US1884422A - Turbine casing - Google Patents
Turbine casing Download PDFInfo
- Publication number
- US1884422A US1884422A US459802A US45980230A US1884422A US 1884422 A US1884422 A US 1884422A US 459802 A US459802 A US 459802A US 45980230 A US45980230 A US 45980230A US 1884422 A US1884422 A US 1884422A
- Authority
- US
- United States
- Prior art keywords
- turbine
- blade
- webs
- casing
- sections
- 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.)
- Expired - Lifetime
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
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
- F01D1/023—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines the working-fluid being divided into several separate flows ; several separate fluid flows being united in a single flow; the machine or engine having provision for two or more different possible fluid flow paths
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles
Definitions
- a more particular object is to provide a construction of the character set forth involving a minimum number of parts of which a turbine stator is constructed.
- I provide a casting which includes a part of the turbine casing and one or more integral webs, for supporting the blade carrying member, each web being of a dimension equal to the maximum dimension which may be required in the turbine.
- the blade carrying members are of a regular form, and are also of the maximum axial length which may be required.
- the blade carrying member is cut to the required size, if necessary.
- the webs are also cut to the proper dimensions, so that the inner edge meets the mainbody of the blade carrying member with the latter in the desired axial position in the turbine. Said edge is then welded to the main body of the blade carrying member.
- Fig. 1 is a longitudinal, sectional view 1930. Serial No. 459,802.
- Fig. 2 is a detail sectional view showing the form of the casting as carried in stock.
- an elastic fluid turbine 10 comprising a casing 11 and a rotor 12.
- the casing 11 is divided along the hori ontal plane of the turbine axis, and the upper and lower parts are formed wit-h flanges 13 at the meeting plane by means of which said parts may be secured together.
- the casing 11 is also divided longitudinall v into three sections '14, 15 and 16.
- the section. 16 provides the exhaust chamber and is secured to the section 15 by a conventional ,flangeand bolt joint 17.
- the sections 14 and 15 are connected by a telescopic joint 18.
- the sections are also Welded to each other at 19 and 21, and a number of radially-extending, circumferentially-distributed, pins 22 extend through the telescopic partsto fix the relative position of the sections 14 and 15 and to transmitlongitudinal andv circumferential thrusts.
- the purpose of the telescoping type of joint is to permit a variation in the length of the casing, as hereinafter explained.
- the section 15 is formed with integral webs 26, 27 and 28, extending inwardly in a direction which is at least partly radial.
- the webs support blade-carrying members 29 and 30, which are secured to the webs by welding the inneredgesof the we-bsto the main body of the blade-carrying members,
- The-blade-carrying members are of tubular form, extending in a direction one component of which is axial, and they each carry aplnrality of annular rows of stationary blades.
- the -blade-carrying members are preferably of relatively regularform, that is, they do not have projections .for fitting the blade-carrying members; sothatthey may be secured atany axial point thereof to the webs, and disposed in any one of various axial positions-
- the section 15 is cast and carried in stock in the form shown in Fig. 2; an additional web 25 beingprovided at the end 23 at which I In constructing a turbine for the particular steam conditions required, the blade-carrying members are reduced to the correct axial length, if such is less than the original maximum length.
- the axial position of the blade- I carrying members relative to the webs supporting the same is determined and the webs are cut at the points at which they meet the 'main body of the blade-carrying members, and are then welded thereto. It will be apparent that a substantial variation is provided in the axial position in which the bladecarrying members may be disposed relative to the casing.
- the end 23 is cut at 24, removing the web 25.
- the webs 26, 27 and 28 are cut at 45, 46, and 47, respectively.
- the remainder of the turbine may be of any suitable construction, such as shown on the drawing, in which the rotor is supported in bearings 41 and 42, and in which the section 11 carries dummy rings 43 and the stationalry blades and nozzles of an impulse stage 44.
- e chamber 48 formed between the webs 27 and 28 and an outlet 49 communicating therewith may be used for extraction of partially expanded motive fluid.
- each of these sizes is adapted for different operating conditions within a. limited portion of the total range.
- Different diameters of the sections 14 and 16 which fit the different sizes of the sections 15 are provided.
- Each size of the section 15 will provide for a suliicient range of different operating conditions so that a reasonable number thereof may be carriedin stockt From the above description, it will be seen that I have provided a turbine stator construction which involves relatively few parts which may be standardized, and that the turbine stator may readily be constructed from said standardized parts. It will be apparent that by this construction it is possible to deliver a turbine suited for any desired conditions in a much shorter period of time than heretofore.
- What I claim is 1.
- the method of assembling and constructing a turbine stator of desired capacity from standardized parts including a tubular portion made of cast metal having an integral approximately radial web portion and a separate tubular blade-carrying member, which comprises cutting the inner ed e of the web portion to a diameter fitting t e exterior of a tubular blade-carrying member of a size providing the desired capacity, positioning the blade-carrying member in the web portion in the desired axial position relative thereto, and welding the inner edge of the web portion to the main body of the bladecarrying member.
- a turbine stator of desired capacity comprising intermediate and end sections for connection together in end-to-end relation and the intermediate section having inwardly extending webs connected to blade rings, which comprises cutting the intermediate section to suitable length, cutting the webs to define openings of desired diameters, placing a blade ring or rings of desired size in the openings, welding the blade ring or rings to the webs, and securing the intermediate section to the end sections.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
Oct.- 25, 193-2. J. B. WALBRlDGE I 1,834,422
TURBINE CAS ING Filed June 7, 1930 W TNESS INVENTOR 24 J. B. Walbridge. I BY a ATTORN EY Patented Oct. 25, 1932 UNITED STATES JOHN B. WALBRIDGE, OF DREXEL HILL, PENNSYLVANIA, ASSIGNOR T0 WESTING- PATENT OFFICE HOUSE ELECTRIC & MANUFACTURING COMPANY, A CORPORATION OF PENNSYL- VANIA TURBINE CASING Application filed June 7,
accordance with its operating conditions.
This means that patterns must be made and the complete manufacturing operation must be carried out after an order for a turbine is received.
It is an object of my invention to provide a construction of turbine stator which comprises standardized parts from which a turbine may be constructed for various operating conditions, so that the parts may be carried in stock and readily assembled into a turbine.
A more particular object is to provide a construction of the character set forth involving a minimum number of parts of which a turbine stator is constructed.
In accordance with my invention, I provide a casting which includes a part of the turbine casing and one or more integral webs, for supporting the blade carrying member, each web being of a dimension equal to the maximum dimension which may be required in the turbine. The blade carrying members are of a regular form, and are also of the maximum axial length which may be required. In constructing a turbine from said parts, the blade carrying member is cut to the required size, if necessary. The webs are also cut to the proper dimensions, so that the inner edge meets the mainbody of the blade carrying member with the latter in the desired axial position in the turbine. Said edge is then welded to the main body of the blade carrying member.
The above and other objects are efiected by my invention, as will be apparent from the following description and claims taken in connection with the accompanying drawing, forming a part of this application, in V which:
Fig. 1 is a longitudinal, sectional view 1930. Serial No. 459,802.
through a turbine constructed in accordance with the present invention; and,
Fig. 2 is a detail sectional view showing the form of the casting as carried in stock.
Referring now to the drawing more in detail, I show an elastic fluid turbine 10 comprising a casing 11 and a rotor 12. The casing 11 is divided along the hori ontal plane of the turbine axis, and the upper and lower parts are formed wit-h flanges 13 at the meeting plane by means of which said parts may be secured together.
The casing 11 is also divided longitudinall v into three sections '14, 15 and 16. The section. 16 provides the exhaust chamber and is secured to the section 15 by a conventional ,flangeand bolt joint 17. The sections 14 and 15 are connected by a telescopic joint 18. The sections are also Welded to each other at 19 and 21, and a number of radially-extending, circumferentially-distributed, pins 22 extend through the telescopic partsto fix the relative position of the sections 14 and 15 and to transmitlongitudinal andv circumferential thrusts. 'The purpose of the telescoping type of joint is to permit a variation in the length of the casing, as hereinafter explained.
The section 15 is formed with integral webs 26, 27 and 28, extending inwardly in a direction which is at least partly radial. The webs support blade-carrying members 29 and 30, which are secured to the webs by welding the inneredgesof the we-bsto the main body of the blade-carrying members,
as indicated at 32, 33 and 34.
The-blade-carrying members are of tubular form, extending in a direction one component of which is axial, and they each carry aplnrality of annular rows of stationary blades. The -blade-carrying members are preferably of relatively regularform, that is, they do not have projections .for fitting the blade-carrying members; sothatthey may be secured atany axial point thereof to the webs, and disposed in any one of various axial positions- The section 15 is cast and carried in stock in the form shown in Fig. 2; an additional web 25 beingprovided at the end 23 at which I In constructing a turbine for the particular steam conditions required, the blade-carrying members are reduced to the correct axial length, if such is less than the original maximum length. The axial position of the blade- I carrying members relative to the webs supporting the same is determined and the webs are cut at the points at which they meet the 'main body of the blade-carrying members, and are then welded thereto. It will be apparent that a substantial variation is provided in the axial position in which the bladecarrying members may be disposed relative to the casing.
For the turbine shown in Fig. 1, the end 23 is cut at 24, removing the web 25. The webs 26, 27 and 28 are cut at 45, 46, and 47, respectively.
The remainder of the turbine may be of any suitable construction, such as shown on the drawing, in which the rotor is supported in bearings 41 and 42, and in which the section 11 carries dummy rings 43 and the stationalry blades and nozzles of an impulse stage 44. e chamber 48 formed between the webs 27 and 28 and an outlet 49 communicating therewith may be used for extraction of partially expanded motive fluid.
To cover a wide range of steam conditions, a number of different sizes of castings of the section 15 are provided, and each of these sizes is adapted for different operating conditions within a. limited portion of the total range. Different diameters of the sections 14 and 16 which fit the different sizes of the sections 15 are provided. Each size of the section 15 will provide for a suliicient range of different operating conditions so that a reasonable number thereof may be carriedin stockt From the above description, it will be seen that I have provided a turbine stator construction which involves relatively few parts which may be standardized, and that the turbine stator may readily be constructed from said standardized parts. It will be apparent that by this construction it is possible to deliver a turbine suited for any desired conditions in a much shorter period of time than heretofore.
imposed by the prior art or as are specifically set forth in the appended claims.
What I claim is 1. The method of assembling and constructing a turbine stator of desired capacity from standardized parts including a tubular portion made of cast metal having an integral approximately radial web portion and a separate tubular blade-carrying member, which comprises cutting the inner ed e of the web portion to a diameter fitting t e exterior of a tubular blade-carrying member of a size providing the desired capacity, positioning the blade-carrying member in the web portion in the desired axial position relative thereto, and welding the inner edge of the web portion to the main body of the bladecarrying member.
2. The method of manufacturing a turbine stator of desired capacity, the stator comprising intermediate and end sections for connection together in end-to-end relation and the intermediate section having inwardly extending webs connected to blade rings, which comprises cutting the intermediate section to suitable length, cutting the webs to define openings of desired diameters, placing a blade ring or rings of desired size in the openings, welding the blade ring or rings to the webs, and securing the intermediate section to the end sections.
In testimony whereof, I have hereunto subscribed my name this 5th day of June, 1930.
JOHN B. WALBRIDGE.
While I have shown my invention in but one form, it will be obvious to those skilled in the art that it is not so limited, but is susceptible of various changes and modifications without departing from the spirit thereof, and I desire therefore, that only such limitations shall be placed thereupon as are
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US459802A US1884422A (en) | 1930-06-07 | 1930-06-07 | Turbine casing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US459802A US1884422A (en) | 1930-06-07 | 1930-06-07 | Turbine casing |
Publications (1)
Publication Number | Publication Date |
---|---|
US1884422A true US1884422A (en) | 1932-10-25 |
Family
ID=23826207
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US459802A Expired - Lifetime US1884422A (en) | 1930-06-07 | 1930-06-07 | Turbine casing |
Country Status (1)
Country | Link |
---|---|
US (1) | US1884422A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2505217A (en) * | 1945-03-19 | 1950-04-25 | Elliott Co | High-temperature rotating machinery |
US2934316A (en) * | 1955-11-18 | 1960-04-26 | Worthington Corp | Turbine casing |
US3043559A (en) * | 1954-10-22 | 1962-07-10 | Maschf Augsburg Nuernberg Ag | Gas turbine |
US20050039333A1 (en) * | 2001-11-22 | 2005-02-24 | Michael Wechsung | Method for manufacturing steam turbines |
-
1930
- 1930-06-07 US US459802A patent/US1884422A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2505217A (en) * | 1945-03-19 | 1950-04-25 | Elliott Co | High-temperature rotating machinery |
US3043559A (en) * | 1954-10-22 | 1962-07-10 | Maschf Augsburg Nuernberg Ag | Gas turbine |
US2934316A (en) * | 1955-11-18 | 1960-04-26 | Worthington Corp | Turbine casing |
US20050039333A1 (en) * | 2001-11-22 | 2005-02-24 | Michael Wechsung | Method for manufacturing steam turbines |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2347034A (en) | Turbine bucket wheel and the like | |
US11009039B2 (en) | Intermittent spigot joint for gas turbine engine casing connection | |
US2771622A (en) | Diaphragm apparatus | |
GB1008526A (en) | Axial flow bladed rotor, e.g. for a turbine | |
CA2767702C (en) | Rotor centralization for turbine engine assembly | |
US3370830A (en) | Turbine cooling | |
US2380276A (en) | Welded structure | |
US1884422A (en) | Turbine casing | |
US20190128126A1 (en) | Turbine blisk and method of manufacturing thereof | |
US1366605A (en) | Blade-securing means and method of making the same | |
US3408045A (en) | Turbine nozzle seal structure | |
US1625541A (en) | Elastic-fluid turbine | |
CN101131092B (en) | Methods and apparatus for fabricating a rotor for a steam turbine | |
US2530908A (en) | Turbine diaphragm | |
US2928586A (en) | Stator for multi-stage axial-flow compressor | |
US9702267B2 (en) | Engine structure assembly procedure | |
JPH09505377A (en) | Ceramic / metal stator blade device with brazing part | |
US2729260A (en) | Screw locked by deforming pin | |
US2849209A (en) | Nozzle construction for turbines | |
US2197335A (en) | Turbine blade shroud | |
US1470503A (en) | Method of making blade rings | |
GB819814A (en) | Improvements in or relating to axial-flow fluid machines, for example axial-flow compressors | |
US2151699A (en) | Casing for turbines | |
US10655682B2 (en) | Bearing system with a rotary bush and turbomachine | |
EP0217837B1 (en) | Internal housing for a turbo-engine |