RU2000117931A - COMBUSTION CAMERA OF A GAS TURBINE ENGINE - Google Patents

COMBUSTION CAMERA OF A GAS TURBINE ENGINE

Info

Publication number
RU2000117931A
RU2000117931A RU2000117931/06A RU2000117931A RU2000117931A RU 2000117931 A RU2000117931 A RU 2000117931A RU 2000117931/06 A RU2000117931/06 A RU 2000117931/06A RU 2000117931 A RU2000117931 A RU 2000117931A RU 2000117931 A RU2000117931 A RU 2000117931A
Authority
RU
Russia
Prior art keywords
gas turbine
turbine engine
combustion chamber
combustion
combustion camera
Prior art date
Application number
RU2000117931/06A
Other languages
Russian (ru)
Other versions
RU2196906C2 (en
Inventor
Михаил Леонидович Кузменко
Василий Иванович Богданов
Original Assignee
Открытое акционерное общество "Рыбинские моторы"
Filing date
Publication date
Application filed by Открытое акционерное общество "Рыбинские моторы" filed Critical Открытое акционерное общество "Рыбинские моторы"
Priority to RU2000117931A priority Critical patent/RU2196906C2/en
Priority claimed from RU2000117931A external-priority patent/RU2196906C2/en
Publication of RU2000117931A publication Critical patent/RU2000117931A/en
Application granted granted Critical
Publication of RU2196906C2 publication Critical patent/RU2196906C2/en

Links

Claims (3)

1. Камера сгорания газотурбинного двигателя с постоянным объемом сгорания топлива, содержащая корпус, установленную в нем жаровую трубу, выполненную в виде вращающегося сферического золотника со срезом, канальные входное и выходное устройства, отличающаяся тем, что ось выходного устройства смещена относительно центра вращения золотника.1. The combustion chamber of a gas turbine engine with a constant volume of fuel combustion, comprising a housing, a heat pipe installed in it, made in the form of a rotating spherical spool with a slice, channel input and output devices, characterized in that the axis of the output device is offset from the center of rotation of the spool. 2. Камера сгорания по п. 1, отличающаяся тем, что в выходном устройстве образован по крайней мере, еще один канал. 2. The combustion chamber according to claim 1, characterized in that at least one more channel is formed in the output device. 3. Камера сгорания по п. 1 или 2, отличающаяся тем, что на срезе золотника установлено сопло. 3. The combustion chamber according to claim 1 or 2, characterized in that a nozzle is installed on a slice of the valve.
RU2000117931A 2000-07-05 2000-07-05 Combustion chamber of gas turbine engine RU2196906C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2000117931A RU2196906C2 (en) 2000-07-05 2000-07-05 Combustion chamber of gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2000117931A RU2196906C2 (en) 2000-07-05 2000-07-05 Combustion chamber of gas turbine engine

Publications (2)

Publication Number Publication Date
RU2000117931A true RU2000117931A (en) 2002-09-10
RU2196906C2 RU2196906C2 (en) 2003-01-20

Family

ID=20237461

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2000117931A RU2196906C2 (en) 2000-07-05 2000-07-05 Combustion chamber of gas turbine engine

Country Status (1)

Country Link
RU (1) RU2196906C2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202009013789U1 (en) 2009-10-09 2010-03-04 Kostiukov, Vladimir Nikolaevich Pulsating engine
DE202012013035U1 (en) 2011-12-14 2014-08-01 Vladimir Nikolaevich Kostyukov Turbo-Rotor-engine
RU2553589C2 (en) * 2012-08-28 2015-06-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Method of functioning of supersonic pulsing detonation straight-jet engine
CN104949154B (en) * 2015-03-11 2017-10-31 龚雨晋 Realize the device of constant volume burning and the dynamical system including the device
RU185450U1 (en) * 2018-04-04 2018-12-05 Открытое акционерное общество "КБ Электроприбор" COMBUSTION CAMERA OF A GAS TURBINE ENGINE WITH CONSTANT VOLUME OF COMBUSTION OF FUEL

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