JPS61163177U - - Google Patents
Info
- Publication number
- JPS61163177U JPS61163177U JP4597485U JP4597485U JPS61163177U JP S61163177 U JPS61163177 U JP S61163177U JP 4597485 U JP4597485 U JP 4597485U JP 4597485 U JP4597485 U JP 4597485U JP S61163177 U JPS61163177 U JP S61163177U
- Authority
- JP
- Japan
- Prior art keywords
- radius
- groove
- blade
- tip
- utility
- 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.)
- Pending
Links
Landscapes
- Percussive Tools And Related Accessories (AREA)
- Milling, Broaching, Filing, Reaming, And Others (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4597485U JPS61163177U (OSRAM) | 1985-03-30 | 1985-03-30 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4597485U JPS61163177U (OSRAM) | 1985-03-30 | 1985-03-30 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS61163177U true JPS61163177U (OSRAM) | 1986-10-09 |
Family
ID=30559947
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4597485U Pending JPS61163177U (OSRAM) | 1985-03-30 | 1985-03-30 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS61163177U (OSRAM) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2013531158A (ja) * | 2010-01-22 | 2013-08-01 | シーメンス エナジー インコーポレイテッド | タービンエンジンの差込み翼の取外し方法および装置 |
-
1985
- 1985-03-30 JP JP4597485U patent/JPS61163177U/ja active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2013531158A (ja) * | 2010-01-22 | 2013-08-01 | シーメンス エナジー インコーポレイテッド | タービンエンジンの差込み翼の取外し方法および装置 |
| US8863365B2 (en) | 2010-01-22 | 2014-10-21 | Siemens Energy, Inc. | Removal of stuck blade in a turbine engine |