WO2013143894A1 - Refroidisseur à hélice pour turbomachine - Google Patents
Refroidisseur à hélice pour turbomachine Download PDFInfo
- Publication number
- WO2013143894A1 WO2013143894A1 PCT/EP2013/055506 EP2013055506W WO2013143894A1 WO 2013143894 A1 WO2013143894 A1 WO 2013143894A1 EP 2013055506 W EP2013055506 W EP 2013055506W WO 2013143894 A1 WO2013143894 A1 WO 2013143894A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- housing
- cooling channel
- cooling
- screw
- channel
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/14—Casings modified therefor
- F01D25/145—Thermally insulated casings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/243—Flange connections; Bolting arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/31—Application in turbines in steam turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/31—Retaining bolts or nuts
Definitions
- the invention relates to a turbomachine comprising a housing comprising an upper housing part, a lower housing part and a flow channel arranged in the housing, wherein the Strö ⁇ flow channel has a Strömungskanalabdampf syndromem, wherein the housing part via screws ver ⁇ bindable to the lower housing part, wherein the screw is designed as a stud and a cooling channel formed along the axial direction of the stud, the cooling passage having a cooling passage inlet and a cooling passage outlet.
- steam turbines In steam power plants, steam turbines are used, which apply an electrical output of up to 1,600 megawatts Kings ⁇ nen. For thermodynamic reasons, a steam turbine is divided into so-called sub-turbines, which have a common shaft.
- the high-pressure turbine part comprises a réellege ⁇ housing, which consists of an upper part and a lower part and is held together by means of screw connections. Due to the high temperatures and the temporal behavior of the temperature change, time- and temperature-dependent relaxations occur. As a result, it is possible that the tension of the housing and thus the tightness during operation diminishes, which can lead to leakage and is accompanied by a loss of efficiency.
- a turbomachine umfas ⁇ send a housing of an upper housing part, a housing ⁇ lower part and, disposed in the housing flow channel, said flow channel having a Strömungskanalabdampf syndromem, wherein the upper housing part by means of screws with the Ge ⁇ koruseunterteil is connectable, said screw is designed as a pin ⁇ screw and has a trained along the axial direction of the stud screw cooling channel where ⁇ at the cooling channel has a cooling duct inlet and adekanal- outlet, wherein the cooling duct inlet is Strömungstech ⁇ nisch connected to the flow channel, thedekanalauslass aerodynamically is connected to the Strömungskanalab ⁇ steam room.
- the invention proposes to use a known cooling hole in the stud bolts used for the screw, which is supplied on the one hand with a vapor located in the flow channel and on the other hand ⁇ connected via adekanalauslass with the Strömungskanalab ⁇ steam room.
- the steam from the flow channel has a higher pressure than the steam in Strömungskanalabdampfhoffm so that a forced flow through the cooling channel in the stud has resulted, resulting in a kuh ⁇ ment of the screw as a whole.
- the stud bolt comprises a nut, wherein the nut comprises cooling channel slots, which fluidly connects the cooling passage with the flow channel evaporation chamber.
- the lower housing part has a bore which connects the cooling channel inlet with the Strö mungskanal.
- This bore can be performed in an axial direction of the upper and lower housing upper part. It is important that at a suitable location, the bore has a flow ⁇ technical connection that provides the appropriate steam for the cooling steam.
- FIG. 2 upper housing part FIG. 3 lower housing part
- FIG. 4 shows a plan view of a nut according to the invention
- Figure 5 is a schematic side view of the housing upper ⁇ part and the lower housing part.
- FIG. 1 shows a schematic view of a partial view ei Nes housing upper part 1 and a lower housing part 2.
- the Ge housing upper part 1 and the lower housing part 2 together a housing which is used in a turbomachine, not shown.
- a flow channel is angeord ⁇ net (not shown).
- blades and vanes are arranged, which convert the thermal energy Ener ⁇ a vapor into rotational energy of a rotor.
- the upper housing part 1 and the lower housing part 2 are connected to one another via screws 3.
- the screw 3 is designed as a stud, which means that the screw has by no 3 nen screw head, but a Ge ⁇ threaded at both ends.
- a cooling channel 4 is formed, which is connected to a cooling channel inlet 5 and a cooling channel outlet 6 on the one hand.
- a steam flowing in the cooling channel inlet 5 will flow through the cooling channel 4 in the axial direction through the stud bolt and thereby cool the stud.
- the cooling steam enters the cooling channel outlet 6.
- a slot 8 is arranged in the nut 7, through which the steam can flow into the cooling channel outlet 6.
- Thedekanalauslass 6 is fluidly connected via a first fluid ⁇ technical connection 9 with the Strömungskanalabdampf syndromem (not shown in detail).
- Thedekanalauslass 6 is fluidically connected via a between the stud and the housing, in particular hous ⁇ seoberteil 1 arranged screw cooling channel 14 with the flow channel evacuation chamber.
- the channel inlet is connected to the flow channel via a second fluidic connection 10, expediently a fluidic connection after a blade stage is realized, in which the steam parameters are ideal for adeka ⁇ nalnikank.
- FIG. 3 shows the housing lower part 2 with the second fluidic connection 10 and the cooling channel inlet 5.
- FIG. 4 shows the nut 7 of the screw 3.
- the nut 7 has at least one slot 8 in the region of the thread 11, through which the cooling steam can flow.
- FIG. 5 shows a side view in the axial direction 12 of the turbomachine. The arrangement of the flow channel 13 as well as the cooling channel inlet 5 and the cooling channel outlet 6 and the first fluidic connection 9 and the second fluidic connection 10 can be seen in FIG.
Abstract
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/386,795 US20150050132A1 (en) | 2012-03-27 | 2013-03-18 | Screw cooling for a fluid flow machine |
EP13713767.5A EP2802748B1 (fr) | 2012-03-27 | 2013-03-18 | Turbomachine avec refroidissement de vis |
IN7089DEN2014 IN2014DN07089A (fr) | 2012-03-27 | 2013-03-18 | |
JP2015502200A JP5883986B2 (ja) | 2012-03-27 | 2013-03-18 | 流体機械のためのスクリュー冷却 |
CN201380017521.1A CN104395562B (zh) | 2012-03-27 | 2013-03-18 | 用于流体机械的螺丝冷却装置 |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP12161469.7A EP2644843A1 (fr) | 2012-03-27 | 2012-03-27 | Refroidissement à vis pour une turbomachine |
EP12161469.7 | 2012-03-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2013143894A1 true WO2013143894A1 (fr) | 2013-10-03 |
Family
ID=48045422
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2013/055506 WO2013143894A1 (fr) | 2012-03-27 | 2013-03-18 | Refroidisseur à hélice pour turbomachine |
Country Status (6)
Country | Link |
---|---|
US (1) | US20150050132A1 (fr) |
EP (2) | EP2644843A1 (fr) |
JP (1) | JP5883986B2 (fr) |
CN (1) | CN104395562B (fr) |
IN (1) | IN2014DN07089A (fr) |
WO (1) | WO2013143894A1 (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105507963A (zh) * | 2015-12-23 | 2016-04-20 | 上海电气电站设备有限公司 | 用于冷却在高温下工作的螺栓的冷却系统 |
RU2641782C2 (ru) * | 2016-05-30 | 2018-01-22 | Общество с ограниченной ответственностью "Газпром трансгаз Казань" | Способ охлаждения высокотемпературных шпилек паровых турбин и устройство для его осуществления |
RU2641787C2 (ru) * | 2016-05-30 | 2018-01-22 | Общество с ограниченной ответственностью "Газпром трансгаз Казань" | Способ охлаждения высокотемпературных шпилек газовых турбин и устройство для его осуществления |
RU173973U1 (ru) * | 2016-05-30 | 2017-09-22 | Общество с ограниченной ответственностью "Газпром трансгаз Казань" | Устройство охлаждения высокотемпературных шпилек паровых и газовых турбин |
EP3591176A1 (fr) * | 2018-07-05 | 2020-01-08 | Siemens Aktiengesellschaft | Raccord à bride refroidi pour une turbomachine |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH306453A (de) * | 1952-12-12 | 1955-04-15 | Bbc Brown Boveri & Cie | Flanschverbindungsschraube für Gehäuse von Dampfturbinen, Gasturbinen und dergleichen. |
DE19850470A1 (de) * | 1998-11-02 | 2000-02-03 | Siemens Ag | Turbinengehäuse einer Dampfturbine |
WO2003078799A1 (fr) * | 2002-03-20 | 2003-09-25 | Alstom (Switzerland) Ltd | Vis de liaison de brides pour turbines |
US20100003071A1 (en) * | 2008-03-26 | 2010-01-07 | Siemens Power Generation, Inc. | Fastener Assembly with Cyclone Cooling |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS54142704U (fr) * | 1978-03-29 | 1979-10-03 | ||
JPS54132008A (en) * | 1978-04-05 | 1979-10-13 | Hitachi Ltd | Turbine casing |
JPS57119109A (en) * | 1981-01-14 | 1982-07-24 | Hitachi Ltd | Cleaning device for steam turbine wheel chamber horizontal flange clamping bolt |
JPS59131906U (ja) * | 1983-02-25 | 1984-09-04 | 株式会社東芝 | タ−ビン車室締付ボルト冷却装置 |
US4820097A (en) * | 1988-03-18 | 1989-04-11 | United Technologies Corporation | Fastener with airflow opening |
JP4015284B2 (ja) * | 1998-06-09 | 2007-11-28 | 三菱重工業株式会社 | 蒸気タービンケーシングのフランジ冷却構造 |
JP2006037855A (ja) * | 2004-07-28 | 2006-02-09 | Mitsubishi Heavy Ind Ltd | 車室ケーシング及びガスタービン |
EP2187004A1 (fr) * | 2008-11-13 | 2010-05-19 | Siemens Aktiengesellschaft | Boîtier intérieur pour une turbomachine |
-
2012
- 2012-03-27 EP EP12161469.7A patent/EP2644843A1/fr not_active Withdrawn
-
2013
- 2013-03-18 JP JP2015502200A patent/JP5883986B2/ja not_active Expired - Fee Related
- 2013-03-18 WO PCT/EP2013/055506 patent/WO2013143894A1/fr active Application Filing
- 2013-03-18 EP EP13713767.5A patent/EP2802748B1/fr not_active Not-in-force
- 2013-03-18 IN IN7089DEN2014 patent/IN2014DN07089A/en unknown
- 2013-03-18 CN CN201380017521.1A patent/CN104395562B/zh not_active Expired - Fee Related
- 2013-03-18 US US14/386,795 patent/US20150050132A1/en not_active Abandoned
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH306453A (de) * | 1952-12-12 | 1955-04-15 | Bbc Brown Boveri & Cie | Flanschverbindungsschraube für Gehäuse von Dampfturbinen, Gasturbinen und dergleichen. |
DE19850470A1 (de) * | 1998-11-02 | 2000-02-03 | Siemens Ag | Turbinengehäuse einer Dampfturbine |
WO2003078799A1 (fr) * | 2002-03-20 | 2003-09-25 | Alstom (Switzerland) Ltd | Vis de liaison de brides pour turbines |
US20100003071A1 (en) * | 2008-03-26 | 2010-01-07 | Siemens Power Generation, Inc. | Fastener Assembly with Cyclone Cooling |
Also Published As
Publication number | Publication date |
---|---|
CN104395562A (zh) | 2015-03-04 |
JP2015511683A (ja) | 2015-04-20 |
IN2014DN07089A (fr) | 2015-04-24 |
CN104395562B (zh) | 2016-05-25 |
EP2802748A1 (fr) | 2014-11-19 |
EP2644843A1 (fr) | 2013-10-02 |
JP5883986B2 (ja) | 2016-03-15 |
EP2802748B1 (fr) | 2016-02-17 |
US20150050132A1 (en) | 2015-02-19 |
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