Comb for inlet barrier filter system
An inlet barrier filter system for mounting on an aircraft to filter air prior to intake into an engine of the aircraft includes a frame having at least two curved frame members defining an opening. A filter element has a curved inward face and is received in the opening of the frame. The filter element includes filter media having pleats. A comb is attached to the frame and includes spaced-apart teeth that support the pleats. The comb is curved to generally conform to the curved inward face of the filter.
1. An inlet barrier filter system for mounting on an aircraft to filter air prior to intake into an engine of the aircraft, the filter system comprising:
a frame including at least two curved frame members defining an opening;
a filter element having a curved inward face and received in the opening of the frame;
the filter element including filter media having pleats;
a comb attached to the frame and including spaced-apart teeth, the comb supporting the pleats of the filter media; and
the comb being curved to generally conform to the curved inward face of the filter element;
a strut for stiffening the comb and the filter system.
2. The filter system of claim 1 wherein the comb includes at least two, separate, curved segments, the two segments being joined together and extending from one of the frame members to another of the frame members.
3. The filter system of claim 1 wherein each segment includes less than about 25 teeth.
4. The filter system of claim 1 wherein the comb includes at least three separate, curved segments, a first of the segments being attached at an end to one of the frame members and at an opposite end to a second segment, and a third segment being attached at an end to the second segment and at an opposite end to the frame.
5. The filter system of claim 4 wherein the frame includes opposing top and bottom members and opposing left and right side members, wherein the side members are curved to conform to the aircraft.
6. The filter system of claim 1 wherein a first strut member extends from the right frame member to the comb, and a second strut member extends from the left frame member to the comb, the struts extending generally perpendicular to the respective frame members and the comb.
7. The filter system of claim 1 wherein the frame is adjacent an outer moldline of the aircraft, a convex outer face of the filter element conforming to the outer moldline.
8. The filter system of claim 7 in combination with the aircraft and wherein the aircraft is a helicopter.
9. An inlet barrier filter system mounted on a helicopter to filter air prior to intake into an engine of the helicopter, the filter system comprising:
a curved frame including at least two curved frame members and defining an opening, the frame being attached to the helicopter and disposed to filter air prior to intake into the engine;
a filter element having a curved face and received in the opening of the frame;
the filter element including filter media having pleats;
a comb attached to the frame and supporting the pleats of the filter media;
the comb being curved to generally conform to the curved face of the filter element; and
the comb including at least two separate, curved segments, the two segments being joined together and extending from one of the frame members to another of the frame members.
10. The filter system of claim 9 wherein each segment includes less than about 25 teeth.
11. The filter system of claim 10 wherein the comb includes at least three separate, curved segments, a first of the segments being attached at an end to one of the frame members and at an opposite end to a second segment, and a third segment being attached at an end to the second segment and at an opposite end to the frame.
12. The filter system of claim 10 wherein the frame includes opposing top and bottom members and opposing left and right side members, wherein the side members are curved to conform to the aircraft.
13. The filter system of claim 12 further comprising a strut for stiffening the comb and the filter system.
14. The filter system of claim 13 wherein a first strut member extends from the right frame member to the comb, and a second strut member extends from the left frame member to the comb, the struts extending generally perpendicular to the respective frame members and the comb.
15. The filter system of claim 14 wherein the frame is adjacent an outer moldline of the aircraft, a convex outer face of the filter element conforming to the outer moldline.
16. An inlet barrier filter system for mounting on an aircraft to filter air prior to intake into an engine of the aircraft, the filter system comprising:
a frame including at least two curved frame members defining an opening;
a filter element having a curved inward face and received in the opening of the frame;
the filter element including filter media having pleats;
a comb attached to the frame and including spaced-apart teeth, the comb supporting the pleats of the filter media;
the comb having less than about 25 teeth and being curved to generally conform to the curved inward face of the filter element.