GB702773A - Improvements in and relating to corner vane elements for example for diffusers in radial flow compressors - Google Patents
Improvements in and relating to corner vane elements for example for diffusers in radial flow compressorsInfo
- Publication number
- GB702773A GB702773A GB1049751A GB1049751A GB702773A GB 702773 A GB702773 A GB 702773A GB 1049751 A GB1049751 A GB 1049751A GB 1049751 A GB1049751 A GB 1049751A GB 702773 A GB702773 A GB 702773A
- Authority
- GB
- United Kingdom
- Prior art keywords
- corner
- corner vane
- diffuser
- duct
- diffusers
- 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
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/441—Fluid-guiding means, e.g. diffusers especially 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
702,773. Radial-flow compressors. ENGLISH ELECTRIC CO., Ltd. April 25, 1952 [May 4, 1951], No. 10497/51: Class 110 (1) A corner vane element for the connection of two channels (for example, one of the diffuser channels 2, Fig. 1, of a radial-flow compressor and one of the diffuser trumpets 7) including an angle with one another comprises a cylindrical body 4 having its axis in alignment with the trumpet 7, a port in its circumference linking up with the channel 2, and an angular duct in its interior leading from the port into the axial direction, one or more corner vanes 6 being arranged within the duct so as to form a cascade. Each body 4 is fitted into a cylindrical recess 3 machined into the wall 1 of the diffuser, being restrained from turning by a dowel pin 5. To give access to the angular duct and corner vane 6, each body 4 is split parallel to its axis, preferably, as shown in Fig. 2 (which is a section along line II-II of Fig. 1) at one end of the corner vane 6, the two parts of the body being secured together by bolts 8.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1049751A GB702773A (en) | 1951-05-04 | 1951-05-04 | Improvements in and relating to corner vane elements for example for diffusers in radial flow compressors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1049751A GB702773A (en) | 1951-05-04 | 1951-05-04 | Improvements in and relating to corner vane elements for example for diffusers in radial flow compressors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB702773A true GB702773A (en) | 1954-01-20 |
Family
ID=9968933
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1049751A Expired GB702773A (en) | 1951-05-04 | 1951-05-04 | Improvements in and relating to corner vane elements for example for diffusers in radial flow compressors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB702773A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2192229A (en) * | 1986-07-04 | 1988-01-06 | Rolls Royce Plc | A compressor and air bleed system |
WO2003042545A1 (en) * | 2001-11-12 | 2003-05-22 | Fläkt Woods AB | High-pressure fan |
US20170114797A1 (en) * | 2015-10-27 | 2017-04-27 | Pratt & Whitney Canada Corp. | Diffuser pipe with splitter vane |
US11187243B2 (en) | 2015-10-08 | 2021-11-30 | Rolls-Royce Deutschland Ltd & Co Kg | Diffusor for a radial compressor, radial compressor and turbo engine with radial compressor |
US11286952B2 (en) | 2020-07-14 | 2022-03-29 | Rolls-Royce Corporation | Diffusion system configured for use with centrifugal compressor |
US11441516B2 (en) | 2020-07-14 | 2022-09-13 | Rolls-Royce North American Technologies Inc. | Centrifugal compressor assembly for a gas turbine engine with deswirler having sealing features |
US11578654B2 (en) | 2020-07-29 | 2023-02-14 | Rolls-Royce North American Technologies Inc. | Centrifical compressor assembly for a gas turbine engine |
-
1951
- 1951-05-04 GB GB1049751A patent/GB702773A/en not_active Expired
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2192229A (en) * | 1986-07-04 | 1988-01-06 | Rolls Royce Plc | A compressor and air bleed system |
US4844689A (en) * | 1986-07-04 | 1989-07-04 | Rolls-Royce Plc | Compressor and air bleed system |
GB2192229B (en) * | 1986-07-04 | 1990-05-02 | Rolls Royce Plc | A compressor and air bleed system |
WO2003042545A1 (en) * | 2001-11-12 | 2003-05-22 | Fläkt Woods AB | High-pressure fan |
US7125219B2 (en) | 2001-11-12 | 2006-10-24 | Flakt Woods Ab | High-pressure fan |
US11187243B2 (en) | 2015-10-08 | 2021-11-30 | Rolls-Royce Deutschland Ltd & Co Kg | Diffusor for a radial compressor, radial compressor and turbo engine with radial compressor |
US10570925B2 (en) * | 2015-10-27 | 2020-02-25 | Pratt & Whitney Canada Corp. | Diffuser pipe with splitter vane |
US20170114797A1 (en) * | 2015-10-27 | 2017-04-27 | Pratt & Whitney Canada Corp. | Diffuser pipe with splitter vane |
US11215196B2 (en) | 2015-10-27 | 2022-01-04 | Pratt & Whitney Canada Corp. | Diffuser pipe with splitter vane |
US11286952B2 (en) | 2020-07-14 | 2022-03-29 | Rolls-Royce Corporation | Diffusion system configured for use with centrifugal compressor |
US11441516B2 (en) | 2020-07-14 | 2022-09-13 | Rolls-Royce North American Technologies Inc. | Centrifugal compressor assembly for a gas turbine engine with deswirler having sealing features |
US11815047B2 (en) | 2020-07-14 | 2023-11-14 | Rolls-Royce North American Technologies Inc. | Centrifugal compressor assembly for a gas turbine engine with deswirler having sealing features |
US11578654B2 (en) | 2020-07-29 | 2023-02-14 | Rolls-Royce North American Technologies Inc. | Centrifical compressor assembly for a gas turbine engine |
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