System and method for controlling dual starter air valve
A system may comprise a sensor configured to measure a characteristic of an engine component. A valve assembly may have an airflow outlet in fluid communication with the engine component. The valve assembly may include a first valve. A first valve control device may be coupled to the first valve and configured to control the first valve based on a measurement by the sensor. A second valve may be in fluidic series with the first valve. A second valve control device may be coupled to the second valve and configured to control the second valve based on the measurement by the sensor.
1. A system for a gas turbine engine, comprising:
an air turbine starter operatively coupled to the gas turbine engine and configured to rotate the gas turbine engine during a startup condition;
a valve assembly having an airflow outlet in fluid communication with the air turbine starter, the valve assembly including:
a first valve,
a first valve control device coupled to the first valve and configured to control the first valve, wherein the first valve comprises a first piston, and wherein a position of the first piston is configured to control a pressure at the airflow outlet of the valve assembly,
a second valve in fluidic series with the first valve, and a second valve control device coupled to the second valve and configured to control the second valve;
a full authority digital engine control (FADEC) coupled to the valve assembly;
a sensor configured to measure a rotational speed of the gas turbine engine; and
a tangible, non-transitory memory configured to communicate with the FADEC, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the FADEC, cause the FADEC to perform operations comprising:
receiving, by the FADEC, a rotational speed measurement from the sensor;
determining, by the FADEC, an engine speed adjustment based on the rotational speed measurement, a position of at least one of the first valve or the second valve, and a desired speed;
generating, by the FADEC, a command for at least one of the first valve control device or the second valve control device based on the engine speed adjustment and the desired speed;
sending, by the FADEC, the command to at least one of the first valve control device or the second valve control device and, in response, controlling the pressure at the airflow outlet of the valve assembly to maintain the rotational speed measurement at the desired speed,
determining, by the FADEC, a valve condition indicative of a failure of at least one of the first valve or the second valve; and
modulating, by the FADEC, at least one of the first valve or the second valve in response to the valve condition.
2. The system of claim 1 , wherein the first valve control device comprises a torque motor servovalve.
3. The system of claim 2 , wherein the torque motor servovalve is configured to receive the command from the FADEC and to position the first valve.
4. The system of claim 3 , wherein the second valve control device comprises a solenoid and wherein the solenoid is configured to receive the command from the FADEC and to open or close the second valve.
5. The system of claim 1 , wherein the second valve comprises a second piston, and wherein a position of the second piston is configured to control the pressure at the airflow outlet of the valve assembly.
6. The system of claim 1 , wherein the first valve control device and the second valve control device are in electrical communication with the FADEC, and wherein the first valve control device comprises a first torque motor servovalve and the second valve control device comprises a second torque motor servovalve.
7. The system of claim 1 , wherein in response to the command, at least one of the first valve or the second valve is transitioned to an incremental position between a fully open position and a fully closed position.