GB588088A - Improvements in or relating to compressors and turbines - Google Patents
Improvements in or relating to compressors and turbinesInfo
- Publication number
- GB588088A GB588088A GB1224743A GB1224743A GB588088A GB 588088 A GB588088 A GB 588088A GB 1224743 A GB1224743 A GB 1224743A GB 1224743 A GB1224743 A GB 1224743A GB 588088 A GB588088 A GB 588088A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- compressor
- rings
- turbine
- rotor
- 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
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/02—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
- F04D17/04—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal of transverse-flow type
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Wind Motors (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
588,088. Centrifugal pumps; gas turbines. POWER JETS (RESEARCH & DEVELOPMENT), Ltd., and HOWELL, A. R. July 28, 1943, No. 12247. [Classes 110 (i) and 110(iii)] [Also in Group XXXIII] A compressor with radial flow turbine-type blades is arranged for a diametral flow of the fluid being pumped. As shown, there are two rings of rotating blades 1 and segments of guide blades 2, 3. Suitable fairings 9, 12 guide the flow across the centre of the wheel. The rotating blades are of the impulse type and the stator blades of the reaction type. The blades may be mounted on end discs in the Ljungstrom manner and several rotors may be arranged end to end on one shaft. A rotor may have one or any number of rings of rotor blades and oppositely-rotating rotors may be used. One or more rings of rotor and/or stator blades may be used to turn the delivery-into an axial or other direction. The compressor may be used as part of a gas turbine plant and the turbines may be of similar construction. In one case, the H.P. turbine drives the H.P. compressor and the L.P. turbine two L.P. compressors in series. The compressors may be used to provide a stream of fluid for jet-propulsion and may be placed in ducts in nacelles, fuselages or thick wings. The jets may be directed downwards for imparting lift.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1224743A GB588088A (en) | 1943-07-28 | 1943-07-28 | Improvements in or relating to compressors and turbines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1224743A GB588088A (en) | 1943-07-28 | 1943-07-28 | Improvements in or relating to compressors and turbines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB588088A true GB588088A (en) | 1947-05-14 |
Family
ID=10001067
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1224743A Expired GB588088A (en) | 1943-07-28 | 1943-07-28 | Improvements in or relating to compressors and turbines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB588088A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106194827A (en) * | 2016-07-11 | 2016-12-07 | 沈阳航空航天大学 | Improve the birotor blade wheel structure of cross flow fan total pressure efficiency |
| US11326609B2 (en) | 2016-02-29 | 2022-05-10 | Honeywell International Inc. | Cross flow blower |
-
1943
- 1943-07-28 GB GB1224743A patent/GB588088A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11326609B2 (en) | 2016-02-29 | 2022-05-10 | Honeywell International Inc. | Cross flow blower |
| CN106194827A (en) * | 2016-07-11 | 2016-12-07 | 沈阳航空航天大学 | Improve the birotor blade wheel structure of cross flow fan total pressure efficiency |
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