GB567368A - Improvements in or relating to rotary compressors - Google Patents
Improvements in or relating to rotary compressorsInfo
- Publication number
- GB567368A GB567368A GB2692/43A GB269243A GB567368A GB 567368 A GB567368 A GB 567368A GB 2692/43 A GB2692/43 A GB 2692/43A GB 269243 A GB269243 A GB 269243A GB 567368 A GB567368 A GB 567368A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- feb
- sound
- relating
- velocity
- 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
- 230000006835 compression Effects 0.000 abstract 1
- 238000007906 compression Methods 0.000 abstract 1
- JHIVVAPYMSGYDF-UHFFFAOYSA-N cyclohexanone Chemical compound O=C1CCCCC1 JHIVVAPYMSGYDF-UHFFFAOYSA-N 0.000 abstract 1
- 239000012530 fluid Substances 0.000 abstract 1
- 230000002093 peripheral effect Effects 0.000 abstract 1
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
- 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
567,368. Centrifugal compressors. SULZER FRERES SOC. ANON. Feb. 18, 1943, No. 2692. Convention date, Feb. 21, 1942. [Class 110 (i)] In a high-pressure compressor, in which the peripheral speed of the rotor 1 exceeds the speed of sound, the blades 2 are curved in the form of a helix in the direction opposite to the direction of flow, so that the absolute velocity of the compressed fluid at the outlet does not exceed the velocity of sound to such an extent that pressure waves are formed. A compression ratio of at least 2 may be reached in a single-stage machine.. Short blades may be arranged between the blades 2, or the blades 2 may be discontinuous and staggered to prevent turbulence.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH567368X | 1942-02-21 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB567368A true GB567368A (en) | 1945-02-12 |
Family
ID=4520674
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2692/43A Expired GB567368A (en) | 1942-02-21 | 1943-02-18 | Improvements in or relating to rotary compressors |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB567368A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1706644A2 (en) * | 2003-12-05 | 2006-10-04 | Argo-Tech Corporation | High performance inducer |
-
1943
- 1943-02-18 GB GB2692/43A patent/GB567368A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1706644A2 (en) * | 2003-12-05 | 2006-10-04 | Argo-Tech Corporation | High performance inducer |
| US7455497B2 (en) * | 2003-12-05 | 2008-11-25 | Carter Cryogenics Company, Llc | High performance inducer |
| EP1706644A4 (en) * | 2003-12-05 | 2009-12-09 | Carter Cryogenics Company Llc | High performance inducer |
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