SU1371146A1 - RING FLASH CHAMBER OF A GAS TURBINE ENGINE - Google Patents
RING FLASH CHAMBER OF A GAS TURBINE ENGINEInfo
- Publication number
- SU1371146A1 SU1371146A1 SU3938489/06A SU3938489A SU1371146A1 SU 1371146 A1 SU1371146 A1 SU 1371146A1 SU 3938489/06 A SU3938489/06 A SU 3938489/06A SU 3938489 A SU3938489 A SU 3938489A SU 1371146 A1 SU1371146 A1 SU 1371146A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- gas turbine
- turbine engine
- housing
- outer shell
- flash chamber
- Prior art date
Links
Abstract
Кольцевая камера сгорания газотурбинного двигателя, содержащая корпус, установленную в нем жаровую трубу с внутренней и наружной обечайками и закрепленную на валу двигателя вращающуюся топливную форсунку с сопловыми отверстиями, оси которых расположены в одной поперечной плоскости, отличающаяся тем, что, с целью повышения полноты сгорания и снижения токсичности продуктов сгорания в широком диапазоне режимов работы камеры, она дополнительно содержит неподвижные топливные форсунки, размещенные на наружной обечайке и ориентированные параллельно оси корпуса, и кольцевую заслонку, установленную с возможностью осевого перемещения перед наружной обечайкой и образующую с ней канал для подвода воздуха в зону вращающейся форсунки.An annular combustion chamber of a gas turbine engine, comprising a housing, a flame tube installed therein with inner and outer shells and a rotating fuel nozzle mounted on the motor shaft with nozzle openings, the axes of which are located in the same transverse plane, characterized in that reduce the toxicity of combustion products in a wide range of operating modes of the chamber, it additionally contains stationary fuel injectors placed on the outer shell and oriented p A parallel to the axis of the housing, and an annular damper installed with the possibility of axial movement in front of the outer shell and forming with it a channel for supplying air to the zone of the rotating nozzle.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3938489/06A SU1371146A1 (en) | 1985-08-01 | 1985-08-01 | RING FLASH CHAMBER OF A GAS TURBINE ENGINE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3938489/06A SU1371146A1 (en) | 1985-08-01 | 1985-08-01 | RING FLASH CHAMBER OF A GAS TURBINE ENGINE |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1371146A1 true SU1371146A1 (en) | 2004-07-27 |
Family
ID=60535289
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU3938489/06A SU1371146A1 (en) | 1985-08-01 | 1985-08-01 | RING FLASH CHAMBER OF A GAS TURBINE ENGINE |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1371146A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2506499C2 (en) * | 2009-11-09 | 2014-02-10 | Дженерал Электрик Компани | Fuel atomisers of gas turbine with opposite swirling directions |
-
1985
- 1985-08-01 SU SU3938489/06A patent/SU1371146A1/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2506499C2 (en) * | 2009-11-09 | 2014-02-10 | Дженерал Электрик Компани | Fuel atomisers of gas turbine with opposite swirling directions |
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