RU93044777A - METHOD OF STABILIZATION OF THE RADIAL PROFILE OF THE TEMPERATURE OF THE WORKING BODY AT THE OUTPUT FROM THE RINGING CAMERA OF COMBUSTION OF A GAS TURBINE ENGINE AND DEVICE FOR ITS IMPLEMENTATION - Google Patents

METHOD OF STABILIZATION OF THE RADIAL PROFILE OF THE TEMPERATURE OF THE WORKING BODY AT THE OUTPUT FROM THE RINGING CAMERA OF COMBUSTION OF A GAS TURBINE ENGINE AND DEVICE FOR ITS IMPLEMENTATION

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Publication number
RU93044777A
RU93044777A RU93044777/06A RU93044777A RU93044777A RU 93044777 A RU93044777 A RU 93044777A RU 93044777/06 A RU93044777/06 A RU 93044777/06A RU 93044777 A RU93044777 A RU 93044777A RU 93044777 A RU93044777 A RU 93044777A
Authority
RU
Russia
Prior art keywords
gas turbine
turbine engine
stabilization
working body
ringing
Prior art date
Application number
RU93044777/06A
Other languages
Russian (ru)
Other versions
RU2064134C1 (en
Inventor
Л.К. Хохлов
Original Assignee
Научно-технический центр энергосберегающих процессов и установок
Filing date
Publication date
Application filed by Научно-технический центр энергосберегающих процессов и установок filed Critical Научно-технический центр энергосберегающих процессов и установок
Priority to RU93044777A priority Critical patent/RU2064134C1/en
Priority claimed from RU93044777A external-priority patent/RU2064134C1/en
Publication of RU93044777A publication Critical patent/RU93044777A/en
Application granted granted Critical
Publication of RU2064134C1 publication Critical patent/RU2064134C1/en

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Claims (1)

Изобретение относится к области газотурбинного двигателе - строения. Решается задача стабилизации радиального температурного профиля рабочего теля на выходе из кольцевой камеры сгорания газотурбинного двигателя путем организации стабилизации давления воздуха в полостях, окружающих снаружи и внутри жаровую трубу путем перепуска воздуха по каналам, сообщающим эти кольцевые каналы на входе в жаровую трубу.The invention relates to the field of gas turbine engine - structure. The task of stabilizing the radial temperature profile of the working body at the exit from the annular combustion chamber of a gas turbine engine is solved by organizing the stabilization of air pressure in cavities surrounding the inside and outside of the heat pipe by passing air through the channels that communicate these ring channels at the entrance to the heat pipe.
RU93044777A 1993-09-06 1993-09-06 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 RU2064134C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU93044777A RU2064134C1 (en) 1993-09-06 1993-09-06 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

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU93044777A RU2064134C1 (en) 1993-09-06 1993-09-06 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

Publications (2)

Publication Number Publication Date
RU93044777A true RU93044777A (en) 1996-04-10
RU2064134C1 RU2064134C1 (en) 1996-07-20

Family

ID=20147469

Family Applications (1)

Application Number Title Priority Date Filing Date
RU93044777A RU2064134C1 (en) 1993-09-06 1993-09-06 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

Country Status (1)

Country Link
RU (1) RU2064134C1 (en)

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