SU1376684A1 - NOZZLE FOR FUEL SUPPLY IN THE COMBUSTION CAMERA OF A GAS TURBINE ENGINE - Google Patents
NOZZLE FOR FUEL SUPPLY IN THE COMBUSTION CAMERA OF A GAS TURBINE ENGINEInfo
- Publication number
- SU1376684A1 SU1376684A1 SU4110470/06A SU4110470A SU1376684A1 SU 1376684 A1 SU1376684 A1 SU 1376684A1 SU 4110470/06 A SU4110470/06 A SU 4110470/06A SU 4110470 A SU4110470 A SU 4110470A SU 1376684 A1 SU1376684 A1 SU 1376684A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- nozzle
- fuel
- gas turbine
- turbine engine
- fuel supply
- Prior art date
Links
Landscapes
- Nozzles For Spraying Of Liquid Fuel (AREA)
Abstract
1. Форсунка для подачи топлива в камеру сгорания газотурбинного двигателя, содержащая неподвижную топливоподающую магистраль и охватывающую ее вращающуюся втулку в виде полого обода с соосными коническими поверхностями торцовых стенок, сопряженных с боковой цилиндрической стенкой, в которой выполнены выходные топливные отверстия, отличающаяся тем, что, с целью повышения надежности и увеличения ресурса, конические поверхности выполнены расходящимися от оси форсунки, а топливные отверстия расположены в зонах сопряжения торцовых стенок с цилиндрической.2. Форсунка по п.1, отличающаяся тем, что топливные отверстия расположены в шахматном порядке.1. Nozzle for supplying fuel to the combustion chamber of a gas turbine engine, comprising a stationary fuel supply line and a rotating sleeve enclosing it in the form of a hollow rim with coaxial conical surfaces of the end walls associated with a lateral cylindrical wall, in which the outlet fuel ports are made, characterized in that in order to increase reliability and increase resource, the conical surfaces are made diverging from the nozzle axis, and the fuel holes are located in the interface zones of the end walls with tsilindricheskoy.2. The nozzle according to claim 1, characterized in that the fuel holes are arranged in a checkerboard pattern.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4110470/06A SU1376684A1 (en) | 1986-06-19 | 1986-06-19 | NOZZLE FOR FUEL SUPPLY IN THE COMBUSTION CAMERA OF A GAS TURBINE ENGINE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4110470/06A SU1376684A1 (en) | 1986-06-19 | 1986-06-19 | NOZZLE FOR FUEL SUPPLY IN THE COMBUSTION CAMERA OF A GAS TURBINE ENGINE |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1376684A1 true SU1376684A1 (en) | 2004-07-27 |
Family
ID=60533893
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU4110470/06A SU1376684A1 (en) | 1986-06-19 | 1986-06-19 | NOZZLE FOR FUEL SUPPLY IN THE COMBUSTION CAMERA OF A GAS TURBINE ENGINE |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1376684A1 (en) |
-
1986
- 1986-06-19 SU SU4110470/06A patent/SU1376684A1/en active
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