Method of fabricating fiber reinforced composite structure having stepped surface

1. A method of fabricating a window frame for an aircraft, wherein the window frame includes a curved joggle surrounding a central opening, comprising the steps of:

laying up a plurality of plies over a tool such that corresponding axes of fiber orientations for the plies radiate substantially from a fixed point, the tool having a curved stepped tool surface for forming the curved joggle in the window frame, a curvature of the stepped tool surface comprising a compound curvature including an S-shaped curvature in a direction substantially parallel to a direction of a step comprising the curved stepped tool surface, and the plurality of plies comprising a composite material;

forming corresponding slits in corresponding areas of each of the plies where fibers in the plies cross and bridge the curved joggle such that, for each of the corresponding slits, a given slit is oriented in a direction perpendicular to a corresponding given axis of orientation of fibers for a corresponding given ply;

forming the window frame by compressing the plurality of plies on the tool with a pinch plate and a plug; and,

consolidating the plurality of plies.

2. The method of claim 1 , wherein laying up includes orienting the plurality of plies relative to each other about the fixed point as the plurality of plies are being laid up.

3. The method of claim 1 wherein laying up includes orienting at least certain of the plurality of plies such that the fiber orientations in the plurality of plies are further disposed at angles of approximately +22.5, −22.5, +67.5, and −67.5 degrees.

4. The method of claim 1 , wherein laying up includes orienting the plurality of plies relative to each other such that the slits are angularly spaced from each other.

5. The method of claim 1 wherein fiber orientations in the plurality of plies are disposed at angles of approximately 0, +45, −45 and 90 degrees.

6. A method comprising:

laying up a first ply on a tool, the first ply having first fibers oriented in a first direction, the tool comprising a curved structure having a curved joggle;

cutting a first slit in a first area of the first ply along a second direction that is perpendicular to the first direction, the first area defined by a first location where the first ply overlies and bridges the joggle;

laying up a second ply on the tool over the first ply, the second ply having second fibers oriented in a third direction;

cutting a second slit in a second area of the second ply along a fourth direction that is perpendicular to the third direction, the second area defined by a second location where the second ply overlies and bridges the joggle, and further where a first axis defined along the first slit intersects a point also intersected by a second axis defined along the second slit.

7. The method of claim 6 further comprising:

laying up a third ply on the tool over the second ply, the third ply having third fibers oriented in a fifth direction;

cutting a third slit in a third area of the third ply along a sixth direction that is perpendicular to the fifth direction, the third area defined by a third location where the third ply overlies and bridges the joggle, and further where a third axis defined along the third slit intersects the point.

8. The method of claim 6 wherein laying up the second ply includes rotating the second ply by an angle relative to the first ply.

9. The method of claim 6 further comprising:

laying up additional plies on the tool to create a completed layup, and wherein the completed layup forms a pattern comprising a fixed axis rosette.

10. The method of claim 9 wherein the completed layup comprises a window frame for an aircraft.

11. The method of claim 6 wherein the joggle comprises an S-shaped curve.