SU1287696A1 - RING FLASH CHAMBER OF A MULTI-SIZED GAS TURBINE ENGINE - Google Patents
RING FLASH CHAMBER OF A MULTI-SIZED GAS TURBINE ENGINEInfo
- Publication number
- SU1287696A1 SU1287696A1 SU3876659/06A SU3876659A SU1287696A1 SU 1287696 A1 SU1287696 A1 SU 1287696A1 SU 3876659/06 A SU3876659/06 A SU 3876659/06A SU 3876659 A SU3876659 A SU 3876659A SU 1287696 A1 SU1287696 A1 SU 1287696A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- sleeve
- gas turbine
- turbine engine
- annular channel
- sized gas
- Prior art date
Links
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Кольцевая камера сгорания малоразмерного газотурбинного двигателя, содержащая корпус, установленную в нем жаровую трубу с внутренней и наружной обечайками, последняя из которых образует с корпусом кольцевой канал, и расположенные между обечайками втулку с топливными и воздушными каналами и вращающуюся топливную форсунку коробчатого типа с отверстиями на боковой поверхности, закрепленную на валу двигателя, отличающаяся тем, что, с целью повышения надежности и увеличения ресурса, втулка и внутренняя обечайка снабжены кольцевыми козырьками, расположенными с зазорами относительно форсунки и образующими с ней полости, сообщенные с кольцевым каналом и через зазоры с жаровой трубой, причем полость со стороны втулки сообщена с кольцевым каналом через воздушные каналы втулки.An annular combustion chamber of a small-sized gas turbine engine, comprising a housing, a heat pipe installed therein with internal and external shells, the latter of which forms an annular channel with the housing, and a sleeve with fuel and air channels located between the shells and a rotating fuel nozzle of box-like type with side holes surface mounted on the motor shaft, characterized in that, in order to increase reliability and increase the resource, the sleeve and the inner shell are provided with a ring trump Kami located with gaps relative to the nozzle and forming cavities with it, communicated with the annular channel and through the gaps with the flame tube, and the cavity on the side of the sleeve is connected to the annular channel through the air channels of the sleeve.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3876659/06A SU1287696A1 (en) | 1985-04-02 | 1985-04-02 | RING FLASH CHAMBER OF A MULTI-SIZED GAS TURBINE ENGINE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3876659/06A SU1287696A1 (en) | 1985-04-02 | 1985-04-02 | RING FLASH CHAMBER OF A MULTI-SIZED GAS TURBINE ENGINE |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1287696A1 true SU1287696A1 (en) | 2004-07-27 |
Family
ID=60539978
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU3876659/06A SU1287696A1 (en) | 1985-04-02 | 1985-04-02 | RING FLASH CHAMBER OF A MULTI-SIZED GAS TURBINE ENGINE |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1287696A1 (en) |
-
1985
- 1985-04-02 SU SU3876659/06A patent/SU1287696A1/en active
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