GB605361A - Improvements in or relating to multi-stage axial flow compressors - Google Patents
Improvements in or relating to multi-stage axial flow compressorsInfo
- Publication number
- GB605361A GB605361A GB34539/45A GB3453945A GB605361A GB 605361 A GB605361 A GB 605361A GB 34539/45 A GB34539/45 A GB 34539/45A GB 3453945 A GB3453945 A GB 3453945A GB 605361 A GB605361 A GB 605361A
- Authority
- GB
- United Kingdom
- Prior art keywords
- axial flow
- relating
- stage axial
- flow compressors
- compressors
- 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
- JHIVVAPYMSGYDF-UHFFFAOYSA-N cyclohexanone Chemical compound O=C1CCCCC1 JHIVVAPYMSGYDF-UHFFFAOYSA-N 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
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/324—Blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
605,361. Axial flow compressors. SULZER FRERES SOC. ANON. Dec. 20, 1945, No. 34539. Convention date, Jan. 19. Drawings to Specification. [Class 110 (i)] In a multi-stage axial flow compressor with at least three running blade rings, the pitch of each rotor blade near the blade root is at least 1.25 times the chord length and the blades are so shaped and positioned that they work in normal service with a coefficient of lift of at least 0.7.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH605361X | 1945-01-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB605361A true GB605361A (en) | 1948-07-21 |
Family
ID=4523021
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB34539/45A Expired GB605361A (en) | 1945-01-19 | 1945-12-20 | Improvements in or relating to multi-stage axial flow compressors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB605361A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5221181A (en) * | 1990-10-24 | 1993-06-22 | Westinghouse Electric Corp. | Stationary turbine blade having diaphragm construction |
ES2063605A2 (en) * | 1990-10-24 | 1995-01-01 | Westinghouse Electric Corp | Stationary blade design for L-OC row |
-
1945
- 1945-12-20 GB GB34539/45A patent/GB605361A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5221181A (en) * | 1990-10-24 | 1993-06-22 | Westinghouse Electric Corp. | Stationary turbine blade having diaphragm construction |
ES2063605A2 (en) * | 1990-10-24 | 1995-01-01 | Westinghouse Electric Corp | Stationary blade design for L-OC row |
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