GB1271807A - Improvements in and relating to an adjustable stator blade assembly for a rotary fluid-flow machine - Google Patents
Improvements in and relating to an adjustable stator blade assembly for a rotary fluid-flow machineInfo
- Publication number
- GB1271807A GB1271807A GB5714069A GB5714069A GB1271807A GB 1271807 A GB1271807 A GB 1271807A GB 5714069 A GB5714069 A GB 5714069A GB 5714069 A GB5714069 A GB 5714069A GB 1271807 A GB1271807 A GB 1271807A
- Authority
- GB
- United Kingdom
- Prior art keywords
- adjustable
- housing
- blades
- ring
- blade assembly
- 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
1,271,807. Centrifugal and axial-How fans. SOC ANON DES ETABS NEU. Nov. 21, 1969 [Nov. 21, 1968], No. 57140/69. Heading F1C. In an adjustable stator blade assembly for creating pre-whirl of the inflow into a rotary fluid-flow machine, e.g. a centrifugal or axialflow fan, the stator blades (6), Fig. 2 (not shown), are each pivotally supported by a respective bearing (4) in a cylindrical housing 1 via a shaft 5, Fig. 1, rigidly attached to the blade and connected to a respective cam member 8, located in an arcuate slot 7 formed in, or in a member carried by, a rotatable and axially slidable ring 3. Thus, angular adjustment of the blades is achieved by rotating the ring 3 about the housing 1 as by a lever (9), Fig. 3 (not shown), rigidly attached to one of the shafts and pivoted on a pin 11. The blades may be arranged to fully close the flow passage through housing 1 when in their coplanar position, and to be angularly adjustable in either direction from that position. Alternatively, they may be adjustable in either direction from a fully open position, or be adjustable between fully closed and fully open positions. The ring 3 may be in surface-tosurface contact with housing 1 or mounted thereon via ball, roller or needle elements. The cam member 8 may be rigid or formed of resilient material or made up of a number of relativelymovable sections.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR59019226 | 1968-11-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1271807A true GB1271807A (en) | 1972-04-26 |
Family
ID=9693861
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5714069A Expired GB1271807A (en) | 1968-11-21 | 1969-11-21 | Improvements in and relating to an adjustable stator blade assembly for a rotary fluid-flow machine |
Country Status (4)
Country | Link |
---|---|
BE (1) | BE738155A (en) |
DE (1) | DE1957298A1 (en) |
FR (1) | FR1592922A (en) |
GB (1) | GB1271807A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2410066A (en) * | 2004-01-13 | 2005-07-20 | Rolls Royce Plc | A stator vane arrangement |
JP2017501334A (en) * | 2013-12-19 | 2017-01-12 | スネクマ | Turbine engine compressors, especially aircraft turboprops or turbofans |
GB2513435B (en) * | 2012-12-21 | 2019-11-13 | Elta Group Africa Pty Ltd | Downstream variable guide vanes for a fan |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE854652A (en) * | 1977-05-16 | 1977-11-16 | Acec | IMPROVEMENTS IN THE CONSTRUCTION OF GAS TURBINES |
-
1968
- 1968-11-21 FR FR1592922D patent/FR1592922A/fr not_active Expired
-
1969
- 1969-08-29 BE BE738155D patent/BE738155A/xx unknown
- 1969-11-14 DE DE19691957298 patent/DE1957298A1/en active Pending
- 1969-11-21 GB GB5714069A patent/GB1271807A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2410066A (en) * | 2004-01-13 | 2005-07-20 | Rolls Royce Plc | A stator vane arrangement |
GB2513435B (en) * | 2012-12-21 | 2019-11-13 | Elta Group Africa Pty Ltd | Downstream variable guide vanes for a fan |
JP2017501334A (en) * | 2013-12-19 | 2017-01-12 | スネクマ | Turbine engine compressors, especially aircraft turboprops or turbofans |
Also Published As
Publication number | Publication date |
---|---|
FR1592922A (en) | 1970-05-19 |
DE1957298A1 (en) | 1970-12-03 |
BE738155A (en) | 1970-02-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |