SU1371146A1 - RING FLASH CHAMBER OF A GAS TURBINE ENGINE - Google Patents

RING FLASH CHAMBER OF A GAS TURBINE ENGINE

Info

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
Application number
SU3938489/06A
Other languages
Russian (ru)
Inventor
А.Г. Зданович
В.В. Владимиров
В.Ф. Мусаткин
Р.М. Раянов
Original Assignee
А.Г. Зданович
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by А.Г. Зданович filed Critical А.Г. Зданович
Priority to SU3938489/06A priority Critical patent/SU1371146A1/en
Application granted granted Critical
Publication of SU1371146A1 publication Critical patent/SU1371146A1/en

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.

SU3938489/06A 1985-08-01 1985-08-01 RING FLASH CHAMBER OF A GAS TURBINE ENGINE SU1371146A1 (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (1)

* Cited by examiner, † Cited by third party
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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