CA482528A - Structure de pourtour de rotor - Google Patents
Structure de pourtour de rotorInfo
- Publication number
- CA482528A CA482528A CA482528A CA482528DA CA482528A CA 482528 A CA482528 A CA 482528A CA 482528 A CA482528 A CA 482528A CA 482528D A CA482528D A CA 482528DA CA 482528 A CA482528 A CA 482528A
- Authority
- CA
- Canada
- Prior art keywords
- rotor rim
- rim construction
- construction
- rotor
- rim
- 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 |
|---|---|---|---|
| CA482528T |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA482528A true CA482528A (fr) | 1952-04-15 |
Family
ID=35622219
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA482528A Expired CA482528A (fr) | Structure de pourtour de rotor |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA482528A (fr) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5071313A (en) * | 1990-01-16 | 1991-12-10 | General Electric Company | Rotor blade shroud segment |
| US7229245B2 (en) * | 2004-07-14 | 2007-06-12 | Power Systems Mfg., Llc | Vane platform rail configuration for reduced airfoil stress |
-
0
- CA CA482528A patent/CA482528A/fr not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5071313A (en) * | 1990-01-16 | 1991-12-10 | General Electric Company | Rotor blade shroud segment |
| US7229245B2 (en) * | 2004-07-14 | 2007-06-12 | Power Systems Mfg., Llc | Vane platform rail configuration for reduced airfoil stress |
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