COMPOSITE GUSSET FILLER AND METHOD OF MANUFACTURE OF SAID COMPOSITE GUSSET FILLER
A composite gusset filler ( 1 ) of cut-off material from fiber fabrics ( 2, 3 ) trimmed into fragments of 2 min-10 mm length, separated into single yarn or roving elements mixed to quasi-homogeneous raw material for a semi-finished gusset filler ( 1 ). The present invention relates as well to specific shapes and a method of manufacture of said composite gusset filler ( 1 ) and to applications of said composite gusset filler ( 1 ).
1 . A composite gusset filler for a skin-stiffener transition assembly, comprising quasi-homogeneous raw material of mixed single yarn and/or roving elements from cut-off material from at least one textile CFRP ply, trimmed into fragments of 2 mm-10 mm length.
2 . The composite gusset filler according to claim 1 , wherein the raw material is stored with a random fiber orientation.
3 . The composite gusset filler according to claim 1 , wherein the quasi-homogeneous raw material is provided with single yarn or roving elements oriented according to the main load direction in the gusset area.
4 . The composite gusset filler according to claim 1 , wherein the fiber volume content is 40% to 60%.
5 . The composite gusset filler according to claim 1 , wherein an endless extrusion profile of dry fiber material is provided from the raw material.
6 . The composite gusset filler according to claim 1 , further comprising a specific net shaped section after press forming of the raw material or applying a propagation cone to the raw material.
7 . The composite gusset filler according to claim 6 , further comprising a net shaped section using catenoid-shaped section geometries or geometries developed from analytical or numerical optimization routines.
8 . A method of manufacture of a composite gusset filler according to claim 1 , comprising the steps of:
(a) cutting material from textile CFRP plies ( 2 , 3 ),
(b) trimming the cut material into fragments of 2 mm-10 mm length,
(c) sorting the fragments into single yarns and/or roving elements,
(d) mixing the single yarns and/or roving elements to quasi-homogeneous raw material, and
(e) processing the quasi-homogeneous raw material to a desired geometry for the semi-finished composite gusset filler.
9 . The method according to claim 8 , wherein the processing step is press-forming or customized extrusion.
10 . The method according to claim 8 , wherein heat is applied to activate a binder on the cut-off fibers of the textile CFRP plies.
11 . An application of said composite gusset filler according to claim 1 for a semi-finished skin-stiffener transition of helicopter airframes, helicopter structural parts, airplane doors, airplane frame manufacturing and/or non-aerospace applications.