RU98102637A - TUBE-RING GAS TURBINE COMBUSTION CHAMBER - Google Patents

TUBE-RING GAS TURBINE COMBUSTION CHAMBER

Info

Publication number
RU98102637A
RU98102637A RU98102637/06A RU98102637A RU98102637A RU 98102637 A RU98102637 A RU 98102637A RU 98102637/06 A RU98102637/06 A RU 98102637/06A RU 98102637 A RU98102637 A RU 98102637A RU 98102637 A RU98102637 A RU 98102637A
Authority
RU
Russia
Prior art keywords
tube
flame
combustion chamber
wall
gas turbine
Prior art date
Application number
RU98102637/06A
Other languages
Russian (ru)
Other versions
RU2151960C1 (en
Inventor
В.В. Токарев
Ю.Е. Кириевский
Original Assignee
Открытое акционерное общество "Авиадвигатель"
Filing date
Publication date
Application filed by Открытое акционерное общество "Авиадвигатель" filed Critical Открытое акционерное общество "Авиадвигатель"
Priority to RU98102637A priority Critical patent/RU2151960C1/en
Priority claimed from RU98102637A external-priority patent/RU2151960C1/en
Publication of RU98102637A publication Critical patent/RU98102637A/en
Application granted granted Critical
Publication of RU2151960C1 publication Critical patent/RU2151960C1/en

Links

Claims (1)

Трубчато-кольцевая камера сгорания газовой турбины, содержащая жаровые трубы, соединенные с газосборником, скрепленным с внешним и внутренним корпусами, полость которого образована его собственными кольцевыми стенками, при этом каждая из жаровых труб содержит на выходе в поперечном потоку направлении лобовую стенку, скрепленную со стенкой жаровой трубы и соединенную с газосборником, отличающаяся тем, что выше по потоку от лобовой стенки в каждой из жаровых труб выполнен ряд отверстий, от которых на расстоянии не более чем диаметр этих отверстий размещены генераторы звуковых колебаний, а от последних стенка жаровой трубы сплошная, при этом каждый генератор размещен в скрепленном со стенкой жаровой трубы патрубке, центральная ось которого расположена в радиальной плоскости жаровой трубы, проходящей через угол лобовой стенки.A tubular-annular combustion chamber of a gas turbine containing flame tubes connected to a gas collector fastened to the outer and inner bodies, the cavity of which is formed by its own annular walls, while each of the flame tubes contains a frontal wall fastened to the wall at the outlet in the transverse flow direction a flame tube and connected to a gas collector, characterized in that a number of holes are made upstream of the frontal wall in each of the flame tubes, from which at a distance of no more than the diameter of these generations of sound vibrations are placed, and the walls of the flame tube are solid from the last, each generator is placed in a branch pipe attached to the flame tube wall, the central axis of which is located in the radial plane of the flame tube passing through the angle of the frontal wall.
RU98102637A 1998-02-02 1998-02-02 Tubular-annular combustion chamber of gas turbine RU2151960C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU98102637A RU2151960C1 (en) 1998-02-02 1998-02-02 Tubular-annular combustion chamber of gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU98102637A RU2151960C1 (en) 1998-02-02 1998-02-02 Tubular-annular combustion chamber of gas turbine

Publications (2)

Publication Number Publication Date
RU98102637A true RU98102637A (en) 1999-12-20
RU2151960C1 RU2151960C1 (en) 2000-06-27

Family

ID=20202266

Family Applications (1)

Application Number Title Priority Date Filing Date
RU98102637A RU2151960C1 (en) 1998-02-02 1998-02-02 Tubular-annular combustion chamber of gas turbine

Country Status (1)

Country Link
RU (1) RU2151960C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9423132B2 (en) * 2010-11-09 2016-08-23 Opra Technologies B.V. Ultra low emissions gas turbine combustor

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