GB711717A - Improvements in and relating to multistage axial flow compressors - Google Patents
Improvements in and relating to multistage axial flow compressorsInfo
- Publication number
- GB711717A GB711717A GB318252A GB318252A GB711717A GB 711717 A GB711717 A GB 711717A GB 318252 A GB318252 A GB 318252A GB 318252 A GB318252 A GB 318252A GB 711717 A GB711717 A GB 711717A
- Authority
- GB
- United Kingdom
- Prior art keywords
- axial
- shutters
- compressor
- flow
- path
- 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
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
- F04D29/524—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps shiftable members for obturating part of the flow path
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
711,717. Axial-flow compressors. ENGLISH ELECTRIC CO., Ltd. Feb. 6, 1953 [Feb. 6, 1952], No. 3182/52. Class 110(1) The onset of surging in a multi-stage axial-flow compressor is delayed by influencing the radial distribution of axial velocity at the inlet to the blading. The intake of the compressor is divided into a number of coaxial annular paths by means of one or more surfaces of revolution 5 which may be of sheet metal and preferably extend right up to the first row of blades. Movable shutters 6, 7 and 8 at the entrance to each path can be completely withdrawn from or completely or partly obstruct the respective paths. Alternatively or in addition, shutters 6<SP>1</SP>, 7<SP>1</SP> and 8' may similarly be provided at the exit from each path. The shutters may be constructed similarly to an iris shutter of a photographic camera and may be either solid or formed of partly permeable material, say grids or gauze or both. Compressed air can be introduced downstream into any one or all of the paths through one or more pipes 9 having nozzles 10. The supply to the nozzles 10 of each path is controlled by separate valves. When the compressor forms part of a gas turbine plant, the shutters or valves may be connected with the controls of the plant so as to operate automatically during the starting period. The blades 3. 4 are those of the initial stages of a purely axial-flow compressor or of a combined axial-flow and radial-flow compressor.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB318252A GB711717A (en) | 1952-02-06 | 1952-02-06 | Improvements in and relating to multistage axial flow compressors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB318252A GB711717A (en) | 1952-02-06 | 1952-02-06 | Improvements in and relating to multistage axial flow compressors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB711717A true GB711717A (en) | 1954-07-07 |
Family
ID=9753475
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB318252A Expired GB711717A (en) | 1952-02-06 | 1952-02-06 | Improvements in and relating to multistage axial flow compressors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB711717A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1042828B (en) * | 1955-10-13 | 1958-11-06 | Bristol Aero Engines Ltd | Axial compressor |
US5487643A (en) * | 1994-01-18 | 1996-01-30 | Alliedsignal Inc. | Partial admission axial impulse turbine including cover for turbine wheel rotating assembly |
-
1952
- 1952-02-06 GB GB318252A patent/GB711717A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1042828B (en) * | 1955-10-13 | 1958-11-06 | Bristol Aero Engines Ltd | Axial compressor |
US5487643A (en) * | 1994-01-18 | 1996-01-30 | Alliedsignal Inc. | Partial admission axial impulse turbine including cover for turbine wheel rotating assembly |
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