Dirt evacuation devices

1. A system for reducing debris in a gas turbine engine comprising:

a component that defines a component cooling channel for receiving a cooling airflow;

a casing at least partially enclosing the component; and

a debris evacuation door coupled to the casing and having an open state in which the debris can exit the casing and a closed state,

wherein the gas turbine engine includes an axis and wherein the debris evacuation door is axially aligned with an opening to the component.

2. The system of claim 1 , wherein the debris evacuation door is at least one of a hinged door, a sliding door, a valve, or a plug.

3. The system of claim 1 , wherein the component is at least one of a vane, a vane support, or a blade outer air seal (BOAS).

4. The system of claim 1 , further comprising a controller configured to control the debris evacuation door to switch from the open state to the closed state and to switch from the closed state to the open state.

5. The system of claim 4 , wherein the controller is configured to control the debris evacuation door to be in the open state for at least a period of time after the gas turbine engine is initialized and before the gas turbine engine is at a ground idle state.

6. The system of claim 4 , wherein the controller is configured to control the debris evacuation door to be in the open state for a predetermined amount of time and to be in the closed state in response to the predetermined amount of time expiring.

7. The system of claim 4 , further comprising an input device coupled to the controller and configured to receive user input and wherein the controller is further configured to control the debris evacuation door to be in the open state or the closed state based on the user input.

8. The system of claim 1 , wherein the casing at least partially defines the component cooling channel.

9. The system of claim 8 , wherein a pressure of pressurized air within the component cooling channel is greater than an ambient air pressure outside the casing such that pressurized air within the component cooling channel forces the debris through the debris evacuation door in response to the debris evacuation door being in the open state.

10. The system of claim 1 , wherein the debris evacuation door is positioned in a high pressure turbine section of the gas turbine engine, and the debris evacuation door is located at a position along the axis at which the casing is at a largest radial distance from the axis relative to other locations in the high pressure turbine section.

11. The system of claim 1 , further comprising a nacelle at least partially enclosing the casing and an evacuation lead pipe coupled between the debris evacuation door and the nacelle and configured to channel the debris from the debris evacuation door through the nacelle to an area outside of the nacelle.

12. The system of claim 1 , wherein the debris evacuation door is at least one of magnetized or configured to be switched between a magnetized state and a non-magnetized state.

13. A system for reducing debris in a gas turbine engine comprising:

a component defining a component cooling channel for receiving a cooling airflow;

a casing at least partially enclosing the component;

a debris evacuation door coupled to the casing and having an open state in which debris can exit the casing and a closed state;

an input device configured to receive user input; and

a controller coupled to the input device and configured to control the debris evacuation door to switch from the open state to the closed state and to switch from the closed state to the open state based on the user input.

14. The system of claim 13 , wherein the debris evacuation door is at least one of a hinged door, a sliding door, a valve, or a plug.

15. The system of claim 13 , wherein the controller is further configured to control the debris evacuation door to be in the open state for at least a period of time after the gas turbine engine is initialized and before the gas turbine engine is at a ground idle state.

16. The system of claim 13 , wherein the casing at least partially defines the component cooling channel and wherein a pressure of pressurized air within the component cooling channel is greater than an ambient air pressure outside the casing such that pressurized air within the component cooling channel forces the debris through the debris evacuation door in response to the debris evacuation door being in the open state.

17. A method for removing debris from a turbine section of a gas turbine engine comprising:

determining, by a controller, that the debris should be removed from the turbine section of the gas turbine engine;

controlling, by the controller, a debris evacuation door coupled to a casing of the gas turbine engine to be in an open state in which the debris can exit the casing in response to determining that the debris should be removed; and

controlling, by the controller, the debris evacuation door to be in a closed state in response to at least one of receiving a user input or expiration of a predetermined amount of time.

18. The method of claim 17 , wherein the determining that the debris should be removed further includes determining, by the controller, that at least one of the gas turbine engine is initializing or a request has been made to initialize the gas turbine engine.

19. The method of claim 17 , further comprising controlling, by the controller, the debris evacuation door to switch to a non-magnetized state in response to determining that the debris should be removed.