摘要:
The present application provides an inlet air cooling system for cooling a flow air in a gas turbine engine. The inlet air cooling system may include an inlet filter house, a transition piece, an inlet duct, and an inlet ultrasonic water atomization system positioned about the inlet filter house, the transition piece, or the inlet duct to cool the flow of air.
摘要:
The present application provides an inlet air cooling system for cooling a flow air in a gas turbine engine. The inlet air cooling system may include an inlet filter house, a transition piece, an inlet duct, and an inlet ultrasonic water atomization system positioned about the inlet filter house, the transition piece, or the inlet duct to cool the flow of air.
摘要:
A system includes a turbine air quality device. The turbine air quality device includes a liquid desiccant path configured to circulate a liquid desiccant through an air flow directed to a turbine inlet. The turbine air quality device also includes a porous media disposed in the liquid desiccant path, wherein the porous media is configured to pass the air flow in direct contact with the liquid desiccant.
摘要:
A filter system for an air inlet of a gas turbine engine. The filter system may include a number of filters positioned about the air inlet and a water spray system positioned to spray the filters. The filters may include a hydrophobic or an oleophobic filter media.
摘要:
A filter system for an air inlet of a gas turbine engine. The filter system may include a number of filters positioned about the air inlet and a water spray system positioned to spray the filters. The filters may include a hydrophobic or an oleophobic filter media.