RU2015112487A - RING COMBUSTION CAMERA OF A GAS-TURBINE ENGINE - Google Patents

RING COMBUSTION CAMERA OF A GAS-TURBINE ENGINE Download PDF

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Publication number
RU2015112487A
RU2015112487A RU2015112487A RU2015112487A RU2015112487A RU 2015112487 A RU2015112487 A RU 2015112487A RU 2015112487 A RU2015112487 A RU 2015112487A RU 2015112487 A RU2015112487 A RU 2015112487A RU 2015112487 A RU2015112487 A RU 2015112487A
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RU
Russia
Prior art keywords
turbine engine
flame tube
gas
combustion chamber
outer casing
Prior art date
Application number
RU2015112487A
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Russian (ru)
Inventor
Владимир Евгеньевич Николаев
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Открытое Акционерное Общество "Кузнецов"
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Priority to RU2015112487A priority Critical patent/RU2015112487A/en
Publication of RU2015112487A publication Critical patent/RU2015112487A/en

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Abstract

Кольцевая камера сгорания газотурбинного двигателя, содержащая наружный корпус, жаровую трубу с воздушным коллектором, узел перепуска воздуха из полости, образованной наружным корпусом и жаровой трубой, во внутреннюю полость жаровой трубы, отличающаяся тем, что узел перепуска включает по меньшей мере восемь блоков перепуска воздуха, симметрично расположенных по окружности кольцевой камеры сгорания с внутренними заслонками.An annular combustion chamber of a gas turbine engine comprising an outer casing, a flame tube with an air manifold, an air bypass assembly from a cavity formed by the outer casing and the flame tube, into an internal cavity of the flame tube, characterized in that the bypass assembly includes at least eight air bypass blocks, symmetrically located around the circumference of the annular combustion chamber with internal flaps.

Claims (1)

Кольцевая камера сгорания газотурбинного двигателя, содержащая наружный корпус, жаровую трубу с воздушным коллектором, узел перепуска воздуха из полости, образованной наружным корпусом и жаровой трубой, во внутреннюю полость жаровой трубы, отличающаяся тем, что узел перепуска включает по меньшей мере восемь блоков перепуска воздуха, симметрично расположенных по окружности кольцевой камеры сгорания с внутренними заслонками. An annular combustion chamber of a gas turbine engine comprising an outer casing, a flame tube with an air manifold, an air bypass assembly from a cavity formed by the outer casing and the flame tube, into an internal cavity of the flame tube, characterized in that the bypass assembly includes at least eight air bypass blocks, symmetrically located around the circumference of the annular combustion chamber with internal flaps.
RU2015112487A 2015-04-06 2015-04-06 RING COMBUSTION CAMERA OF A GAS-TURBINE ENGINE RU2015112487A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2015112487A RU2015112487A (en) 2015-04-06 2015-04-06 RING COMBUSTION CAMERA OF A GAS-TURBINE ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2015112487A RU2015112487A (en) 2015-04-06 2015-04-06 RING COMBUSTION CAMERA OF A GAS-TURBINE ENGINE

Publications (1)

Publication Number Publication Date
RU2015112487A true RU2015112487A (en) 2016-10-20

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Family Applications (1)

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RU2015112487A RU2015112487A (en) 2015-04-06 2015-04-06 RING COMBUSTION CAMERA OF A GAS-TURBINE ENGINE

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RU (1) RU2015112487A (en)

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