FIELD: power industry.
SUBSTANCE: proposed method consists in the fact that the time-dependant signal that characterises the ignition current of igniter (14) is compared to upper limit value and lower limit value, and at the same time, the characteristic signal is compared to average value of the specified current, relative to which the ignition current shall randomly oscillate at igniter (14) in operation.
EFFECT: monitoring of the gas turbine ignition process, thus preventing unsuccessful start-up of gas turbine.
24 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
BURNER OF GAS TURBINE, AND GAS TURBINE | 2007 |
|
RU2439433C2 |
AIRCRAFT GAS TURBINE ENGINE CAPACITIVE IGNITION SYSTEM CONTROL DEVICE | 2021 |
|
RU2767663C1 |
METHOD FOR MONITORING SERVICEABILITY OF HIGH-VOLTAGE CAPACITIVE IGNITION SYSTEMS OF GAS TURBINE ENGINES | 2021 |
|
RU2767662C1 |
AIRCRAFT ENGINES CAPACITIVE IGNITION SYSTEM CONTROL DEVICE | 2015 |
|
RU2614388C2 |
GAS BURNER | 2018 |
|
RU2705536C1 |
GAS BURNER IGNITION SYSTEM (VERSIONS) | 2008 |
|
RU2486411C2 |
ONBOARD DIAGNOSTICS OF IGNITION COIL UNDER COMPLEX ELECTROMAGNETIC CONDITIONS | 2014 |
|
RU2557806C1 |
GAS TURBINE BURNER | 1996 |
|
RU2156405C2 |
VORTEX BURNER FOR GAS TURBINE | 2016 |
|
RU2635958C1 |
GAS TURBINE ENGINE RUNNING ON LEAN FUEL MIX | 2011 |
|
RU2521179C2 |
Authors
Dates
2013-03-10—Published
2009-01-20—Filed