SU1524592A1 - COOLED GAS TURBINE BLADE - Google Patents
COOLED GAS TURBINE BLADEInfo
- Publication number
- SU1524592A1 SU1524592A1 SU4411232/06A SU4411232A SU1524592A1 SU 1524592 A1 SU1524592 A1 SU 1524592A1 SU 4411232/06 A SU4411232/06 A SU 4411232/06A SU 4411232 A SU4411232 A SU 4411232A SU 1524592 A1 SU1524592 A1 SU 1524592A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- gas turbine
- insert
- blade
- turbine blade
- cooled gas
- Prior art date
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 210000003746 feather Anatomy 0.000 abstract 2
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
1. Охлаждаемая лопатка газовой турбины, содержащая полое перо, в зоне входной кромки которого в продольном пазу расположена вставка из материала, отличного от материала лопатки, отличающаяся тем, что, с целью повышения надежности, перо снабжено поперечными выступами, размещенными в пазу пара, а вставка выполнена составной из нескольких элементов, каждый из которых со стороны полости пера имеет хвостовик с наклонными боковыми поверхностями, контактирующими с выступами.2. Лопатка по п.1, отличающаяся тем, что каждый выступ снабжен по крайней мере одним поперечным ребром, а хвостовик - ответной канавкой.3. Лопатка по пп.1 и 2, отличающаяся тем, что внешняя поверхность вставки наклонена к оси турбины под углом, не превышающим 90°.1. The cooled blade of the gas turbine, containing a hollow feather, in the zone of the input edge of which in the longitudinal groove is an insert made of a material different from the material of the blade, characterized in that, in order to improve reliability, the feather is provided with transverse projections placed in the steam groove the insert is made up of several elements, each of which, from the side of the pen cavity, has a shank with inclined side surfaces in contact with the protrusions. A blade according to claim 1, characterized in that each protrusion is provided with at least one transverse edge, and the shank is provided with a reciprocal groove. The blade according to claims 1 and 2, characterized in that the outer surface of the insert is inclined to the axis of the turbine at an angle not exceeding 90 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU4411232/06A SU1524592A1 (en) | 1988-04-18 | 1988-04-18 | COOLED GAS TURBINE BLADE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU4411232/06A SU1524592A1 (en) | 1988-04-18 | 1988-04-18 | COOLED GAS TURBINE BLADE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU1524592A1 true SU1524592A1 (en) | 2004-08-20 |
Family
ID=60528490
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU4411232/06A SU1524592A1 (en) | 1988-04-18 | 1988-04-18 | COOLED GAS TURBINE BLADE |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU1524592A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2387845C1 (en) * | 2008-09-09 | 2010-04-27 | Владимир Михайлович Низовцев | Gas turbine plant |
| RU2397328C1 (en) * | 2006-04-21 | 2010-08-20 | Сименс Акциенгезелльшафт | Turbine blade |
-
1988
- 1988-04-18 SU SU4411232/06A patent/SU1524592A1/en active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2397328C1 (en) * | 2006-04-21 | 2010-08-20 | Сименс Акциенгезелльшафт | Turbine blade |
| RU2387845C1 (en) * | 2008-09-09 | 2010-04-27 | Владимир Михайлович Низовцев | Gas turbine plant |
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