CA401686A - Pale en composition d'helice - Google Patents
Pale en composition d'heliceInfo
- Publication number
- CA401686A CA401686A CA401686A CA401686DA CA401686A CA 401686 A CA401686 A CA 401686A CA 401686 A CA401686 A CA 401686A CA 401686D A CA401686D A CA 401686DA CA 401686 A CA401686 A CA 401686A
- Authority
- CA
- Canada
- Prior art keywords
- propeller blade
- composite propeller
- composite
- blade
- propeller
- 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 |
---|---|---|---|
CA401686T |
Publications (1)
Publication Number | Publication Date |
---|---|
CA401686A true CA401686A (fr) | 1941-12-23 |
Family
ID=35412132
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA401686A Expired CA401686A (fr) | Pale en composition d'helice |
Country Status (1)
Country | Link |
---|---|
CA (1) | CA401686A (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2206597A2 (fr) | 2009-01-07 | 2010-07-14 | GE Aviation Systems Limited | Procédé et dispositif pour la fabrication des longerons composites |
-
0
- CA CA401686A patent/CA401686A/fr not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2206597A2 (fr) | 2009-01-07 | 2010-07-14 | GE Aviation Systems Limited | Procédé et dispositif pour la fabrication des longerons composites |
US8061253B2 (en) | 2009-01-07 | 2011-11-22 | Ge Aviation Systems Limited | Composite spars |
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