GB615219A - Improvements relating to rotary power conversion machines - Google Patents
Improvements relating to rotary power conversion machinesInfo
- Publication number
- GB615219A GB615219A GB3383645A GB3383645A GB615219A GB 615219 A GB615219 A GB 615219A GB 3383645 A GB3383645 A GB 3383645A GB 3383645 A GB3383645 A GB 3383645A GB 615219 A GB615219 A GB 615219A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- relative
- blades
- stage according
- power conversion
- 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
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage pumps
- F04D19/022—Multi-stage pumps with concentric rows of vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D21/00—Pump involving supersonic speed of pumped fluids
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
615,219. Air compressors. POWER JETS (RESEARCH & DEVELOPMENT), Ltd., and DAVIDSON, 1. M. Dec. 13, 1945, No. 33836. Drawings to Specification. [Class 110 (i)] In an axial or radial flow bladed compressor the gas enters the rotor with supersonic velocity relative to the rotor blades causing a compression shock system which rotates with the rotor. The leading edge of each blade has its trailing surface substantially in the line of the relative velocity and its leading surface at an angle sufficient to set up a shock system, but not so great as to cause the shock waves to form up-stream in the stator passages. Preferably, the gas velocity relative to the stator blades and that relative to the rotor blades at outlet are sub-sonic. The blades may have a bi-convex profile. A stage according to the invention may be compounded with ordinary stages, and, with oppositely-running rotors. There may be more than one stage according to the invention. Reference has been directed by the Comptroller to Specification 622,049.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3383645A GB615219A (en) | 1945-12-13 | 1945-12-13 | Improvements relating to rotary power conversion machines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3383645A GB615219A (en) | 1945-12-13 | 1945-12-13 | Improvements relating to rotary power conversion machines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB615219A true GB615219A (en) | 1949-01-04 |
Family
ID=10358078
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3383645A Expired GB615219A (en) | 1945-12-13 | 1945-12-13 | Improvements relating to rotary power conversion machines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB615219A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2805818A (en) * | 1951-12-13 | 1957-09-10 | Ferri Antonio | Stator for axial flow compressor with supersonic velocity at entrance |
US3804335A (en) * | 1973-05-21 | 1974-04-16 | J Sohre | Vaneless supersonic nozzle |
USRE29128E (en) * | 1973-05-21 | 1977-02-01 | Vaneless supersonic nozzle |
-
1945
- 1945-12-13 GB GB3383645A patent/GB615219A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2805818A (en) * | 1951-12-13 | 1957-09-10 | Ferri Antonio | Stator for axial flow compressor with supersonic velocity at entrance |
US3804335A (en) * | 1973-05-21 | 1974-04-16 | J Sohre | Vaneless supersonic nozzle |
USRE29128E (en) * | 1973-05-21 | 1977-02-01 | Vaneless supersonic nozzle |
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