GB704936A - Improvements in or relating to multi-stage axial-flow compressors - Google Patents
Improvements in or relating to multi-stage axial-flow compressorsInfo
- Publication number
- GB704936A GB704936A GB2183252A GB2183252A GB704936A GB 704936 A GB704936 A GB 704936A GB 2183252 A GB2183252 A GB 2183252A GB 2183252 A GB2183252 A GB 2183252A GB 704936 A GB704936 A GB 704936A
- Authority
- GB
- United Kingdom
- Prior art keywords
- compressor
- drawings
- relating
- flow compressors
- oct
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0246—Surge control by varying geometry within the pumps, e.g. by adjusting vanes
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
Abstract
704,936. Axial-flow compressors; gas turbine plant. ROLLS-ROYCE, Ltd. Oct. 16, 1950 [Oct. 28, 1949], No. 21832/52. Divided out of 704,849. Drawings to Specification. Classes 110 (1) and 110 (3) In a muiti-stage compressor having at least one row of adjustable stator blades, means are provided to be operative over part only of the range of rotational speeds of the compressor, for automatically and progressively varying the pitch of said blades in a manner corresponding to the rotational speed of the compressor. Specifications 652,095 and 704,849 are referred to. The drawings and description, which relate to a compressor supplying combustion air to a gas turbine, are identical with Figs. 1 and 2 of the drawings in the latter Specification and the description relating thereto.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2183252A GB704936A (en) | 1949-10-28 | 1949-10-28 | Improvements in or relating to multi-stage axial-flow compressors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2183252A GB704936A (en) | 1949-10-28 | 1949-10-28 | Improvements in or relating to multi-stage axial-flow compressors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB704936A true GB704936A (en) | 1954-03-03 |
Family
ID=10169560
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2183252A Expired GB704936A (en) | 1949-10-28 | 1949-10-28 | Improvements in or relating to multi-stage axial-flow compressors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB704936A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2888809A (en) * | 1955-01-27 | 1959-06-02 | Carrier Corp | Gas compression apparatus |
DE1102493B (en) * | 1957-12-30 | 1961-03-16 | Rolls Royce | Dual-circuit gas turbine jet engine |
DE1140029B (en) * | 1959-07-06 | 1962-11-22 | Gen Electric | Control device for a turbo jet engine with compressor guide vanes |
-
1949
- 1949-10-28 GB GB2183252A patent/GB704936A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2888809A (en) * | 1955-01-27 | 1959-06-02 | Carrier Corp | Gas compression apparatus |
DE1102493B (en) * | 1957-12-30 | 1961-03-16 | Rolls Royce | Dual-circuit gas turbine jet engine |
DE1140029B (en) * | 1959-07-06 | 1962-11-22 | Gen Electric | Control device for a turbo jet engine with compressor guide vanes |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1357713A (en) | Cooled rotor blades for gas turbines | |
GB790836A (en) | Improvements in or relating to gas-turbine engine cooling arrangements | |
IL37791A (en) | Turbine blade tip cooling air expander | |
GB1099677A (en) | Improvements in axial-flow turbines and compressors | |
GB1151177A (en) | Improvements in and relating to Gas Turbine Engines | |
GB689353A (en) | Improvements in centrifugal compressors | |
GB1325716A (en) | Metallurgical furnace plants incorporating a compressor driven by a furnace-gas-powered turbine | |
GB1419381A (en) | Fan for gas turbine engines | |
GB695519A (en) | Wind turbines | |
GB621551A (en) | Improvements in or relating to axial-flow compressors and turbines | |
GB704936A (en) | Improvements in or relating to multi-stage axial-flow compressors | |
GB1450133A (en) | Cooling of gas turbine engines | |
GB742288A (en) | Improvements in the cooling of turbines | |
GB609322A (en) | Improvements relating to axial-flow compressors and like machines, and blading thereof | |
GB834800A (en) | Turbine-driven fans | |
GB704856A (en) | Improvements relating to air compressors | |
GB1072145A (en) | Fluid flow machine for exampls a gas turbine engine or lift fan | |
GB586573A (en) | Improvements in or relating to internal combustion turbine plant | |
GB1070130A (en) | Aeofoil shaped blade for a fluid flow machine such as a gas turbine engine | |
GB913620A (en) | Improvements in or relating to axial-flow compressors | |
GB1223999A (en) | Gas turbine engine | |
GB640969A (en) | Improvements in compressor and turbine rotors | |
GB1179064A (en) | Gas turbine power plant. | |
GB1387639A (en) | Turbine blade cooling | |
GB596510A (en) | Improvements relating to screw fans |