GB702265A - Improvements in or relating to multi-stage axial-flow compressors having means to regulate the characteristics thereof - Google Patents
Improvements in or relating to multi-stage axial-flow compressors having means to regulate the characteristics thereofInfo
- Publication number
- GB702265A GB702265A GB1612449A GB1612449A GB702265A GB 702265 A GB702265 A GB 702265A GB 1612449 A GB1612449 A GB 1612449A GB 1612449 A GB1612449 A GB 1612449A GB 702265 A GB702265 A GB 702265A
- Authority
- GB
- United Kingdom
- Prior art keywords
- inlet
- blade
- adjustable
- stator
- duct
- 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
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
702,265. Axial flow compressors. ROLLS ROYCE, Ltd. June 16. 1950 [June 16, 1949], No. 16124/49. Class 110 (1) In a multi-stage axial flow compressor having an annular duct, at least a portion of each stator blade of the inlet row adjacent to the inner duct wall is adjustable so as to permit variation of the ratio of the-swirl velocity to the axial velocity. As shown, Fig. 3, the radially. inner portion 28 of the blades of the inlet blade row of the stator is adjustable about shaft 29. In alternative embodiments (not shown), 28 may be adjusted by means of a spindle projecting radially inwards through the fixed section of the blade supported on the duct outer casing or the blade may be in one piece and subjected to torsion at its inner end. In Fig. 4, the movable parts 27, 28 of the inlet stator blades are respectively movable by shafts 30, 29 which project through the outer and inner duct surfaces. In Fig. 5, the inlet stator blades consist of a fixed part 31 and an adjustable part 32 which is movabte about the diagonal spindle 35.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1612449A GB702265A (en) | 1949-06-16 | 1949-06-16 | Improvements in or relating to multi-stage axial-flow compressors having means to regulate the characteristics thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1612449A GB702265A (en) | 1949-06-16 | 1949-06-16 | Improvements in or relating to multi-stage axial-flow compressors having means to regulate the characteristics thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB702265A true GB702265A (en) | 1954-01-13 |
Family
ID=10071619
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1612449A Expired GB702265A (en) | 1949-06-16 | 1949-06-16 | Improvements in or relating to multi-stage axial-flow compressors having means to regulate the characteristics thereof |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB702265A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2834536A (en) * | 1955-09-29 | 1958-05-13 | Westinghouse Electric Corp | Spin vane controls for fans |
| US5281087A (en) * | 1992-06-10 | 1994-01-25 | General Electric Company | Industrial gas turbine engine with dual panel variable vane assembly |
| WO2010094274A1 (en) * | 2009-02-19 | 2010-08-26 | Mtu Aero Engines Gmbh | Compressor having a guide vane assembly with a radially variable outflow |
| CN114542515A (en) * | 2022-03-08 | 2022-05-27 | 大连海事大学 | A series inlet adjustable guide vane mechanism |
-
1949
- 1949-06-16 GB GB1612449A patent/GB702265A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2834536A (en) * | 1955-09-29 | 1958-05-13 | Westinghouse Electric Corp | Spin vane controls for fans |
| US5281087A (en) * | 1992-06-10 | 1994-01-25 | General Electric Company | Industrial gas turbine engine with dual panel variable vane assembly |
| WO2010094274A1 (en) * | 2009-02-19 | 2010-08-26 | Mtu Aero Engines Gmbh | Compressor having a guide vane assembly with a radially variable outflow |
| CN114542515A (en) * | 2022-03-08 | 2022-05-27 | 大连海事大学 | A series inlet adjustable guide vane mechanism |
| CN114542515B (en) * | 2022-03-08 | 2024-05-03 | 大连海事大学 | Series inlet adjustable guide vane mechanism |
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