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RU2008121033A - GAS-TURBINE ENGINE COMPRESSOR CONTROL DEVICE - Google Patents

GAS-TURBINE ENGINE COMPRESSOR CONTROL DEVICE Download PDF

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Publication number
RU2008121033A
RU2008121033A RU2008121033/06A RU2008121033A RU2008121033A RU 2008121033 A RU2008121033 A RU 2008121033A RU 2008121033/06 A RU2008121033/06 A RU 2008121033/06A RU 2008121033 A RU2008121033 A RU 2008121033A RU 2008121033 A RU2008121033 A RU 2008121033A
Authority
RU
Russia
Prior art keywords
compressor
pressure sensor
air pressure
output
inlet
Prior art date
Application number
RU2008121033/06A
Other languages
Russian (ru)
Other versions
RU2392498C2 (en
Inventor
Юрий Петрович Дудкин (RU)
Юрий Петрович Дудкин
Виктор Александрович Гладких (RU)
Виктор Александрович Гладких
Геннадий Викторович Фомин (RU)
Геннадий Викторович Фомин
Сергей Владимирович Остапенко (RU)
Сергей Владимирович Остапенко
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 RU2008121033/06A priority Critical patent/RU2392498C2/en
Publication of RU2008121033A publication Critical patent/RU2008121033A/en
Application granted granted Critical
Publication of RU2392498C2 publication Critical patent/RU2392498C2/en

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  • Control Of Positive-Displacement Air Blowers (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)

Abstract

Устройство для управления механизацией компрессора ГТД, содержащее датчик давления воздуха на входе в компрессор, датчик давления воздуха на выходе из компрессора, счетно-решающее устройство, устройство сравнения, выход которого соединен с золотником управления гидроцилиндром привода лопаток ВНА, отличающееся тем, что дополнительно счетно-решающее устройство выполнено в виде пространственного кулачка, первый вход которого соединен с датчиком давления воздуха на входе в компрессор, второй - с гидроцилиндром привода лопаток ВНА, а выход - с устройством сравнения, второй вход которого соединен с выходом датчика давления воздуха за компрессором.A device for controlling the mechanization of a gas turbine compressor, comprising an air pressure sensor at the compressor inlet, an air pressure sensor at the compressor outlet, a counting device, a comparison device, the output of which is connected to the control valve of the hydraulic drive cylinder of the VNA blades, characterized in that it is additionally countable the decisive device is made in the form of a spatial cam, the first input of which is connected to the air pressure sensor at the inlet to the compressor, the second to the hydraulic cylinder for driving the VNA blades, and the output - a comparison device, a second input coupled to an output air pressure sensor of the compressor.

Claims (1)

Устройство для управления механизацией компрессора ГТД, содержащее датчик давления воздуха на входе в компрессор, датчик давления воздуха на выходе из компрессора, счетно-решающее устройство, устройство сравнения, выход которого соединен с золотником управления гидроцилиндром привода лопаток ВНА, отличающееся тем, что дополнительно счетно-решающее устройство выполнено в виде пространственного кулачка, первый вход которого соединен с датчиком давления воздуха на входе в компрессор, второй - с гидроцилиндром привода лопаток ВНА, а выход - с устройством сравнения, второй вход которого соединен с выходом датчика давления воздуха за компрессором. A device for controlling the mechanization of a gas turbine compressor, comprising an air pressure sensor at the compressor inlet, an air pressure sensor at the compressor outlet, a counting device, a comparison device, the output of which is connected to the control valve of the hydraulic drive cylinder of the VNA blades, characterized in that it is additionally countable the decisive device is made in the form of a spatial cam, the first input of which is connected to the air pressure sensor at the inlet to the compressor, the second to the hydraulic cylinder for driving the VNA blades, and the output - a comparison device, a second input coupled to an output air pressure sensor of the compressor.
RU2008121033/06A 2008-05-26 2008-05-26 Control device of mechanisation of gas turbine engine compressor RU2392498C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2008121033/06A RU2392498C2 (en) 2008-05-26 2008-05-26 Control device of mechanisation of gas turbine engine compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2008121033/06A RU2392498C2 (en) 2008-05-26 2008-05-26 Control device of mechanisation of gas turbine engine compressor

Publications (2)

Publication Number Publication Date
RU2008121033A true RU2008121033A (en) 2009-12-10
RU2392498C2 RU2392498C2 (en) 2010-06-20

Family

ID=41488871

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2008121033/06A RU2392498C2 (en) 2008-05-26 2008-05-26 Control device of mechanisation of gas turbine engine compressor

Country Status (1)

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RU (1) RU2392498C2 (en)

Families Citing this family (5)

* 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
DE102013202982A1 (en) * 2013-02-22 2014-08-28 Siemens Aktiengesellschaft Method for operating a gas turbine below its rated power
RU174395U1 (en) * 2016-11-08 2017-10-11 Виктор Васильевич Попов Gas turbine compressor mechanization control device
RU2658709C2 (en) * 2016-11-15 2018-06-22 Виктор Васильевич Попов Gas turbine engine compressor mechanization control device
RU2639923C1 (en) * 2017-01-27 2017-12-25 Виктор Васильевич Попов Method of mechanization control of gas turbine engine compressor

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1469511A (en) * 1973-07-05 1977-04-06 Lucas Industries Ltd Fluid pressure operated actuator device
RU1588027C (en) * 1988-02-01 1994-10-30 Акционерное общество "Авиадвигатель" Method and apparatus for control of position of rotating guide blades of gas-turbine engine
DE3805119A1 (en) * 1988-02-18 1989-08-31 Gutehoffnungshuette Man METHOD AND DEVICE FOR REGULATING TURBO COMPRESSORS
RU2287089C2 (en) * 2004-10-13 2006-11-10 Открытое акционерное общество "СТАР" Gas-turbine engine compressor control device

Also Published As

Publication number Publication date
RU2392498C2 (en) 2010-06-20

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Legal Events

Date Code Title Description
PD4A Correction of name of patent owner
MM4A The patent is invalid due to non-payment of fees

Effective date: 20200527

NF4A Reinstatement of patent

Effective date: 20211126