JPS648301A - Tap welding method for stationary blade of turbine - Google Patents
Tap welding method for stationary blade of turbineInfo
- Publication number
- JPS648301A JPS648301A JP15980687A JP15980687A JPS648301A JP S648301 A JPS648301 A JP S648301A JP 15980687 A JP15980687 A JP 15980687A JP 15980687 A JP15980687 A JP 15980687A JP S648301 A JPS648301 A JP S648301A
- Authority
- JP
- Japan
- Prior art keywords
- blocks
- nozzle
- turbine
- stationary blade
- welding
- 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.)
- Granted
Links
- 238000003466 welding Methods 0.000 title abstract 5
- 238000000034 method Methods 0.000 title abstract 3
- 239000011324 bead Substances 0.000 abstract 2
- 238000010008 shearing Methods 0.000 abstract 2
- 238000007599 discharging Methods 0.000 abstract 1
- 238000005553 drilling Methods 0.000 abstract 1
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
PURPOSE:To weld taps without the need of drilling, reaming and preheating by circumferentially welding beads on each of side faces of divided sections of inner ring blocks and outer ring blocks perpendicular to the slits formed between those inner and outer blocks. CONSTITUTION:For operation, after a plurality of nozzle blocks each consisting of a nozzle 1 and inner and outer ring blocks 2 and 3 which tighten said nozzle 1 are arranged circumferentially in circle, the wrapping welding is executed on both faces of each of the nozzle blocks by the electronic beam welding method, whereby assembling a turbine stationary blade 6 in a integral form. Then to incorporate the turbine stationary blade 6 in a turbine, said blade 6 is cut into a plurality of sector blocks along shearing lines 7 parallel to slit lines 8 by the electric discharging method. Marking for this cutting is made before it. Then a bead 10 is formed circumferentially by welding on each of the side faces of the inner and outer ring blocks 2 and 3 perpendicular to the shearing lines 7 or the slit lines 8 between the divided blocks.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15980687A JPH0676763B2 (en) | 1987-06-29 | 1987-06-29 | Turbine vane stopper welding method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15980687A JPH0676763B2 (en) | 1987-06-29 | 1987-06-29 | Turbine vane stopper welding method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS648301A true JPS648301A (en) | 1989-01-12 |
| JPH0676763B2 JPH0676763B2 (en) | 1994-09-28 |
Family
ID=15701666
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP15980687A Expired - Lifetime JPH0676763B2 (en) | 1987-06-29 | 1987-06-29 | Turbine vane stopper welding method |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0676763B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPWO2016103340A1 (en) * | 2014-12-24 | 2017-11-02 | 三菱重工コンプレッサ株式会社 | Nozzle structure and rotating machine |
-
1987
- 1987-06-29 JP JP15980687A patent/JPH0676763B2/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPWO2016103340A1 (en) * | 2014-12-24 | 2017-11-02 | 三菱重工コンプレッサ株式会社 | Nozzle structure and rotating machine |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0676763B2 (en) | 1994-09-28 |
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