GB433800A - Improvements in or relating to turbines for expanding gases for the purpose of producing low temperatures - Google Patents
Improvements in or relating to turbines for expanding gases for the purpose of producing low temperaturesInfo
- Publication number
- GB433800A GB433800A GB6846/33A GB684634A GB433800A GB 433800 A GB433800 A GB 433800A GB 6846/33 A GB6846/33 A GB 6846/33A GB 684634 A GB684634 A GB 684634A GB 433800 A GB433800 A GB 433800A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- gases
- turbines
- shaft
- turbine
- 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
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B9/00—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
- F25B9/002—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the refrigerant
- F25B9/004—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the refrigerant the refrigerant being air
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
433,800. Turbines. ZERKOWITZ, G., 8, Giselastrasse, Munich, Germany. March 3, 1934, No. 6846. Convention date, March 24, 1933. [Class 110 (iii)] Gases are expanded through a turbine, doing work, and also for the purpose of cooling the gases which are used in a cooling plant. In the arrangement shown, gases may be admitted through a pipe 2, pass through a nozzle 3, and blade ring 4 to an exhaust 6, or the direction of flow may be reversed. Insulation material 1, 15, surrounds the turbine casing. The turbine shaft 10 supports gearing or a driven machine in a casing 11. Bearings 13, 14, are provided, the rotor 5 being at a considerable distance from the bearing 13. The rotor may be cone-shaped, the blade ring extending beyond the end of the shaft. Several stages of blade rings may be arranged on the rotor. The shaft is constructed of chromium nickel steel, and the rotor and blading of aluminium or an aluminium alloy.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE177365X | 1933-03-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB433800A true GB433800A (en) | 1935-08-21 |
Family
ID=5701793
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB6846/33A Expired GB433800A (en) | 1933-03-24 | 1934-03-03 | Improvements in or relating to turbines for expanding gases for the purpose of producing low temperatures |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB433800A (en) |
-
1934
- 1934-03-03 GB GB6846/33A patent/GB433800A/en not_active Expired
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB516781A (en) | Improvements in gas turbines | |
GB433800A (en) | Improvements in or relating to turbines for expanding gases for the purpose of producing low temperatures | |
GB577017A (en) | Improvements in turbines | |
GB585331A (en) | Improvements in or relating to internal-combustion turbines | |
GB586554A (en) | Improvements in or relating to turbines | |
GB883530A (en) | Improvements in and relating to gas turbine plant | |
GB544909A (en) | High speed propulsion plant | |
GB380315A (en) | Improvements in and relating to power aggregates | |
GB696558A (en) | Stator and rotor cooling means in gas turbines | |
GB432652A (en) | Improved constant pressure gas turbine plant | |
GB529786A (en) | Improvements in or relating to gas turbine installations | |
GB436709A (en) | Improvements in internal combustion turbines | |
GB740944A (en) | Improvements in and relating to thermal turbines | |
GB439773A (en) | Improvements in steam and gas turbines | |
GB585342A (en) | Compound internal-combustion turbine plant | |
GB585509A (en) | Improvements in or relating to power plants | |
GB713647A (en) | Improvements in or relating to water-cooled gas turbines | |
GB634554A (en) | Improvements in and relating to gas turbine plants | |
SU77120A2 (en) | Turbo expander for refrigeration cycle of deep cooling units | |
GB808410A (en) | Improvements in or relating to bearing arrangements for gas turbine engines | |
GB626706A (en) | Improvements in power plant | |
GB536061A (en) | Improvements in or relating to gas turbine installations | |
GB659714A (en) | Improvements in units comprising a gas turbine driving an electric generator | |
GB447945A (en) | Improvements in or relating to steam turbines | |
GB381899A (en) | Improvements in or relating to means for the cooling of the vanes of rotors of rotary gas engines |