RU95118606A - TUBULAR-RING COMBUSTION CHAMBER OF A GAS-TURBINE ENERGY UNIT - Google Patents

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

Info

Publication number
RU95118606A
RU95118606A RU95118606/06A RU95118606A RU95118606A RU 95118606 A RU95118606 A RU 95118606A RU 95118606/06 A RU95118606/06 A RU 95118606/06A RU 95118606 A RU95118606 A RU 95118606A RU 95118606 A RU95118606 A RU 95118606A
Authority
RU
Russia
Prior art keywords
wall
flame tube
gas
tubular
combustion chamber
Prior art date
Application number
RU95118606/06A
Other languages
Russian (ru)
Other versions
RU2107227C1 (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 RU95118606/06A priority Critical patent/RU2107227C1/en
Priority claimed from RU95118606/06A external-priority patent/RU2107227C1/en
Publication of RU95118606A publication Critical patent/RU95118606A/en
Application granted granted Critical
Publication of RU2107227C1 publication Critical patent/RU2107227C1/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 на выходе в поперечном потоку направлении лобовую стенку, скрепленную со стенкой жаровой трубы и соединенную с газосборником с возможностью перемещения вдоль оси жаровой трубы, причем перед лобовой стенкой выше по потоку в жаровой трубе выполнен минимум один ряд отверстий, от которых стенка жаровой трубы сплошная, а по периметру стенки жаровой трубы выполнены щелевые каналы в плоскости лобовой стенки, обращенной к потоку, 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 frontal wall fastened to the flame tube wall and connected to the flame tube at the outlet in the transverse flow direction gas collector with the ability to move along the axis of the flame tube, and in front of the frontal wall upstream in the flame tube, at least one row of holes is made, from which the wall of the flame tube is split shnaya, and on the perimeter wall of the flame tube slotted channels formed in the frontal plane wall facing the flow, the gas plenum is formed by a cavity own annular walls.
RU95118606/06A 1995-11-01 1995-11-01 Tubular-annular combustion chamber of gas-turbine power plant RU2107227C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU95118606/06A RU2107227C1 (en) 1995-11-01 1995-11-01 Tubular-annular combustion chamber of gas-turbine power plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU95118606/06A RU2107227C1 (en) 1995-11-01 1995-11-01 Tubular-annular combustion chamber of gas-turbine power plant

Publications (2)

Publication Number Publication Date
RU95118606A true RU95118606A (en) 1997-11-20
RU2107227C1 RU2107227C1 (en) 1998-03-20

Family

ID=20173398

Family Applications (1)

Application Number Title Priority Date Filing Date
RU95118606/06A RU2107227C1 (en) 1995-11-01 1995-11-01 Tubular-annular combustion chamber of gas-turbine power plant

Country Status (1)

Country Link
RU (1) RU2107227C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2920525B1 (en) * 2007-08-31 2014-06-13 Snecma SEPARATOR FOR SUPPLYING THE COOLING AIR OF A TURBINE

Similar Documents

Publication Publication Date Title
JPS56124834A (en) Gas-turbine combustor
RU95118606A (en) TUBULAR-RING COMBUSTION CHAMBER OF A GAS-TURBINE ENERGY UNIT
RU95115895A (en) COMBUSTION CAMERA OF A GAS TURBINE POWER INSTALLATION
RU95118605A (en) TUBULAR-RING COMBUSTION CHAMBER OF A GAS-TURBINE ENERGY UNIT
RU95109827A (en) COMBUSTION CAMERA OF A GAS TURBINE POWER INSTALLATION
SU1307067A1 (en) System for releasing exhaust gases of combined internal combustion engine
RU96102191A (en) TUBE-RING GAS TURBINE COMBUSTION CHAMBER
RU2002115646A (en) Wind power plant
RU97118971A (en) TUBE-RING GAS TURBINE COMBUSTION CHAMBER
RU95118607A (en) TUBULAR-RING COMBUSTION CHAMBER OF A GAS-TURBINE ENERGY UNIT
RU96102197A (en) TUBE-RING GAS TURBINE COMBUSTION CHAMBER
RU1795224C (en) Flue device
RU2064134C1 (en) Method for stabilizing radial profile of working medium temperature at outlet of annular combustion chamber of gas-turbine engine and annular chamber of gas-turbine engine
RU95118604A (en) TUBULAR-RING COMBUSTION CHAMBER OF A GAS-TURBINE ENERGY UNIT
RU97119773A (en) TUBE-RING GAS TURBINE COMBUSTION CHAMBER
RU98102637A (en) TUBE-RING GAS TURBINE COMBUSTION CHAMBER
RU96105118A (en) COMBUSTION CAMERA OF A GAS TURBINE ENGINE
RU2136907C1 (en) Internal combustion engine exhaust system device
SU861860A1 (en) Exhaust pipe nozzle
SU1213228A1 (en) Exhaust system of internal combustion system with gas turbine supercharging
RU1793154C (en) Burner
RU97105664A (en) GAS TURBINE COMBUSTION CHAMBER
SU676820A1 (en) Exhaust tube
SU982406A1 (en) Acoustic damper of afterburning chamber of turbojet engine
RU95111944A (en) RING COMBUSTION CAMERA OF A GAS-TURBINE ENGINE