Importance

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Abstract

Portable aircraft turbine engine washing systems and methods are provided. One such washing system has a portable base unit, a wash line connectable to the portable base unit and configured to be connected to an aircraft turbine engine or a fluid delivery cleaning device, and a water tank movable with the portable base unit and can hold water. A water pump apparatus is movable with the portable base unit and can pump water out of the water tank and into the wash line. A solution tank is movable with the portable base unit and can hold a solution. A solution pump apparatus is also movable with the portable base unit and can pump solution from the solution tank into fluid communication with the wash line. A controller apparatus adjustably controls a dilution ratio of the solution with water while the solution and water are pumped into the wash line.

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First Claim