RU733362C - GAS TURBINE ENGINE REGULATION SYSTEM - Google Patents

GAS TURBINE ENGINE REGULATION SYSTEM Download PDF

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Publication number
RU733362C
RU733362C SU2666461/06A SU2666461A RU733362C RU 733362 C RU733362 C RU 733362C SU 2666461/06 A SU2666461/06 A SU 2666461/06A SU 2666461 A SU2666461 A SU 2666461A RU 733362 C RU733362 C RU 733362C
Authority
RU
Russia
Prior art keywords
gas turbine
turbine engine
regulation system
acceleration
limiter
Prior art date
Application number
SU2666461/06A
Other languages
Russian (ru)
Inventor
Г.В. Карягин
В.И. Шеронкин
Л.Г. Штеренберг
Filing date
Publication date
Application filed filed Critical
Priority to SU2666461/06A priority Critical patent/SU733362A1/en
Priority claimed from SU2666461/06A external-priority patent/SU733362A1/en
Application granted granted Critical
Publication of RU733362C publication Critical patent/RU733362C/en
Publication of SU733362A1 publication Critical patent/SU733362A1/en

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Claims (2)

1. Система регулирования газотурбинного двигателя, содержащая качающий узел, в выходном канале которого последовательно расположены автомат запуска и совмещенный с автоматом разгона регулятор вращения, гидравлически связанные с клапаном постоянного перепада, и высотный корректор, дозирующее сечение которого соединено входным и выходным каналами соответственно со входом и выходом дозирующего сечения регулятора частоты вращения, отличающаяся тем, что, с целью повышения надежности разгона двигателя, в одном из каналов установлен ограничитель работы высотного корректора.1. A control system for a gas turbine engine containing a pumping unit, in the output channel of which an automatic start-up and a rotation regulator combined with an automatic acceleration are located in series, hydraulically connected to a constant differential valve, and an altitude corrector, the metering section of which is connected to the input and output channels, respectively, to the input outlet of the dosing section of the speed controller, characterized in that, in order to increase the reliability of the engine acceleration, a limiter for the operation of the altitude corrector is installed in one of the channels. 2. Система по п. 1, отличающаяся тем, что ограничитель выполнен в виде золотника, кинематически соединенного с автоматом разгона.2. The system of claim. 1, characterized in that the limiter is made in the form of a spool, kinematically connected to the automatic acceleration.
SU2666461/06A 1978-09-18 1978-09-18 GAS TURBINE ENGINE REGULATION SYSTEM SU733362A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2666461/06A SU733362A1 (en) 1978-09-18 1978-09-18 GAS TURBINE ENGINE REGULATION SYSTEM

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2666461/06A SU733362A1 (en) 1978-09-18 1978-09-18 GAS TURBINE ENGINE REGULATION SYSTEM

Publications (2)

Publication Number Publication Date
RU733362C true RU733362C (en) 2021-07-01
SU733362A1 SU733362A1 (en) 2021-07-01

Family

ID=76756057

Country Status (1)

Country Link
SU (1) SU733362A1 (en)

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