RU96102244A - GAS TURBINE COMBUSTION CHAMBER - Google Patents

GAS TURBINE COMBUSTION CHAMBER

Info

Publication number
RU96102244A
RU96102244A RU96102244/06A RU96102244A RU96102244A RU 96102244 A RU96102244 A RU 96102244A RU 96102244/06 A RU96102244/06 A RU 96102244/06A RU 96102244 A RU96102244 A RU 96102244A RU 96102244 A RU96102244 A RU 96102244A
Authority
RU
Russia
Prior art keywords
mixer
combustion chamber
gas turbine
flame
turbine combustion
Prior art date
Application number
RU96102244/06A
Other languages
Russian (ru)
Other versions
RU2107229C1 (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 RU96102244A priority Critical patent/RU2107229C1/en
Priority claimed from RU96102244A external-priority patent/RU2107229C1/en
Application granted granted Critical
Publication of RU2107229C1 publication Critical patent/RU2107229C1/en
Publication of RU96102244A publication Critical patent/RU96102244A/en

Links

Claims (1)

Камера сгорания газовой турбины, содержащая жаровые трубы, соединенные с газосборником, скрепленным с внешним и внутренним корпусами, отличающаяся тем, что каждая из жаровых труб содержит во внутренней полости ниже по потоку за факелом пламени смеситель с отверстиями в его стенке и расположенные концентрично ему внешний и внутренний осевые лопаточные завихрители, при этом лопатки внешнего завихрителя выполнены полыми и скреплены со стенками жаровой трубы и смесителя, а лопатки внутреннего завихрителя скреплены со стенкой смесителя и центральным телом, расположенным концентрично смесителю, причем смеситель и центральное тело выполнены каждый в виде конуса или гиперболоида вращения, вершины которых направлены против потока.The combustion chamber of a gas turbine containing flame tubes connected to a gas collector fastened to the outer and inner bodies, characterized in that each of the flame tubes contains in the inner cavity downstream of the flame torch a mixer with holes in its wall and an external and concentric internal axial blade swirls, while the blades of the external swirl are hollow and bonded to the walls of the flame tube and mixer, and the blades of the internal swirl are bonded to the wall of the mixer and a central body located concentrically to the mixer, the mixer and the central body each made in the form of a cone or hyperboloid of revolution, the vertices of which are directed against the flow.
RU96102244A 1996-02-06 1996-02-06 Gas-turbine combustion chamber RU2107229C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU96102244A RU2107229C1 (en) 1996-02-06 1996-02-06 Gas-turbine combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU96102244A RU2107229C1 (en) 1996-02-06 1996-02-06 Gas-turbine combustion chamber

Publications (2)

Publication Number Publication Date
RU2107229C1 RU2107229C1 (en) 1998-03-20
RU96102244A true RU96102244A (en) 1998-04-27

Family

ID=20176573

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96102244A RU2107229C1 (en) 1996-02-06 1996-02-06 Gas-turbine combustion chamber

Country Status (1)

Country Link
RU (1) RU2107229C1 (en)

Similar Documents

Publication Publication Date Title
CA2453532A1 (en) Premixing nozzle, combustor,and gas turbine
RU2002134607A (en) IMPROVED FIRE PIPE OR “INTERNAL FACING” FOR A CAMERA OF COMBUSTION OF A GAS TURBINE WITH A SMALL EMISSION LEVEL OF THE POLLUTION
RU96102244A (en) GAS TURBINE COMBUSTION CHAMBER
RU96116186A (en) TWO FLOW GAS BURNER
RU95115895A (en) COMBUSTION CAMERA OF A GAS TURBINE POWER INSTALLATION
RU95118605A (en) TUBULAR-RING COMBUSTION CHAMBER OF A GAS-TURBINE ENERGY UNIT
RU95118604A (en) TUBULAR-RING COMBUSTION CHAMBER OF A GAS-TURBINE ENERGY UNIT
RU97119773A (en) TUBE-RING GAS TURBINE COMBUSTION CHAMBER
RU97105664A (en) GAS TURBINE COMBUSTION CHAMBER
RU95118607A (en) TUBULAR-RING COMBUSTION CHAMBER OF A GAS-TURBINE ENERGY UNIT
RU2004137975A (en) RING COMBUSTION CAMERA OF A GAS-TURBINE ENGINE
RU2001124100A (en) FUEL AIR BURNER OF THE COMBUSTION CHAMBER OF A GAS TURBINE ENGINE
RU2106579C1 (en) Tubular-and-annular combustion chamber of gas-turbine power plant
RU2136907C1 (en) Internal combustion engine exhaust system device
RU96102191A (en) TUBE-RING GAS TURBINE COMBUSTION CHAMBER
RU96110311A (en) GAS TURBINE COMBUSTION CHAMBER
RU98102637A (en) TUBE-RING GAS TURBINE COMBUSTION CHAMBER
RU2001135485A (en) Device for burning fuel
RU2000125408A (en) GAS MIXING AIR HEATER
RU2002122026A (en) Two-component nozzle
RU96102197A (en) TUBE-RING GAS TURBINE COMBUSTION CHAMBER
RU98108347A (en) TUBULAR-RING COMBUSTION CHAMBER OF A GAS-TURBINE ENGINE
SU1184960A1 (en) Exhaust silencer
SU1694946A1 (en) Silencer
RU95120876A (en) COMBUSTION CAMERA OF A GAS TURBINE ENGINE