Aircraft fuel ice capture filter housing, aircraft fuel ice capture filter device, and usage

摘要

PROBLEM TO BE SOLVED: To provide a novel aircraft fuel ice capture filter device housing, an aircraft fuel ice capture filter device, and a method of use. An aircraft fuel ice capture filter device housing of the present invention comprises a fuel inlet, a fuel outlet, a main housing body comprising a cylindrical element that receives the flow of aircraft fuel from the fuel inlet, and a plurality of isolated ice capture filters. It comprises a cylindrical hollow insert having. Each isolated ice capture filter has a front end, a rear end, an upper wall, first and second sides, a bottom opening and a plurality of openings penetrating the upper wall, and the upper wall of the front end of each isolated ice capture filter is: Lifted from the inner surface of the cylindrical element to form an opening, the fuel inlet is configured to provide a tangentially moving fuel flow around the cylindrical element and the cylindrical insert. , Configured to accept aviation fuel filters with porous aviation fuel filter elements. [Selection diagram] FIG. 1A