Systems and methods for dry fog inlet particle separator

1. An inlet particle separator system, for a gas turbine engine that is installed onboard a vehicle, comprising:

a source of pressurized water;

a source of pressurized air;

a separator manifold including a manifold inlet upstream from a first manifold outlet and a second manifold outlet, the manifold inlet configured to receive an incoming airflow, the first manifold outlet configured to be fluidly coupled to an inlet of the gas turbine engine to direct the incoming airflow into the inlet of the gas turbine engine, the inlet of the gas turbine engine including an inlet door, the separator manifold defining a tortuous path between the manifold inlet and the first manifold outlet, the first manifold outlet including a first sealing member coupled to a first sidewall of the separator manifold at the first manifold outlet and a second sealing member coupled to a second sidewall of the separator manifold at the first manifold outlet, the first sealing member configured to form a first seal between the separator manifold and the vehicle, and the second sealing member configured to form a second seal between the separator manifold and the inlet door;

at least one dry fog nozzle coupled proximate the manifold inlet so as to face at least partially away from the manifold inlet, the at least one dry fog nozzle fluidly coupled to the source of pressurized water to receive pressurized water and the source of pressurized air to receive pressurized air, the at least one dry fog nozzle configured to generate a spray of dry fog based on the pressurized water and pressurized air, the at least one dry fog nozzle positioned external to the separator manifold, and the at least one dry fog nozzle is configured to direct the spray of dry fog in a direction transverse to the incoming airflow outward and away from the manifold inlet to agglomerate with fine particles in the incoming airflow to form agglomerated particles; and

a scavenging system coupled to the separator manifold downstream from the manifold inlet, and the scavenging system is configured to remove the agglomerated particles from the separator manifold.

2. The inlet particle separator system of claim 1 , wherein the second manifold outlet is separated from the first manifold outlet by a splitter.

3. The inlet particle separator system of claim 2 , wherein the scavenging system is fluidly coupled to the second manifold outlet and is configured to exhaust the agglomerated particles through the second manifold outlet.

4. The inlet particle separator system of claim 1 , wherein the separator manifold is removably coupled to the inlet of the gas turbine engine.

5. The inlet particle separator system of claim 1 , wherein the pressurized water supply and the pressurized air supply are a ground-based system, and the at least one dry fog nozzle, the separator manifold and the scavenging system are a vehicle-based system onboard the vehicle.

6. The inlet particle separator system of claim 1 , wherein the pressurized water supply, the pressurized air supply, the at least one dry fog nozzle, the separator manifold and the scavenging system are a vehicle-based system onboard the vehicle.

7. The inlet particle separator system of claim 1 , wherein the first sidewall interconnects the manifold inlet and the first manifold outlet, a third sidewall is opposite the first sidewall, a first end of the first sidewall comprises a first bellmouth curvature at the manifold inlet, a second end of the third sidewall comprises a second bellmouth curvature at the manifold inlet and the dry fog nozzle is positioned wholly external to the manifold inlet of the separator manifold proximate and upstream of the first bellmouth curvature and faces away from the manifold inlet to direct the spray of dry fog away from the manifold inlet.

8. The inlet particle separator system of claim 1 , wherein the first sidewall further includes a convex curve downstream of the manifold inlet.

9. A method of providing a clean airflow to an inlet of a gas turbine engine installed onboard a vehicle, comprising:

fluidly coupling a separator manifold including at least one dry fog nozzle to an inlet duct of the gas turbine engine such that a first manifold outlet of the separator manifold is fluidly coupled to the inlet duct, the inlet duct including an inlet door, the at least one dry fog nozzle positioned external to a manifold inlet of the separator manifold, the manifold inlet upstream from the first manifold outlet, the separator manifold defining a tortuous path from the manifold inlet to the first manifold outlet, the first manifold outlet including a first sealing member coupled to a first sidewall of the separator manifold at the first manifold outlet and a second sealing member coupled to a second sidewall of the separator manifold at the first manifold outlet, the first sealing member configured to form a first seal between the separator manifold and the vehicle, and the second sealing member configured to form a second seal between the separator manifold and the inlet door;

fluidly coupling a pressurized water supply to the at least one dry fog nozzle to supply the at least one dry fog nozzle with pressurized water;

fluidly coupling a pressurized air supply to the at least one dry fog nozzle to supply the at least one dry fog nozzle with pressurized air;

outputting a spray of dry fog by the at least one dry fog nozzle based on the receipt of the pressurized water and the pressurized air outward and away from the manifold inlet in a direction transverse to an incoming airflow into the manifold inlet to agglomerate with fine particles in the incoming airflow to form agglomerated particles;

separating the agglomerated particles from the incoming airflow with the tortuous path defined between the manifold inlet and the first manifold outlet; and

exhausting the agglomerated particles though a second manifold outlet with a scavenging system.

10. An inlet particle separator system for a gas turbine engine that is installed onboard a vehicle, comprising:

a source of pressurized water;

a source of pressurized air;

a separator manifold including a manifold inlet upstream from a first manifold outlet, the manifold inlet configured to receive an incoming airflow, the first manifold outlet configured to be fluidly coupled to an inlet of the gas turbine engine to direct the incoming airflow into the inlet of the gas turbine engine, the inlet of the gas turbine engine including an inlet door, the separator manifold defining a tortuous path from the manifold inlet to the first manifold outlet, the first manifold outlet including a first sealing member coupled to a first sidewall of the separator manifold at the first manifold outlet and a second sealing member coupled to a second sidewall of the separator manifold at the first manifold outlet, the first sealing member configured to form a first seal between the separator manifold and the vehicle, and the second sealing member configured to form a second seal between the separator manifold and the inlet door;

at least one dry fog nozzle coupled proximate the manifold inlet so as to face at least partially away from the manifold inlet, the at least one dry fog nozzle fluidly coupled to the source of pressurized water to receive pressurized water and the source of pressurized air to receive pressurized air, the at least one dry fog nozzle configured to generate a spray of dry fog based on the pressurized water and pressurized air, the at least one dry fog nozzle external to the separator manifold, and the at least one dry fog nozzle is configured to direct the spray of dry fog in a direction transverse to the incoming airflow outward and away from the manifold inlet to agglomerate with fine particles in the incoming airflow to form agglomerated particles; and

a scavenging system coupled to the separator manifold downstream from the manifold inlet, and the scavenging system is configured to remove the agglomerated particles from the separator manifold.

11. The inlet particle separator system of claim 10 , wherein the separator manifold includes a second manifold outlet, the second manifold outlet downstream from the first manifold outlet and separated from the first manifold outlet by a splitter, the scavenging system is fluidly coupled to the second manifold outlet and is configured to exhaust the agglomerated particles through the second manifold outlet.

12. The inlet particle separator system of claim 10 , wherein the first sidewall interconnects the manifold inlet and the first manifold outlet, a third sidewall is opposite the first sidewall, a first end of the first sidewall comprises a first bellmouth curvature at the manifold inlet, a first end of the third sidewall comprises a second bellmouth curvature at the manifold inlet and the at least one dry fog nozzle is positioned external to the manifold inlet proximate and upstream of the first bellmouth curvature.

13. The inlet particle separator system of claim 10 , wherein the pressurized water supply and the pressurized air supply are a ground-based system, and the at least one dry fog nozzle, the separator manifold and the scavenging system are a vehicle-based system onboard the vehicle.

14. The inlet particle separator system of claim 10 , wherein the separator manifold is removably coupled to the inlet of the gas turbine engine.