Mist and vapor eliminating filter, device, system and method of use

A method of filtering aircraft cabin air, the method comprising passing aircraft air through a system for filtering aircraft air, the system comprising:

• (A) a mist and vapor eliminating (MaVE) filter device comprising
• a main housing including a main housing body, an inlet duct connected to a first end of the main housing body, and an outlet duct connected to a second end of the main housing body;
• and,
• a MaVE filter comprising a first stage filter and a second stage filter;
• (a) the first stage hollow filter comprising
• a first housing having a first housing first end and a first housing second end;
• and, arranged in the first housing:
• (i) a first adsorption element comprising activated carbon and/or activated clay;
• and,
• (ii) a first hydrophobic pleated hollow porous medium surrounding the first adsorption element;
• the first stage hollow filter including a first end cap connected to the first housing first end;
• (b) the second stage hollow filter comprising
• a second housing having second housing first end and a second housing second end;
• and, arranged in the second housing:
• (iii) a second adsorption element comprising activated carbon and/or activated clay;
• (iv) a second hydrophobic pleated hollow porous medium surrounding the second adsorption element;
• the second stage hollow filter including a second end cap connected to the second housing second end;
• wherein the first housing second end is connected to the second housing first end by an intermediate end cap;
• the intermediate end cap including a first drain channel between the first housing second end and the second housing first end, wherein the first drain channel is arranged to receive free water passing along an upstream surface of the first hydrophobic pleated hollow porous medium;
• and,
• the second end cap including a second drain channel at the second housing second end, wherein the second drain channel is arranged to receive free water passing along an upstream surface of the second hydrophobic pleated hollow porous medium;
• wherein the MaVE filter device is arranged in the main housing between the inlet duct and the outlet duct;
• wherein the MaVE filter includes a horizontal axis, and the first and second drain channels are arranged perpendicular to the horizontal axis of the mist and vapor eliminating filter;
• the system further comprising
• (B) a bypass valve including a pivotable bypass plate, arranged in a hollow sleeve, wherein the hollow sleeve is arranged between the main housing body and the outlet duct, the hollow sleeve providing an aircraft air flow path through the MaVE filter device partially bypassing the MaVE filter when the bypass valve is opened;
• the method including collecting free water on an upstream surface of the first hydrophobic pleated hollow porous medium and collecting free water on an upstream surface of the second hydrophobic pleated hollow porous medium;
• opening the bypass valve;
• and
• flowing aircraft air through the MaVE filter device while partially bypassing the MaVE filter.