GB990543A - Improvements in or relating to high-pressure axial-flow machines such as compressorsand turbines - Google Patents
Improvements in or relating to high-pressure axial-flow machines such as compressorsand turbinesInfo
- Publication number
- GB990543A GB990543A GB2564361A GB2564361A GB990543A GB 990543 A GB990543 A GB 990543A GB 2564361 A GB2564361 A GB 2564361A GB 2564361 A GB2564361 A GB 2564361A GB 990543 A GB990543 A GB 990543A
- Authority
- GB
- United Kingdom
- Prior art keywords
- welded
- spherical
- housing
- blade carrier
- ring
- 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
Links
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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/26—Double casings; Measures against temperature strain in casings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
990,543. Axial-flow compressors and turbines. ESCHER WYSS A.G. July 14, 1961 [July 20, 1960], No. 25643/61. Headings F1C and F1T. A high-pressure axial-flow machine comprises a welded sheet-metal housing of spherical form and a guide-blade carrier mounted within the housing and connected to the latter by an annular partition which divides the housing cavity into an inlet chamber and and outlet chamber. In the compressor shown, a spherical housing is split on a horizontal plane into two sheet-metal hemispheres 2, 3 and 4, 5 which are bolted together at flanges provided at the horizontal plane. A cylindrical guide blade carrier 11 is supported at its discharge end by means of a ring 14 welded to a conical partition 12, the latter being welded to a reinforcing ring 13 which is welded to the spherical portions 2, 3, 4, 5. The guide blade carrier 11 and the conical partition 14 are each in two halves, bolted together at flanges 29 or 30. At its inlet end, the guide blade carrier 11 is carried by a ring 22 attached to the spherical housing by ribs 21. A conical member 16 welded to the ring 14 co-operates with a conical member 15 to form a diffuser discharging into an outlet chamber 24, the latter being separated from an inlet chamber 23 by the partition 12. The spherical portions 3, 5 may be of different radius from the spherical portions 2, 4. The invention may be applied to a turbine.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH830460A CH379838A (en) | 1960-07-20 | 1960-07-20 | Axial flow machine for high pressure |
Publications (1)
Publication Number | Publication Date |
---|---|
GB990543A true GB990543A (en) | 1965-04-28 |
Family
ID=4338253
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2564361A Expired GB990543A (en) | 1960-07-20 | 1961-07-14 | Improvements in or relating to high-pressure axial-flow machines such as compressorsand turbines |
Country Status (2)
Country | Link |
---|---|
CH (1) | CH379838A (en) |
GB (1) | GB990543A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3773431A (en) * | 1970-12-08 | 1973-11-20 | Bbc Brown Boveri & Cie | Multiple shell turbine casing for high pressures and high temperatures |
WO2010012252A2 (en) * | 2008-07-30 | 2010-02-04 | Man Turbo Ag | Continuous flow machine, method and module system for production of a continuous flow machine such as this |
-
1960
- 1960-07-20 CH CH830460A patent/CH379838A/en unknown
-
1961
- 1961-07-14 GB GB2564361A patent/GB990543A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3773431A (en) * | 1970-12-08 | 1973-11-20 | Bbc Brown Boveri & Cie | Multiple shell turbine casing for high pressures and high temperatures |
WO2010012252A2 (en) * | 2008-07-30 | 2010-02-04 | Man Turbo Ag | Continuous flow machine, method and module system for production of a continuous flow machine such as this |
DE102008035427A1 (en) * | 2008-07-30 | 2010-02-04 | Man Turbo Ag | Turbomachine, method and modular system for producing such a turbomachine |
WO2010012252A3 (en) * | 2008-07-30 | 2011-02-24 | Man Diesel & Turbo Se | Continuous flow machine, method and module system for production of a continuous flow machine such as this |
Also Published As
Publication number | Publication date |
---|---|
CH379838A (en) | 1964-07-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB700012A (en) | Improvements in the mounting and fixing of the fixed blades of axial flow turbines and compressors | |
GB1240568A (en) | Outlet housing of an axial-flow turbomachine | |
GB589541A (en) | Improvements in axial flow turbines, compressors and the like | |
US2925954A (en) | Compressor group with intercooler | |
GB626044A (en) | Improvements in or relating to gas turbine power plants | |
GB608514A (en) | Improvements in or relating to drum structures | |
GB604121A (en) | Improvements in diffusers for centrifugal type compressors and pumps | |
GB695212A (en) | Improvements in discharge casing for axial-flow machines, especially compressors andturbines | |
GB990543A (en) | Improvements in or relating to high-pressure axial-flow machines such as compressorsand turbines | |
GB621551A (en) | Improvements in or relating to axial-flow compressors and turbines | |
GB891278A (en) | A gas turbine power unit | |
GB1107050A (en) | Improvements relating to multi-stage centrifugal pumps | |
GB897907A (en) | Hydraulic machines for hydraulic storage power stations | |
GB815032A (en) | Improvements in or relating to multi-stage axial-flow turbines and compressors | |
GB844020A (en) | Stator vane assemblies for axial-flow compressors and turbines | |
GB711528A (en) | Elastic fluid turbine plant | |
GB268677A (en) | Improvements in and relating to turbine pumps and the like | |
US3265290A (en) | Axial flow compressors for jet engines | |
GB780240A (en) | Improvements in or relating to the construction of axial flow turbines or compressors | |
GB981476A (en) | Gas turbine engine vane assembly | |
GB989581A (en) | High power steam turbine | |
JPS5793607A (en) | Guide for fluid inlet port | |
US3110437A (en) | High-pressure axial flow machine | |
GB1009619A (en) | Improvements relating to compressors and turbines | |
GB606526A (en) | Improvements in or relating to means for supporting gas-turbine power-plants |