SU886535A1 - Cooled blade of turbine nozzle assembly - Google Patents
Cooled blade of turbine nozzle assemblyInfo
- Publication number
- SU886535A1 SU886535A1 SU2827623/06A SU2827623A SU886535A1 SU 886535 A1 SU886535 A1 SU 886535A1 SU 2827623/06 A SU2827623/06 A SU 2827623/06A SU 2827623 A SU2827623 A SU 2827623A SU 886535 A1 SU886535 A1 SU 886535A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- nozzle assembly
- turbine nozzle
- cooled blade
- blade
- feather
- Prior art date
Links
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
FIELD: gas-turbine engines. SUBSTANCE: cooled blade of turbine nozzle assembly has hollow feather provided with at least one flange; feather walls are thickened at portion abutting flange and its length is 0.25-0.3 of blade chord; maximum wall thickness is at least 0.2 of maximum profile thickness. EFFECT: improved reliability.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2827623/06A SU886535A1 (en) | 1979-10-10 | 1979-10-10 | Cooled blade of turbine nozzle assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2827623/06A SU886535A1 (en) | 1979-10-10 | 1979-10-10 | Cooled blade of turbine nozzle assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
SU886535A1 true SU886535A1 (en) | 1996-08-20 |
Family
ID=60518499
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU2827623/06A SU886535A1 (en) | 1979-10-10 | 1979-10-10 | Cooled blade of turbine nozzle assembly |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU886535A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU199563U1 (en) * | 2020-03-04 | 2020-09-08 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Рыбинский государственный авиационный технический университет имени П.А. Соловьева" | Block of cooled blades of a GTE turbine with a cooled asymmetrical end flange |
-
1979
- 1979-10-10 SU SU2827623/06A patent/SU886535A1/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU199563U1 (en) * | 2020-03-04 | 2020-09-08 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Рыбинский государственный авиационный технический университет имени П.А. Соловьева" | Block of cooled blades of a GTE turbine with a cooled asymmetrical end flange |
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