Detachable integral slat trailing edge structure
A detachable, slatted technology, applied in multi-layer structures, wings, aircraft parts, etc., can solve the problems of high cost, inability to disassemble, weak bonding surface strength, etc., to achieve easy maintenance and replacement, less structural parts, and cost. low effect
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[0016] Below in conjunction with accompanying drawing, the present invention is described in further detail:
[0017] The integral detachable slat trailing edge structure is in the shape of a triangular wedge and is composed of an upper wall panel 1 , a composite material enclosure 2 and a foam core 3 .
[0018] The upper wall panel 1 is paved with CF3052 carbon fiber fabric, and a layer of aluminum mesh is arranged on the outermost layer to prevent lightning strikes.
[0019] The composite frame 2 is interlaced with CF3052 carbon fiber fabric to form its lower skin 4, sealing ribs 5, and partitions 6. The outermost layer of the lower skin 4 is arranged with a wear-resistant plate 7 to prevent the front edge 11 from being fixed. contact causes trailing edge wear. For spanwise and chordwise layups, see figure 2 , image 3 , and fill the gap formed by the corners of the two layers of fabrics with CCF300 fiber filler. The sealing ribs meet at the lowest airfoil height. This ...
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