RU2003109907A - FUEL SUPPLY CONTROL SYSTEM FOR GAS-TURBINE ENGINE - Google Patents

FUEL SUPPLY CONTROL SYSTEM FOR GAS-TURBINE ENGINE

Info

Publication number
RU2003109907A
RU2003109907A RU2003109907/06A RU2003109907A RU2003109907A RU 2003109907 A RU2003109907 A RU 2003109907A RU 2003109907/06 A RU2003109907/06 A RU 2003109907/06A RU 2003109907 A RU2003109907 A RU 2003109907A RU 2003109907 A RU2003109907 A RU 2003109907A
Authority
RU
Russia
Prior art keywords
turbine engine
gas
control system
fuel supply
supply control
Prior art date
Application number
RU2003109907/06A
Other languages
Russian (ru)
Other versions
RU2241133C1 (en
Inventor
Валерий Георгиевич Ширшов
Original Assignee
ОАО Омское машиностроительное конструкторское бюро
Filing date
Publication date
Application filed by ОАО Омское машиностроительное конструкторское бюро filed Critical ОАО Омское машиностроительное конструкторское бюро
Priority to RU2003109907/06A priority Critical patent/RU2241133C1/en
Priority claimed from RU2003109907/06A external-priority patent/RU2241133C1/en
Publication of RU2003109907A publication Critical patent/RU2003109907A/en
Application granted granted Critical
Publication of RU2241133C1 publication Critical patent/RU2241133C1/en

Links

Claims (1)

Система регулирования подачи топлива в газотурбинный двигатель, содержащая дозатор топлива с сервопоршнем, управляющий клапан дозатора, пневмогидропреобразователь, гидравлическую проточную камеру с дросселями и междроссельной камерой, связанной через один из дросселей с пневмогидропреобразователем, задатчик режима, электрогидропреобразователь и датчик положения, соединенные с дозатором, отличающаяся тем, что другой дроссель гидравлической проточной камеры соединен с дозатором, а управляющий клапан дозатора соединен через пружину с задатчиком режима и гидравлически - с сервопоршнем дозатора и межроссельной камерой.A system for regulating the supply of fuel to a gas turbine engine, comprising a fuel metering valve with a servo piston, a metering valve, a pneumohydraulic converter, a hydraulic flow chamber with throttles and an orifice chamber connected through one of the throttles with a pneumatic hydraulic converter, a mode dial, an electrohydrogen converter, and a position sensor connected to the metering unit in that the other throttle of the hydraulic flow chamber is connected to the dispenser, and the control valve of the dispenser is connected through a spring with the mode dial and hydraulically - with the servo piston of the dispenser and the inter-throttle chamber.
RU2003109907/06A 2003-04-07 2003-04-07 System to control delivery of fuel into gas-turbine engine RU2241133C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2003109907/06A RU2241133C1 (en) 2003-04-07 2003-04-07 System to control delivery of fuel into gas-turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2003109907/06A RU2241133C1 (en) 2003-04-07 2003-04-07 System to control delivery of fuel into gas-turbine engine

Publications (2)

Publication Number Publication Date
RU2003109907A true RU2003109907A (en) 2004-10-10
RU2241133C1 RU2241133C1 (en) 2004-11-27

Family

ID=34310659

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2003109907/06A RU2241133C1 (en) 2003-04-07 2003-04-07 System to control delivery of fuel into gas-turbine engine

Country Status (1)

Country Link
RU (1) RU2241133C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2504677C1 (en) * 2012-10-18 2014-01-20 Открытое акционерное общество "Омское машиностроительное конструкторское бюро" Two-channel gas turbine fuel feed and adjustment system

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