling part cooling said high-temperature turbine rotor constituent part by ejecting cooling steam to a position, the position being located on said high-temperature turbine rotor constituent part with a predetermined distance from a welded portion between said high-temperature turbine rotor constituent part and each of said low-temperature turbine rotor constituent parts, the predetermined distance being satisfied that the predetermined distance divided by a turbine rotor diameter of the high-temperature turbine rotor constituent part is equal to or more than 0.3,wherein said cooling part ejects the cooling steam toward a side surface or a root portion of as rotor wheel part in said high-temperature turbine rotor constituent part. 2. The turbine rotor as set forth in claim 1, wherein said cooling part includes a cooling steam pipe for ejecting the cooling steam to said high-temperature turbine rotor constituent part. 3. The turbine rotor as set forth in claim 1, wherein said cooling part ejects the cooling steam toward a side surface or a root portion of a second rotor wheel part, in said high-temperature turbine rotor constituent part, on one-stage upstream side of a first rotor wheel part implanted with a moving blade where the temperature of the steam becomes 550° C. or lower. 4. The turbine rotor as set forth in claim 1, wherein the welded portion is formed at a position substantially corresponding to a downstream end portion of a nozzle diaphragm inner ring positioned on an immediate upstream side of a moving blade on a stage where the temperature of the steam becomes 550° C. or lower, or a position substantially corresponding to a downstream end portion of a nozzle labyrinth provided in the nozzle diaphragm inner ring. 5. The turbine rotor as set forth in claim 1, wherein joint end surfaces of said high-temperature turbine rotor constituent part and said low-temperature turbine rotor constituent part have: circular recessed portions formed in center portions; and annular surfaces formed in peripheral edge portions, and joined to each other by welding, and a space portion is formed inside the turbine rotor. 6. The turbine rotor as set forth in claim 5, wherein a cooling steam inlet port for introducing part of the cooling steam into the space portion is formed in said high-temperature turbine rotor constituent part and a cooling steam discharge port for discharging the cooling steam introduced into the space portion is formed in said low-temperature turbine rotor constituent part. 7. A steam turbine to which high-temperature steam is introduced and which comprises: a casing; anda turbine rotor penetratingly provided in the casing, wherein said turbine rotor comprises: high-temperature turbine rotor constituent part where the high-temperature steam passes;low-temperature turbine rotor constituent parts sandwiching and weld-connected to said high-temperature turbine rotor constituent part and made of a material different from a material of said high-temperature turbine rotor constituent part; anda cooling part cooling said high-temperature turbine rotor constituent part by ejecting cooling steam to a position, the position being located on said high-temperature turbine rotor constituent part with a predetermined distance from a welded portion between said high-temperature turbine rotor constituent part and each of said low-temperature turbine rotor constituent parts, and the predetermined distance being satisfied that the predetermined distance divided by a turbine rotor diameter of the high-temperature turbine rotor constituent part is equal to or more than 0.3,wherein said cooling part ejects the cooling steam toward a side surface or a root portion of a rotor wheel part in said high-temperature turbine rotor constituent part. 8. The steam turbine as set forth in claim 7, wherein said cooling part includes a cooling steam pipe for ejecting the cooling steam to said high-temperature turbine rotor constituent part. 9. The steam turbine as set forth in claim 7, wherein said cooling part ejects the cooling steam toward a side surface or a root portion of a second rotor wheel part, in said high-temperature turbine rotor constituent part, on one-stage upstream side of a first rotor wheel part implanted with a moving blade where the temperature of the steam becomes 550° C. or lower. 10. The steam turbine as set forth in claim 7, wherein the welded portion is formed at a position substantially corresponding to a downstream end portion of a nozzle diaphragm inner ring positioned on an immediate upstream side of a moving blade on a stage where the temperature of the steam becomes 550° C. or lower, or a position substantially corresponding to a downstream end portion of a nozzle labyrinth provided in the nozzle diaphragm inner ring. 11. The steam turbine as set forth in claim 7, wherein joint end surfaces of said high-temperature turbine rotor constituent part and said low-temperature turbine rotor constituent part have; circular recessed portions formed in center portions; and annular surfaces formed in peripheral edge portions and joined to each other by welding, and a space portion is formed inside the turbine rotor. 12. The steam turbine as set forth in claim 1wherein a cooling steam inlet port for introducing part of the cooling steam into the space portion is formed in said high-temperature turbine rotor constituent part and a cooling steam discharge port for discharging the cooling steam introduced into the space portion is formed in said low-temperature turbine rotor constituent part. 13. The steam turbine as set forth in claim 9, further comprising an extension member provided on a nozzle diaphragm inner ring on an immediate downstream side of said second rotor wheel part, extending along said high-temperature turbine rotor constituent part up to a position near said second rotor wheel part, in an area which is between said second rotor wheel part and said nozzle diaphragm inner ring and in which said cooling steam pipe is inserted, and provided with a through hole for having the cooling steam pipe pass therethrough.
이 특허에 인용된 특허 (7)
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Schroder Mark Stewart ; Butkiewicz Jeffrey John, Apparatus and methods for cooling rotary components in a turbine.
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Kreis Erhard (Otelfingen CHX) Meylan Pierre (Neuenhof CHX), Process for the operation of a fluid flow engine.
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Hiegemann,Michael; Reigl,Martin, Rotor for a steam turbine.
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Hirokawa Kazuharu,JPX ; Chikami Rintaro,JPX, Seal device between fastening bolt and bolthole in gas turbine disc.
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Chikami Rintaro,JPX ; Sakata Kaoru,JPX ; Nakamura Takeshi,JPX, Seal structure between gas turbine discs.
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Konishi Tetsu,JPX ; Magoshi Ryotaro,JPX, Steam turbine different material welded rotor.
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Endres Wilhelm,CHX ; Schaub Fritz,CHX, Welded rotor of a turbo-engine.
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