SU1287696A1 - RING FLASH CHAMBER OF A MULTI-SIZED GAS TURBINE ENGINE - Google Patents

RING FLASH CHAMBER OF A MULTI-SIZED GAS TURBINE ENGINE

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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
Application number
SU3876659/06A
Other languages
Russian (ru)
Inventor
Ф.И. Шуйский
В.Ф. Куницкий
Е.И. Зимарев
Original Assignee
Ф.И. Шуйский
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 Ф.И. Шуйский filed Critical Ф.И. Шуйский
Priority to SU3876659/06A priority Critical patent/SU1287696A1/en
Application granted granted Critical
Publication of SU1287696A1 publication Critical patent/SU1287696A1/en

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  • 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.

SU3876659/06A 1985-04-02 1985-04-02 RING FLASH CHAMBER OF A MULTI-SIZED GAS TURBINE ENGINE SU1287696A1 (en)

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)

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