GB613780A - Improvements in turbines - Google Patents
Improvements in turbinesInfo
- Publication number
- GB613780A GB613780A GB19803/46A GB1980346A GB613780A GB 613780 A GB613780 A GB 613780A GB 19803/46 A GB19803/46 A GB 19803/46A GB 1980346 A GB1980346 A GB 1980346A GB 613780 A GB613780 A GB 613780A
- Authority
- GB
- United Kingdom
- Prior art keywords
- nozzle
- members
- lugs
- turbines
- inlet
- 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
- F01D25/246—Fastening of diaphragms or stator-rings
-
- 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
- F01D1/04—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 traversed by the working-fluid substantially axially
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/025—Fixing blade carrying members on shafts
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
613,780. Turbines. TYE, W. D., MacPHAIL, D. C., and DAVIES, D. I. T. P. LLEWELYN-. July 2, 1946, No. 19803. [Class 110 (iii)] A turbine stator comprises an end inlet member 1, an end outlet member 8 and intervening nozzle members 21 and casing members 12. The members have spigot-and-socket engagements and are clamped together by bolts 10. The member 8 has a number of radial lugs 9 and an exhaust deflecting member 16 fits over the lugs and is secured in place by screws 18. Bearings 19, 26 for the rotor are' provided in the first nozzle member and the exhaust deflecting member. The bladed wheels 23 are splined upon the shaft 20. The final nozzle member has a full circle of nozzle passages: the others have nozzle passages over segments that increase from the inlet end. A conical guide member 27 covers the bearing 26.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB19803/46A GB613780A (en) | 1946-07-02 | 1946-07-02 | Improvements in turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB19803/46A GB613780A (en) | 1946-07-02 | 1946-07-02 | Improvements in turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB613780A true GB613780A (en) | 1948-12-02 |
Family
ID=10135481
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB19803/46A Expired GB613780A (en) | 1946-07-02 | 1946-07-02 | Improvements in turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB613780A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011102852A1 (en) * | 2010-02-18 | 2011-08-25 | Thermal Power Technology Llc | Gas turbine and thermodynamic power generation system |
WO2010096540A3 (en) * | 2009-02-20 | 2011-11-24 | Thermal Power Technology Llc | Gas turbine and thermodynamic power generation system |
US8522552B2 (en) | 2009-02-20 | 2013-09-03 | American Thermal Power, Llc | Thermodynamic power generation system |
-
1946
- 1946-07-02 GB GB19803/46A patent/GB613780A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010096540A3 (en) * | 2009-02-20 | 2011-11-24 | Thermal Power Technology Llc | Gas turbine and thermodynamic power generation system |
US8522552B2 (en) | 2009-02-20 | 2013-09-03 | American Thermal Power, Llc | Thermodynamic power generation system |
WO2011102852A1 (en) * | 2010-02-18 | 2011-08-25 | Thermal Power Technology Llc | Gas turbine and thermodynamic power generation system |
CN102869855A (en) * | 2010-02-18 | 2013-01-09 | 热力技术有限责任公司 | Gas turbine and thermodynamic power generation system |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB803137A (en) | Improvements in or relating to axial-flow fluid machines for example turbines and compressors of gas-turbine engines | |
GB692524A (en) | Improvements in rotors for turbines or compressors | |
US3620020A (en) | Gas turbine engine | |
GB613780A (en) | Improvements in turbines | |
GB1318167A (en) | Inlet structure for turbo machine | |
GB891278A (en) | A gas turbine power unit | |
GB693727A (en) | Improvements relating to bladed rotary fluid-flow machines | |
GB927207A (en) | Improvements in gas turbine units | |
GB577017A (en) | Improvements in turbines | |
GB380067A (en) | Improvements in and relating to the cooling of electrical machines | |
GB631163A (en) | Improvements in or relating to turbine and like rotors | |
GB197914A (en) | Improvements in or relating to turbine-driven blowers | |
GB864545A (en) | An engine super-charger unit | |
GB586551A (en) | Improvements in or relating to internal combustion power turbine plant for propulsion in air | |
GB618193A (en) | Improvements relating to elastic fluid turbines | |
GB820337A (en) | Improvements in and relating to gas turbines | |
GB635270A (en) | Improvements in or relating to centrifugal pumps and compressors | |
GB775548A (en) | Vane wheel blower or pump plant | |
GB599829A (en) | Improvements relating to the construction of turbine rotors | |
GB839622A (en) | Improvements in centrifuges | |
GB680040A (en) | Improvements in or relating to blade supporting rings for preliminary rotor blades of blowers and compressors | |
GB595011A (en) | Improvements in or relating to blowers | |
GB586555A (en) | Improvements in internal combustion gas turbine plant, supercharger plant, air conditioning plant and the like | |
GB622411A (en) | Improvements relating to gas-turbine-engines | |
GB647400A (en) | Improvements in or relating to guide means for impellers for centrifugal pumps or blowers |