CN102587996A - Steam turbine rotor with mechanically coupled high and low temperature sections using different materials - Google Patents

Steam turbine rotor with mechanically coupled high and low temperature sections using different materials Download PDF

Info

Publication number
CN102587996A
CN102587996A CN2012100141301A CN201210014130A CN102587996A CN 102587996 A CN102587996 A CN 102587996A CN 2012100141301 A CN2012100141301 A CN 2012100141301A CN 201210014130 A CN201210014130 A CN 201210014130A CN 102587996 A CN102587996 A CN 102587996A
Authority
CN
China
Prior art keywords
section
turbine rotor
rotor according
grade
rotor
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.)
Pending
Application number
CN2012100141301A
Other languages
Chinese (zh)
Inventor
D·帕拉沙
S·库马
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of CN102587996A publication Critical patent/CN102587996A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/026Shaft to shaft connections
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/06Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • F01D5/066Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/50Intrinsic material properties or characteristics
    • F05D2300/502Thermal properties
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/50Intrinsic material properties or characteristics
    • F05D2300/502Thermal properties
    • F05D2300/5021Expansivity
    • F05D2300/50212Expansivity dissimilar

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

The Inverter relates to a steam turbine rotor with mechanically coupled high and low temperature sections using different materials. The turbine rotor including an elongated shaft having at least an HP region 12, the HP region having a first section supporting a stage 1 rotor wheel 14 and a second section supporting a stage 2 rotor wheel 16, the first section formed of a relatively higher-temperature-capability material and the second section formed of a relatively lower-temperature-capability material. Various mechanical couplings 26, 28, 30, 32 are described for securing the first and second sections.

Description

The steam turbine rotor of high and low temperature section with different materials of mechanical coupling
Technical field
The present invention relates to be used for the rotor of turbo machine, and relate more specifically to the formation of rotor in the axial section of different materials.
Background technique
In recent steam turbine rotor, and, used 12% chromium steel along with high temperature trend for steam, this owing to it at the excellent properties aspect hot strength and the toughness.In this kind rotor, for the two, used 12% identical chromium steel for the high-temperature part that is exposed to high-temperature steam and the low temperature part that is exposed to Low Temperature Steam.But because rotor has become bigger in recent years, thus utilize a kind of material make rotor with satisfy high-temperature part and low temperature partly the two characteristic also become increasingly difficult and costliness.
Though 12% expensive chromium steel satisfies the required heat resistance of the part that is exposed to high-temperature steam, creep properties etc., as long as keep necessary toughness just need not use this kind expensive material to be used for the low temperature part.In order to tackle these problems, attempted through welding the rotor portion of different materials linked together and processed single rotor.
Summary of the invention
Exemplary but in the non-restrictive example first; The present invention relates to a kind of turbine rotor; It comprises the axis of elongation that has the HP zone at least; This HP zone has first axial section and second axial section that supports the 2nd grade of rotor wheel of the 1st grade of rotor wheel of supporting, and first axial section is formed by the material of relative higher temperature performance and second axial section is formed by the material of relatively lower temp performance; And the device that is used for mechanically connecting first axial section and second axial section.
On the other hand; The present invention relates to comprise the turbine rotor of the axis of elongation; This axis of elongation comprises HP and IP zone at least; Combined type HP/IP zone has first section of the 1st grade of rotor wheel of supporting and second section of the 2nd grade of rotor wheel of supporting at least, and first section is formed by the material of relative higher temperature performance and second section is formed by the material of relatively lower temp performance; And wherein, (or joint coupling) links through mechanical coupling for said first section and second section.
The accompanying drawing that at present will combine hereinafter to identify is described the present invention.
Description of drawings
Fig. 1 is the schematic representation according to the turbine rotor area with mechanical coupling formula section of the first exemplary but non-limiting example;
Fig. 2 is similar to Fig. 1 but the schematic representation that between turbine, has alternative mechanical coupling according to exemplary but non-limiting example;
Fig. 3 is similar to Fig. 2 but the schematic representation that between turbine, has alternative mechanical coupling according to exemplary but non-limiting example;
Fig. 4 is similar to Fig. 3 but the schematic representation that between turbine, has alternative mechanical coupling according to exemplary but non-limiting example;
Fig. 5 is similar to Fig. 4 but the schematic representation that between turbine, has alternative mechanical coupling according to exemplary but non-limiting example; And
Fig. 6 is similar to Fig. 5 but the schematic representation that between turbine, has alternative mechanical coupling according to exemplary but non-limiting example.
List of parts
10 rotors
12 HP/IP zone
14 first order rotor wheel
15 hub portions
16 second level rotor wheel
18,20 wheel blades (bucket) in a row
22,24 rotor sections
26,28 radial flanges
30,32 fastening pieces
34 end sections
36 blind holes
38 fastening pieces
40 studs (stud)
42 blind holes
44 through holes
46 threaded end
48 opposite ends
50 nuts
51 flanges
52 public type splines (spline)
54 parent form splines
56 spline notches
58 elongation ribs
60 public type splines
62 ribs
64 parent form splines
66 aligned notches
Embodiment
At first referring to Fig. 1; Steam turbine rotor 10 illustrates with the sketch form and comprises (or combined type HP and middle pressure (IP) zone) 12, high pressure (HP) zone at least; This zone 12 forms and comprises first order rotor wheel 14 and second level rotor wheel 16 at least, and each person in them supports row's wheel blade 18,20 respectively.In HP or combined type HP/IP zone 12, rotor 10 is formed in the section 22,24 of two axial orientation and aligning.Section 22 comprises first order rotor wheel 14 and section 24 comprises second level rotor wheel 16.With what recognize be, section 22 is in the high-temperature area, and being exposed to temperature is about 1050 ° of F and higher steam.On the other hand, section 24 is in the lower temperature region, and being exposed to temperature is about 1050 ° of F and lower steam.
The inventor has recognized that, through in HP or combined type HP/IP zone 12, using material different can save cost significantly for rotor section 22,24.
For rotor section 22, comparatively expensive 12%Cr material (for example, ASTM A982, B level) is fit to, and for section 24, the Cr material of lower-cost low percentage (%) for example Cr-MO-V material (for example, ASTM A470, D level, 8 types) is fit to.
During rotor section 22 and 24 is preferably arranged through some suitable mechanical coupling any links together.In Fig. 1; For example; Rotor section 22 and 24 provide (or being formed with) sagittal plane to flange 26; 28, they be positioned at respectively between the first rotor wheel 14 and the second level rotor wheel 16 and through circumference array extend axially that bolt 30 that fastening piece for example passes flange links and fixing through nut 32.
Fig. 2 shows alternative linkage arrangement, wherein, has removed radial flange 28 and flange 26 and has used similar fasteners 30,32 directly to be bolted in the hub portion 15 of rotor wheel 16.
Another mechanical coupling that Fig. 3 shows between rotor section 22,24 is arranged.In this exemplary embodiment, the diameter of section 24 reduces end sections 34 and is accommodated in the blind hole 36, and this blind hole 36 is formed in the section 22 and is in vertically between the rotor wheel 14,16.The section that connects is through fixing about rotor longitudinal axis radially directed two or three fastening pieces (for example bolt) 38.
Fig. 4 shows another exemplary embodiment, and wherein the stud 40 of band portion screw thread extends between the rotor section 22,24.Particularly, threaded blind hole 42 is formed in the end of rotor section 24, aims at the level and smooth through hole 44 in being formed on rotor section 22.Stud 40 inserts and passes level and smooth through hole 44 and the threaded end 46 of stud is screwed in the blind hole 42.Stud 40 threaded opposite ends 48 give prominence to and nut 50 are applied in place with locking column bolt 40 on it from rotor section 22, and section 22,24 links together between rotor wheel 14,16 vertically.As alternative, the smooth of stud 40 possibly not reach flange 51 as yet and just stops, and that independent bolt can be screwed in the end in hole 44 is in place with the locking column bolt.
Fig. 5 shows the another exemplary mechanical coupling that adopts spline to arrange.Particularly, the public type spline 52 that reduces of diameter is formed on an end of rotor section 24.Parent form spline 54 is formed in the rotor section 22, has through aiming at the elongation notch (complementary splines notch also promptly) 56 with the elongation rib 58 of admitting public type spline 52.As in the aforementioned embodiment, connection occurs between the rotor wheel 14,16.
Fig. 6 shows the modification of the splined among Fig. 5.Here, the public type spline 60 of rotor section 24 is an X-shape, has the rib 62 that four equi-spaced apart are opened.Similarly be that the parent form spline 64 in the rotor section 22 is formed with four aligned notches 66 of taking in rib 62.
For the embodiment shown in Fig. 5 and Fig. 6, with what recognize be, spline arranges and can put upside down, wherein, public type spline is arranged in rotor section 22 and the parent form spline is on the rotor section 24.
Other mechanical coupling is arranged also within the scope of the invention.In all scenario, need prevent that all the safety of relative rotor section rotation from axially connecting.
Although the present invention has combined currently to think the most practical and preferred embodiment is described; But be understood that; The present invention is not limited to the disclosed embodiments, but opposite, the invention is intended to contain the spirit and interior various modification and the equivalent arrangements of scope that are included in accompanying claims.

Claims (15)

1. a turbine rotor (10) comprising:
At least the axis of elongation that comprises HP zone (12); Said HP zone has first axial section of the 1st grade of rotor wheel of supporting (14) and second axial section of the 2nd grade of rotor wheel of supporting (16), and said first axial section is formed by the material of relative higher temperature performance and said second axial section is formed by the material of relatively lower temp performance; And
Be used for mechanically connecting the device (26,28,30,32) of said first axial section and said second axial section.
2. turbine rotor according to claim 1 is characterized in that the material of said relative higher temperature performance comprises the 12%Cr material.
3. turbine rotor according to claim 1 is characterized in that the material of said relatively lower temp performance comprises the CrMoV material.
4. turbine rotor according to claim 2 is characterized in that the material of said relatively lower temp performance comprises the CrMoV material.
5. turbine rotor according to claim 1 is characterized in that, said first axial section and said second axial section are connected between said the 1st grade of rotor wheel (14) and said the 2nd grade of rotor wheel (16).
6. a turbine rotor (10) comprising:
At least the axis of elongation (10) that comprises HP and IP zone; Combined type HP zone (12) has first section of the 1st grade of rotor wheel of supporting (14) and second section of the 2nd grade of rotor wheel of supporting (16), and said first section is formed by the material of relative higher temperature performance and said second section is formed by the material of relatively lower temp performance; And
Wherein, said first section and said second section link through mechanical coupling (26,28,30,32).
7. turbine rotor according to claim 7 is characterized in that, said mechanical coupling comprises a plurality of bolts (30) that are positioned at the adjacent flanges (26,28) on said first section and said second section and pass said adjacent flanges.
8. turbine rotor according to claim 7; It is characterized in that; Said mechanical coupling comprises and is positioned at the flange (26) that engages with hub (15) said the 2nd grade of rotor wheel (16) on said first section, and a plurality of bolts (30) that pass said flange and said hub.
9. turbine rotor according to claim 7; It is characterized in that; Said mechanical coupling comprises that one diameter in said first section and said second section reduces end (34), and said diameter reduces end (34) and is accommodated in another the blind hole (36) in said first section and said second section.
10. turbine rotor according to claim 7; It is characterized in that; Said mechanical coupling comprises first hole (44) of passing said first section and is positioned at second blind hole (42) on said second section, and stud (40) extends between said first hole and said second blind hole.
11. turbine rotor according to claim 10 is characterized in that, said stud (40) is screwed in the said blind hole (42).
12. turbine rotor according to claim 6 is characterized in that, said mechanical coupling comprises public type spline (52), and said public type spline (52) is from said second section extension and be accommodated in the parent form spline (54) that is arranged in said first section.
13. turbine rotor according to claim 12 is characterized in that, said public type spline (60) is formed with four radially projecting teeths (62), around spaced apart roughly 90 ° of the spin axis of said turbine rotor.
14. turbine rotor according to claim 7 is characterized in that, the material of said relative higher temperature performance comprises the 12%Cr material.
15. turbine rotor according to claim 7 is characterized in that, the material of said relatively lower temp performance comprises CrMoV.
CN2012100141301A 2011-01-06 2012-01-06 Steam turbine rotor with mechanically coupled high and low temperature sections using different materials Pending CN102587996A (en)

Applications Claiming Priority (2)

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
US12/985508 2011-01-06

Publications (1)

Publication Number Publication Date
CN102587996A true CN102587996A (en) 2012-07-18

Family

ID=45442969

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2012100141301A Pending CN102587996A (en) 2011-01-06 2012-01-06 Steam turbine rotor with mechanically coupled high and low temperature sections using different materials

Country Status (5)

Country Link
US (1) US20120177494A1 (en)
EP (1) EP2479377A2 (en)
JP (1) JP2012145104A (en)
CN (1) CN102587996A (en)
RU (1) RU2011154008A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103470309A (en) * 2013-08-21 2013-12-25 东方电气集团东方汽轮机有限公司 Segmented combined type rotor
CN105351011A (en) * 2015-11-26 2016-02-24 北京全三维能源科技股份有限公司 Steam turbine, pin-assembled rotor of stream turbine, and assembly method of pin-assembled rotor
CN107856056A (en) * 2017-12-18 2018-03-30 浙江钱江机器人有限公司 A kind of wrist part of robot

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105317465B (en) * 2015-11-26 2017-04-12 北京全三维能源科技股份有限公司 Steam turbine and bolt combination rotor thereof and assembly method of combination rotor
IT201600069753A1 (en) * 2016-07-05 2018-01-05 Exergy Spa SET OF TURBINES AND TURBINE TRAIN INCLUDING AT LEAST ONE OF THESE ASSEMBLIES
CN112678148B (en) * 2020-12-22 2022-05-20 大连理工大学 Independent high-low temperature connecting structure with arch-shaped support
US11674394B2 (en) * 2021-02-11 2023-06-13 Pratt & Whitney Canada Corp. Gas turbine engine rotor assembly and method of using same

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1399816A (en) * 1919-04-12 1921-12-13 Spiess Paul Rotor for multistage high-speed engines
US4123199A (en) * 1976-03-31 1978-10-31 Tokyo Shibaura Electric Co., Ltd. Rotor-shaft assembly
JPS5793605A (en) * 1980-12-01 1982-06-10 Hitachi Ltd Steam turbine rotor assembly
US6352385B1 (en) * 2000-07-31 2002-03-05 General Electric Company Mechanical coupling for cooperating rotatable members
CN1573020A (en) * 2003-05-20 2005-02-02 通用电气公司 Apparatus and methods for coupling axially aligned turbine rotors
CN1954133A (en) * 2004-03-17 2007-04-25 西门子公司 Welded turbine shaft and method for producing said shaft
CN101063414A (en) * 2006-04-26 2007-10-31 株式会社东芝 Steam turbine and rotor
JP2007321630A (en) * 2006-05-31 2007-12-13 Toshiba Corp Steam turbine rotor and steam turbine
US20100272504A1 (en) * 2005-11-17 2010-10-28 Schlumberger Technology Corporation Pump apparatus, systems and methods

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4683714A (en) * 1986-06-17 1987-08-04 General Motors Corporation Oil scavenge system
DE10160847A1 (en) * 2001-12-12 2003-07-17 Valeo Auto Electric Gmbh Actuating device, in particular for actuating limited slip differentials of vehicles
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

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1399816A (en) * 1919-04-12 1921-12-13 Spiess Paul Rotor for multistage high-speed engines
US4123199A (en) * 1976-03-31 1978-10-31 Tokyo Shibaura Electric Co., Ltd. Rotor-shaft assembly
JPS5793605A (en) * 1980-12-01 1982-06-10 Hitachi Ltd Steam turbine rotor assembly
US6352385B1 (en) * 2000-07-31 2002-03-05 General Electric Company Mechanical coupling for cooperating rotatable members
CN1573020A (en) * 2003-05-20 2005-02-02 通用电气公司 Apparatus and methods for coupling axially aligned turbine rotors
CN1954133A (en) * 2004-03-17 2007-04-25 西门子公司 Welded turbine shaft and method for producing said shaft
US20100272504A1 (en) * 2005-11-17 2010-10-28 Schlumberger Technology Corporation Pump apparatus, systems and methods
CN101063414A (en) * 2006-04-26 2007-10-31 株式会社东芝 Steam turbine and rotor
JP2007321630A (en) * 2006-05-31 2007-12-13 Toshiba Corp Steam turbine rotor and steam turbine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103470309A (en) * 2013-08-21 2013-12-25 东方电气集团东方汽轮机有限公司 Segmented combined type rotor
CN105351011A (en) * 2015-11-26 2016-02-24 北京全三维能源科技股份有限公司 Steam turbine, pin-assembled rotor of stream turbine, and assembly method of pin-assembled rotor
CN105351011B (en) * 2015-11-26 2017-03-29 北京全三维能源科技股份有限公司 Steam turbine and its pin combined rotor, the assemble method of combined rotor
CN107856056A (en) * 2017-12-18 2018-03-30 浙江钱江机器人有限公司 A kind of wrist part of robot
CN107856056B (en) * 2017-12-18 2024-02-20 浙江钱江机器人有限公司 Wrist part of robot

Also Published As

Publication number Publication date
JP2012145104A (en) 2012-08-02
US20120177494A1 (en) 2012-07-12
EP2479377A2 (en) 2012-07-25
RU2011154008A (en) 2013-07-10

Similar Documents

Publication Publication Date Title
CN102587996A (en) Steam turbine rotor with mechanically coupled high and low temperature sections using different materials
CN103161523B (en) Bolt flange assembly, anterior bearing arrangement and gas-turbine unit
JP5968475B2 (en) Gas turbine with damping clamp
US9151178B2 (en) Bellcrank for a variable vane assembly
US8651820B2 (en) Dovetail connection for turbine rotating blade and rotor wheel
EP2601384B1 (en) Gas turbine engine comprising a tension stud
JP4064370B2 (en) Method and apparatus for assembling a gas turbine engine
US20160102556A1 (en) Shaft arrangement
US20120189373A1 (en) Rotor Disk for a Turbo Machine
CN104364472A (en) Threaded shank, connection assembly, gas turbine engine and method for assembling for improved fatigue life of threads
CN104619954A (en) Method for assembling and disassembling a rotor having a number of rotor components of an axial flow turbomachine and such a rotor
JP2009079592A (en) Bolt assembly for steam turbine engine and method of assembling the same
CN108843410A (en) Fan disk and jet engine for jet engine
US8926290B2 (en) Impeller tube assembly
US8622696B2 (en) Steam turbine rotor
KR20080018821A (en) Methods and apparatus for fabricating a rotor for a steam turbine
CN103510994B (en) System having blade segment with curved mounting geometry
US20210404341A1 (en) Stiffened torque tube for gas turbine engine
CN105003392A (en) Flange of a wind turbine
US8932020B2 (en) Low-pressure turbine
US20120020775A1 (en) Flow splitter assembly for steam turbomachine and method
US20160047313A1 (en) Bushing for joining turbomachine components
EP2938825B1 (en) Turbomachine with clamp coupling shaft and rotor hub together
JP2009216094A (en) Steam turbine rotor and method of assembling the same
US20130323074A1 (en) Friction welded turbine disk and shaft

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C05 Deemed withdrawal (patent law before 1993)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20120718