RU95118604A - TUBULAR-RING COMBUSTION CHAMBER OF A GAS-TURBINE ENERGY UNIT - Google Patents

TUBULAR-RING COMBUSTION CHAMBER OF A GAS-TURBINE ENERGY UNIT

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Publication number
RU95118604A
RU95118604A RU95118604/06A RU95118604A RU95118604A RU 95118604 A RU95118604 A RU 95118604A RU 95118604/06 A RU95118604/06 A RU 95118604/06A RU 95118604 A RU95118604 A RU 95118604A RU 95118604 A RU95118604 A RU 95118604A
Authority
RU
Russia
Prior art keywords
gas
flame
tubular
combustion chamber
mixer
Prior art date
Application number
RU95118604/06A
Other languages
Russian (ru)
Other versions
RU2106578C1 (en
Inventor
М.Л. Кузменко
А.А. Снитко
В.В. Токарев
О.В. Брындин
Ю.Е. Кириевский
М.С. Хрящиков
М.Ф. Хайруллин
Original Assignee
Акционерное общество "Авиадвигатель"
Filing date
Publication date
Application filed by Акционерное общество "Авиадвигатель" filed Critical Акционерное общество "Авиадвигатель"
Priority to RU95118604A priority Critical patent/RU2106578C1/en
Priority claimed from RU95118604A external-priority patent/RU2106578C1/en
Publication of RU95118604A publication Critical patent/RU95118604A/en
Application granted granted Critical
Publication of RU2106578C1 publication Critical patent/RU2106578C1/en

Links

Claims (1)

Трубчато-кольцевая камера сгорания газотурбинной энергетической установки, содержащая жаровые трубы, соединенные с газосборником, скрепленным с внешним и внутренним корпусами, отличающаяся тем, что каждая из жаровых труб содержит расположенный во внутренней полости ниже по потоку за факелом пламени смеситель, скрепленный полыми стойками со стенкой жаровой трубы и выполненный в виде днища и конусной оболочки с прямолинейной образующей или образующей в форме дуг окружностей, выпуклая сторона которых направлена к оси жаровой трубы, вершина конуса направлена против потока в стенках днища и оболочки смесителя, а также жаровой трубы, в пределах длины смесителя выполнены отверстия и щели, при этом полость газосборника образована собственными кольцевыми стенками.A tubular-annular combustion chamber of a gas turbine power plant, comprising flame tubes connected to a gas collector bonded to the external and internal bodies, characterized in that each of the flame tubes contains a mixer mounted in the hollow cavity downstream of the flame torch, fastened by hollow struts to the wall flame tube and made in the form of a bottom and a conical shell with a rectilinear generatrix or arcing in the form of arcs of circles, the convex side of which is directed to the axis of the flame tube, top the cone is directed against the flow in the walls of the bottom and shell of the mixer, as well as the flame tube, holes and slots are made within the length of the mixer, while the gas collector cavity is formed by its own annular walls.
RU95118604A 1995-11-01 1995-11-01 Tubular-and-annular combustion chamber of gas-turbine power plant RU2106578C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU95118604A RU2106578C1 (en) 1995-11-01 1995-11-01 Tubular-and-annular combustion chamber of gas-turbine power plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU95118604A RU2106578C1 (en) 1995-11-01 1995-11-01 Tubular-and-annular combustion chamber of gas-turbine power plant

Publications (2)

Publication Number Publication Date
RU95118604A true RU95118604A (en) 1997-11-20
RU2106578C1 RU2106578C1 (en) 1998-03-10

Family

ID=20173396

Family Applications (1)

Application Number Title Priority Date Filing Date
RU95118604A RU2106578C1 (en) 1995-11-01 1995-11-01 Tubular-and-annular combustion chamber of gas-turbine power plant

Country Status (1)

Country Link
RU (1) RU2106578C1 (en)

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