CA594523A - Multi-stage axial-flow compressors - Google Patents
Multi-stage axial-flow compressorsInfo
- Publication number
- CA594523A CA594523A CA594523A CA594523DA CA594523A CA 594523 A CA594523 A CA 594523A CA 594523 A CA594523 A CA 594523A CA 594523D A CA594523D A CA 594523DA CA 594523 A CA594523 A CA 594523A
- Authority
- CA
- Canada
- Prior art keywords
- stage axial
- flow compressors
- compressors
- flow
- axial
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA594523T |
Publications (1)
Publication Number | Publication Date |
---|---|
CA594523A true CA594523A (en) | 1960-03-15 |
Family
ID=35808050
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA594523A Expired CA594523A (en) | Multi-stage axial-flow compressors |
Country Status (1)
Country | Link |
---|---|
CA (1) | CA594523A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5486091A (en) * | 1994-04-19 | 1996-01-23 | United Technologies Corporation | Gas turbine airfoil clocking |
-
0
- CA CA594523A patent/CA594523A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5486091A (en) * | 1994-04-19 | 1996-01-23 | United Technologies Corporation | Gas turbine airfoil clocking |
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