BYPASS TURBINE INTAKE
A system, that includes a bypass turbine intake configured to route a bypass supply of air to a turbine engine to bypass an air filter of a main turbine intake, wherein the bypass turbine intake comprises a louvered door having a plurality of louvers configured to move between a closed position and an open position, the open position enables flow of the bypass supply of air to the turbine engine, and the closed position disables flow of the bypass supply of air to the turbine engine.
1 . A system, comprising:
a bypass turbine intake configured to route a bypass supply of air to a turbine engine to bypass an air filter of a main turbine intake, wherein the bypass turbine intake comprises a louvered door having a plurality of louvers configured to move between a closed position and an open position, the open position enables flow of the bypass supply of air to the turbine engine, and the closed position disables flow of the bypass supply of air to the turbine engine.
2 . The system of claim 1 , wherein the louvered door comprises a sealing system configured to seal the plurality of louvers relative to one another in the closed position.
3 . The system of claim 2 , wherein each louver of the plurality of louvers comprises a first seal portion disposed along a leading edge portion of the louver, a second seal portion disposed along a trailing edge portion of the louver, a third seal portion disposed along a first end portion of the louver, and a fourth seal portion disposed along a second end portion of the louver.
4 . The system of claim 1 , wherein the louvered door comprises a drive coupled to a louver actuator, and the louvered actuator is configured to move the plurality of louvers between the closed position and the open position in response to the drive.
5 . The system of claim 4 , comprising a controller coupled to the drive, wherein the controller is configured to control the drive to move the plurality of louvers from the closed position to the open position in response to a condition of the main turbine intake.
6 . The system of claim 5 , comprising at least one sensor configured to indicate the condition of the main turbine intake, wherein the condition comprises a change in a main supply of air through the main turbine intake outside a threshold range.
7 . The system of claim 1 , comprising the main turbine intake having the air filter, wherein the main turbine intake is configured to route a main supply of air to the turbine engine.
8 . The system of claim 1 , comprising the turbine engine.
9 . The system of claim 8 , comprising a propulsion system coupled to the turbine engine.
10 . The system of claim 9 , comprising a watercraft having the turbine engine, the propulsion system, the main turbine intake, and the bypass turbine intake.
11 . A system, comprising:
a bypass engine intake configured to route a bypass supply of air to an engine to bypass an air filter of a main engine intake, wherein the bypass engine intake comprises:
a louvered door having a plurality of louvers;
a drive having a louver actuator; and
a controller configured to control the drive to move the plurality of louvers between a closed position and an open position in response to a condition of the main engine intake, the open position enables flow of the bypass supply of air to the engine, the closed position disables flow of the bypass supply of air to the engine, and the condition comprises a change in a main supply of air through the main air intake outside a threshold range.
12 . The system of claim 11 , wherein the louvered door comprises a sealing system configured to seal the plurality of louvers relative to one another in the closed position.
13 . The system of claim 11 , wherein the bypass engine intake comprises a first screen disposed upstream of the louvered door or a second screen disposed downstream from the louvered door.
14 . The system of claim 11 , comprising at least one sensor configured to indicate the condition of the main engine intake, wherein the sensor comprises a flow sensor or a pressure sensor.
15 . The system of claim 11 , comprising the main engine intake having the air filter, wherein the main engine intake is configured to route a main supply of air to the engine.
16 . The system of claim 11 , comprising the engine.
17 . The system of claim 16 , comprising a propulsion system coupled to the engine.
18 . A system, comprising:
a bypass engine intake configured to route a bypass supply of air to an engine to bypass an air filter of a main engine intake, wherein the bypass engine intake comprises:
a louvered door having a plurality of louvers;
a drive having a louver actuator;
a sensor configured to indicate the condition of the main turbine intake; and
a controller configured to control the drive to move the plurality of louvers between a closed position and an open position in response to an indication of the condition of the main engine intake from the sensor, the open position enables flow of the bypass supply of air to the engine, the closed position disables flow of the bypass supply of air to the engine, and the condition comprises a change in a main supply of air through the main air intake outside a threshold range.
19 . The method of claim 18 , wherein the sensor senses a pressure differential across the air filter in the main engine intake.
20 . The method of claim 18 , wherein the sensor senses a flow rate below a threshold flow rate.