EP2479377A2 - Rotor de turbine à vapeur avec sections à température élevée et basse couplée mécaniquement utilisant différents matériaux - Google Patents
Rotor de turbine à vapeur avec sections à température élevée et basse couplée mécaniquement utilisant différents matériaux Download PDFInfo
- Publication number
- EP2479377A2 EP2479377A2 EP11195293A EP11195293A EP2479377A2 EP 2479377 A2 EP2479377 A2 EP 2479377A2 EP 11195293 A EP11195293 A EP 11195293A EP 11195293 A EP11195293 A EP 11195293A EP 2479377 A2 EP2479377 A2 EP 2479377A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- turbine rotor
- rotor
- section
- stage
- axial section
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Images
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/026—Shaft to shaft connections
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
- F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/502—Thermal properties
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/502—Thermal properties
- F05D2300/5021—Expansivity
- F05D2300/50212—Expansivity dissimilar
Definitions
- This invention relates to rotors for turbomachines and, more specifically, to the construction of rotors in axial sections of different materials.
- This invention resides in a turbine rotor comprising an elongated shaft including at least an HP region, the HP region having a first axial section supporting a stage 1 rotor wheel and a second axial section supporting a stage 2 rotor wheel, the first axial section formed of a relatively higher-temperature-capability material and the second axial section formed of a relatively lower-temperature-capability material; and means for mechanically coupling the first axial section and the second axial section.
- the elongated shaft may include at least HP and IP regions, a combined HP/IP region having the at least first section supporting the stage 1 rotor wheel and the second section supporting the stage 2 rotor wheel.
- a steam turbine rotor 10 is shown in schematic from and includes at least a high pressure (HP) region (or combined HP and intermediate pressure (IP) region) 12 that is formed to include at least first and second stage rotor wheels 14, 16, each of which supports a row of buckets 18, 20, respectively.
- HP high pressure
- IP intermediate pressure
- the rotor 10 is formed in two axially-oriented and aligned sections 22, 24.
- Section 22 includes the first stage rotor wheel 14 while section 24 includes the second stage rotor wheel 16. It will be appreciated that section 22 is in a high temperature region, exposed to steam at temperatures of about and above 1050°F.
- Section 24, on the other hand, is in a lower temperature region, exposed to steam at a temperature of about and less than 1050°F.
- the inventors have recognized that significant cost savings can be realized by using different materials for the rotor sections 22, 24 within the HP or combined HP/IP region 12.
- a more expensive 12% Cr material e.g., ASTM A982, Grade B
- a less expensive, lower % Cr material such as a Cr-MO-V material (e.g. ASTM A470, Grade D, Class 8) is suitable.
- the rotor sections 22 and 24 are preferably joined together by any of several suitable mechanical coupling arrangements.
- the rotor sections 22 and 24 are provided with (or formed with) facing radial flanges 26, 28, respectively, located between the first and second stage rotor wheels 14, 16 and joined by a circumferential array of axially-extending fasteners such as bolts 30 passing through the flanges and secured by nuts 32.
- Figure 2 illustrates an alternative coupling arrangement where the radial flange 28 is eliminated and flange 26 is bolted directly to a hub portion 15 of the rotor wheel 16 using similar fasteners 30, 32.
- Fig. 3 illustrates another mechanical coupling arrangement between the rotor sections 22, 24.
- a reduced diameter end portion 34 of the section 24 is received within a blind bore 36 formed in section 22 axially between the rotor wheels 14, 16.
- the coupled sections are secured by two or three fasteners (e.g. bolts) 38 oriented radially with respect to the longitudinal axis of the rotor.
- Fig. 4 illustrates another example embodiment wherein a partially-threaded stud 40 extends between the rotor sections 22, 24.
- a threaded, blind bore 42 is formed in the end of rotor section 24, aligned with a smooth through-bore 44 formed in rotor section 22.
- the stud 40 is inserted through the smooth through-bore 44 and the threaded end 46 of the stud is threaded into the blind bore 42.
- a threaded opposite end 48 of the stud 40 projects from the rotor section 22 and a nut 50 is applied there to lock the stud 40 in place, with sections 22, 24 joined together axially between the rotor wheels 14, 16.
- the smooth portion of the stud 40 could terminate short of the flange 51 and a separate bolt could be threaded into the end of the bore 44 to lock the stud in place.
- Fig. 5 illustrates yet another exemplary mechanical coupling utilizing a spline arrangement.
- a reduced-diameter male spline 52 is formed at one end of the rotor section 24.
- a female spline 54 is formed in the rotor section 22, with elongated slots (i.e., complimentary spline slots) 56 aligned to receive the elongated ribs 58 of the male spline 52.
- the coupling occurs between the rotor wheels 14, 16.
- Fig. 6 illustrates a variation of the spline coupling of Fig. 5 .
- the male spline 60 of the rotor section 24 is in a cross-shape, with four equally-spaced ribs 62.
- the female spline 64 in rotor section 22 is formed with four aligned slots 66 that receive the ribs 62.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/985,508 US20120177494A1 (en) | 2011-01-06 | 2011-01-06 | Steam turbine rotor with mechanically coupled high and low temperature sections using different materials |
Publications (1)
Publication Number | Publication Date |
---|---|
EP2479377A2 true EP2479377A2 (fr) | 2012-07-25 |
Family
ID=45442969
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP11195293A Withdrawn EP2479377A2 (fr) | 2011-01-06 | 2011-12-22 | Rotor de turbine à vapeur avec sections à température élevée et basse couplée mécaniquement utilisant différents matériaux |
Country Status (5)
Country | Link |
---|---|
US (1) | US20120177494A1 (fr) |
EP (1) | EP2479377A2 (fr) |
JP (1) | JP2012145104A (fr) |
CN (1) | CN102587996A (fr) |
RU (1) | RU2011154008A (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT201600069753A1 (it) * | 2016-07-05 | 2018-01-05 | Exergy Spa | Assieme di turbine e treno di turbine comprendente almeno uno di detti assiemi |
CN112678148A (zh) * | 2020-12-22 | 2021-04-20 | 大连理工大学 | 一种独立的拱形带支撑的高低温连接结构 |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103470309A (zh) * | 2013-08-21 | 2013-12-25 | 东方电气集团东方汽轮机有限公司 | 一种分段组合式转子 |
CN105317465B (zh) * | 2015-11-26 | 2017-04-12 | 北京全三维能源科技股份有限公司 | 汽轮机及其螺栓组合转子、组合转子的组装方法 |
CN105351011B (zh) * | 2015-11-26 | 2017-03-29 | 北京全三维能源科技股份有限公司 | 汽轮机及其销钉组合转子、组合转子的组装方法 |
CN107856056B (zh) * | 2017-12-18 | 2024-02-20 | 浙江钱江机器人有限公司 | 一种机器人的腕部件 |
US11674394B2 (en) * | 2021-02-11 | 2023-06-13 | Pratt & Whitney Canada Corp. | Gas turbine engine rotor assembly and method of using same |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH83747A (de) * | 1919-04-12 | 1920-06-01 | Der Maschinenfabriken Escher & | Umlaufender Teil für Mehrstufige, rasch laufende Maschinen, insbesondere Dampfturbinen |
JPS5924242B2 (ja) * | 1976-03-31 | 1984-06-08 | 株式会社東芝 | タ−ビンロ−タ−構体 |
JPS5944481B2 (ja) * | 1980-12-01 | 1984-10-30 | 株式会社日立製作所 | 蒸気タ−ビンロ−タ系 |
US4683714A (en) * | 1986-06-17 | 1987-08-04 | General Motors Corporation | Oil scavenge system |
US6352385B1 (en) * | 2000-07-31 | 2002-03-05 | General Electric Company | Mechanical coupling for cooperating rotatable members |
DE10160847A1 (de) * | 2001-12-12 | 2003-07-17 | Valeo Auto Electric Gmbh | Betätigungsvorrichtung, insbesondere zur Betätigung von Sperrdifferentialen von Fahrzeugen |
US6994519B2 (en) * | 2003-05-20 | 2006-02-07 | General Electric Company | Apparatus and methods for coupling axially aligned turbine rotors |
EP1577494A1 (fr) * | 2004-03-17 | 2005-09-21 | Siemens Aktiengesellschaft | Arbre soudé de turbine à vapeur et procédé de fabrication |
US7775779B2 (en) * | 2005-11-17 | 2010-08-17 | Sclumberger Technology Corporation | Pump apparatus, systems and methods |
JP2007291966A (ja) * | 2006-04-26 | 2007-11-08 | Toshiba Corp | 蒸気タービンおよびタービンロータ |
JP4805728B2 (ja) * | 2006-05-31 | 2011-11-02 | 株式会社東芝 | 蒸気タービンロータ及び蒸気タービン |
US8251643B2 (en) * | 2009-09-23 | 2012-08-28 | General Electric Company | Steam turbine having rotor with cavities |
US8465259B2 (en) * | 2010-04-29 | 2013-06-18 | Siemens Energy, Inc. | Gas turbine spindle bolt structure with reduced fretting motion |
-
2011
- 2011-01-06 US US12/985,508 patent/US20120177494A1/en not_active Abandoned
- 2011-12-22 EP EP11195293A patent/EP2479377A2/fr not_active Withdrawn
- 2011-12-28 JP JP2011287521A patent/JP2012145104A/ja active Pending
- 2011-12-29 RU RU2011154008/06A patent/RU2011154008A/ru not_active Application Discontinuation
-
2012
- 2012-01-06 CN CN2012100141301A patent/CN102587996A/zh active Pending
Non-Patent Citations (1)
Title |
---|
None |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT201600069753A1 (it) * | 2016-07-05 | 2018-01-05 | Exergy Spa | Assieme di turbine e treno di turbine comprendente almeno uno di detti assiemi |
WO2018007909A1 (fr) * | 2016-07-05 | 2018-01-11 | Exergy S.P.A. | Ensemble de turbines et train de turbine comprenant au moins un tel ensemble |
US11021960B2 (en) | 2016-07-05 | 2021-06-01 | Exergy International S.R.L. | Set of turbines and a turbine train comprising at least one such set |
CN112678148A (zh) * | 2020-12-22 | 2021-04-20 | 大连理工大学 | 一种独立的拱形带支撑的高低温连接结构 |
CN112678148B (zh) * | 2020-12-22 | 2022-05-20 | 大连理工大学 | 一种独立的拱形带支撑的高低温连接结构 |
Also Published As
Publication number | Publication date |
---|---|
RU2011154008A (ru) | 2013-07-10 |
US20120177494A1 (en) | 2012-07-12 |
JP2012145104A (ja) | 2012-08-02 |
CN102587996A (zh) | 2012-07-18 |
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