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RU2005106019A - DEVICE FOR GAS-TURBINE ENGINE CONTROL - Google Patents

DEVICE FOR GAS-TURBINE ENGINE CONTROL Download PDF

Info

Publication number
RU2005106019A
RU2005106019A RU2005106019/06A RU2005106019A RU2005106019A RU 2005106019 A RU2005106019 A RU 2005106019A RU 2005106019/06 A RU2005106019/06 A RU 2005106019/06A RU 2005106019 A RU2005106019 A RU 2005106019A RU 2005106019 A RU2005106019 A RU 2005106019A
Authority
RU
Russia
Prior art keywords
engine
turbine engine
dispenser
supply line
engine control
Prior art date
Application number
RU2005106019/06A
Other languages
Russian (ru)
Other versions
RU2289708C2 (en
Inventor
Юрий Петрович Дудкин (RU)
Юрий Петрович Дудкин
Сергей Владимирович Остапенко (RU)
Сергей Владимирович Остапенко
Петр Исаевич Алексеев (RU)
Петр Исаевич Алексеев
Виктор Александрович Гладких (RU)
Виктор Александрович Гладких
Геннадий Викторович Фомин (RU)
Геннадий Викторович Фомин
Original Assignee
Открытое акционерное общество "СТАР" (RU)
Открытое акционерное общество "СТАР"
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 Открытое акционерное общество "СТАР" (RU), Открытое акционерное общество "СТАР" filed Critical Открытое акционерное общество "СТАР" (RU)
Priority to RU2005106019/06A priority Critical patent/RU2289708C2/en
Publication of RU2005106019A publication Critical patent/RU2005106019A/en
Application granted granted Critical
Publication of RU2289708C2 publication Critical patent/RU2289708C2/en

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  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Control Of Turbines (AREA)

Claims (1)

Устройство для управления ГТД, содержащее топливный насос, выход которого подключен к регулятору механизации компрессора и соединен с магистралью подачи топлива в двигатель, в которой последовательно установлены дозатор и распределительный клапан (РК), причем дозатор подключен к регулятору режима работы двигателя, а к магистрали подачи топлива в двигатель подключен электромагнитный клапан останова (КО) двигателя, отличающееся тем, что, с целью повышения надежности работы ГТД, дополнительно введен золотник минимального давления, установленный непосредственно на выходе дозатора, причем торцевая полость золотника минимального давления соединена с магистралью подачи топлива в двигатель, а пружинная - со сливом, а КО установлен непосредственно перед РК.A gas turbine engine control device comprising a fuel pump, the output of which is connected to a compressor mechanization regulator and connected to a fuel supply line to the engine, in which a dispenser and a distribution valve (PK) are installed in series, the dispenser connected to an engine operating mode regulator and to a supply line fuel in the engine is connected to the electromagnetic shutdown valve (KO) of the engine, characterized in that, in order to increase the reliability of the gas turbine engine, an additional minimum pressure valve is introduced, it is set manifested directly at the outlet of the dispenser, the end cavity of the minimum pressure valve being connected to the fuel supply line to the engine, and the spring cavity to the drain, and the CO is installed directly in front of the RC.
RU2005106019/06A 2005-03-03 2005-03-03 Gas-turbine engine control device RU2289708C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2005106019/06A RU2289708C2 (en) 2005-03-03 2005-03-03 Gas-turbine engine control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2005106019/06A RU2289708C2 (en) 2005-03-03 2005-03-03 Gas-turbine engine control device

Publications (2)

Publication Number Publication Date
RU2005106019A true RU2005106019A (en) 2006-08-10
RU2289708C2 RU2289708C2 (en) 2006-12-20

Family

ID=37059394

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2005106019/06A RU2289708C2 (en) 2005-03-03 2005-03-03 Gas-turbine engine control device

Country Status (1)

Country Link
RU (1) RU2289708C2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2514463C1 (en) * 2012-09-07 2014-04-27 Закрытое Акционерное Общество Научно-Производственная Фирма "Газ-Система-Сервис" Control over gas turbine engine compressor actuators
RU2658709C2 (en) * 2016-11-15 2018-06-22 Виктор Васильевич Попов Gas turbine engine compressor mechanization control device

Also Published As

Publication number Publication date
RU2289708C2 (en) 2006-12-20

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PD4A Correction of name of patent owner