RU97107079A - METHOD FOR AUTOMATIC CONTROL OF AIRCRAFT GAS TURBINE ENGINE - Google Patents

METHOD FOR AUTOMATIC CONTROL OF AIRCRAFT GAS TURBINE ENGINE

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Publication number
RU97107079A
RU97107079A RU97107079/06A RU97107079A RU97107079A RU 97107079 A RU97107079 A RU 97107079A RU 97107079/06 A RU97107079/06 A RU 97107079/06A RU 97107079 A RU97107079 A RU 97107079A RU 97107079 A RU97107079 A RU 97107079A
Authority
RU
Russia
Prior art keywords
gas turbine
turbine engine
compressor
aircraft gas
automatic control
Prior art date
Application number
RU97107079/06A
Other languages
Russian (ru)
Other versions
RU2118681C1 (en
Inventor
А.Ф. Масолов
Original Assignee
Московское авиационное производственное объединение "МИГ"
Filing date
Publication date
Application filed by Московское авиационное производственное объединение "МИГ" filed Critical Московское авиационное производственное объединение "МИГ"
Priority to RU97107079A priority Critical patent/RU2118681C1/en
Priority claimed from RU97107079A external-priority patent/RU2118681C1/en
Application granted granted Critical
Publication of RU2118681C1 publication Critical patent/RU2118681C1/en
Publication of RU97107079A publication Critical patent/RU97107079A/en

Links

Claims (1)

Способ автоматического регулирования газотурбинного двигателя летательного аппарата, состоящий в изменении угла установки аппаратов компрессора в зависимости от температуры торможения потока на входе в газотурбинный двигатель и физических оборотов компрессора, отличающийся тем, что дополнительно с помощью датчиков пульсаций измеряют на входе газотурбинного двигателя пульсации полного (или статического) давления, рассчитывают спектральную плотность мощности в рабочем диапазоне частот, сравнивают их мощность на характерных частотах с эталоном (на границе газодинамической устойчивости) и подают сигналы в систему автоматического регулирования газотурбинного двигателя для изменения углов установки направляющих аппаратов компрессора.A method for automatically controlling an aircraft gas turbine engine, which consists in changing the installation angle of the compressor apparatuses depending on the braking temperature of the flow at the inlet of the gas turbine engine and the physical speed of the compressor, characterized in that pulsation sensors additionally measure the pulsation of the full (or static) at the inlet of the gas turbine engine ) pressure, calculate the spectral power density in the operating frequency range, compare their power at characteristic frequencies x c standard (border dynamic stability) and provide signals to the automatic regulation of the gas turbine engine to change the angles of the compressor guide apparatus.
RU97107079A 1997-04-28 1997-04-28 Method of automatic control of gas-turbine engine of flying vehicle RU2118681C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU97107079A RU2118681C1 (en) 1997-04-28 1997-04-28 Method of automatic control of gas-turbine engine of flying vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU97107079A RU2118681C1 (en) 1997-04-28 1997-04-28 Method of automatic control of gas-turbine engine of flying vehicle

Publications (2)

Publication Number Publication Date
RU2118681C1 RU2118681C1 (en) 1998-09-10
RU97107079A true RU97107079A (en) 1999-02-27

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU97107079A RU2118681C1 (en) 1997-04-28 1997-04-28 Method of automatic control of gas-turbine engine of flying vehicle

Country Status (1)

Country Link
RU (1) RU2118681C1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2454557C2 (en) * 2010-09-22 2012-06-27 Закрытое Акционерное Общество Научно-Производственная Фирма "Газ-Система-Сервис" Method of control over gas turbine unit
RU2488009C2 (en) * 2011-10-10 2013-07-20 Федеральное государственное унитарное предприятие "Научно-производственный центр газотурбостроения "Салют" Method of control over gas turbine engine compressor distributors

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2678237C1 (en) * 2017-11-17 2019-01-24 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Method for operation of turbo-jet engines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2454557C2 (en) * 2010-09-22 2012-06-27 Закрытое Акционерное Общество Научно-Производственная Фирма "Газ-Система-Сервис" Method of control over gas turbine unit
RU2488009C2 (en) * 2011-10-10 2013-07-20 Федеральное государственное унитарное предприятие "Научно-производственный центр газотурбостроения "Салют" Method of control over gas turbine engine compressor distributors

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