US3630635A - Turbine casing with raised horizontal joint - Google Patents
Turbine casing with raised horizontal joint Download PDFInfo
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- US3630635A US3630635A US71158A US3630635DA US3630635A US 3630635 A US3630635 A US 3630635A US 71158 A US71158 A US 71158A US 3630635D A US3630635D A US 3630635DA US 3630635 A US3630635 A US 3630635A
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- Prior art keywords
- inner casing
- horizontal
- casing
- centerline
- joint
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- Expired - Lifetime
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- 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
- F01D25/26—Double casings; Measures against temperature strain in casings
Definitions
- the inner casing of a low-pressure steam turbine has top and bottom sections which are connected along a horizontal joint disposed substantially higher than the horizontal centerline of the machine.
- the connectors at the joint can thus be located outside the inner casing because of the smaller sealing surface area at the raised joint.
- This invention relates to elastic fluid turbines and particularly to an improvement in the inner casing construction of a low-pressure steam turbine.
- the low-pressure units of large steam turbines are often arranged so that the lowest pressure turbine sections are disposed in an inner casing which is located in an outer casing or exhaust hood leading to the condenser.
- the space between the inner and outer casings is at a vacuum corresponding roughly to exhaust or condenser pressure, while the steam pressure inside the inner casing varies as it is expanded from one stage of buckets and nozzle diaphragms to the next.
- Low-pressure turbines are also generally constructed to provide for extraction of steam at various points along the low-pressure turbine sections in order to supply various feedwater heaters.
- passages within the inner casing must. be provided to lead the extracted steam from selected turbine stages and to remove it through pipes leading from the outer casing or exhaust hood.
- These extraction passages are generally formed between longitudinally spaced radial walls and the wrapper walls of the inner casing.
- the inner casing must be split into two or more sections to allow for removal of the stationary nozzle diaphragms separating the turbine stages, and also for removal of the rotor itself.
- the inner casing upper and lower sections have been divided along a horizontal joint which is located roughly at the horizontal centerline of the machine, and the upper and lower halves of the nozzle diaphragms have also been supported substantially at the horizontal centerline. Because of the fact that the space between the outer casing and inner casing is at a vacuum, a tight seal must be maintained at this horizontal joint between the upper and lower inner casing halves.
- one object of the present invention is to provide an improved inner casing construction for a low-pressure steam turbine, wherein the connecting means for sealing the upper and lower inner casing halves may all be disposed on the outside of the inner casing.
- Another object of the invention is to provide an improved inner casing construction for a low-pressure steam turbine, wherein the connecting means for joining the casing halves is arranged to minimize obstructions in the steam flow paths.
- the invention is practiced by locating the horizontal joint of the inner casing substantially above the turbine horizontal centerline and at a location of smaller sealing area around the extraction passages, and locating the connecting members on the outside of the inner casing.
- FIG. la is a transverse cross section through one-half of a low-pressure steam turbine illustrating the prior art
- FIG. lb is a similar cross section through the other half and illustrating the present invention.
- FIG. 2 is a horizontal cross section taken along lines Il-lI of FIG. la illustrating the prior art
- FIG. 3 is a horizontal cross section taken along lines IllIlI of FIG. lb, illustrating the invention.
- an outer casing l which in this case is the exhaust hood, is arranged in upper and lower halves connected at a horizontal joint 2 and supported on a foundation 3. At its lower end, the outer casing l communicates with the condenser (not shown). Disposed inside the outer casing is an inner casing 4 comprising an upper section 40 and a lower section 4b. Sections 40 and 4b are connected along a horizontal joint 5 disposed substantially along the horizontal centerline 6 of the turbine rotor (not shown). Joint 5 is sealed by external connecting bolts 7 and internal connecting bolts 8. Access to internal bolts 8 is provided by a removable cover 9.
- Extraction passages 16 are formed inside the inner casing 4 by an outer wrapper wall 17 and a number of spaced dial dividing walls 18. The wrapper and radial walls are arranged so that the cross-sectional flow area of extraction passages 16 increase gradually from the top of the inner casing around the unit until they finally empty into an extraction steam removal pipe 19 toward the lower part of the inner casing.
- FIG. 2 of the drawing which also illustrates the prior art, shows a horizontal cross section of a portion of the turbine, looking downward just above the horizontal joint.
- the configuration of the wall sections of the inner casing 4 is rather complex in order to provide the various extraction passages such as 16, as well as to accommodate the varying sizes of the outer diaphragm rings such as I2, 12a and 12b along the steam flow path.
- additional radial wall portions 18a, 18b are longitudinally spaced along the unit, these being joined to additional circumferential well portions 17a, 17b which in turn cooperate with the outer diaphragm rings. These members together seal off regions of fluid pressure leading into extraction conduit 16.
- FIGS. lb and 3 relate to the improved construction of the present invention.
- the outer casing l is arranged as before, as are the members 10, I1 and 12 making up the diaphragm.
- the improvement of the present invention relates to the inner casing shown as 21, constructed with a top section 21a and a bottom section 21b.
- a wrapper wall 22 and a group of radial wall portions 23, together with the diaphragm outer rings 12 define, as before, extraction passages 24. Passages 24 gradually increase in cross-sectional area from the top toward the lower part of casing 21 and are led from the casing through extraction pipes 25.
- the upper and lower casing sections are connected at a horizontaljoint 26.
- Joint 26 is disposed substantially higher than the centerline 6 of the unit, perhaps on the order of 2 feet in a large lowpressure turbine. Since the radius of the inner casing will vary from 4 feet to 8 feet or more, the joint is thus raised on the order of onequarter to one-half of the inner casing radius.
- Mounting pads 27 arranged on selected radial walls 23 support the diaphragm lugs 13 substantially at the horizontal centerline as before, and removable square-headed pins 28 hold the lugs 13 in position.
- Means for connecting the upper and lower sections at horizontal joint 26 include bolts 28. These bolts are all located and accessible from the outside of inner casing 21.
- FIG. 3 shows the inner casing to include additional diaphragm rings 12, 12b and additional radial wall portions 23a, 23b as before, together defining extraction passages such as 24. Passages 24 become smaller in cross-sectional area as the top of the inner casing is approached. Hence the total area for sealing the raised horizontal joint is substantially smaller than in FIG. 2 for a comparable unit and the lengths of the radial walls are also shorter. This enables a sufficient seal at the joint to be obtained by the use of bolts 28 which are all external to the inner casing. Sealing keys 29 at the horizontal joint may be employed if desired to give additional sealing capability.
- an elastic fluid turbine having a rotor with a plurality of bucket wheels and a plurality of stationary nozzle diaphragms separating said wheels and having outer ring portions dividing regions of gradually decreasing fluid pressure, the improvement comprising:
- an inner casing disposed thin said outer casing and having a wrapper wall and a plurality of spaced radial wall portions, said wall portions and said outer diaphragm ring portions cooperating to define extraction conduits from said diaphragm pressure regions, said conduits gradually increasing in cross-sectional area from the top of the inner casing to the horizontal centerline of the rotor,
- said inner casing being divided into upper and lower sections along a horizontal joint disposed substantially higher than said centerline, whereby the sealing surface at the joint is smaller than it would be if located at the centerline, and
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
The inner casing of a low-pressure steam turbine has top and bottom sections which are connected along a horizontal joint disposed substantially higher than the horizontal centerline of the machine. The connectors at the joint can thus be located outside the inner casing because of the smaller sealing surface area at the raised joint.
Description
llnited States Patent [72] Inventor Arthur F. Fatum Schenectady, N.Y. [21] App1.No. 71,158 [22] Filed Sept. 10, 1970 [45] Patented Dec. 28, 1971 [7 3] Assignee General Electric Company [54] TURBINE CASING WITII RAISED HORIZONTAL JOINT 4 Claims, 4 Drawing Figs.
[52] 11.5. CI 415/219, 415/ 199 [51] Int. Cl F0ld1/00 [50] Field of Search 415/138, 139,140,199, 219,108,168
[56] References Cited UNITED STATES PATENTS 2,199,595 5/1940 Millard 415/201 2,282,894 5/1942 Sheldon 415/168 2,683,017 7/1954 Gallaway... 415/139 2,975,600 3/1961 Wilson 415/219 3,058,720 10/1962 Hart et a1 415/168 3,520,634 7/1970 Bellatiet a1 415/219 FOREIGN PATENTS 707,153 6/1941 Germany 415/168 1,301,686 2/1964 France 415/219 Primary Examiner-Henry F. Raduazo Attorneys-William C. Crutcher. Frank L. Neuhauser.
Oscar B. Waddell, and Joseph B. Forman ABSTRACT: The inner casing of a low-pressure steam turbine has top and bottom sections which are connected along a horizontal joint disposed substantially higher than the horizontal centerline of the machine. The connectors at the joint can thus be located outside the inner casing because of the smaller sealing surface area at the raised joint.
PATENIEU M628 l97l SHEET 1 OF 2 FlG.l0
(PRIOR ART) INVENTOR:
ARTHUR F. FATUM, BY 8M HIS ATTORNEY.
PATENTED UEB28 um SHEET 2 [1F 2 QQQIJ INVENTORZI ARTHUR FIFATUM,
mdE
f9 W& C.m moi:
@QQQQQQQ EP O 3 9* BY 441 W HIS ATTORNEY.
TURBINE CASING WITI-I RAISED HORIZONTAL JOINT BACKGROUND OF THE INVENTION This invention relates to elastic fluid turbines and particularly to an improvement in the inner casing construction of a low-pressure steam turbine.
The low-pressure units of large steam turbines are often arranged so that the lowest pressure turbine sections are disposed in an inner casing which is located in an outer casing or exhaust hood leading to the condenser. Thus the space between the inner and outer casings is at a vacuum corresponding roughly to exhaust or condenser pressure, while the steam pressure inside the inner casing varies as it is expanded from one stage of buckets and nozzle diaphragms to the next.
Low-pressure turbines are also generally constructed to provide for extraction of steam at various points along the low-pressure turbine sections in order to supply various feedwater heaters. Thus passages within the inner casing must. be provided to lead the extracted steam from selected turbine stages and to remove it through pipes leading from the outer casing or exhaust hood. These extraction passages are generally formed between longitudinally spaced radial walls and the wrapper walls of the inner casing.
As is known to those skilled in the art, the inner casing must be split into two or more sections to allow for removal of the stationary nozzle diaphragms separating the turbine stages, and also for removal of the rotor itself. In the past, the inner casing upper and lower sections have been divided along a horizontal joint which is located roughly at the horizontal centerline of the machine, and the upper and lower halves of the nozzle diaphragms have also been supported substantially at the horizontal centerline. Because of the fact that the space between the outer casing and inner casing is at a vacuum, a tight seal must be maintained at this horizontal joint between the upper and lower inner casing halves. Furthermore, because of the fact that the passages for extraction of steam inside the inner casing are so large at the centerline, it has been necessary to provide additional connecting bolts inside the wrapper of the inner casing in order to provide an adequate seal. These internal connecting bolts can only be reached by providing access holes in the wrapper.
It is undesirable, both in terms of time requirements and safety of personnel, to require them to remove bolts which are inside the wrapper. Furthermore, the number of connectors and flanges necessary to accomplish sealing at the horizontal centerline joint, obstruct the steam flow both in the extraction passages and in the space between the inner and outer casings.
Accordingly, one object of the present invention is to provide an improved inner casing construction for a low-pressure steam turbine, wherein the connecting means for sealing the upper and lower inner casing halves may all be disposed on the outside of the inner casing.
Another object of the invention is to provide an improved inner casing construction for a low-pressure steam turbine, wherein the connecting means for joining the casing halves is arranged to minimize obstructions in the steam flow paths.
SUMMARY OF THE INVENTION Briefly stated, the invention is practiced by locating the horizontal joint of the inner casing substantially above the turbine horizontal centerline and at a location of smaller sealing area around the extraction passages, and locating the connecting members on the outside of the inner casing.
DRAWING The invention, both as to organization and method of practice, together with further objects and advantages thereof, will best be understood by reference to the following description, taken in connection with the accompanying drawings, in which:
FIG. la is a transverse cross section through one-half of a low-pressure steam turbine illustrating the prior art,
FIG. lb is a similar cross section through the other half and illustrating the present invention,
FIG. 2 is a horizontal cross section taken along lines Il-lI of FIG. la illustrating the prior art, and
FIG. 3 is a horizontal cross section taken along lines IllIlI of FIG. lb, illustrating the invention.
DESCRIPTION OF A PRIOR ART CONSTRUCTION Referring to FIG. 1a of the drawing, an outer casing l, which in this case is the exhaust hood, is arranged in upper and lower halves connected at a horizontal joint 2 and supported on a foundation 3. At its lower end, the outer casing l communicates with the condenser (not shown). Disposed inside the outer casing is an inner casing 4 comprising an upper section 40 and a lower section 4b. Sections 40 and 4b are connected along a horizontal joint 5 disposed substantially along the horizontal centerline 6 of the turbine rotor (not shown). Joint 5 is sealed by external connecting bolts 7 and internal connecting bolts 8. Access to internal bolts 8 is provided by a removable cover 9.
The steam flows longitudinally along the turbine through nozzle partition blades 10 which are supported between inner and outer semicircular ring portions II, 12 respectively. Members 10, 11 and 12 together make up a stationary nozzle diaphragm which is supported substantially at the horizontal centerline 6 by means of a lug 13 supported in a suitable recess 14 in the lower casing half. Extraction passages 16 are formed inside the inner casing 4 by an outer wrapper wall 17 and a number of spaced dial dividing walls 18. The wrapper and radial walls are arranged so that the cross-sectional flow area of extraction passages 16 increase gradually from the top of the inner casing around the unit until they finally empty into an extraction steam removal pipe 19 toward the lower part of the inner casing.
Reference to FIG. 2 of the drawing, which also illustrates the prior art, shows a horizontal cross section of a portion of the turbine, looking downward just above the horizontal joint. It will be seen that the configuration of the wall sections of the inner casing 4 is rather complex in order to provide the various extraction passages such as 16, as well as to accommodate the varying sizes of the outer diaphragm rings such as I2, 12a and 12b along the steam flow path. It will be observed that additional radial wall portions 18a, 18b are longitudinally spaced along the unit, these being joined to additional circumferential well portions 17a, 17b which in turn cooperate with the outer diaphragm rings. These members together seal off regions of fluid pressure leading into extraction conduit 16.
Due to the substantial distance between the outer wrapper wall 17 and the various diaphragm rings at the horizontal centerline, a substantial sealing area is required at the joint. This requires internal horizontal sealing flanges 20 which tend to obstruct the flow of extraction steam. Furthermore, extensive internal bolting 8 is necessary to provide an adequate seal.
The foregoing description is illustrative of an inner casing construction of the prior art, although it will be understood that many variations have been suggested in the prior art.
DESCRIPTION OF THE PREFERRED EMBODIMENT FIGS. lb and 3 relate to the improved construction of the present invention. The outer casing l is arranged as before, as are the members 10, I1 and 12 making up the diaphragm.
The improvement of the present invention relates to the inner casing shown as 21, constructed with a top section 21a and a bottom section 21b. A wrapper wall 22 and a group of radial wall portions 23, together with the diaphragm outer rings 12 define, as before, extraction passages 24. Passages 24 gradually increase in cross-sectional area from the top toward the lower part of casing 21 and are led from the casing through extraction pipes 25.
According to the present invention, the upper and lower casing sections are connected at a horizontaljoint 26. Joint 26 is disposed substantially higher than the centerline 6 of the unit, perhaps on the order of 2 feet in a large lowpressure turbine. Since the radius of the inner casing will vary from 4 feet to 8 feet or more, the joint is thus raised on the order of onequarter to one-half of the inner casing radius. Mounting pads 27 arranged on selected radial walls 23 support the diaphragm lugs 13 substantially at the horizontal centerline as before, and removable square-headed pins 28 hold the lugs 13 in position.
Means for connecting the upper and lower sections at horizontal joint 26 include bolts 28. These bolts are all located and accessible from the outside of inner casing 21.
Reference to FIG. 3 of the drawing shows a horizontal cross section taken just above horizontal joint 26. FIG. 3 shows the inner casing to include additional diaphragm rings 12, 12b and additional radial wall portions 23a, 23b as before, together defining extraction passages such as 24. Passages 24 become smaller in cross-sectional area as the top of the inner casing is approached. Hence the total area for sealing the raised horizontal joint is substantially smaller than in FIG. 2 for a comparable unit and the lengths of the radial walls are also shorter. This enables a sufficient seal at the joint to be obtained by the use of bolts 28 which are all external to the inner casing. Sealing keys 29 at the horizontal joint may be employed if desired to give additional sealing capability.
OPERATION The operation of the invention is as follows. Referring to FIGS. 1a and 1b of the prior art and the present invention respectively, it will be noted that the cross-sectional areas of the extraction conduits 16, 24 respectively decrease from the top of the inner casings toward the horizontal centerline. However, in FIG. 1a, because of the inner circumferential walls 170 and the large sealing flanges 20 at the horizontal centerline, the outer dimension of the wrapper 17 is necessarily greater than it is in FlG. 1b, in order to provide the same flow areas at the centerline, these areas being indicated by letters A and A respectively.
By raising the horizontal joint 26 to the location indicated, where the cross-sectional flow area is smaller in passage 24, a much smaller area for scaling is required. In other words, the horizontal distance C on which the bolts 28 must exert sealing force is much smaller in dimension than the comparable horizontal distance C in the left-hand FlG.
Since dimension C was so great with the prior art construction, insufficient force could be obtained with bolts 7, thus requiring internal bolts 8 and the accompanying flanges 20. The internal bolts and flanges compounded the casing construction difficulties, as well as bringing about the aforesaid enlargement of inner casing wrapper diameter in order to accommodate the required extraction flow area. Also the support block with recess 14 blocked the extraction passage 16, thereby causing an additional increase in dimension C.
It will be noted in the improved construction that, since the distance between the inner and outer casings becomes greater as the horizontal joint is raised, more space becomes available for the external bolting flanges carrying bolts 28 and hence the flow area of steam to the condenser between the inner and outer casings is less obstructed with e improved design.
When removing the upper section of the inner casing in FlG. 1b, it is only necessary to remove bolts 28 without requiring entry into the inner casing wrapper as in the old construction. Removal of the square-headed pins 28 then allow the diaphragm sections to be raised in the usual manner.
Thus it will be seen that the foregoing improvement to inner casing design in a low-pressure steam turbine of a raised horizontal joint as indicated offers substantial improvements over the prior art. Removal of the inner casing upper section is greatly facilitated and improved steam flow passages result without increase of the outer casing overall dimensions.
Although the invention has been shown as specifically applied to a large low-pressure steam turbine, the construction is equally applicable to other types of elastic fluid turbines of a two-casing construction. While there has been shown herein what 18 considered to be the preferred embodiment of the mvention, other modifications may be made by those skilled-in the art, and it is intended to cover in the appended claims all such modifications as fall within the true spirit and scope of the invention.
What is claimed is:
1. ln an elastic fluid turbine having a rotor with a plurality of bucket wheels and a plurality of stationary nozzle diaphragms separating said wheels and having outer ring portions dividing regions of gradually decreasing fluid pressure, the improvement comprising:
an outer casing communicating at its bottom side with a region of fluid pressure lower than that in said diaphragm regions,
an inner casing disposed thin said outer casing and having a wrapper wall and a plurality of spaced radial wall portions, said wall portions and said outer diaphragm ring portions cooperating to define extraction conduits from said diaphragm pressure regions, said conduits gradually increasing in cross-sectional area from the top of the inner casing to the horizontal centerline of the rotor,
said inner casing being divided into upper and lower sections along a horizontal joint disposed substantially higher than said centerline, whereby the sealing surface at the joint is smaller than it would be if located at the centerline, and
bolting means sealingly connecting said upper and lower sections and accessible from the outside of said inner cas- 2. The combination according to claim 1, wherein said nozzle diaphragms are supported substantially at the horizontal centerline on pads attached to said radial wall portions in the lower casing section, and further including removable pins holding said diaphragms in place.
3. The combination according to claim 1, wherein said horizontal joint is disposed a distance above said horizontal centerline on the order of one-quarter to one-half of the inner casing radius.
4. The combination according to claim 1, wherein said radial wall portions include sealing keys disposed at the horizontal joint.
# t i t
Claims (4)
1. In an elastic fluid turbine having a rotor with a plurality of bucket wheels and a plurality of stationary nozzle diaphragms separating said wheels and having outer ring portions dividing regions of gradually decreasing fluid pressure, the improvement comprising: an outer casing communicating at its bottom side with a region of fluid pressure lower than that in said diaphragm regions, an inner casing disposed thin said outer casing and having a wrapper wall and a plurality of spaced radial wall portions, said wall portions and said outer diaphragm ring portions cooperating to define extraction conduits from said diaphragm pressure regions, said conduits gradually increasing in crosssectional area from the top of the inner casing to the horizontal centerline of the rotor, said inner casing being divided into upper and lower sections along a horizontal joint disposed substantially higher than said centerline, whereby the sealing surface at the joint is smaller than it would be if located at the centerline, and bolting means sealingly connecting said upper and lower sections and accessible from the outside of said inner casing.
2. The combination according to claim 1, wherein said nozzle diaphragms are supported substantially at the horizontal centerline on pads attached to said radial wall portions in the lower casing section, and further including removable pins holding said diaphragms in place.
3. The combination according to claim 1, wherein said horizontal joint is disposed a distance above said horizontal centerline on the order of one-quarter to one-half of the inner casing radius.
4. The combination according to claim 1, wherein said radial wall portions include sealing keys disposed at the horizontal joint.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US7115870A | 1970-09-10 | 1970-09-10 |
Publications (1)
Publication Number | Publication Date |
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US3630635A true US3630635A (en) | 1971-12-28 |
Family
ID=22099627
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US71158A Expired - Lifetime US3630635A (en) | 1970-09-10 | 1970-09-10 | Turbine casing with raised horizontal joint |
Country Status (7)
Country | Link |
---|---|
US (1) | US3630635A (en) |
JP (1) | JPS5420602B1 (en) |
CH (1) | CH528667A (en) |
DE (1) | DE2142845C3 (en) |
FR (1) | FR2107400A5 (en) |
GB (1) | GB1336384A (en) |
SE (1) | SE360426B (en) |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3752427A (en) * | 1971-03-11 | 1973-08-14 | Bbc Brown Boveri & Cie | Support arrangement for a turbomachine |
US4397608A (en) * | 1980-05-01 | 1983-08-09 | Automation Industries, Inc. | Energy-absorbing turbine missile shield |
US4699566A (en) * | 1984-03-23 | 1987-10-13 | Westinghouse Electric Corp. | Blade ring for a steam turbine |
US4744726A (en) * | 1985-06-27 | 1988-05-17 | Kraftwerk Union Aktiengesellschaft | Turboset with at least one low-pressure turbine stage having an outer housing and an inner housing coaxial thereto, and with high-pressure and/or medium-pressure turbine stage |
US6267556B1 (en) * | 1998-04-21 | 2001-07-31 | Kabushiki Kaisha Toshiba | Steam turbine |
US6419448B1 (en) * | 2000-03-20 | 2002-07-16 | Jerzy A. Owczarek | Flow by-pass system for use in steam turbine exhaust hoods |
US20050063821A1 (en) * | 2003-09-22 | 2005-03-24 | Luniewski Alexander Kenneth | Low pressure steam turbine exhaust hood |
US20080286099A1 (en) * | 2007-05-17 | 2008-11-20 | General Electric Company | Steam turbine exhaust hood and method of fabricating the same |
US20100202879A1 (en) * | 2009-02-10 | 2010-08-12 | General Electric Company | Extraction unit for turbine and related method |
US20100303619A1 (en) * | 2009-05-28 | 2010-12-02 | General Electric Company | Shaped and stiffened lower exhaust hood sidewalls |
US20100303620A1 (en) * | 2009-05-28 | 2010-12-02 | General Electric Company | Corrugated hood for low pressure steam turbine |
US20120121391A1 (en) * | 2010-11-16 | 2012-05-17 | General Electric Company | Adjustment and measurement system for steam turbine nozzle assembly |
US20120183397A1 (en) * | 2011-01-14 | 2012-07-19 | Hitachi, Ltd. | Exhaust System for Steam Turbine |
CN103362576A (en) * | 2013-07-30 | 2013-10-23 | 东方电气集团东方汽轮机有限公司 | Method for sealing air cylinder split |
US20130315721A1 (en) * | 2012-05-22 | 2013-11-28 | Laquinnia Lawson, Jr. | Exhaust Plenum for Gas Turbine |
US20140119886A1 (en) * | 2012-10-31 | 2014-05-01 | General Electric Company | Turbine cowling system |
Families Citing this family (1)
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EP2551473A1 (en) * | 2011-07-27 | 2013-01-30 | Alstom Technology Ltd | Device for the mutual fixation of two gas turbine casing components |
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- 1970-09-10 US US71158A patent/US3630635A/en not_active Expired - Lifetime
-
1971
- 1971-07-14 GB GB3291971A patent/GB1336384A/en not_active Expired
- 1971-08-26 DE DE2142845A patent/DE2142845C3/en not_active Expired
- 1971-08-30 CH CH1268771A patent/CH528667A/en not_active IP Right Cessation
- 1971-09-08 FR FR7132371A patent/FR2107400A5/fr not_active Expired
- 1971-09-10 JP JP6980271A patent/JPS5420602B1/ja active Pending
- 1971-09-10 SE SE11515/71A patent/SE360426B/xx unknown
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DE707153C (en) * | 1938-09-02 | 1941-06-14 | Aeg | Device for separating water from partially relaxed working steam from steam turbines |
US2199595A (en) * | 1939-05-11 | 1940-05-07 | Murray Iron Works Company | Turbine |
US2282894A (en) * | 1940-04-02 | 1942-05-12 | Gen Electric | Elastic fluid turbine |
US2683017A (en) * | 1949-04-27 | 1954-07-06 | Westinghouse Electric Corp | Turbine cylinder joint |
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Cited By (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3752427A (en) * | 1971-03-11 | 1973-08-14 | Bbc Brown Boveri & Cie | Support arrangement for a turbomachine |
US4397608A (en) * | 1980-05-01 | 1983-08-09 | Automation Industries, Inc. | Energy-absorbing turbine missile shield |
US4699566A (en) * | 1984-03-23 | 1987-10-13 | Westinghouse Electric Corp. | Blade ring for a steam turbine |
US4744726A (en) * | 1985-06-27 | 1988-05-17 | Kraftwerk Union Aktiengesellschaft | Turboset with at least one low-pressure turbine stage having an outer housing and an inner housing coaxial thereto, and with high-pressure and/or medium-pressure turbine stage |
US6267556B1 (en) * | 1998-04-21 | 2001-07-31 | Kabushiki Kaisha Toshiba | Steam turbine |
US6443695B2 (en) | 1998-04-21 | 2002-09-03 | Kabushiki Kaisha Toshiba | Steam turbine |
US6702551B2 (en) | 1998-04-21 | 2004-03-09 | Kabushiki Kaisha Toshiba | Steam turbine |
US6419448B1 (en) * | 2000-03-20 | 2002-07-16 | Jerzy A. Owczarek | Flow by-pass system for use in steam turbine exhaust hoods |
US20050063821A1 (en) * | 2003-09-22 | 2005-03-24 | Luniewski Alexander Kenneth | Low pressure steam turbine exhaust hood |
US6971842B2 (en) * | 2003-09-22 | 2005-12-06 | General Electric Company | Low pressure steam turbine exhaust hood |
US7785068B2 (en) | 2007-05-17 | 2010-08-31 | General Electric Company | Steam turbine exhaust hood and method of fabricating the same |
US20080286099A1 (en) * | 2007-05-17 | 2008-11-20 | General Electric Company | Steam turbine exhaust hood and method of fabricating the same |
US8398367B2 (en) * | 2009-02-10 | 2013-03-19 | General Electric Company | Extraction unit for turbine and related method |
US20100202879A1 (en) * | 2009-02-10 | 2010-08-12 | General Electric Company | Extraction unit for turbine and related method |
US20100303619A1 (en) * | 2009-05-28 | 2010-12-02 | General Electric Company | Shaped and stiffened lower exhaust hood sidewalls |
US20100303620A1 (en) * | 2009-05-28 | 2010-12-02 | General Electric Company | Corrugated hood for low pressure steam turbine |
US8221053B2 (en) * | 2009-05-28 | 2012-07-17 | General Electric Company | Shaped and stiffened lower exhaust hood sidewalls |
US8221054B2 (en) * | 2009-05-28 | 2012-07-17 | General Electric Company | Corrugated hood for low pressure steam turbine |
US20120121391A1 (en) * | 2010-11-16 | 2012-05-17 | General Electric Company | Adjustment and measurement system for steam turbine nozzle assembly |
US8690533B2 (en) * | 2010-11-16 | 2014-04-08 | General Electric Company | Adjustment and measurement system for steam turbine nozzle assembly |
RU2601779C2 (en) * | 2010-11-16 | 2016-11-10 | Дженерал Электрик Компани | Segment of casing of steam turbine, steam-turbine unit and steam-turbine plant |
US20120183397A1 (en) * | 2011-01-14 | 2012-07-19 | Hitachi, Ltd. | Exhaust System for Steam Turbine |
US9033656B2 (en) * | 2011-01-14 | 2015-05-19 | Mitsubishi Hitachi Power Systems, Ltd. | Exhaust system for steam turbine |
US20130315721A1 (en) * | 2012-05-22 | 2013-11-28 | Laquinnia Lawson, Jr. | Exhaust Plenum for Gas Turbine |
US8961116B2 (en) * | 2012-05-22 | 2015-02-24 | Braden Manufacturing, Llc | Exhaust plenum for gas turbine |
US20140119886A1 (en) * | 2012-10-31 | 2014-05-01 | General Electric Company | Turbine cowling system |
CN103362576A (en) * | 2013-07-30 | 2013-10-23 | 东方电气集团东方汽轮机有限公司 | Method for sealing air cylinder split |
Also Published As
Publication number | Publication date |
---|---|
GB1336384A (en) | 1973-11-07 |
JPS5420602B1 (en) | 1979-07-24 |
CH528667A (en) | 1972-09-30 |
FR2107400A5 (en) | 1972-05-05 |
DE2142845A1 (en) | 1972-03-16 |
SE360426B (en) | 1973-09-24 |
DE2142845C3 (en) | 1980-01-03 |
DE2142845B2 (en) | 1977-01-27 |
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