CA614179A - Axial flow compressors - Google Patents
Axial flow compressorsInfo
- Publication number
- CA614179A CA614179A CA614179A CA614179DA CA614179A CA 614179 A CA614179 A CA 614179A CA 614179 A CA614179 A CA 614179A CA 614179D A CA614179D A CA 614179DA CA 614179 A CA614179 A CA 614179A
- Authority
- CA
- Canada
- Prior art keywords
- axial flow
- flow compressors
- compressors
- axial
- flow
- 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 |
---|---|---|---|
CA614179T |
Publications (1)
Publication Number | Publication Date |
---|---|
CA614179A true CA614179A (en) | 1961-02-07 |
Family
ID=35856494
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA614179A Expired CA614179A (en) | Axial flow compressors |
Country Status (1)
Country | Link |
---|---|
CA (1) | CA614179A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4053256A (en) * | 1975-09-29 | 1977-10-11 | United Technologies Corporation | Variable camber vane for a gas turbine engine |
-
0
- CA CA614179A patent/CA614179A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4053256A (en) * | 1975-09-29 | 1977-10-11 | United Technologies Corporation | Variable camber vane for a gas turbine engine |
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