SU1718609A1 - Flame tube of gas turbine combustion chamber - Google Patents
Flame tube of gas turbine combustion chamberInfo
- Publication number
- SU1718609A1 SU1718609A1 SU4771161/06A SU4771161A SU1718609A1 SU 1718609 A1 SU1718609 A1 SU 1718609A1 SU 4771161/06 A SU4771161/06 A SU 4771161/06A SU 4771161 A SU4771161 A SU 4771161A SU 1718609 A1 SU1718609 A1 SU 1718609A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- segments
- gas turbine
- flame tube
- combustion chamber
- turbine combustion
- Prior art date
Links
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
FIELD: gas turbine engine engineering. SUBSTANCE: in operation. air enters closed spaces 6 through openings 2 in housing 1 of the flame tube. The spaces are formed by segments 3 secured to housing 1. Air is cooled the segments from the outside. Air flows out from spaces 6 through openings 4 of segments 3 and opening made in side ribs 5 and cools the inner side of segments 3 and ribs 5 made in block with them. A part of cooling air is used to burn out the fuel. EFFECT: enhanced reliability. 4 dwg
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4771161/06A SU1718609A1 (en) | 1989-12-19 | 1989-12-19 | Flame tube of gas turbine combustion chamber |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4771161/06A SU1718609A1 (en) | 1989-12-19 | 1989-12-19 | Flame tube of gas turbine combustion chamber |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1718609A1 true SU1718609A1 (en) | 1996-06-10 |
Family
ID=60532347
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU4771161/06A SU1718609A1 (en) | 1989-12-19 | 1989-12-19 | Flame tube of gas turbine combustion chamber |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1718609A1 (en) |
-
1989
- 1989-12-19 SU SU4771161/06A patent/SU1718609A1/en active
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