SU478531A1 - DEVICE FOR REGULATING THE PARAMETER OF A GAS TURBINE ENGINE - Google Patents

DEVICE FOR REGULATING THE PARAMETER OF A GAS TURBINE ENGINE

Info

Publication number
SU478531A1
SU478531A1 SU2000605/06A SU2000605A SU478531A1 SU 478531 A1 SU478531 A1 SU 478531A1 SU 2000605/06 A SU2000605/06 A SU 2000605/06A SU 2000605 A SU2000605 A SU 2000605A SU 478531 A1 SU478531 A1 SU 478531A1
Authority
SU
USSR - Soviet Union
Prior art keywords
parameter
regulating
turbine engine
gas turbine
reduced pressure
Prior art date
Application number
SU2000605/06A
Other languages
Russian (ru)
Inventor
А.С. Бокарев
М.Е. Остер
Original Assignee
А.С. Бокарев
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by А.С. Бокарев filed Critical А.С. Бокарев
Priority to SU2000605/06A priority Critical patent/SU478531A1/en
Application granted granted Critical
Publication of SU478531A1 publication Critical patent/SU478531A1/en

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  • Supercharger (AREA)
  • Control Of Turbines (AREA)

Abstract

Устройство для регулирования параметра газотурбинного двигателя, например регулирования температуры газа за турбиной, содержащее управляемый датчиком параметра воздушный редуктор, камера редуцированного давления которого подключена при помощи магистрали к исполнительному органу, отличающееся тем, что, с целью повышения надежности и качества регулирования, оно снабжено датчиком температуры воздуха за компрессором, управляющим дополнительным воздушным редуктором, камера редуцированного давления которого подключена через задатчик режима к магистрали, в месте подсоединения которой к основному редуктору установлен жиклер.A device for regulating the parameter of a gas turbine engine, for example, controlling the temperature of the gas behind the turbine, containing an air reducer controlled by a parameter sensor, the reduced pressure chamber of which is connected by means of a line to an actuator, which is equipped with a temperature sensor air behind the compressor, which controls the additional air reducer, the reduced pressure chamber of which is connected through the setpoint adjuster mode to the line, in the place where it is connected to the main gearbox, a jet is installed.

SU2000605/06A 1974-02-28 1974-02-28 DEVICE FOR REGULATING THE PARAMETER OF A GAS TURBINE ENGINE SU478531A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2000605/06A SU478531A1 (en) 1974-02-28 1974-02-28 DEVICE FOR REGULATING THE PARAMETER OF A GAS TURBINE ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2000605/06A SU478531A1 (en) 1974-02-28 1974-02-28 DEVICE FOR REGULATING THE PARAMETER OF A GAS TURBINE ENGINE

Publications (1)

Publication Number Publication Date
SU478531A1 true SU478531A1 (en) 2005-06-27

Family

ID=60518049

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2000605/06A SU478531A1 (en) 1974-02-28 1974-02-28 DEVICE FOR REGULATING THE PARAMETER OF A GAS TURBINE ENGINE

Country Status (1)

Country Link
SU (1) SU478531A1 (en)

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