Electronically controlled pressure relief system for an engine
A fluid system is provided for an aircraft engine. This fluid system includes a lubricant reservoir and a pressure relief system. The lubricant reservoir includes an internal volume. The pressure relief system includes a sensor system, a pressure relieve valve and a controller. The sensor system is configured to provide sensor data indicative of an air pressure within the internal volume. The pressure relief valve is fluidly coupled with the internal volume. The controller is configured to control operation of the pressure relieve valve based on the sensor data.
1. A fluid system for an aircraft engine, comprising:
a lubricant reservoir comprising an internal volume; and
a pressure relief system including a sensor system, a pressure relief valve and a controller, the sensor system configured to provide sensor data indicative of an air pressure within the internal volume, the pressure relief valve fluidly coupled with the internal volume, and the controller configured to control operation of the pressure relief valve based on the sensor data,
wherein the pressure relief valve is a variable area valve with a variable area opening, and
wherein the pressure relief valve comprises a valve actuator and a valve element, and the valve actuator is configured to move the valve element to each of a fully closed position, a fully open position, and a partially open position.
2. The fluid system of claim 1 , wherein the controller is configured to signal the pressure relief valve to vent a fluid comprising air out of the internal volume when the air pressure within the internal volume is greater than a threshold.
3. The fluid system of claim 1 , wherein the controller is configured to signal the pressure relief valve to close when the air pressure within the internal volume is less than a threshold.
4. The fluid system of claim 1 , wherein
the controller is configured to signal the pressure relief valve to change a flow area of the variable area opening from a first value to a second value based on the sensor data.
5. The fluid system of claim 1 , wherein the controller is further configured to control the operation of the pressure relieve relief valve based on an operational parameter of the aircraft engine.
6. The fluid system of claim 1 , wherein the controller is further configured to control the operation of the pressure relief valve based on an altitude of the aircraft engine.
7. The fluid system of claim 1 , wherein the controller is further configured to control the operation of the pressure relief valve based on an ambient parameter outside of the aircraft engine.
8. The fluid system of claim 1 , wherein the pressure relief valve comprises an iris valve.
9. The fluid system of claim 1 , wherein the pressure relief valve comprises a butterfly valve.
10. The fluid system of claim 1 , wherein the pressure relief valve comprises a needle valve.
11. The fluid system of claim 1 , wherein the pressure relieve-relief valve is configured to vent a fluid comprising air out of the internal volume into an environment external to the aircraft engine.
12. The fluid system of claim 1 , further comprising:
an engine component; and
a source circuit configured to direct a lubricant from the internal volume to the engine component.
13. The fluid system of claim 12 , further comprising a return circuit configured to direct the lubricant from the engine component into the internal volume.
14. The fluid system of claim 13 , further comprising a deaerator configured to separate air from the lubricant directed into the internal volume through the return circuit.
15. An apparatus for an aircraft, comprising:
a gas turbine engine comprising a reservoir and a pressure relief system, the reservoir comprising an internal volume, and the pressure relief system including a sensor system, a pressure relief valve and a controller;
the sensor system configured to provide sensor data indicative of a gas pressure within the internal volume;
the pressure relief valve fluidly coupled with the internal volume; and
the controller configured to control operation of the pressure relief valve based on the sensor data,
wherein the pressure relief valve is a variable area valve, and
wherein the pressure relief valve comprises a valve actuator and a valve element, and the valve actuator is configured to move the valve element to each of a fully closed position, a fully open position, and a partially open position.
16. The apparatus of claim 15 , wherein the controller is configured to signal the pressure relief valve to vent a gas out of the internal volume when the gas pressure within the internal volume rises above a threshold.
17. The apparatus of claim 15 , wherein the reservoir is configured to contain a liquid within the internal volume.
18. A fluid system for an aircraft engine, comprising:
a fluid reservoir comprising an internal volume; and
a pressure relief system including a sensor system, a pressure relief valve and a controller, the sensor system configured to determine a fluid pressure within the internal volume and provide sensor data indicative of the fluid pressure, the pressure relief valve comprising a variable area opening fluidly coupled with the internal volume, and the controller configured to signal the pressure relief valve to selectively change a flow area of the variable area opening based on the sensor data to change how much gas is vented out of the internal volume through the variable area opening;
wherein the pressure relief valve comprises a valve actuator and a valve element, and the valve actuator is configured to move the valve element to each of a fully closed position, a fully open position, and a partially open position.
19. The fluid system of claim 18 , wherein the fluid reservoir is configured to contain engine lubricant within the internal volume.