US1693317A - Method of bracing casing structures for elastic fluid turbines and the like - Google Patents
Method of bracing casing structures for elastic fluid turbines and the like Download PDFInfo
- Publication number
- US1693317A US1693317A US195835A US19583527A US1693317A US 1693317 A US1693317 A US 1693317A US 195835 A US195835 A US 195835A US 19583527 A US19583527 A US 19583527A US 1693317 A US1693317 A US 1693317A
- Authority
- US
- United States
- Prior art keywords
- casing
- walls
- bracing
- elastic fluid
- brace
- 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
- 239000012530 fluid Substances 0.000 title description 8
- 238000000034 method Methods 0.000 title description 6
- 238000010276 construction Methods 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 241000209094 Oryza Species 0.000 description 2
- 235000007164 Oryza sativa Nutrition 0.000 description 2
- 230000004927 fusion Effects 0.000 description 2
- 235000009566 rice Nutrition 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 238000000137 annealing Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229920000136 polysorbate Polymers 0.000 description 1
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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/30—Exhaust heads, chambers, or the like
-
- 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
- Y10T29/49229—Prime mover or fluid pump making
-
- 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
- Y10T29/49826—Assembling or joining
- Y10T29/49888—Subsequently coating
Definitions
- the present invention relates to casing structures, such as the exhaust hood structures of elastic fluid turbines for example, the walls of which are subjected to pressures and stresses tending to deform or strain them, and has for its object to provide an improved method for bracing the walls of such casing structures against pressures and stresses of that character.
- Fig. 1 is an end view, partly in section, of an elastic fluid turbine casing embodying the invention
- Fig. 2 is a detail thereof in section, on an enlarged, scale.
- 5 is the exhaust hood or casing of an elastic fluid turbine having walls 6, 7 and 8 and a central interior web 9 which require bracing against atmosphericpressure and expansion stresses which would tend to deform or strain the cas-,.
- bracing construction is comparatively expensive, particularly in the case of large turbines where the bracing members are numerous.
- bracing for the casing shown is indicated at 19, 11, 12, 13, 14 and 15.
- such bracing comprises two or more telescoping members united by suitable means such as fused metal after the ends of the bracing thus formed are cast in the casing walls.
- the telescoping members are studs 16 which are placed in each end of a hollowtube or third member 17.
- the studs and tubes thus assembled are placed in the mold for the casing, with the studs projecting from the tube into positions wherein they become embedded in the casing walls when the mold is formed. In order to hold more securely, the exposed 1927.
- ends of the studs are preferably corrugated as indicated at 18.
- the opposite ends are freely slidable in the hollow tube.
- the studs and tubes are rigidly united by fusion of metal. In the present example this is done by placing a Weld head 19 at the ends of each tube around the studs. The tubes and studs are then united to form a rigid brace 0r strut at each desired point in the turbine casing.
- the strength of the strut or brace is determined, of course, by the size and thickness of tubing employed which may be of any desired size and thickness to meet the stresses to which the casing is subjected at the points where this bracing is employed.
- This type of strut or brace is particularly well adapted to stiffen the side walls of a steam turbine exhaust hood, such as that shown, against atmospheric pressure or other strains, and being made up of hollow tubing and studs cast in the casing walls with a weld head to unite the parts, is of very simple construction. It is far less costly and easier to manufacture than the usual caststud'or brace which must be machined, drilled, carefully fitted and bolted in place.
- This type of strut or brace has further advantages in that it is easily assembled and may be placed in the mold without regard for alignment of the parts because being telescoping they are automatically aligned when assembled and remain so while assembled, and that finally, such as after the final annealing of the casing for example, it may be set too rigidly and permanently brace the walls by a simple welding operation.
- the invention is not limited to turbine casings, but may be applied to any casing structure requiring bracing against undesirable pressures or stresses tending to cause deformation of the walls thereof.
- the method of providing a brace between walls of a cast casing structure having spaced walls which comprises assembling the brace by inserting studs inthe ends of a a composite brace in assembled relation to hollow tube with the stud ends exposed, casteach other and in a position to permit the ing the exposed ends of the studs of the asends of said brace to become embedded in the Sild brace in said walls, and welding the walls when the mold is poured, pouring the 5 studs to the tube after the casing structurev mold, and as a final operation uniting the 15 has been annealed. parts of the brace by fusion of metal.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
C. S. RICE METHOD OF BRACING CASING STRUCTURES FOR ELASTIC FLUID TURBINES AND THE LIKE Nov. 27, 1928.
Filed June 1927 Ill/Illllllllllll/Ill! w Mar Fig.2..
Inventor: Chescew- 5. Rice,
bg His Attorneg.
Patented Nov. 27, 1928.
UNITED. STATES PATENT OFFICE.
CHESTER S. RICE, 0F SCHENEGTADY, NEW YORK, ASSIGNOR T0 GENERAL ELECTRIC COMPANY, A CORPORATION OF NEW YORK.
nnrnon onnnaome CASING STRUCTURES FOR'ELASTIC- FLUID TURBINES AND THE LIKE.
Application filed June 1,
The present invention relates to casing structures, such as the exhaust hood structures of elastic fluid turbines for example, the walls of which are subjected to pressures and stresses tending to deform or strain them, and has for its object to provide an improved method for bracing the walls of such casing structures against pressures and stresses of that character.
The method of the present invention is particularly applicable in the construction of elastic fluid turbine casings. For this reason the invention will be further described in connection with an elastic fluid turbine casing and for a consideration of what is believed to be novel and the invention, attention is directed to the accompanying drawing, description thereof and the appended claims.
In the drawing, Fig. 1 is an end view, partly in section, of an elastic fluid turbine casing embodying the invention, and Fig. 2 is a detail thereof in section, on an enlarged, scale. Referring to Fig. 1 of the drawing, 5 is the exhaust hood or casing of an elastic fluid turbine having walls 6, 7 and 8 and a central interior web 9 which require bracing against atmosphericpressure and expansion stresses which would tend to deform or strain the cas-,.
ing when the turbine is in operation.
To provide against deformation or strains, such walls are usually'connected or braced by cast members which are machined at the ends and carefully fitted and bolted in place after the casing has been annealed. This type of bracing construction is comparatively expensive, particularly in the case of large turbines where the bracing members are numerous.
In the drawing, the location for suitable bracing for the casing shown is indicated at 19, 11, 12, 13, 14 and 15. According to the invention, such bracing (Fig. 2) comprises two or more telescoping members united by suitable means such as fused metal after the ends of the bracing thus formed are cast in the casing walls. In the present example, the telescoping members are studs 16 which are placed in each end of a hollowtube or third member 17. The studs and tubes thus assembled are placed in the mold for the casing, with the studs projecting from the tube into positions wherein they become embedded in the casing walls when the mold is formed. In order to hold more securely, the exposed 1927. I Serial No.-195,835.
ends of the studs are preferably corrugated as indicated at 18. The opposite ends are freely slidable in the hollow tube.
When the turbine casing is cooling, after being cast or later when being annealed, the studs being movable in the tube, permit the walls to expand and contract properly without restraint. Finally, after the casing is in readiness for having its walls braced and definitely spaced apart, the studs and tubes are rigidly united by fusion of metal. In the present example this is done by placing a Weld head 19 at the ends of each tube around the studs. The tubes and studs are then united to form a rigid brace 0r strut at each desired point in the turbine casing.
- The strength of the strut or brace is determined, of course, by the size and thickness of tubing employed which may be of any desired size and thickness to meet the stresses to which the casing is subjected at the points where this bracing is employed.
This type of strut or brace is particularly well adapted to stiffen the side walls of a steam turbine exhaust hood, such as that shown, against atmospheric pressure or other strains, and being made up of hollow tubing and studs cast in the casing walls with a weld head to unite the parts, is of very simple construction. It is far less costly and easier to manufacture than the usual caststud'or brace which must be machined, drilled, carefully fitted and bolted in place.
This type of strut or brace has further advantages in that it is easily assembled and may be placed in the mold without regard for alignment of the parts because being telescoping they are automatically aligned when assembled and remain so while assembled, and that finally, such as after the final annealing of the casing for example, it may be set too rigidly and permanently brace the walls by a simple welding operation.
From the foregoing description it will be be seen that the invention is not limited to turbine casings, but may be applied to any casing structure requiring bracing against undesirable pressures or stresses tending to cause deformation of the walls thereof.
Vhat I claim as new and desire tosecure by Letters Patent of the United States, is
1. The method of providing a brace between walls of a cast casing structure having spaced walls, which comprises assembling the brace by inserting studs inthe ends of a a composite brace in assembled relation to hollow tube with the stud ends exposed, casteach other and in a position to permit the ing the exposed ends of the studs of the asends of said brace to become embedded in the sembled brace in said walls, and welding the walls when the mold is poured, pouring the 5 studs to the tube after the casing structurev mold, and as a final operation uniting the 15 has been annealed. parts of the brace by fusion of metal.
2. The method of providing a brace be- In witness whereof, I have hereunto set my tween the walls of a cast casing structure, hand this 31st day of May, 1927. which comprises inserting in the mold tele- 10 scoping relatively slidable parts providing CHESTERS. RICE.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US195835A US1693317A (en) | 1927-06-01 | 1927-06-01 | Method of bracing casing structures for elastic fluid turbines and the like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US195835A US1693317A (en) | 1927-06-01 | 1927-06-01 | Method of bracing casing structures for elastic fluid turbines and the like |
Publications (1)
Publication Number | Publication Date |
---|---|
US1693317A true US1693317A (en) | 1928-11-27 |
Family
ID=22723019
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US195835A Expired - Lifetime US1693317A (en) | 1927-06-01 | 1927-06-01 | Method of bracing casing structures for elastic fluid turbines and the like |
Country Status (1)
Country | Link |
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US (1) | US1693317A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2453547A (en) * | 1944-01-28 | 1948-11-09 | United Aircraft Corp | Turbine construction |
US3142354A (en) * | 1960-08-09 | 1964-07-28 | Gutehoffnungshuette Sterkrade | Sound absorption device and method of manufacture |
WO1999002822A1 (en) * | 1997-07-09 | 1999-01-21 | Siemens Aktiengesellschaft | Supporting device for a temperature-exposed channel |
-
1927
- 1927-06-01 US US195835A patent/US1693317A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2453547A (en) * | 1944-01-28 | 1948-11-09 | United Aircraft Corp | Turbine construction |
US3142354A (en) * | 1960-08-09 | 1964-07-28 | Gutehoffnungshuette Sterkrade | Sound absorption device and method of manufacture |
WO1999002822A1 (en) * | 1997-07-09 | 1999-01-21 | Siemens Aktiengesellschaft | Supporting device for a temperature-exposed channel |
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